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Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page I

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B-300 N291E S/N: FL-559 TABLE of CONTENTS

System ATA NO. System Title Page --- Table of Contents I --- Revision Record III --- Control Pages V --- Definitions IX --- Preamble XIII --- Procedures XV

21 Air Conditioning 21-1

22 Autoflight 22-1

23 Communications 23-1

24 Electrical Power 24-1

25 Equipment / Furnishings 25-1

26 Fire Protection 26-1

27 Flight Controls 27-1

28 Fuel 28-1

30 Ice and Rain Protection 30-1

31 Indicating / Recording Systems 31-1

32 Landing Gear 32-1

33 Lights 33-1

34 Navigation 34-1

35 Oxygen 35-1

37 Vacuum / Pressure 37-1

38 Water / Waste 38-1

46 Information Systems 46-1

52 Doors 52-1

61 Propellers 61-1

73 Engine Fuel and Control 73-1

74 Ignition 74-1

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page II

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TOC

77 Engine Indicating 77-1

79 Engine Oil 79-1

--- MEL Index IND-1

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page III

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Revision Record

REVISION RECORD

REVISION LOG

REVISION # REVISION DATE AFFECTED PAGES INITIALS Original 11-18-16 All --- --- --- --- --- --- --- ---

REVISION HIGHLIGHTS

REVISION # REVISION DATE HIGHLIGHTS Original 11-18-16 Initial Issue of MEL. --- --- --- --- --- --- --- ---

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page IV

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Revision Record

Intentionally Left Blank

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Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page V

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This manual is applicable to Millbrook Aviation B300 series aircraft and is no less restrictive than revision 9 of the FAA approved Beechcraft Model 300 MMEL dated 08/26/2016, and includes recent FAA MMEL Policy Letter changes.

FAA APPROVED D.O. IDENTIFIER FSDO # NAME EFFECTIVE

DATE SIGNATURE

CONTROL PAGE Page Rev # Date I Original 11-18-16 II Original 11-18-16 III Original 11-18-16 IV Original 11-18-16 V Original 11-18-16 VI Original 11-18-16 VII Original 11-18-16 VIII Original 11-18-16 IX Original 11-18-16 X Original 11-18-16 XI Original 11-18-16 XII Original 11-18-16 XIII Original 11-18-16 XIV Original 11-18-16 XV Original 11-18-16 XVI Original 11-18-16

ATA 21 Air Conditioning 21-1 Original 11-18-16 21-2 Original 11-18-16 21-3 Original 11-18-16 21-4 Original 11-18-16 21-5 Original 11-18-16 21-6 Original 11-18-16 21-7 Original 11-18-16 21-8 Original 11-18-16 21-9 Original 11-18-16 21-10 Original 11-18-16 21-11 Original 11-18-16 21-12 Original 11-18-16 21-13 Original 11-18-16 21-14 Original 11-18-16 21-15 Original 11-18-16 21-16 Original 11-18-16 21-17 Original 11-18-16 21-18 Original 11-18-16

Page Rev # Date 21-19 Original 11-18-16 21-20 Original 11-18-16

ATA 22 Autoflight 22-1 Original 11-18-16 22-2 Original 11-18-16 22-3 Original 11-18-16 22-4 Original 11-18-16 22-5 Original 11-18-16 22-6 Original 11-18-16

ATA 23 Communications 23-1 Original 11-18-16 23-2 Original 11-18-16 23-3 Original 11-18-16 23-4 Original 11-18-16 23-5 Original 11-18-16 23-6 Original 11-18-16 23-7 Original 11-18-16 23-8 Original 11-18-16 23-9 Original 11-18-16 23-10 Original 11-18-16 23-11 Original 11-18-16 23-12 Original 11-18-16 23-13 Original 11-18-16 23-14 Original 11-18-16

ATA 24 Electrical Power 24-1 Original 11-18-16 24-2 Original 11-18-16 24-3 Original 11-18-16 24-4 Original 11-18-16 24-5 Original 11-18-16 24-6 Original 11-18-16 24-7 Original 11-18-16 24-8 Original 11-18-16 24-9 Original 11-18-16 24-10 Original 11-18-16

Page Rev # Date ATA 25 Equipment /

Furnishings 25-1 Original 11-18-16 25-2 Original 11-18-16 25-3 Original 11-18-16 25-4 Original 11-18-16 25-5 Original 11-18-16 25-6 Original 11-18-16 25-7 Original 11-18-16 25-8 Original 11-18-16 25-9 Original 11-18-16 25-10 Original 11-18-16 25-11 Original 11-18-16 25-12 Original 11-18-16 25-13 Original 11-18-16 25-14 Original 11-18-16 25-15 Original 11-18-16 25-16 Original 11-18-16 25-17 Original 11-18-16 25-18 Original 11-18-16

ATA 26 Fire Protection 26-1 Original 11-18-16 26-2 Original 11-18-16

ATA 27 Flight Controls 27-1 Original 11-18-16 27-2 Original 11-18-16 27-3 Original 11-18-16 27-4 Original 11-18-16 27-5 Original 11-18-16 27-6 Original 11-18-16

ATA 28 Fuel 28-1 Original 11-18-16 28-2 Original 11-18-16 28-3 Original 11-18-16 28-4 Original 11-18-16

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Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page VI

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DATE SIGNATURE

Page Rev # Date 28-5 Original 11-18-16 28-6 Original 11-18-16

ATA 30 Ice and Rain 30-1 Original 11-18-16 30-2 Original 11-18-16 30-3 Original 11-18-16 30-4 Original 11-18-16 30-5 Original 11-18-16 30-6 Original 11-18-16 30-7 Original 11-18-16 30-8 Original 11-18-16 30-9 Original 11-18-16 30-10 Original 11-18-16 30-11 Original 11-18-16 30-12 Original 11-18-16

ATA 31 Indicating / Recording

31-1 Original 11-18-16 31-2 Original 11-18-16 31-3 Original 11-18-16 31-4 Original 11-18-16

ATA 32 Landing Gear 32-1 Original 11-18-16 32-2 Original 11-18-16 32-3 Original 11-18-16 32-4 Original 11-18-16 32-5 Original 11-18-16 32-6 Original 11-18-16

ATA 33 Lights 33-1 Original 11-18-16 33-2 Original 11-18-16 33-3 Original 11-18-16 33-4 Original 11-18-16 33-5 Original 11-18-16 33-6 Original 11-18-16 33-7 Original 11-18-16

Page Rev # Date 33-8 Original 11-18-16 33-9 Original 11-18-16 33-10 Original 11-18-16 33-11 Original 11-18-16 33-12 Original 11-18-16 33-13 Original 11-18-16 33-14 Original 11-18-16 33-15 Original 11-18-16 33-16 Original 11-18-16

ATA 34 Navigation 34-1 Original 11-18-16 34-2 Original 11-18-16 34-3 Original 11-18-16 34-4 Original 11-18-16 34-5 Original 11-18-16 34-6 Original 11-18-16 34-7 Original 11-18-16 34-8 Original 11-18-16 34-9 Original 11-18-16 34-10 Original 11-18-16 34-11 Original 11-18-16 34-12 Original 11-18-16 34-13 Original 11-18-16 34-14 Original 11-18-16 34-15 Original 11-18-16 34-16 Original 11-18-16 34-17 Original 11-18-16 34-18 Original 11-18-16 34-19 Original 11-18-16 34-20 Original 11-18-16 34-21 Original 11-18-16 34-22 Original 11-18-16

ATA 35 Oxygen 35-1 Original 11-18-16 35-2 Original 11-18-16 35-3 Original 11-18-16

Page Rev # Date 35-4 Original 11-18-16 ATA 37 Vacuum / Pressure

37-1 Original 11-18-16 37-2 Original 11-18-16 37-3 Original 11-18-16 37-4 Original 11-18-16

ATA 38 Water / Waste 38-1 Original 11-18-16 38-2 Original 11-18-16

ATA 46 Information Systems

46-1 Original 11-18-16 46-2 Original 11-18-16

ATA 52 Doors 52-1 Original 11-18-16 52-2 Original 11-18-16 52-3 Original 11-18-16 52-4 Original 11-18-16 52-5 Original 11-18-16 52-6 Original 11-18-16

ATA 61 Propellers 61-1 Original 11-18-16 61-2 Original 11-18-16 61-3 Original 11-18-16 61-4 Original 11-18-16

ATA 73 Engine Fuel and Control


ATA 74 Ignition 74-1 Original 11-18-16 74-2 Original 11-18-16

ATA 77 Engine Indicating 77-1 Original 11-18-16 77-2 Original 11-18-16 77-3 Original 11-18-16 77-4 Original 11-18-16

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Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page VII

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DATE SIGNATURE

Page Rev # Date ATA 79 Engine Oil


Index IND-1 Original 11-18-16 IND-2 Original 11-18-16 IND-3 Original 11-18-16 IND-4 Original 11-18-16 IND-5 Original 11-18-16 IND-6 Original 11-18-16

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page VIII

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Introduction


Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page IX

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Introduction

DEFINITIONS 1. Administrative Control Item (ACI). An ACI is listed by the aircraft operator in the MEL for tracking and

informational purposes. As an example, ACI may be used to track ETOPS accomplishment of required APU cold-soak, or in-flight verification starts. An ACI may be added to an aircraft operator’s MEL by approval of the POI provided no relief is granted, or provided conditions and limitations are contained in an approved document (e.g., Structural Repair Manual (SRM) or Airworthiness Directive (AD)). If relief other than that granted by an approved document is sought for an ACI, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an ACI.

2. ATA System Page. The ATA system page is divided into six (6) columns (A thru F) and contains: item and repair category; number installed; number required for dispatch; and remarks or exceptions. Standard ATA categories are used. Items are numbered sequentially.

A. Item. Item is the sequence number.

B. Name/Description. Name/Description depicts the equipment, system, component, or function.

C. Repair Category. Repair Category describes the time interval to repair MEL items.

D. Number Installed. This column depicts the number (quantity) of instrument and equipment items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MEL. Should the number be a variable (e.g., fleet configuration differences, cockpit lighting items, cabin lighting items, cargo restraint components) a number is not required and the “-” symbol is used.

E. Number Required for Dispatch. This column depicts the minimum number (quantity) of instrument and equipment items required for operation provided the conditions specified in the “Remarks or Exceptions” column are met. Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

F. Remarks or Exceptions. This column may include a statement(s) either prohibiting or permitting operation with a specific number of instrument and equipment items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

G. Provisos. Provisos are indicated by a number or a lower case letter in “Remarks or Exceptions”. Provisos are conditions or limitations that must be complied with for operation with the listed instrument or equipment item inoperative.

H. Notes. Notes provide additional information for crewmember or maintenance consideration. Notes are used to identify applicable material, which is intended to assist with compliance, but do not relieve the aircraft operator of the responsibility for compliance with all applicable requirements. Additional notes may be amended, deleted, or added to the MEL by the aircraft operator, as appropriate. Notes are not a part of the provisos.

I. Vertical Bar (change bar). A vertical bar indicates a change, addition, or deletion in the adjacent text for the current revision of that page only. All change bars applicable to the previous revision of the MEL are removed prior to the release of the next revision.

3. Airplane Flight Manual (AFM). The FAA approved AFM is the document approved by the responsible FAA Aircraft Certification Office (ACO) during type certification. The approved flight manual for the specific aircraft is listed on the applicable Type Certificate Data Sheet (TCDS). The approved flight manual is the source document for operational limitations and performance parameters for an aircraft. The FAA requires an approved flight manual for aircraft type certification.

4. Code of Federal Regulations (CFR) and Federal Aviation Regulations (FAR). CFR, the current term, and FAR both refer to the applicable portions of the Federal Aviation Act and Code of Federal Regulations.

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Definitions

5. Considered Inoperative. The phrase, “Considered Inoperative”, as used in the provisos, means that an instrument and equipment item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item will not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repair category.

6. Continuing Authorization – Single Extension. An aircraft operator who has the authorization to use an FAA approved MEL may also have the authority to use a continuing authorization to approve a single (one-time) extension to the repair interval for category B or C items in accordance with Operations Specification D095. Continuing Authorization – Single Extension is not authorized for repair category A and D items.

7. Dash (-). Indicates a variable number (quantity) of the instrument and equipment items may be installed or required for dispatch. This is common when a fleet MEL is used since aircraft of the same make and model may have differing numbers of specific instrument and/or equipment items installed.

8. Day of Discovery. This is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance record/logbook. This day is excluded from the calendar days or flight days specified in the MEL for the repair interval of an inoperative instrument and/or equipment item. This provision is applicable to all MEL items; i.e., categories A, B, C, and D.

9. Deactivated and/or Secured. When the MEL refers to an instrument and/or equipment item as deactivated and/or secured, the specified component must be put into an acceptable condition for safe flight. An acceptable method of deactivating and/or securing will be established by the aircraft operator.

10. Flight Day. A flight day is a 24 hour period (from midnight to midnight) local time, during which at least one flight is initiated for the affected aircraft.

11. Heavy Maintenance Visit (HMV). HMV is a scheduled C-check/D-check or airworthiness maintenance program inspection where the aircraft is scheduled to be out of service for 4 or more days.

12. Icing Conditions. An atmospheric environment that may cause ice to form on the aircraft (structural) or in the engine(s) (induction).

13. Inoperative. A system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) and/or tolerance(s).

14. Inoperative Components of an Inoperative System. Inoperative instrument and equipment items, which are components of a system that is inoperative, are usually considered components directly associated with and having no other function than to support that system (warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MEL).

15. Is Not Used. The phrase “Is Not Used” in the provisos, remarks or exceptions for an MEL instrument or equipment item may specify that another item in the MEL “is not used”. In such cases, crewmembers must not activate, actuate, or otherwise utilize that item under normal operations. It is not necessary for aircraft operators to accomplish the (M) procedure(s) associated with the item. However, operational requirements must be complied with, and an additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used. This informs crewmembers that an instrument or equipment item is not to be used under normal operations.

16. Nonessential Equipment and Furnishings (NEF). NEFs are those items installed on the aircraft as part of the original type certification, STC, or other form of alteration that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules. They are those items that, if inoperative, damaged, or missing, have no effect on the aircraft’s ability to be operated safely under all operational conditions. NEF items are not instrument and equipment items already identified in the MEL or CDL of the applicable aircraft. They do not include instrument and equipment items that are functionally required to meet the certification rule or for compliance with any operational rule.

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Definitions

17. Operative. An operative system and/or component will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s). When an MMEL item specifies that an item of equipment must be operative, it does not mean that its operational status must be verified; it’s to be considered operative unless reported or known to be malfunctioning. When an MMEL item specifies that an item of equipment must be verified operative, it means that it must be checked and confirmed operative at the interval(s) specified for that MMEL item. When an MMEL item specifies that an item of equipment must be verified but no interval is specified, verification is required only at the time of deferral.

Other terminology sometimes used interchangeably with “operative” within the MMEL is “operates normally”, "fully operative", and "considered operative”. The aircraft operator's MEL may incorporate standardized terminology of the aircraft operator’s choice to specify that an item of equipment must be operative, provided the aircraft operator's MEL definitions indicate that the selected "operative" terminology means that the required item of equipment will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s).

18. Placarding. Each inoperative instrument or equipment item must be placarded to inform and remind the crewmembers and maintenance personnel of the item condition. To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified (i.e. AFM), placard wording and location will be determined by the aircraft operator.

19. Repair Category. All users of an MEL approved under parts 91K, 121, 125, 129, 135 and 142 must effect repairs of inoperative instrument and equipment items, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

A. Repair Category A. This category item must be repaired within the time interval specified in the “Remarks or Exceptions” column of the aircraft operator’s approved MEL. For time intervals specified in “calendar days” or “flight days”, the day the malfunction was recorded in the aircraft maintenance record/logbook is excluded. For all other time intervals (i.e., flights, flight legs, cycles, hors, etc.), repair tracking begins at the point when the malfunction is deferred in accordance with the operator’s approved MEL.

B. Repair Category B. This category item must be repaired within 3 consecutive calendar days (72 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 3 day interval would begin at midnight the 26th and end at midnight the 29th.

C. Repair Category C. This category item must be repaired within 10 consecutive calendar days (240 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

D. Repair Category D. This category item must be repaired within 120 consecutive calendar days (2880 hours) excluding the day the malfunction was recorded in the aircraft maintenance record/logbook.

20. Takeoff. Takeoff is the act of beginning a flight in which an aircraft is accelerated from a state of rest to that of flight. For the purposes of MEL relief, this translates to the point at which the pilot physically begins to apply power to initiate the takeoff from the runway or takeoff surface.

21. Visible Moisture. An atmospheric environment containing water, in any form, that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

22. Visual Flight Rules (VFR). VFR is as defined in 14 CFR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

23. Visual Meteorological Conditions (VMC). VMC means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules.

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page XII

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Definitions

24. (M). This symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally, these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment, should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as part of the aircraft operator’s manual or MEL.

25. (O). This symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally, these procedures are accomplished by the flightcrew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the aircraft operator. Appropriate procedures are required to be produced as a part of the aircraft operator’s manual or MEL.

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page XIII

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Preamble

Preamble (Effective 6/14/89)

The following is applicable for authorized certificate holders operating under Title 14 Code of Federal Regulations (14 CFR) Parts 121, 125, 129, 135: 14 CFR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety.

A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator's particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator's MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator's MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of 14 CFR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by 14 CFR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by 14 CFR. Such documentation is required prior to operation with any item of equipment inoperative.

Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered. Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

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Preamble


Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page XV

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Procedures

Procedures General

The following are general procedures to be used any time a maintenance (M) or operations (O) procedures are to be accomplished by an authorized person. An authorized person is defined as a person qualified in accordance with applicable Federal Aviation Regulations who has been given responsibility by appropriate company management personnel to perform these procedures.

Circuit Breaker Disengagement, Safetying & Fuse Removal This describes the requirements when authorized personnel disengage circuit breakers (CB) and the maintenance procedure for safetying CBs in the off position and/or fuse removal. Aircraft may continue in service provided authorized personnel comply with the following procedures and/or restrictions:

1. Push button type CBs are locked in the off position by slipping a CB lockout device over the push button shaft.

2. Fuses are inspected and replaced, or removed as necessary.

3. The discrepancy is recorded and deferred in accordance with the company General Operations Manual, recording discrepancies.

Placarding Procedures This describes the requirements when authorized personnel placard an item as required by the MEL. Aircraft may continue in service provided authorized personnel comply with the following procedures and/or restrictions:

Placards must be placed on or adjacent to an inoperative switch, instrument or component as soon as practical. When an item is found to be inoperative, it is to be written up at the end of that flight. Unless authorized personnel correct the discrepancy, the item shall be deferred, if permitted by the MEL, and placarded.

The person installing the placard shall attach or place a self-adhesive inoperative placard immediately on or adjacent to the defective instrument, control, switch, or device. If a self-adhesive inoperative placard is not available, a piece of paper with inoperative written on it shall be taped in place. After installing the placard it is necessary to clearly record the malfunctioning equipment status in the aircraft's maintenance record in accordance with the companies MEL Management Program policy.

Crew Operating Procedures Items marked with a (O) require operating procedures to be performed normally by flightcrew personnel. The following procedures and/or restrictions apply any time an operating procedure is performed and must be complied with before the specific operating procedures outlined in the following pages of the MEL are accomplished. Aircraft may continue in service provided flightcrew personnel comply with the following:

1. It is determined that the item is deferrable according to the MEL.

2. It is determined that the discrepancy will not affect the safety of the flight.

3. It is determined that required alternate equipment is operative.

4. Whenever a two pilot crew is used, the PIC will brief the SIC on the procedure to be used during the flight.

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Procedures

Maintenance Procedures Items marked with an (M) require maintenance procedures to be performed by authorized personnel. The following procedures and/or restrictions apply at any time a maintenance procedure is performed and must be complied with before the specific maintenance procedures outlined in the following pages of the MEL are accomplished. Aircraft may continue in service provided authorized personnel comply with the following:

1. It is determined that the item is deferrable according to the MEL.

2. It is determined that the discrepancy will not affect the safety of the flight.

3. It is determined that required alternate equipment is operative.

4. Authorized personnel should utilize the procedures in the Manufacturer's Maintenance Manuals and Technical Publications any time the maintenance is being performed.

Stowing Electrical Connectors Whenever a procedure calls for disconnecting or unplugging an electrical wire or cannon plug, the following procedures shall be accomplished:

1. For Electrical Wiring:

A. Assure the electrical wire(s) will not arc or short and if necessary, wrap wire ends in a non-conductible material.

B. Place end of the wire(s) in a plastic bag and tie-wrap.

OR

C. Secure the wire(s) to a suitable nearby stationary object.

2. For Cannon Plug:

A. Place cannon plug in plastic bag and tie-wrap.

OR

B. Secure the cannon plug to a suitable nearby stationary object.

NOTE: Fuel lines, hydraulic lines, control cables, etc. are not suitable objects for securing electrical wires or cannon plugs. Protection against chafing, battery acids, fluids, personnel and cargo, high temperatures, and protection in wheel wells and landing gear areas must be assured.

Flight Crew Deferral Procedures: Flight Crew Deferral Item column found in each MEL item indicates whether or not Flight Crews may accomplish the deferral process. For items with a “YES”, Flight Crews have been qualified and authorized to perform all procedures associated with the MEL item. Normally, (M) Maintenance procedures are accomplished by maintenance personnel; however, if the “Flight Crew Deferral Item” column indicates “YES”, after coordinating with Maintenance Control, Flight Crews may perform (M) Maintenance procedures. For MEL items with a “NO” in the Flight Crew Deferral Item column, then Maintenance will be required to defer the item. At any time, the Flight Crew may request Maintenance to defer any MEL item.

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page 21-1

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ATA 21 Air Conditioning

Chapter 21 Air Conditioning Page Number

21-00-01 Cabin Altitude Annunciator System (white) .............................................................................. 21-2

21-00-02 Cabin Altitude Annunciation (red) ............................................................................................. 21-3

21-00-03 Cabin Differential High Annunciation (red) ............................................................................... 21-4

21-00-04 Cabin Altitude Warning Horn System ....................................................................................... 21-5

21-00-05 Bleed Air Off Annunciation System ........................................................................................... 21-6

21-00-06 Bleed Air Fail Annunciator System ........................................................................................... 21-7

21-20-01 Environmental Bleed Air Systems (Environmental) .................................................................. 21-8

21-21-02 Aft Blower System ..................................................................................................................... 21-9

21-31-01 Cabin Pressurization System (Pressurization Control) ........................................................... 21-10

21-32-01 Differential Pressure/Cabin Altitude Indicator ......................................................................... 21-11

21-32-02 Cabin Rate of Climb Indicator ................................................................................................. 21-12

21-33-01 Outflow Valve .......................................................................................................................... 21-13

21-33-02 Safety Valve ............................................................................................................................ 21-14

21-40-01 Aft Heat System ...................................................................................................................... 21-15

21-40-02 Electric Heat System ............................................................................................................... 21-16

21-50-01 Vapor Cycle Air Conditioning System ..................................................................................... 21-17

21-50-02 Ground Air Cooling System .................................................................................................... 21-18

21-60-01 Environmental Temperature Control System .......................................................................... 21-19

21-62-01 Cabin Temperature Indicator System ..................................................................................... 21-20


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21-00-01 Cabin Altitude Annunciator System (white) Repair Category Number Installed

Name/Description Number Required For Dispatch

Item Remarks Or Exceptions -01 Cabin Altitude

Annunciator System (white) (CABIN ALTITUDE) Ann. only

C 1 0 May be inoperative provided the Cabin Altitude Aural Warning Horn and Cabin Altitude High Annunciator are operative.

-02 Cabin Altitude Annunciator System (white) (CABIN ALTITUDE) Ann. only

C 1 0 May be inoperative provided the aircraft is operated at or below 10,000 feet MSL.

-03 Cabin Altitude Annunciator System (white) (CABIN ALTITUDE) Ann. only

C 1 0 (O) May be inoperative provided aircraft is configured and operated unpressurized.

Item MEL Sticker Location Flight Crew Deferral Item

21-00-01-01 21-00-01-02 21-00-01-03

Near Cabin Altitude Indicator YES

Operations (O) 21-00-01-03 Select the BLEED AIR VALVE switches to the PNEU & ENVIR OFF positon.


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21-00-02 Cabin Altitude Annunciation (red) Repair Category Number Installed



Annunciation (red) (ALT WARN) or (CABIN ALT HI) (Cabin Alt High) CAS


-02 Cabin Altitude Annunciation (red) (ALT WARN) or (CABIN ALT HI) (Cabin Alt High) CAS



21-00-02-01 21-00-02-02

Near Cabin Altitude High Annunciator YES



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21-00-03 Cabin Differential High Annunciation (red) Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Differential

High Annunciation (red) (CABIN DIFF HI) Ann. (Cabin Diff High) CAS



21-00-03-01 Near Cabin Altitude High Annunciator YES Operations (O) Select the BLEED AIR VALVE switches to the PNEU & ENVIR OFF positon.

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 -5

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21-00-04 Cabin Altitude Warning Horn System Repair Category Number Installed



Warning Horn System


-02 Cabin Altitude Warning Horn System

C 1 0 May be inoperative provided Cabin Altitude (white) and Cabin Altitude (red) annunciations are both operative.

-03 Cabin Altitude Warning Horn System


-04 Cabin Altitude Warning Horn Cancel Switch



21-00-04-01 thru

21-00-04-04

Near Cabin Altitude Warning Horn Cancel Switch

YES



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21-00-05 Bleed Air Off Annunciation System Repair Category Number Installed


Item Remarks Or Exceptions -01 Bleed Air Off

Annunciation System (amber) (L or R BL AIR OFF) Ann. (L or R Bleed Air Off) CAS

C 2 1 May be inoperative.


21-00-05-01 Near Bleed Air Annunicator YES


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21-00-06 Bleed Air Fail Annunciator System Repair Category Number Installed


Item Remarks Or Exceptions -01 Bleed Air Fail

Annunciator System (L or R BLEED FAIL) Ann. (L or R BLEED AIR FAIL) CAS (Illuminates or Fails to Illuminate)

C 2 1 (O) May be inoperative provided: a) Environmental and Instrument Bleed Air Valves on inoperative

side are verified closed prior to each flight, b) Bleed Air Off Annunciator/CAS is operative on the operative

bleed air source, c) Aircraft is operated at or below Flight Level 250, and d) Aircraft is not operated in known or forecast icing conditions.


21-00-06-01 Near L or R BLEED FAIL Annunciator YES Operations (O) 1. Start the engine on the inoperative side, and with the other engine shutdown, select the inoperative

BLEED AIR VALVE to the PNEU & ENVIR OFF position.

2. Verify the PNEUMATIC PRESSURE gauge indicates zero or near zero.

3. Keep inoperative valve closed.


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21-20-01 Environmental Bleed Air Systems (Environmental) Repair Category Number Installed


Item Remarks Or Exceptions -01 Environmental

Bleed Air Systems (Environmental)

C 2 1 (O) One may be inoperative provided: a) Environmental Bleed Air Valve on inoperative side is verified

closed prior to each flight, b) Bleed Air Off Annunciation is operative on the operative

Environmental Bleed Air System, and c) Aircraft is operated at or below Flight Level 250.

-02 Environmental Bleed Air Systems (Environmental)

C 2 0 (O) May be inoperative provided: a) Aircraft is configured and operated unpressurized, b) Both Environmental Bleed Air Valves are verified closed prior

to each flight, and c) Cabin temperatures remain suitable for operation.


21-20-01-01 21-20-01-02

Near Bleed Air Switch YES

Operations (O) 21-20-01-01 1. Ensure there are no current logbook entries or deferrals related to the Bleed Air Off Annunciation on the

operative Environmental Bleed Air System.

2. Ensure aircraft is operated at or below Flight Level 250.

3. Prior to every flight, the pilot in command will verify the respective BL AIR OFF annunciator functions properly by selecting the operative bleed air switch to ENVIR OFF position and verifying the respective BL AIR OFF annunciator comes ON.

21-20-01-02 1. Select the BLEED AIR VALVE switches to the PNEU & ENVIR OFF position.

2. Ensure the following:

A. Both Environmental Bleed Air Valves are verified closed prior to each fligh.

B. Cabin temperatures remain suitable for operation.


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21-21-02 Aft Blower System Repair Category Number Installed


Item Remarks Or Exceptions -01 Aft Blower

System C 1 0 May be inoperative provided aft electric heat system is considered

inoperative.


21-21-02-01 Near Aft Blower Switch YES


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21-31-01 Cabin Pressurization System (Pressurization Control) Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin

Pressurization System (Pressurization Control)

C 1 0 (O) May be inoperative provided: a) Cabin Dump is verified operative, b) CABIN PRESS switch is selected to DUMP, c) Red Cabin Altitude Warning is operative, and d) Aircraft is operated at 10,000 feet pressure altitude or below.

NOTE: When pressure altitude reaches approximately 10,000 feet, the CABIN ALTITUDE (white) annunciator will illuminate. When the cabin pressure altitude exceeds 11,500 to 12,000 feet, a “CABIN ALT HI” (red) annunciator will illuminate.


21-31-01-01 Near Pressurization System YES Operations (O) 1. Ensure there are no current logbook entries or deferrals related to the Red Cabin Altitude Warning

system.

2. Flight planning must consider the fuel burn and range associated with flight at lower altitudes (maximum altitude is 10,000 feet pressure altitude or below).

3. Minimum enroute altitudes must be taken into account for the planned route.

4. Place both Bleed Air Valves to ENVIR OFF.

5. Place the Cabin Press switch to DUMP position.

6. Passengers must be briefed prior to each flight that cabin pressurization will be unavailable.

NOTE: CABIN ALTITUDE white annunciator may appear at 10,000 feet.


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21-32-01 Differential Pressure/Cabin Altitude Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Differential

Pressure/Cabin Altitude Indicator



21-32-01-01 Near Differential Pressure Indicator YES Operations (O) Select the BLEED AIR VALVE switches to the PNEU & ENVIR OFF position.


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21-32-02 Cabin Rate of Climb Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Rate of

Climb Indicator C 1 0 May be inoperative for pressurized flight provided Differential

Pressure/Cabin Altitude Indicator is operative.

-02 Cabin Rate of Climb Indicator



21-32-02-01 21-32-02-02

Near Cabin Rate of Climb Indicator YES

Operations (O) 21-32-02-02 Select the BLEED AIR VALVE switches to the PNEU & ENVIR OFF position.


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21-33-01 Outflow Valve Repair Category Number Installed


Item Remarks Or Exceptions -01 Outflow Valve C 1 0 (M) May be inoperative provided:

a) Outflow Valve is secured open, and b) Cabin Pressurization System is considered inoperative.


21-33-01-01 Near Cabin Pressurization Control Panel NO Maintenance (M) The outflow valve cannot be secured open. It must be removed from its location and properly stored or stowed. All electrical connections must be secured and all plumbing must be capped and secured. Care must be taken so as not to damage the interior or surrounding structure while removing the valve.


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21-33-02 Safety Valve Repair Category Number Installed


Item Remarks Or Exceptions -01 Safety Valve C 1 0 (M) May be inoperative provided:

a) Safety Valve is secured open, and b) Cabin Pressurization System is considered inoperative.


21-33-02-01 Near Cabin Pressurization Control Panel NO Maintenance (M) The safety valve cannot be secured open. It must be removed from its location and properly stored or stowed. All electrical connections must be secured and all plumbing must be capped and secured. Care must be taken so as not to damage the interior or surrounding structure while removing the valve.


\


21-40-01 Aft Heat System Repair Category Number Installed


Item Remarks Or Exceptions -01 Aft Heat System C 1 0 (M) May be inoperative provided system is deactivated.


21-40-01-01 Near Aft Heat Switch NO Maintenance (M) Pull and secure circuit breaker 36 GROUND HEAT, located beneath the center floorboard, aligned with the fifth row of passenger seats. Doing so will disengage the ground heating mechanism rendering the system inoperative. System is only operation when the airplane is on the ground and the cabin temperature is 55°F (+5°F /-0°F) or below.


\


21-40-02 Electric Heat System Repair Category Number Installed


Item Remarks Or Exceptions -01 Electric Heat

System D 1 0 (M) May be inoperative provided system is deactivated.


21-40-02-01 Near Electric Heat Switch YES Maintenance (M) Pull and secure CB49 FWD ELECT HEAT and CB48 AFT ELECT HEAT circuit breakers.


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21-50-01 Vapor Cycle Air Conditioning System Repair Category Number Installed


Item Remarks Or Exceptions -01 Vapor Cycle Air

Conditioning System

C 1 0 (M) May be inoperative provided system is deactivated.


21-50-01-01 Near Air Conditioning System Switch YES Maintenance (M) Pull and secure C/B 24 – AIR COND CLUTCH (air conditioning clutch) located in the DC power distribution panel inside the lower forward equipment bay.


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21-50-02 Ground Air Cooling System Repair Category Number Installed


Item Remarks Or Exceptions -01 Ground Air

Cooling System D 1 0 (M) May be inoperative provided system is deactivated.


21-50-02-01 Near Air Conditioning System Switch YES Maintenance (M) Pull and secure the compressor-clutch C/B 24 – AIR COND CLUTCH circuit breaker located in the DC power distribution panel inside the lower forward equipment bay.


\


21-60-01 Environmental Temperature Control System Repair Category Number Installed


Item Remarks Or Exceptions -01 Environmental

Temperature Control System

C 1 0 (O) May be inoperative provided: a) Cabin Pressurization system is considered inoperative, b) Both Environmental Bleed Air Valves are verified closed prior

to each flight, and c) Cabin temperatures remain suitable for operation.

-02 Environmental Temperature Control System (Automatic Function)

C 1 0 May be inoperative provided the Manual Function is operative.

-03 Environmental Temperature Control System (Manual Function)

C 1 0 May be inoperative provided the Automatic Function is operative.


21-60-01-01 21-60-01-02 21-60-01-03

Near Temperature Control YES

Operations (O) 21-60-01-01 1. Flight planning must consider the fuel burn and range associated with flight at lower altitudes.

2. Minimum enroute altitudes must be taken into account for the planned route.

3. Place both Bleed Air Valves to ENVIR OFF.

4. Place the Cabin Press switch to DUMP position.

5. Passengers must be briefed prior to each flight that cabin pressurization will be unavailable.

6. Ensure cabin temperatures remain suitable for operation being conducted.

NOTE: CABIN ALTITUDE white annunciator may appear at 10,000 feet.


\


21-62-01 Cabin Temperature Indicator System Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin

Temperature Indicator System



21-62-01-01 Near Cabin Temperature Indicator YES


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ATA 22 Autoflight

Chapter 22 Autoflight Page Number

22-10-01 Autopilot System ................................................................................................................. 22-2

22-10-02 Yaw Damper ....................................................................................................................... 22-3

22-10-03 Autopilot Control Wheel Disengage Switches .................................................................... 22-4

22-10-04 Autopilot/Flight Director Go-Around Button ........................................................................ 22-5

22-13-00 Flight Director System ......................................................................................................... 22-6


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ATA 22 Autoflight

22-10-01 Autopilot System Repair Category Number Installed


Item Remarks Or Exceptions -01 Autopilot System C 1 0 (M) May be inoperative provided:

a) Autopilot is deactivated, b) Rudder Boost System is verified operative prior to

departure in accordance with the Airplane Flight Manual, c) Operations do not require use of autopilot, and d) Aircraft is not operated RVSM.

RVSM Operations Not Authorized


22-10-01-01 Near Autopilot Engage Switch YES Maintenance (M) Perform operational check of Rudder Boost per pilot checklist prior to each takeoff.


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ATA 22 Autoflight

22-10-02 Yaw Damper Repair Category Number Installed


Item Remarks Or Exceptions -01 Yaw Damper

(with Raisbeck Engineering Dual Aft Body Strakes)

C 1 0 (M) May be inoperative provided: a) STC SA5151NM (Raisbeck Engineering Dual Aft Body

Strakes) is installed, and b) Aircraft is operated at or below 19,000 feet MSL.


22-10-02-01 Near Yaw Damper Engage Switch YES Maintenance (M) Perform operational check of autopilot to verify proper operation of autopilot with Yaw Damper inoperative.


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ATA 22 Autoflight

22-10-03 Autopilot Control Wheel Disengage Switches Repair Category Number Installed


Item Remarks Or Exceptions -01 Autopilot Control

Wheel Disengage Switches (AP/YD/RB/TRIM DISC)

C 2 1 One may be inoperative on the non-flying pilot side provided: a) Autopilot is not used below 1,500 feet AGL, and b) Approach minimums do not require the use of the autopilot

-02 Autopilot Control Wheel Disengage Switches (AP/YD/RB/TRIM DISC)

B 2 0 May be inoperative provided: a) Autopilot is considered inoperative, and b) Second level switch trim interrupt function is verified

operative.


-03 Autopilot Control Wheel Disengage Switches (AP/YD/RB/TRIM DISC)

B 2 0 (M) May be inoperative provided: a) Autopilot is considered inoperative, b) Electric Elevator Trim is considered inoperative, and c) Yaw Damp is considered inoperative.



22-10-03-01 22-10-03-02

Near Autopilot Engage Switch YES

22-10-03-03 Near Autopilot Engage Switch NO Maintenance (M) 22-10-03-03 Ensure no electrical/mechanical fault exists that would have an adverse effect on any Flight Control function.


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ATA 22 Autoflight

22-10-04 Autopilot/Flight Director Go-Around Button Repair Category Number Installed


Item Remarks Or Exceptions -01 Autopilot/Flight

Director Go-Around Button

C 2 0 (O) May be inoperative provided: a) Approach minimums do not require AP/FD use, and b) Procedures as noted in the Operations procedure are

followed to disconnect the Autopilot and establish initial pitch and wings level attitude.


22-10-04-01 Near Autopilot Engage Switch YES Operations (O) Flight Director is not available for Takeoff or Go-Around with both TO/GA buttons inoperative. Flight crew shall use raw data for takeoff and go-around. For takeoff, once airborne and above 500 ft AGL, pilot-not-flying (PNF) shall select desired lateral mode (HDG or LNAV) on guidance panel as directed by pilot-flying (PF). Additionally, PNF shall select desired vertical mode (FLCH or VS or FPA) as directed by PF. For go-around, after flaps and landing gear have been retracted and airplane is above 500 ft AGL, PNF shall select desired lateral mode (HDG or LNAV) and vertical mode (FLCH or VS or FPA) on guidance panel at direction of PF.


\

ATA 22 Autoflight

22-13-00 Flight Director System Repair Category Number Installed


Item Remarks Or Exceptions -01 Flight Director

System C 2 0 May be inoperative provided:

a) Approach procedures do not require use of Flight Director, and

b) Autopilot is verified operative.

NOTE: Any operative mode may be used.

-02 Flight Director System

C 2 0 May be inoperative provided: a) Approach procedures do not require use of Flight Director, b) Autopilot is considered inoperative and c) Aircraft is not operated RVSM.



22-13-00-01 22-13-00-02

Near Flight Director Mode Annunciator YES


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ATA 23 Communications

Chapter 23 Communications Page Number

23-00-01 Ground Communication Power System .............................................................................. 23-2

23-00-02 Flight Phone System ........................................................................................................... 23-3

23-12-01 Communications Systems (VHF) ........................................................................................ 23-4

23-20-01 Selective Call Systems (SELCAL) ...................................................................................... 23-5

23-40-02 Flightcrew Intercom System ................................................................................................ 23-6

23-40-03 Passenger Address System (PA) ....................................................................................... 23-7

23-40-04 Recorded Passenger Briefing System ................................................................................ 23-8

23-40-05 Passenger Seat Belt/Safety Chime (chime only) ................................................................ 23-9

23-50-01 Cockpit Speaker System (Includes Audio Amp.) .............................................................. 23-10

23-50-02 Hand Held Microphones ................................................................................................... 23-11

23-50-03 Flight Deck Headset and Boom Microphones .................................................................. 23-12

23-60-01 Static Discharge Wicks ..................................................................................................... 23-13

23-70-01 Cockpit Voice Recorder (CVR) ......................................................................................... 23-14


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23-00-01 Ground Communication Power System Repair Category Number Installed


Item Remarks Or Exceptions -01 Ground

Communication Power System



23-00-01-01 Near Control Panel YES


\


23-00-02 Flight Phone System Repair Category Number Installed


Item Remarks Or Exceptions -01 Flight Phone System D 1 0 May be inoperative provided procedures do not require its use.

-02 Flight Phone System (Cockpit Handset)

D 1 0 May be inoperative provided procedures do not require its use.

-03 Flight Phone System (Cabin Handset)

D 1 0 May be inoperative.

-04 Flight Phone System (Automatic Flight Reporting Functions)

D 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are followed.


23-00-02-01 thru

23-00-02-04

Near Captains Audio Panel YES

Operations (O) 23-00-02-04 Utilize the most appropriate method to report any necessary data to the respective recipient (i.e. VHF radio, etc).


\


23-12-01 Communications Systems (VHF) Repair Category Number Installed


Item Remarks Or Exceptions -01 Communications

Systems (VHF) D 2 1 Number 2 may be inoperative provided:

a) Overwater operations in excess of 30 minutes flying time or 100 nautical miles from the nearest shore are not conducted, and

b) Inoperative system is not powered by an Emergency Power Source and not required for Emergency Procedures.

NOTE: Number 1 VHF must be operative due to powered by an Emergency Power Source.

14 CFR REFERENCE: 14 CFR 135.161, 135.165


23-12-01-01 Near Control Panel YES


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23-20-01 Selective Call Systems (SELCAL) Repair Category Number Installed


Item Remarks Or Exceptions -01 Selective Call

Systems (SELCAL) C 1 0 (O) May be inoperative provided procedures as noted in the

Operations procedure are followed.

-02 Channels C 2 0 (O) May be inoperative provided procedures as noted in the Operations procedure are followed.


23-20-01-01 23-20-01-02

Near SELCAL Panel YES

Operations (O) 23-20-01-01 1. Flight crew must advise ATC of inoperative SELCAL, as appropriate.

2. Flight crew will monitor the appropriate radios at all times in the absence of SELCAL. Consideration should be given to the effect of increased fatigue due to this requirement and the possibility of having only one crew member monitor the radios via headset (especially HF) if required for the given flight.

23-20-01-02 Use operative SELCAL Channel.

NOTE: If all channels are inoperative, use (O) procedure 23-20-01-01.


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23-40-02 Flightcrew Intercom System Repair Category Number Installed


Item Remarks Or Exceptions -01 Flightcrew Intercom

System (Flight Deck to Ground)

C 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are followed.


23-40-02-01 Near Captains Audio Panel YES Operations (O) Crew members will establish communication with ground crew using another means, such as hand signals, cell phone, handheld radio, etc.


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23-40-03 Passenger Address System (PA) Repair Category Number Installed


Item Remarks Or Exceptions -01 Passenger Address

System (PA) (Passenger Configuration)

C 1 0 (O) May be inoperative provided alternate, normal, and emergency procedures and/or operating restrictions are used as noted in the Operations procedure.


23-40-03-01 Near PA Switch YES Operations (O) 1. PRIOR TO EACH DEPARTURE, ensure all passengers have been orally briefed on normal and

emergency procedures.

2. Orally brief passengers during flight any time additional normal or emergency procedures are required.


\


23-40-04 Recorded Passenger Briefing System Repair Category Number Installed


Item Remarks Or Exceptions -01 Recorded

Passenger Briefing System

D 1 0 (O) May be inoperative provided passengers are appropriately briefed.


23-40-04-01 Near PA Switch YES Operations (O) Utilize the PA system, or orally brief passengers during flight any time additional normal or emergency procedures are required.


\


23-40-05 Passenger Seat Belt/Safety Chime (chime only) Repair Category Number Installed


Item Remarks Or Exceptions -01 Passenger Seat

Belt/Safety Chime (chime only)

C 1 0 (O) May be inoperative provided: a) Passenger Address System is operative, and b) Procedures as noted in the Operations procedure are

followed for passenger seat belt briefing.


23-40-05-01 Near Switch YES Operations (O) A crew member must use the PA system from the cockpit to make the appropriate announcements.


\


23-50-01 Cockpit Speaker System (Includes Audio Amp.) Repair Category Number Installed


Item Remarks Or Exceptions -01 Cockpit Speaker

System (Includes Audio Amp.)

C 2 1 One may be inoperative provided an operative headset is available to the flightcrew.

-02 Cockpit Speaker System (Includes Audio Amp.)

C 2 0 May be inoperative provided: a) Two operative Headsets are available to the flightcrew, and b) All aural warnings are available.


23-50-01-01 23-50-01-02

Near Associated Speaker YES


\


23-50-02 Hand Held Microphones Repair Category Number Installed


Item Remarks Or Exceptions -01 Hand Held

Microphones C 2 1 One may be inoperative provided associated Boom

Microphone is available and operative.

-02 Microphone Jack C 2 0 May be inoperative provided: a) Two operative Headsets are available to the flightcrew, and b) All aural warnings are available.

-03 Handheld Microphone Holder

D 2 0 (O) May be inoperative provided associated hand microphone is secured and accessible by alternate means.


23-50-02-01 23-50-02-02 23-50-02-03

Near Microphone YES

Operations (O) 23-50-02-03 Prior to flight, a crew member must ensure that the hand microphone is secured in a manner that will not interfere with aircraft operations. One method is to utilize adhesive hook and loop (Velcro) strips.


\


23-50-03 Flight Deck Headset and Boom Microphones Repair Category Number Installed


Item Remarks Or Exceptions -01 Headset Boom

Microphones A 2 0 May be inoperative provided:

a) Associated hand microphone is installed and operative, and

b) Repairs are made within 3 flight days.

-02 Headset Earphones/ Headphones

C 2 1 May be inoperative provided associated flight deck speaker is operative.


23-50-03-01 23-50-03-02

Near Associated Audio Panel YES


\


23-60-01 Static Discharge Wicks Repair Category Number Installed


Item Remarks Or Exceptions -01 Static Discharge

Wicks C 23 2 May be damaged or missing provided:

a) No more than two total static wicks are damaged or missing, and

b) Only one static wick is missing from each static discharge general area (left wing, right wing, tail).


23-60-01-01 Near Captains Audio Panel YES


\


23-70-01 Cockpit Voice Recorder (CVR) Repair Category Number Installed


Item Remarks Or Exceptions -01 Cockpit Voice

Recorder (CVR) (Without Flight Data Recorder (FDR) Installed)

A 1 0 May be inoperative provided repairs are made within 3 flight days.

-02 Recorder Independent Power Supply (RIPS)


-03 Underwater Locator Device

D 1 0 May be inoperative or missing.

14 CFR REFERENCE: Not required for 14 CFR 135 operations.

-04 Datalink Recording A 1 0 May be inoperative provide repairs are made within 3 flight days.


23-70-01-01 thru

23-70-01-04

Near CVR Panel YES


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ATA 24 Electrical Power

Chapter 24 Electrical Power Page Number

24-00-02 Generator Bus Tie Annunciation (amber) ........................................................................... 24-2

24-00-03 DC Generator Annunciation (amber) .................................................................................. 24-3

24-00-04 External Power Annunciation (amber) ................................................................................ 24-4

24-01-01 Standby Power System ....................................................................................................... 24-5

24-22-01 AC Inverters ........................................................................................................................ 24-6

24-30-01 L or R GEN BUS TIE Relay ................................................................................................ 24-7

24-40-01 External Power System ....................................................................................................... 24-8

24-50-01 Cabin AC Power System .................................................................................................... 24-9


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24-00-02 Generator Bus Tie Annunciation (amber) Repair Category Number Installed


Item Remarks Or Exceptions -01 Generator Bus Tie

Annunciation (amber) (L or R GEN TIE OPEN) Ann. (L or R or L-R Gen Tie Open) CAS

B 2 0 (O) May be inoperative provided: a) Affected Generator Bus Tie Relay is verified CLOSED prior

to each departure, and b) Both DC GEN Annunciators are verified operative prior to

each departure.


24-00-02-01 Near L or R GEN BUS TIE Annunciator YES Operations (O) 1. Rotate the VOLTMETER BUS SELECT switch through the L GEN, R GEN, CTR, and TPL FD positions.

2. Observe the voltages at each position for correct output (nominal 28 volts).

3. Observe that the amber L DC GEN, R DC GEN, R GEN TIE OPEN, L GEN TIE OPEN, and red INVERTER warning annunciators are NOT illuminated.


\


24-00-03 DC Generator Annunciation (amber) Repair Category Number Installed


Item Remarks Or Exceptions -01 DC Generator

Annunciation (amber) (L or R DC GEN) Ann. (L or R DC Generator) CAS

B 2 1 One may be inoperative provided both DC load meters are operative and monitored.


24-00-03-01 Near Associated DC Generator Annunciator YES


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24-00-04 External Power Annunciation (amber) Repair Category Number Installed


Item Remarks Or Exceptions -01 External Power

Annunciation (amber) (EXT PWR) Ann. (Ext Pwr-Active or Ext Pwr-Cart) CAS

C 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are followed.


24-00-04-01 Near External Power Annunciation YES Operations (O) Prior to towing and/or taxi, a member of the flight crew must verify the ground power unit is not connected to the aircraft.


\


24-01-01 Standby Power System Repair Category Number Installed


Item Remarks Or Exceptions -01 Standby Power

System B 1 0 (M) May be inoperative provided:

a) Airplane is operated day VFR only, and b) Standby Battery is disconnected and removed.

-02 Sonalert Standby Power Aural Warning

B 1 0 May be inoperative provided the Standby Power Annunciator is operative.

-03 Standby Power Annunciator

B 1 0 May be inoperative provided the Sonalert Standby Power Aural Warning is operative.


24-01-01-01 24-01-01-02 24-01-01-03

Near Standby Power Annunciator YES

Maintenance (M) 24-01-01-01 1. Ensure all aircraft power is off and no equipment is operating.

2. Gain access to standby battery through the right side avionics compartment door.

3. Disconnect battery leads and remove battery.

4. Cap and secure leads.

5. Placard "Standby Battery Removed" on forward instrument panel.

6. If necessary, make appropriate adjustments to airplane weight and balance.


\


24-22-01 AC Inverters Repair Category Number Installed


Item Remarks Or Exceptions -01 AC Inverters B 2 1 One may be inoperative provided:

a) Aircraft is operated in day VMC only, and b) AC Bus Transfer is operative.


24-22-01-01 Near Inverter Switch YES


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24-30-01 L or R GEN BUS TIE Relay Repair Category Number Installed


Item Remarks Or Exceptions -01 L or R GEN BUS

TIE Relay B 2 1 One may be inoperative provided:

a) Aircraft is operated day VMC only, and b) Both DC GEN Annunciators are operative.


24-30-01-01 Near BUS TIE Indication YES


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24-40-01 External Power System Repair Category Number Installed


Item Remarks Or Exceptions -01 External Power

System C 1 0 (M) May be inoperative provided Ground Power Relay is

verified open.


24-40-01-01 Near External Power Switch YES Maintenance (M) PULL and secure circuit breaker External Power Control.

NOTE: Before connecting an external power unit, turn all radio equipment, the generator switches, the battery switch, and the external power switch to OFF. Place the overhead voltmeter select switch in the EXT PWR position.

CAUTION: Voltage is required to energize the avionics master power relays to remove the power from the avionics equipment; therefore, never apply external power to the airplane without first applying battery voltage.


\


24-50-01 Cabin AC Power System Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin AC Power

System C 1 0 (M) May be inoperative provided system is deactivated.


24-50-01-01 Near Cabin AC Power Switch NO Maintenance (M) Pull and secure C/B 270 Inverter Control located under the center floorboard, just aft of the wing spar.


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\

ATA 25 Equipment / Furnishings

Chapter 25 Equipment / Furnishings Page Number

25-10-01 Flashlight ............................................................................................................................. 25-2

25-10-02 Crew Assist Straps (Cockpit Overhead) ............................................................................. 25-3

25-10-03 Cockpit Sun Visors .............................................................................................................. 25-4

25-10-04 Flightcrew Seats .................................................................................................................. 25-5

25-20-01 Passengers Seat(s) ............................................................................................................. 25-6

25-20-02 Non-Essential Equipment and Furnishings (NEF) .............................................................. 25-7

25-20-03 Emergency Medical Services (EMS) Equipment (Medical Transport Equipment) ............. 25-8

25-25-01 “FASTEN SEAT BELT”/“FASTEN SEAT BELT WHILE SEATED” Signs or Placards ....... 25-9

25-50-01 Cargo Restraint Systems .................................................................................................. 25-10

25-50-02 Cabin Storage Compartments/ Closets ............................................................................ 25-11

25-50-03 Wing Locker Door Gas Spring .......................................................................................... 25-13

25-60-01 Emergency Medical Equipment ........................................................................................ 25-14

25-60-03 Emergency Vision Assurance System .............................................................................. 25-15

25-61-01 Flotation / Overwater Equipment ...................................................................................... 25-16

25-62-01 Emergency Locator Transmitter (ELT).............................................................................. 25-17


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25-10-01 Flashlight Repair Category Number Installed


Item Remarks Or Exceptions -01 Flashlight C 1 0 May be inoperative or missing provided affected crewmember

has a flashlight of equivalent characteristics readily available.

-02 Flashlight Holder C 1 0 May be damaged or inoperative provided affected Flashlight remains readily available to crewmember while seated.


25-10-01-01 25-10-01-02

Near Flashlight Holder YES


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25-10-02 Crew Assist Straps (Cockpit Overhead) Repair Category Number Installed


Item Remarks Or Exceptions -01 Crew Assist Straps

(Cockpit Overhead) D 1 0 May be damaged or missing.


25-10-02-01 Near Crew Assist Strap YES


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25-10-03 Cockpit Sun Visors Repair Category Number Installed


Item Remarks Or Exceptions -01 Cockpit Sun Visors C 2 0 May be inoperative or missing provided there are no visual

restrictions to the flightcrew.


25-10-03-01 Near Associated Sun Visor YES


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25-10-04 Flightcrew Seats Repair Category Number Installed


Item Remarks Or Exceptions -01 Armrest(s) C 4 0 May be inoperative provided the affected Armrest can be

placed in the normal up or down position.

-02 Armrest(s) C 4 0 (M) May be inoperative provided affected armrest is secured in the up position.

-03 Lumbar Support C 2 0 May be inoperative. -04 Seat Adjustment A 2 0 (M) May be inoperative provided:

a) Affected Seat is locked in a position that permits normal pilot visibility,

b) Full Flight Control movement is available to the flightcrew, c) Position of the affected Seat is acceptable to the flightcrew,

and d) Repairs are made within 1 flight day.


25-10-04-01 25-10-04-03

Near Associated Instrument Panel YES

25-10-04-02 25-10-04-04

Near Associated Instrument Panel NO

Maintenance (M) 25-10-04-02 1. Move the affected armrest to the full up or down position.

2. Secure the armrest in place with strong cord or tape, making sure that the method, which is used to secure the armrest, does not interfere with crew movement or operations of any panels and/or controls.

3. If it is not possible to move the armrest to the full up or full down position, remove and securely stow the armrest.

25-10-04-04 Using the appropriate seat manual, secure the seat in the desired position.

NOTE: Refer to the appropriate Beechcraft Maintenance Manual and/or seat manual for information of the individual aircraft installation.


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25-20-01 Passengers Seat(s) Repair Category Number Installed


Item Remarks Or Exceptions -01 Passengers Seat(s) D 8 0 May be inoperative provided:

a) Seat does not block an Emergency Exit, b) Seat does not restrict any passenger from access to the

main aircraft aisle, and c) The affected Seat(s) are blocked and placarded

“DO NOT OCCUPY”.

NOTE: NOTE: A Seat with an inoperative Seat Belt or Shoulder Harness is considered inoperative.

-02 Seat Controls (Recline, Swivel, or Tracing)

D 8 0 May be inoperative and seat occupied provided seat is immovable in the taxi, takeoff, and landing position.


D 8 0 (M) May be inoperative and seat occupied provided seatback is secured in the taxi, takeoff, and landing position.


D 8 0 May be inoperative provided affected seat is considered inoperative.

-05 Armrest C 8 0 May be inoperative or missing and Seat occupied provided: a) Armrest does not block an Emergency Exit, b) Armrest does not restrict any passenger from access to the

main aircraft aisle, and c) For an armrest with a recline mechanism, seat is secure in

the upright position.


25-20-01-01 25-20-01-02 25-20-01-04 25-20-01-05

Prominent Position To Be Seen By Flight Crew

YES

25-20-01-03 Prominent Position To Be Seen By Flight Crew

NO

Maintenance (M) 25-20-01-03 Reference the appropriate vendor component maintenance manual.

1. If the recline mechanism is failed in the upright position and is locked in place, proceed to step 3.

2. If the seat back is failed in any other position and not locked in place, the recline lock mechanism must be manually locked with seat back in the upright position. Remove the recline cylinder and replace with a same length fixed rod or bar using the existing hardware.

3. Place a placard stating "RECLINE INOP - DO NOT USE" on the front of the seat.


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25-20-02 Non-Essential Equipment and Furnishings (NEF) Repair Category Number Installed


Item Remarks Or Exceptions -01 Non-Essential

Equipment and Furnishings (NEF)

- 0 May be inoperative, damaged, or missing provided that the item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures, and processes are outlined in the operators NEP Program Manual. (M) and (O) procedures, if required, must be available to the flightcrew and included in the operator’s appropriate document.

NOTE: Exterior Lavatory Door Ashtrays are not considered NEF items.


25-20-02-01 N/A YES


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25-20-03 Emergency Medical Services (EMS) Equipment (Medical Transport Equipment) Repair Category Number Installed


Item Remarks Or Exceptions -01 Emergency Medical

Services (EMS) Equipment (Medical Transport Equipment)

C 1 0 (M) May be inoperative provided inoperative system/component is deactivated and secured.

NOTE: Individual EMS components may be listed in the MEL provided the operator develops the procedure to deactivate the affected system/component and provides Remarks to restrict operations to patients not dependent on the inoperative system/component.



YES

Maintenance (M) Deactivate/secure inoperative equipment as required.


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25-25-01 “FASTEN SEAT BELT”/“FASTEN SEAT BELT WHILE SEATED” Signs or Placards Repair Category Number Installed


Item Remarks Or Exceptions -01 “FASTEN SEAT

BELT”/ “FASTEN SEAT BELT WHILE SEATED” Signs or Placards

C 2 1 One or more signs or placards may be illegible or missing provided a legible sign or placard is visible from each occupied passenger seat.



YES


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25-50-01 Cargo Restraint Systems Repair Category Number Installed


Item Remarks Or Exceptions -01 Cargo Restraint

Systems C 1 0 (M) May be inoperative, or missing provided acceptable cargo

loading limits from an approved source (i.e., an Approved Cargo Loading Manual, Cargo Handling Manual, or Weight and Balance Document) are observed.

-02 Cargo Restraint Systems

C 1 0 May be inoperative or missing provided affected compartment remains empty.


25-50-01-01 25-50-01-02


YES

Maintenance (M) 25-50-01-01 1. Using the weight and balance section of the POH/AFM, load the aircraft according to approved loading

zone and limitation data.

2. Any affected area must not have cargo loaded in that location.


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25-50-02 Cabin Storage Compartments/ Closets Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Storage

Compartments/ Closets

C 7 0 (M) May be inoperative provided: a) Procedures are established to secure compartment closed, b) Associated compartment is placarded “DO NOT USE”, c) Any emergency equipment located in affected

compartment is considered inoperative, and d) Affected compartment is not used for storage of any item(s)

except for those permanently affixed.

-02 Cabin Storage Compartments/ Closets

C 7 0 (M)(O) May be inoperative provided: a) Affected door is removed, b) Associated compartment is not used for storage of any

items, except those permanently affixed, c) Associated compartment is placarded “DO NOT USE”, and d) Passengers are briefed that associated compartment is not

used.

NOTE: Any permanently affixed Emergency Equipment located in the associated storage compartment is available for use.


25-50-02-01 25-50-02-02


YES

Maintenance (M) 25-50-02-01 Inoperative cabin and galley storage compartments and closets must be secured CLOSED as follows:

1. Remove loose items from affected location (If affixed, the item(s) must be relocated to another compartment or considered inoperative).

2. Close and latch affected Compartment/Closet (or use silver tape if needed) to secure affected door(s)/drawer(s) in CLOSED position.

3. Place a placard stating "INOP-DO NOT USE" next to the affected component's latch/handle assembly.

25-50-02-02 1. Remove the associated door.

2. Place a placard stating "INOP-DO NOT USE" next to the affected component's latch/handle assembly.

(Continued)


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Operations (O) 25-50-02-02 Ensure Passengers are briefed that associated compartment is not to be used..


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25-50-03 Wing Locker Door Gas Spring Repair Category Number Installed


Item Remarks Or Exceptions -01 Wing Locker Door

Gas Spring (Raisbeck Engineering STC only)

D 2 0 (M) May be inoperative provided: a) Gas spring shaft moves freely without impeding operation

of the door, and b) Affected Wing Locker Door closes flush with the nacelle.



YES

Maintenance (M) Ensure the following:

1. Gas spring shaft moves freely without impeding operation of the door.

2. Affected Wing Locker Door closes flush with the nacelle.


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25-60-01 Emergency Medical Equipment Repair Category Number Installed


Item Remarks Or Exceptions -01 First Aid Kit (FAK)

and/or Associated Equipment

D 1 1 Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative.



YES


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25-60-03 Emergency Vision Assurance System Repair Category Number Installed


Item Remarks Or Exceptions -01 Emergency Vision

Assurance System (STC SA1050WI)



25-60-03-01 Near Associated Item YES


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25-61-01 Flotation / Overwater Equipment Repair Category Number Installed


Item Remarks Or Exceptions -01 Life Preservers

(TSO-C13) D 11 0 May be inoperative or missing provided:

a) Power off gliding distance from shore is not exceeded, and

b) Distance of 50 nautical miles from nearest shore is not exceeded.

NOTE: One approved flotation device must be readily available to each occupant when conducting operations over water:

14 CFR REFERENCE: 14 CFR 135.167


25-61-01-01 Near Captains Instrument Panel YES


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25-62-01 Emergency Locator Transmitter (ELT) Repair Category Number Installed


Item Remarks Or Exceptions -01 Fixed ELTs A 1 0 May be inoperative or missing provided repairs are made

within 90 days.

-02 Remote Switch D 1 0 (M) May be inoperative provided: a) Remote switch is disconnected from the ELT, and b) ELT is ARMED.



YES


NO

Maintenance (M) 25-62-01-02 Remove wire from pin 11 on plug 2371P3 and ensure ELT is armed.


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ATA 26 Fire Protection

Chapter 26 Fire Protection Page Number

26-20-01 Engine Fire Extinguisher PUSH TO EXTINGUISH Guard .................................................. 26-2


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ATA 26 Fire Protection

26-20-01 Engine Fire Extinguisher PUSH TO EXTINGUISH Guard Repair Category Number Installed


Item Remarks Or Exceptions -01 Engine Fire

Extinguisher PUSH TO EXTINGUISH Guard

A 2 0 May be broken, missing, or lacking Safety Wire provided: a) Broken Guard shall not interfere with the proper indication

or activation of the Extinguisher, and b) Repairs are made within 1 flight day.


26-20-01-01 Near PUSH TO EXTINGUISH Guard YES


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ATA 27 Flight Controls

Chapter 27 Flight Controls Page Number

27-11-01 Aileron Trim Tab Indicator ........................................................................................................ 27-2

27-21-01 Rudder Trim Tab Indicator ........................................................................................................ 27-3

27-31-01 Electric Elevator Trim System ................................................................................................... 27-4

27-51-01 Flap Position Indicator .............................................................................................................. 27-5


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27-11-01 Aileron Trim Tab Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Aileron Trim Tab

Indicator C 1 0 May be inoperative provided:

a) Tab is visually checked for full range of operation, b) Tab operation is not restricted, and c) Tab is positioned to neutral prior to each departure and

neural position is verified by visual inspection.

NOTE: Controls must be held neutral to determine Tab Settings.


27-11-01-01 Near Trim Tab Indicator YES


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27-21-01 Rudder Trim Tab Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Rudder Trim Tab


a) Tab is visually checked for full range of operation, b) Tab operation is not restricted, and c) Tab is positioned to neutral prior to each departure and

neural position is verified by visual inspection.

NOTE: Controls must be held neutral to determine Tab Settings.


27-21-01-01 Near Trim Tab Indicator YES


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27-31-01 Electric Elevator Trim System Repair Category Number Installed


Item Remarks Or Exceptions -01 Electric Elevator

Trim System C 1 0 (M) May be inoperative provided:

a) Electric Trim is deactivated, b) Manual Trim is verified operative with full and free

movement, and c) Autopilot is considered inoperative.


-02 Electric Trim Switches


NOTE: Any operative Switch may be used.

-03 ELEC TRIM OFF (green) Annunciator


-04 Pitch Trim ON-OFF Switch

C 1 0 (M) May be inoperative provided: a) Electric Pitch Trim is deactivated, b) Manual Trim is verified operative, and c) Autopilot is considered inoperative.



27-31-01-01 thru

27-31-01-04

Near PITCH TRIM OFF Annunciation YES

Maintenance (M) 27-31-01-01 1. Operate all controls through their full range. No binding or resistance should be noted.

2. Conduct a functional check of the manual trim system to determine proper operation, full range of travel and freedom of movement.

3. Pull and collar the PITCH TRIM circuit breaker on the right side breaker panel.

27-31-01-04 1. Operate all controls through their full range. No binding or resistance should be noted.

2. Conduct a functional check of the manual trim system to determine proper operation, full range of travel and freedom of movement.


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27-51-01 Flap Position Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Flap Position


a) Flaps are visually checked for full travel and Flap operation is not restricted, and

b) Flaps are visually checked for proper setting prior to each departure.


27-51-01-01 Near Flap Position Indicator YES


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ATA 28 Fuel

Chapter 28 Fuel Page Number

28-22-01 Standby Electric Boost Pumps ................................................................................................. 28-2

28-23-01 Fuel Crossfeed Annunciation .................................................................................................... 28-3

28-24-01 Auxiliary Fuel Transfer System ................................................................................................. 28-4

28-40-01 Fuel Quantity Annunciator ........................................................................................................ 28-5

28-41-10 Fuel Quantity Indicator System ................................................................................................. 28-6


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ATA 28 Fuel

28-22-01 Standby Electric Boost Pumps Repair Category Number Installed


Item Remarks Or Exceptions -01 Standby Electric

Boost Pumps C 2 1 (M) One may be inoperative provided:

a) Affected pump is deactivated, b) AFM defined Emergency Engine Fuels are not used, c) AFM Limitations On Use Of Aviation Gasoline are

observed, and d) Aircraft is not operated more than 1 hour, at

one-engine-inoperative cruise, from a suitable airport.


28-22-01-01 Near Standby Electric Boost Pump Switch YES Maintenance (M) Pull and secure affected circuit breaker STANDBY PUMP (CB12 – LEFT ENGINE, CB2 – RIGHT ENGINE) on the left side fuel control circuit breaker panel.


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ATA 28 Fuel

28-23-01 Fuel Crossfeed Annunciation Repair Category Number Installed


Item Remarks Or Exceptions -01 Fuel Crossfeed

Annunciation (FUEL CROSSFEED )Ann. (green) (Fuel Crossfeed) CAS (cyan)

C 1 0 May be inoperative provided: a) Crossfeed System is verified operative prior to engine start,

and b) Both Fuel Pressure Annunciator Lights are operative.


28-23-01-01 Near Fuel Crossfeed Annunciator YES


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ATA 28 Fuel

28-24-01 Auxiliary Fuel Transfer System Repair Category Number Installed


Item Remarks Or Exceptions -01 Auxiliary Fuel

Transfer System C 2 0 May be inoperative provided:

a) Any fuel in affected Auxiliary Tank is considered unusable, b) AFM Fuel Imbalance Limitations are observed, and c) Auxiliary Tanks are not used.

-02 Auxiliary Fuel Transfer Annunciation (amber) (L or R NO FUEL XFR) Ann. (L or R No Fuel XFR) CAS

C 2 0 May be inoperative provided Auxiliary Tanks are not used.


28-24-01-01 28-24-01-02

Near Auxiliary Fuel Transfer Annunciation YES


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ATA 28 Fuel

28-40-01 Fuel Quantity Annunciator Repair Category Number Installed


Item Remarks Or Exceptions -01 Fuel Quantity

Annunciator (L or R FUEL QTY) Annunciator (L or R Fuel Quantity) CAS

C 2 1 One may be inoperative provided both Fuel Quantity Indicators are operative.


28-40-01-01 Near Fuel Quantity Annunciator YES


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ATA 28 Fuel

28-41-10 Fuel Quantity Indicator System Repair Category Number Installed


Item Remarks Or Exceptions -01 Fuel Quantity

Indicator System C 2 1 (O) One may be inoperative provided:

a) A reliable means is established to determine that fuel quantity on board meets the regulatory requirements for the flight,

b) Both Fuel Flow Indicators are operative, and c) Both Fuel Quantity Annunciators are operative.


28-41-10-01 Near Fuel Quantity Indicator YES Operations (O) 1. To achieve a known quantity in the affected tank, the tank may be defueled then fueled to a known

quantity. It may be completely fueled, or fuel may be transferred out of the tank until it is empty.

2. To track fuel use, operators may use a fuel log or develop their own procedure. This can include matched fuel flow techniques, use of the FMS fuel quantity system or other means.

3. Ensure there are no current logbook entries or deferrals related to the following:

A. Either Fuel Flow Indicators.

B. Either Fuel Quantity Annunciators.


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ATA 30 Ice and Rain Protection

Chapter 30 Ice and Rain Protection Page Number

30-00-10 Stall Warning Heat (Lift Transducer and Mounting Plate Heater) ............................................ 30-2

30-00-20 Engine Ice Vane Annunciation .................................................................................................. 30-3

30-10-01 Surface Deice System (Wings and Horizontal Stabilizer) ........................................................ 30-4

30-10-20 Surface Deice Annunciation ..................................................................................................... 30-5

30-20-01 Engine Inertial Ice Vane Actuator Motors ................................................................................. 30-6

30-30-01 Pitot Heaters ............................................................................................................................. 30-7

30-40-01 Windshield Wipers .................................................................................................................... 30-8

30-40-10 Windshield Heat ........................................................................................................................ 30-9

30-50-01 Heated Fuel Vents .................................................................................................................. 30-10

30-60-10 Propeller Deice System .......................................................................................................... 30-11


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30-00-10 Stall Warning Heat (Lift Transducer and Mounting Plate Heater) Repair Category Number Installed


Item Remarks Or Exceptions -01 Stall Warning Heat

(Lift Transducer and Mounting Plate Heater)

C 1 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions.


30-00-10-01 Near Pitot Heat Switch YES


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30-00-20 Engine Ice Vane Annunciation Repair Category Number Installed


Item Remarks Or Exceptions -01 Engine Ice Vane

Annunciation (L or R ENG ICE FAIL) Ann. (amber) (L and R ENG ANTI-ICE) Ann. (green) (L or R Engine Ice Fail) CAS (amber) (L or R Engine Anti-Ice) CAS (cyan)

C 4 2 (O) One may be inoperative on each side.

-02 Engine Ice Vane Annunciation (L or R ENG ICE FAIL) Ann. (amber) (L and R ENG ANTI-ICE) Ann. (green) (L or R Engine Ice Fail) CAS (amber) (L or R Engine Anti-Ice) CAS (cyan)

C 4 0 (M) Both may be inoperative on one or both sides provided: a) Inertial Ice Vanes are secured in the extended position, b) Appropriate Engine Anti-Ice On Performance data is used,

and c) Ambient surface temperature is +10 degrees C or below for

takeoff.


30-00-20-01 Near Engine Ice Vane Annunciation YES

30-00-20-02 Near Engine Ice Vane Annunciation NO Maintenance (M) 30-00-20-02 Manually extend the inertial ice vanes and secure in position. Reference 30-20 of the maintenance manual.

Operations (O) 30-00-20-01 Prior to each flight, the flight crew must verify operation of Ice Vane, and that the remaining annunciators are accurate.


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30-10-01 Surface Deice System (Wings and Horizontal Stabilizer) Repair Category Number Installed


Item Remarks Or Exceptions -01 Surface Deice

System (Wings and Horizontal Stabilizer)



30-10-01-01 Near Surface Deice Switches YES


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30-10-20 Surface Deice Annunciation Repair Category Number Installed


Item Remarks Or Exceptions -01 Surface Deice

Annunciation (WING DEICE & TAIL DEICE) Ann. (green) (Wing Deice & Tail Deice) CAS (cyan)



30-10-20-01 Near Surface Deice Annunciator YES


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30-20-01 Engine Inertial Ice Vane Actuator Motors Repair Category Number Installed


Item Remarks Or Exceptions -01 Engine Inertial Ice

Vane Actuator Motors

C 4 2 (O) One Actuator Motor on each inlet may be inoperative provided aircraft is not operated in visible moisture at +5 degrees C or below.

-02 Engine Inertial Ice Vane Actuator Motors

C 4 2 (O) One Actuator Motor on each inlet may be inoperative provided: a) Inertial Ice Vanes are in the extended position, b) Appropriate Engine Anti-Ice On Performance Data is used,

and c) Ambient temperature is +10 degrees C or below for takeoff.

-03 Engine Inertial Ice Vane Actuator Motors

C 4 0 (M) Both Actuator Motors of each Inlet may be inoperative provided: a) Inertial Ice Vanes are in the extended position, b) Appropriate Engine Anti-Ice On Performance Data is used,

and c) Ambient temperature is +10 degrees C or below for takeoff.


30-20-01-01 30-20-01-02

Near Engine Anti-Ice Switch YES

30-20-01-03 Near Engine Anti-Ice Switch NO Maintenance (M) 30-20-01-03 1. Fully manually extend the inertial ice vanes then pull and secure the following circuit breakers on the

A146 cockpit circuit breaker panel: engine anti-ice, LEFT STBY circuit breaker on the L GEN bus or L STBY ENG ANTI-ICE , engine anti-ice RIGHT STBY circuit breaker on the R GEN bus or R STBY ENG ANTI-ICE, MN ENG ANTI-ICE LEFT, or L MAIN ENGINE ANTI-ICE and MN ENG ANTI-ICE RIGHT, or R MAIN ENGINE ANTI-ICE circuit breakers on the triple-fed bus on the right circuit breaker panel. (nomenclatures may vary depending on model)

2. Place a placard with the wording "Inertial Ice Vanes Secured in Extended Position", and place the placard on the forward instrument panel in clear view of the aircrew, and airplane limited to 10° C or colder.

Operations (O) 30-20-01-01 Ensure aircraft is not operated in visible moisture at +5 degrees C or below.

30-20-01-02 1. Prior to each departure the flight crew will verify the Inertial Ice Vanes are in the extended position.

2. Flight crew will use the appropriate performance data for Engine Anti-Ice On for all phases of flight.

3. Flight crew will ensure that the ambient temperature is +10 degrees C or below for all phases of flight.


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30-30-01 Pitot Heaters Repair Category Number Installed


Item Remarks Or Exceptions -01 Pitot Heaters B 2 1 Right side may be inoperative provided:

a) SIC is not required, b) RVSM is not conducted, and c) Aircraft is not operated in known or forecast icing

conditions.


-02 Pitot Heaters C 2 0 May be inoperative provided: a) Aircraft is operated VFR only, and b) Aircraft is not operated in known or forecast icing

conditions.

-03 Pitot Heat Annunciation (amber) (L or R PITOT HEAT) Ann. (L or R Pitot Heat) CAS

C 2 0 (O) May be inoperative provided both pitot heaters are verified operative.


30-30-01-01 30-30-01-02 30-30-01-03

Near Pitot Heat Switch YES

Operations (O) 30-30-01-03 Flight crew will perform an operational check of the pitot heaters by engaging to ON and verifying heat form the pitot tubes.

CAUTION: Surface may be hot. Do not come into contact with skin as sever burning may occur. NOTE: Do not operate pitot heaters on ground for more than 5 min or damage may result.


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30-40-01 Windshield Wipers Repair Category Number Installed


Item Remarks Or Exceptions -01 Windshield Wipers C 2 0 May be inoperative provided aircraft is not operated in

precipitation within 5 nautical miles of the airport of takeoff or intended landing.


30-40-01-01 Near Windshield Wiper Switches YES


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30-40-10 Windshield Heat Repair Category Number Installed


Item Remarks Or Exceptions -01 Windshield Heat C 2 0 May be inoperative provided aircraft is not operated in known

or forecast icing conditions.


30-40-10-01 Near Windshield Heat Switch YES


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30-50-01 Heated Fuel Vents Repair Category Number Installed


Item Remarks Or Exceptions -01 Heated Fuel Vents C 2 0 May be inoperative provided aircraft is not operated in known



30-50-01-01 Near Engine Anti-Ice Switch YES


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30-60-10 Propeller Deice System Repair Category Number Installed


Item Remarks Or Exceptions -01 Propeller Deice

System C 1 0 May be inoperative provided aircraft is not operated in known


-02 Automatic Control C 1 0 May be inoperative provided Manual System is operative

-03 Manual Control C 1 0 May be inoperative provided Automatic System is operative.

-04 Propeller Deice Ammeter



30-60-10-01 thru

30-60-10-04

Near Prop Deice Switch YES


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ATA 31 Indicating / Recording Systems

Chapter 31 Indicating / Recording Systems Page Number

31-20-01 Clock With Sweep Second Hand or Electrical Digital Clock ............................................... 31-2

31-20-10 Flight Hour Recorder ........................................................................................................... 31-3

31-50-10 Unassigned Annunciators (---) ............................................................................................ 31-4


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31-20-01 Clock With Sweep Second Hand or Electrical Digital Clock Repair Category Number Installed


Item Remarks Or Exceptions -01 Clock With Sweep

Second Hand or Electrical Digital Clock

C 2 0 May be inoperative for VFR operation.

-02 Clock With Sweep Second Hand or Electrical Digital Clock



31-20-01-01 31-20-01-02

Near Associated Clock YES


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31-20-10 Flight Hour Recorder Repair Category Number Installed


Item Remarks Or Exceptions -01 Flight Hour

Recorder C 1 0 (O) May be inoperative provided procedures as noted in the

Operations procedure are followed to track flight time.


31-20-10-01 Near Flight Hour Meter YES Operations (O) 1. A clock is used to record the flight time. Aircraft flight time is recorded in hours and minutes and then

converted to hours and tenths and written on the flight log.

2. The maintenance personnel responsible for the aircraft's permanent maintenance logs shall record the time into summaries in the aircraft logbook, with special attention to the sequence of time to ensure that accurate times are recorded and tracked not only for the aircraft but also for other time limited maintenance items.

NOTE: A tenth of an hour is represented as 6 minutes. During conversion, it is necessary to round to the NEXT tenth of an hour. (Example: 122 Minute Flight time is recorded as 2.1 Hours).


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31-50-10 Unassigned Annunciators (---) Repair Category Number Installed


Item Remarks Or Exceptions -01 Unassigned

Annunciators (---) D 2 0 May be inoperative.


31-50-10-01 Near Annunciator YES


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ATA 32 Landing Gear

Chapter 32 Landing Gear Page Number

32-30-01 Hydraulic Fluid Low Annunciation ............................................................................................. 32-2

32-34-10 Landing Gear Control Down Lock Solenoid ............................................................................. 32-3

32-40-01 Parking Brake ........................................................................................................................... 32-4

32-60-01 Landing Gear Down Annunciator Lights (NOSE – L – R) (green) ............................................ 32-5

32-60-10 Landing Gear Control In-Transit Lights (Red) .......................................................................... 32-6


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ATA 32 Landing Gear

32-30-01 Hydraulic Fluid Low Annunciation Repair Category Number Installed


Item Remarks Or Exceptions -01 Hydraulic Fluid Low

Annunciation (amber) (HYD FLUID LOW) Ann. (Hyd Fluid Low) CAS

C 1 0 (M) May be inoperative provided hydraulic fluid level is verified full each flight day.


32-30-01-01 Near Hydraulic Fluid Low Annunciator NO Maintenance (M) A charging gauge is mounted on the landing gear accumulator. A fill reservoir, located above the power pack, contains a cap and dipstick assembly graduated in degrees of fluid temperature. Add hydraulic fluid as required to fill the system. Reference maintenance manual 12-10-05.


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ATA 32 Landing Gear

32-34-10 Landing Gear Control Down Lock Solenoid Repair Category Number Installed


Item Remarks Or Exceptions -01 Landing Gear

Control Down Lock Solenoid

C 1 0 (O) May be inoperative provided: a) Down Lock Latch is verified operative, and b) Down Lock Release Button is verified operative.


32-34-10-01 Near Landing Gear Control YES Operations (O) Depress the red button on the landing gear handle downlock latch and visibly observe the release operation of the latch. Release the red button and ensure that the latch returns to the latched position.


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ATA 32 Landing Gear

32-40-01 Parking Brake Repair Category Number Installed


Item Remarks Or Exceptions -01 Parking Brake C 1 0 (O) May be inoperative provided procedures as noted in the

Operations procedure are followed to prevent unintended movement when stopped or parked.


32-40-01-01 Near Parking Brake Handle YES Operations (O) 1. Parked aircraft must be chocked at all times.

2. During engine start, PIC will apply normal braking and take precautions that all persons are clear of the aircraft.

3. Do not stop aircraft on a sloping ramp unless there is someone there to chock the airplane while the PIC is holding the brakes, after engine shutdown.


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ATA 32 Landing Gear

32-60-01 Landing Gear Down Annunciator Lights (NOSE – L – R) (green) Repair Category Number Installed


Item Remarks Or Exceptions -01 Landing Gear Down

Annunciator Lights (NOSE – L – R) (green)

A 6 3 One Lamp in each Indicator may be inoperative provided: a) One Lamp in each Indicator is operative and provides

sufficient illumination for positive Down and Locked Indication, and

b) Repairs are made within 1 flight day.


32-60-01-01 Near Landing Gear Down Annunciator YES


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ATA 32 Landing Gear

32-60-10 Landing Gear Control In-Transit Lights (Red) Repair Category Number Installed


Item Remarks Or Exceptions -01 Landing Gear

Control In-Transit Lights (Red)

C 2 1 One Bulb may be inoperative provided all Landing Gear Down Annunciator Lights are operative.


32-60-10-01 Near In-Transit Light YES


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ATA 33 Lights

Chapter 33 Lights Page Number

33-10-10 Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System ........................... 33-2

33-20-01 Passenger Notice Signs ........................................................................................................ 33-3

33-20-10 Cabin Lights ........................................................................................................................... 33-4

33-30-20 Boarding Lighting System ..................................................................................................... 33-5

33-30-10 Baggage Compartment Lights ............................................................................................... 33-6

33-40-01 Strobe Lights System ............................................................................................................ 33-7

33-40-10 Taxi Light ............................................................................................................................... 33-8

33-40-20 Landing Lights ....................................................................................................................... 33-9

33-40-40 Position Lights ..................................................................................................................... 33-10

33-40-50 Anti-Collision Beacon Light System .................................................................................... 33-11

33-40-60 Recognition Lights ............................................................................................................... 33-12

33-40-70 Wing Ice Inspection Light .................................................................................................... 33-13

33-40-80 Logo Lights .......................................................................................................................... 33-14

33-50-80 Emergency Instrument Light System .................................................................................. 33-15


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ATA 33 Lights

33-10-10 Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System Repair Category Number Installed


Item Remarks Or Exceptions -01 Cockpit/Flight

Deck/Flight Compartment and Instrument Lighting System (excludes indication lighting)

C 1 0 May be inoperative provided the aircraft is not operated at night.

-02 Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System (excludes indication lighting)

C 1 0 Individual Lights may be inoperative provided remaining Lights are: a) Sufficient to clearly illuminate all required instruments,

controls, and other devices for which it is provided, b) Positioned so that direct rays are shielded from flightcrew

members’ eyes, and c) Lighting configuration and intensity is acceptable to the

flightcrew.


33-10-10-01 33-10-10-02

Near Associated Control YES


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ATA 33 Lights

33-20-01 Passenger Notice Signs Repair Category Number Installed


Item Remarks Or Exceptions -01 Passenger Notice

Signs (Fasten Seat Belt) (No Smoking)

C 2 0 (O) Procedures as noted in the Operations procedure are followed to verbally brief the passengers.


33-20-01-01 Near Switch YES Operations (O) 1. Notify the passengers before the flight that the NO SMOKING and FASTEN SEAT BELT signs are

inoperative and that you will give the appropriate verbal commands from the cockpit during flight.

2. Utilize the passenger address (PA) system (If available) or keep the cockpit divider open during flight to be able to give verbal commands or authorizations to the passengers.


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ATA 33 Lights

33-20-10 Cabin Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Lights D 11 0 May be inoperative provided:

a) No Passengers are carried, and b) Cabin Emergency Exit Lighting is operative.

-02 Cabin Lights C 11 0 (O) May be partially inoperative provided: a) Cabin Emergency Exit Lighting is operative, b) Sufficient Lighting is available for crew to perform

required duties, c) Sufficient Lighting is operative for passenger carrying

operations at night, and d) Both Cabin Exit Lights are operative.


33-20-10-01 33-20-10-02

Near Associated Light Control YES

Operations (O) 33-20-10-02 During the Cockpit/Cabin Inspection, make sure all Emergency Exit and Cabin Exit lights are operative.


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ATA 33 Lights

33-30-20 Boarding Lighting System Repair Category Number Installed


Item Remarks Or Exceptions -01 Boarding Lighting

System (Includes Lights Within the Airstair and in the Entryway Foyer)

C 1 0 May be inoperative provided both Cabin Exit Lights are operative.

NOTE: Any operative light(s) may be used.


33-30-20-01 Near Associated Switch YES


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ATA 33 Lights

33-30-10 Baggage Compartment Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Baggage

Compartment Lights C 1 0 May be inoperative.


33-30-10-01 Near Baggage Compartment Light Switch YES


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ATA 33 Lights

33-40-01 Strobe Lights System Repair Category Number Installed


Item Remarks Or Exceptions -01 Strobe Lights

System (excluding Anti-Collision lights)



33-40-01-01 Near Strobe Light Switch YES


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ATA 33 Lights

33-40-10 Taxi Light Repair Category Number Installed


Item Remarks Or Exceptions -01 Taxi Light C 1 0 May be inoperative.


33-40-10-01 Near Taxi Light Switch YES


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ATA 33 Lights

33-40-20 Landing Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Landing Lights C 2 1 One may be inoperative.

-02 Landing Lights C 2 0 Both may be inoperative provided the aircraft is not operated at night.


33-40-20-01 33-40-20-02

Near Landing Light Switch YES


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ATA 33 Lights

33-40-40 Position Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Position Lights C 3 0 May be inoperative sunrise to sunset.


33-40-40-01 Near Position Light Switch YES


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ATA 33 Lights

33-40-50 Anti-Collision Beacon Light System Repair Category Number Installed


Item Remarks Or Exceptions -01 Anti-Collision

Beacon Light System

B 1 0 May be inoperative provided the aircraft is not operated at night.


33-40-50-01 Near Anti-Collision Switch YES


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ATA 33 Lights

33-40-60 Recognition Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Recognition Lights C 2 0 May be inoperative.


33-40-60-01 Near Recognition Light Switch YES


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ATA 33 Lights

33-40-70 Wing Ice Inspection Light Repair Category Number Installed


Item Remarks Or Exceptions -01 Wing Ice Inspection

Light C 2 0 May be inoperative provided:

a) Aircraft is not operated in known or forecast icing conditions at night, and

b) Ground deicing procedures do not require use of Wing Ice Lights.

-02 Wing Ice Inspection Light

C 2 1 One may be inoperative provided: a) The left light is operative for single-pilot operations, and b) Ground deicing procedures do not require use of Wing Ice

Lights.


33-40-70-01 33-40-70-02

Near Wing Ice Inspection Light Switch YES


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ATA 33 Lights

33-40-80 Logo Lights Repair Category Number Installed


Item Remarks Or Exceptions -01 Logo Lights C 2 0 May be inoperative.


33-40-80-01 Near Logo Light Switch YES


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ATA 33 Lights

33-50-80 Emergency Instrument Light System Repair Category Number Installed


Item Remarks Or Exceptions -01 Emergency

Instrument Light System

C 1 0 May be inoperative for Day VFR operations.


33-50-80-01 Near Captains Instrument Panel YES


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ATA 33 Lights



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ATA 34 Navigation

Chapter 34 Navigation Page Number

34-13-01 Vertical Speed Indicators .......................................................................................................... 34-2

34-16-20 Altitude Alerting System ............................................................................................................ 34-3

34-21-10 Standby Attitude Indicator ......................................................................................................... 34-4

34-22-30 Radio Magnetic Indicator .......................................................................................................... 34-5

34-23-01 Non-Stabilized Magnetic Compass........................................................................................... 34-6

34-31-01 ILS Systems .............................................................................................................................. 34-7

34-32-01 Glide Slope ............................................................................................................................... 34-8

34-34-01 Marker Beacon System ............................................................................................................ 34-9

34-42-00 Weather Radar ........................................................................................................................ 34-10

34-42-10 Thunderstorm Detection Equipment ....................................................................................... 34-11

34-44-10 Radar Altimeter ....................................................................................................................... 34-12

34-44-12 Terrain Awareness and Warning System Class B .................................................................. 34-13

34-45-10 Traffic Alert and Collision Avoidance System ......................................................................... 34-15

34-50-10 Area Navigation ...................................................................................................................... 34-17

34-51-10 Distance Measuring Equipment (DME) Systems ................................................................... 34-18

34-52-01 ATC Transponders and Automatic Altitude Reporting Systems ............................................. 34-19

34-54-01 VHF Omni Range Systems (VOR) ......................................................................................... 34-20

34-55-10 Automatic Direction Finder (ADF) ........................................................................................... 34-21

34-61-10 Flight Management System .................................................................................................... 34-22


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ATA 34 Navigation

34-13-01 Vertical Speed Indicators Repair Category Number Installed


Item Remarks Or Exceptions -01 Vertical Speed

Indicators B 2 0 May be inoperative provided aircraft is operated VFR only.


34-13-01-01 Near Vertical Speed Indicator YES


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ATA 34 Navigation

34-16-20 Altitude Alerting System Repair Category Number Installed


Item Remarks Or Exceptions -01 Altitude Alerting

System A 1 0 (O) May be inoperative provided:

a) Autopilot with Altitude Hold is operative, b) Aircraft is not operated RVSM, c) Enroute operations do not require its use, and d) Repairs are made within 3 flight days.


-02 Altitude Alerting System

A 1 0 (O) May be inoperative provided: a) Aircraft is operated with a Second-in-Command, b) Aircraft is not operated RVSM, c) Enroute operations do not require its use, and d) Repairs are made within 3 flight days.



34-16-20-01 34-16-20-02

Near Altitude Alerting Panel YES

Operations (O) 34-16-20-01 1. Crew briefings must include a reminder that the altitude alerting system is inoperative.

2. The flight crew will use aural callouts pertaining to approach target altitudes as assigned by ATC or depicted on approach charts.

3. Ensure there are no current logbook entries or deferrals related to the Autopilot Altitude Hold function.

34-16-20-02

1. Crew briefings will make reference to inoperative altitude alerting system.

2. When flying with an inoperative altitude alerting system be especially careful of flying through assigned altitudes (climbing or descending) or drifting off of an assigned altitude. To avoid such:

3. When within 1,000 feet of an assigned altitude the pilot not flying will announce:

"Out of xxxx feet (or FL) for xxx feet (or FL)"

4. When within 300 feet of an assigned altitude either climbing, descending or drifting off of an assigned altitude the pilot not flying would state:

"Altitude - Altitude"


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ATA 34 Navigation

34-21-10 Standby Attitude Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Standby Attitude

Indicator B 1 0 May be inoperative provided:

a) Operations are conducted in Day VMC only, and b) Operations are not conducted into known or forecast

over-the-top conditions.


34-21-10-01 Near Standby Attitude Indicator YES


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ATA 34 Navigation

34-22-30 Radio Magnetic Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Radio Magnetic

Indicator (RMI) C 2 0 May be inoperative provided:

a) Magnetic Compass is operative, and b) Any navigation source not displayed on another indicator is

considered inoperative.


34-22-30-01 Near Associated RMI YES


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ATA 34 Navigation

34-23-01 Non-Stabilized Magnetic Compass Repair Category Number Installed


Item Remarks Or Exceptions -01 Non-Stabilized

Magnetic Compass B 1 0 (O) May be inoperative provided any combination of three

Gyro, AHRS, or INS (IRU) Stabilized Compass Systems are operative.

-02 Non-Stabilized Magnetic Compass

B 1 0 (O) May be inoperative provided: a) Any combination of two Gyro, AHRS or INS (IRU)

Stabilized Compass Systems operate normally, and b) Airplane is operated with Dual Independent Navigation

Capability and under Positive Radar Control by ATC on the enroute portion of the flight.


34-23-01-01 34-23-01-02

Near STBY Compass YES

Operations (O) 34-23-01-01 Ensure that combinations of three gyro or INS (IRU) stabilized compass systems are operative.

34-23-01-02

Ensure that either two gyros or INS (IRU) stabilized compass systems operate normally, or the airplane is operated with DUAL independent navigation capability and under positive radar control by ATC on the enroute portion of the flight.


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ATA 34 Navigation

34-31-01 ILS Systems Repair Category Number Installed


Item Remarks Or Exceptions -01 ILS Systems

(localizer only) C 2 0 May be inoperative provided approach procedures do not

require use of ILS.

NOTE: See Item 34-54-01 for VOR.



34-31-01-01 Near Nav Panel YES


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ATA 34 Navigation

34-32-01 Glide Slope Repair Category Number Installed


Item Remarks Or Exceptions -01 Glide Slope C 2 0 May be inoperative provided approach procedures do not

require use of Glide Slope.





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ATA 34 Navigation

34-34-01 Marker Beacon System Repair Category Number Installed


Item Remarks Or Exceptions -01 Marker Beacon

System C 2 0 May be inoperative provided approach procedures do not

require use of Marker Beacon.





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ATA 34 Navigation

34-42-00 Weather Radar Repair Category Number Installed


Item Remarks Or Exceptions -01 Weather Radar C 1 0 With radar systems inoperative, do not operate the aircraft in

IFR or night VFR conditions when current weather reports indicate that thunderstorms, or other potentially hazardous weather conditions that can be detected with airborne weather radar, may be reasonably be expected along the route to be flown. ER operations are not authorized.


-02 Weather Radar (Radar Antenna Gyro Stabilization)

C 1 0 May be inoperative provided: a) Antenna sweep is parallel with lateral axis, and b) Antenna tilt control is operative.


34-42-00-01 34-42-00-02

Near Weather Radar Indication YES


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ATA 34 Navigation

34-42-10 Thunderstorm Detection Equipment Repair Category Number Installed


Item Remarks Or Exceptions -01 Thunderstorm

Detection Equipment

C 1 0 May be inoperative provided Weather Radar operates normally.


-02 Thunderstorm Detection Equipment

C 1 0 With Thunderstorm Detection Equipment and Weather Radar systems inoperative, do not operate the aircraft in IFR or night VFR conditions when current weather reports indicate that thunderstorms, or other potentially hazardous weather conditions that can be detected with airborne weather radar, may be reasonably be expected along the route to be flown. ER operations are not authorized.



34-42-10-01 34-42-10-02


YES


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ATA 34 Navigation

34-44-10 Radar Altimeter Repair Category Number Installed


Item Remarks Or Exceptions -01 Radar Altimeter C 1 0 (M)(O) May be inoperative provided:

a) Class A TAWS and/or GPWS are considered inoperative, b) TCAS II is considered inoperative, c) Approach procedures do not require its use, and d) Procedures as noted in the Operations procedure are

followed.


34-44-10-01 Near Radar Altimeter Indication YES Maintenance (M) Pull and secure the RADIO ALTM circuit breaker on the right side circuit breaker panel.

Operations (O) 1. Pre-Flight planning shall include the inoperative radio altimeter and operations must not require the use

of TCAS, TAWS or GPWS.

2. Copilot will call out altitudes during approach including minimum altitudes.

NOTE 1: TCAS II is inoperative and red RA flag on the PFD will remain. NOTE 2: As per Part 91, Appendix A, a radio altimeter or marker beacon receiver providing aural and visual

indications of the inner marker is required for Category II and Category Ill operations with decision heights below 150 feet.


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ATA 34 Navigation

34-44-12 Terrain Awareness and Warning System Class B Repair Category Number Installed


Item Remarks Or Exceptions Terrain Awareness

and Warning System (TAWS) (Class B required by 14 CFR)


-01 Ground Proximity Warning System (GPWS)

A 1 0 (O) May be inoperative provided: a) Procedures as noted in the Operations procedure are

followed, and b) Repairs are made within 2 flight days.

-02 Modes 1 and 3 A 2 0 (O) May be inoperative provided: a) Procedures as noted in the Operations procedure are

followed, and b) Repairs are made within 2 flight days.

-03 Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative, and b) Repairs are made within 2 flight days.

-04 Modes 2, 4, and 5 C 3 0 May be inoperative.

-05 Advisory Callouts B 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are followed.

-06 Terrain System-Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions

B 1 0 May be inoperative.

-07 Terrain Displays C 3 0 May be inoperative.


34-44-12-01 Thru

34-44-12-07

Near GPWS Indication YES

Operations (O) 34-44-12-01, 34-44-12-02 1. Crew briefings will include aural callouts through use of appropriate aircraft equipment to ensure obstacle

and terrain clearance.

2. Flight crew will review MEA, MSA, DH, MDA, as appropriate of the route being flown.

3. Flight manual and operating manual can be consulted for climb gradients available for the phase of flight being approached, and the ambient conditions (weight, temp, altitude).

(Continued)


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ATA 34 Navigation

34-44-12-05

NOTE: Advisory callouts may also be referred to as “Mode 6” or “Altitude Callouts” in the GPWS Pilots Guide.

Crew briefings must include aural callouts during approach through the use of appropriate aircraft equipment to make sure obstacle and terrain clearance. Briefing must include MDA or DH and a procedure for a crew member to call out 500 feet above airport elevation, and any other agreed upon by the flight crew.


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ATA 34 Navigation

34-45-10 Traffic Alert and Collision Avoidance System Repair Category Number Installed


Item Remarks Or Exceptions -01 Traffic Alert and

Collision Avoidance System (TCAS II)

C 1 0 (M) May be inoperative provided: a) System is deactivated and secured, and b) Enroute or approach procedures do not require its use.


-02 Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System(s)

C 2 1 May be inoperative on the non-flying pilot side provided: a) TA and RA visual display is operative on the flying pilot

side, and b) TA and RA audio function is operative on the flying pilot

side.

-03 Resolution Advisory (RA) Display System(s)

C 2 1 May be inoperative on non-flying pilot side.

-04 Resolution Advisory (RA) Display System(s)

C 1 0 (O) May be inoperative provided: a) Traffic Alert (TA) visual display and audio functions are

verified operative, b) TA ONLY Mode is selected by the crew, and c) Enroute or approach procedures do not require its use.

-05 Traffic Alert (TA) Display System(s)

C 1 0 (O) May be inoperative provided: a) RA visual display and audio functions are verified

operative, and b) Enroute or approach procedures do not require its use.

-06 Audio Functions B 1 0 May be inoperative provided enroute or approach procedures do not require use of TCAS.


34-45-10-01 Thru

34-45-10-06

Near TCAS Panel YES

Maintenance (M) 34-45-10-01 Pull and secure the CB 120 “TCAS" circuit breaker.

(Continued)


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ATA 34 Navigation

Operations (O) 34-45-10-04 1. Using test function, confirm that traffic advisory display elements and voice command audio functions are

operative.

2. Select TA only mode of operation.

34-45-10-05 During the Before Taxi: Avionics check, verify a Resolution Advisory along with the aural warning when the TCAS is tested.


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ATA 34 Navigation

34-50-10 Area Navigation Repair Category Number Installed


Item Remarks Or Exceptions -01 Area Navigation

(RNAV) (FMS)

C 1 0 May be inoperative provided approach procedures do not require use of FMS.

NOTE: RNAV Systems identified as FMS must only defer FMS functions limited to navigation and not affecting operation of other aircraft systems.


-02 Area Navigation (RNAV) (GPS)

C 1 0 May be inoperative provided approach procedures do not require use of GPS.


-03 Navigation Databases (FMS)

C 1 0 (O) May be out of currency provided: a) Current aeronautical charts are used to verify navigation

fixes prior to each departure, b) Procedures as noted in the Operations procedure are

followed to verify status and suitability of navigation facilities used to define route of flight,

c) Approach navigation radios are manually tuned and identified, and

d) RNAV departures, RNAV arrivals, RNAV instrument approaches, and published RNAV routes based on RNAV guidance are not used.


34-50-10-01 34-50-10-02 34-50-10-03

Near Associated Control Panel YES

Operations (O) 34-50-10-03 The navigation database can only be used for enroute and terminal navigation when out of currency. Before using the FMS to navigate to a facility, verify the status, identifier, frequency and lat/long position with an alternate, current source of information.


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ATA 34 Navigation

34-51-10 Distance Measuring Equipment (DME) Systems Repair Category Number Installed


Item Remarks Or Exceptions -01 Distance Measuring

Equipment (DME) Systems

C 1 0 May be inoperative provided a suitable operative RNAV system is available for DME substitution.

-02 Distance Measuring Equipment (DME) Systems

C 1 0 May be inoperative provided operations do not require the use of DME.


34-51-10-01 34-51-10-02

Near DME Indication YES


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ATA 34 Navigation

34-52-01 ATC Transponders and Automatic Altitude Reporting Systems Repair Category Number Installed


Item Remarks Or Exceptions -01 ATC Transponders

and Automatic Altitude Reporting Systems

B 2 0 May be inoperative provided: a) Operations do not require its use, and b) Prior to flight, approval is obtained from ATC facilities

having jurisdiction over the planned route of flight.


-02 ATC Transponders and Automatic Altitude Reporting Systems

D 2 1 May be inoperative.

14 CFR REFERENCE: 14 CFR 91.130, 91.131, 91.135, 91.215

-03 Control Wheel Transponder Ident Switch (separate transponder unit)

C 2 0 May be inoperative provided Transponder Ident Selection is operative.


34-52-01-01 34-52-01-02 34-52-01-03

Near Transponder Panel YES


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ATA 34 Navigation

34-54-01 VHF Omni Range Systems (VOR) Repair Category Number Installed


Item Remarks Or Exceptions -01 VHF Omni Range

Systems (VOR) C 2 0 May be inoperative provided approach procedures do not

require use of VOR.





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ATA 34 Navigation

34-55-10 Automatic Direction Finder (ADF) Repair Category Number Installed


Item Remarks Or Exceptions -01 Automatic Direction

Finder (ADF) C 1 0 May be inoperative provided operations do not require the use

of ADF.




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ATA 34 Navigation

34-61-10 Flight Management System Repair Category Number Installed


Item Remarks Or Exceptions -01 Flight Management

System (Aircraft Integrated Systems)

A 1 0 May be inoperative provided: a) Operations do not require its use, b) Affected systems are identified and considered inoperative,

and c) Repairs are made within 2 flight cycles.

NOTE: Navigation functions and systems identified as FMS that provide only navigation functions are deferred with Area Navigation.


34-61-10-01 Near Associated FMC Control YES


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ATA 35 Oxygen

Chapter 35 Oxygen Page Number

35-00-01 External Oxygen Gauge ........................................................................................................... 35-2

35-20-00 Passenger Oxygen System ...................................................................................................... 35-3

35-20-10 Passenger Oxygen Mask .......................................................................................................... 35-4


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ATA 35 Oxygen

35-00-01 External Oxygen Gauge Repair Category Number Installed


Item Remarks Or Exceptions -01 External Oxygen

Gauge C 1 0 (M) May be inoperative provided the Internal Oxygen Gauge is

monitored during servicing to avoid over-servicing.


35-00-01-01 Near External Oxygen Gauge NO Maintenance (M) A crewmember or qualified mechanic shall occupy the cockpit and monitor the oxygen pressure while another maintenance personnel services the oxygen.


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ATA 35 Oxygen

35-20-00 Passenger Oxygen System Repair Category Number Installed


Item Remarks Or Exceptions -01 Passenger Oxygen

System C 1 0 May be inoperative provided flight is conducted at or below

10,000 feet MSL.

NOTE: Cockpit Crew Oxygen System must be operative.




YES


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ATA 35 Oxygen

35-20-10 Passenger Oxygen Mask Repair Category Number Installed


Item Remarks Or Exceptions -01 Passenger Oxygen

Mask C 11 0 (M) May be inoperative provided:

a) Corresponding Passenger Seat is blocked and placarded “DO NOT OCCUPY”, and

b) Affected Mask does not permit flow when Cabin Oxygen System is activated.



NO

Maintenance (M) 1. If necessary, remove the affected mask cover (lid).

2. Using a tie wrap or other appropriate device, secure the affected mask lanyard to the shutoff valve.

3. Replace the cover (lid) provided the cover is not being deferred in addition to the mask.


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ATA 37 Vacuum / Pressure

Chapter 37 Vacuum / Pressure Page Number

37-10-00 Instrument Air Valve ................................................................................................................. 37-2

37-20-00 Suction Gauge .......................................................................................................................... 37-3


\


37-10-00 Instrument Air Valve Repair Category Number Installed


Item Remarks Or Exceptions -01 Instrument Air Valve C 2 1 (O) One may be inoperative provided:

a) Inoperative Valve is verified closed, b) Aircraft is not operated in known or forecast icing

conditions, and c) Aircraft is operated at or below Flight Level 250.


37-10-00-01 Near Instrument Air Valve Control YES Operations (O) 1. Start the engine on the inoperative side, and with the other engine shutdown, select the inoperative

BLEED AIR VALVE to the PNEU & ENVIR OFF position.

2. Verify the PNEUMATIC PRESSURE gauge indicates Zero or near zero.

3. Keep inoperative valve closed.

4. Do not operate aircraft in known or forecast icing conditions.

5. Operate aircraft at or below FL250.


\


37-20-00 Suction Gauge Repair Category Number Installed


Item Remarks Or Exceptions -01 Suction Gauge C 1 0 May be inoperative provided aircraft is not operated in known



37-20-00-01 Near Suction Gauge YES


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ATA 38 Water / Waste

Chapter 38 Water / Waste Page Number

38-30-00 Lavatory Waste Systems (Electric Circulation Toilet) ............................................................... 38-2


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ATA 38 Water / Waste

38-30-00 Lavatory Waste Systems (Electric Circulation Toilet) Repair Category Number Installed


Item Remarks Or Exceptions -01 Lavatory Waste

Systems (Electric Circulation Toilet)

C 1 0 (M) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have

leaks.

NOTE: Any portion of the system which operates normally may be used

-02 Lavatory Waste Systems (Electric Circulation Toilet)

D 1 0 (M) May be inoperative provided: a) Toilet system is deactivated, b) Toilet Assembly is inspected for leaks, and c) Toilet is placarded “INOPERATIVE – DO NOT USE”.



NO


Place INOPERATIVE - DO NOT ENTER placard on Lavatory Door

Place DO NOT SERVICE placard on inside of Lavatory Service Door

NO

Maintenance (M) 38-30-00-01, 38-30-00-02 Refer to the maintenance manual chapter 38-30-00 for deactivation and chapter 12-20-09 for servicing.


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Chapter 46 Information Systems Page Number

46-10-10 Integrated Flight Information System ........................................................................................... 46-2


\


46-10-10 Integrated Flight Information System Repair Category Number Installed


Item Remarks Or Exceptions Integrated Flight

Information System NOTE: Single FSU is not authorized for sole source of

aeronautical information.

-01 File Server Unit (FSU) (FSU INOP Message)

C 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are used to ensure all information pertinent to the flight is accessible at the pilot station in current and appropriate form.

NOTE: If alternate source is electronic, dual redundancy is required for operation.

-02 Cursor Control Panel (CCP)

C 1 0 (O) May be inoperative provided procedures as noted in the Operations procedure are used to ensure all information pertinent to the flight is accessible at the pilot station in current and appropriate form.

NOTE: If alternate source is electronic, dual redundancy is required for operation.

-03 XM Satellite Weather System



46-10-10-01 46-10-10-02 46-10-10-03

Near CCP YES

Operations (O) 46-10-10-01 As an alternative to electronic charts, a current (paper or electronic) copy of navigational en route, terminal area, and instrument approach procedure charts applicable to the route being flown will be onboard prior to departure.

46-10-10-02

Traditional paper data will be carried and used for intended flight.

or

Operations are to be conducted in accordance with FAA approved EFB Policy and procedures manual.


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ATA 52 Doors

Chapter 52 Doors Page Number

52-10-10 Cabin Door Snubber ................................................................................................................. 52-2

52-10-11 Cabin Door Cable Covers ......................................................................................................... 52-3

52-10-20 Cabin Door Seal ........................................................................................................................ 52-4

52-70-02 Cabin Door Annunciation (red) (DOOR UNLOCKED) Ann. (Door Unlocked) CAS ................. 52-5

52-70-10 Cabin Door Lock and Upper Door Latch Observation Light System ........................................ 52-6


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ATA 52 Doors

52-10-10 Cabin Door Snubber Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Door Snubber C 1 0 (O) May be inoperative provided precautions are used when

opening.



YES

Operations (O) 1. The flight crew should brief any occupants that the main cabin door snubber is inoperative.

2. When opened, the step cable should be used to ease the step down until it is fully deployed and the stay is resting on the fuselage. Do not allow the door to freefall.

3. Brief ground crew of inoperative snubber to prevent injury to ground crew or damage to door.


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ATA 52 Doors

52-10-11 Cabin Door Cable Covers Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Door Cable

Covers D 2 0 May be damaged or missing provided it does not interfere with

normal operation of the Cabin Door.



YES


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ATA 52 Doors

52-10-20 Cabin Door Seal Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Door Seal C 1 0 May be damaged and/or inoperative provided:

a) Door Seal does not interfere with door operation, and b) Cabin Pressurization System is considered inoperative.



YES


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ATA 52 Doors

52-70-02 Cabin Door Annunciation (red) (DOOR UNLOCKED) Ann. (Door Unlocked) CAS Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Door

Annunciation (red) (DOOR UNLOCKED) Ann. (Door Unlocked) CAS

C 1 0 May be inoperative provided a crewmember confirms, by visual inspection, that all monitored doors are closed and latched prior to each departure.


52-70-02-01 Near DOOR UNLOCKED Annunciator YES


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ATA 52 Doors

52-70-10 Cabin Door Lock and Upper Door Latch Observation Light System Repair Category Number Installed


Item Remarks Or Exceptions -01 Cabin Door Lock

and Upper Door Latch Observation Light System

C 1 0 May be inoperative provided a crewmember confirms, by visual inspection, using a flashlight that latches are in the locked position prior to each departure.



YES


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ATA 61 Propellers

Chapter 61 Propellers Page Number

61-21-01 Propeller Synchrophase Synchronizer System ........................................................................ 61-2

61-23-01 Autofeather Annunciation (amber) (AUTOFTHER OFF) Ann. (Autofeather Off) CAS ............. 61-3


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ATA 61 Propellers

61-21-01 Propeller Synchrophase Synchronizer System Repair Category Number Installed


Item Remarks Or Exceptions -01 Propeller

Synchrophaser/ Synchronizer System


-02 Propeller Synchroscope



61-21-01-01 61-21-01-02

Near Propeller Synchrophaser YES


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ATA 61 Propellers

61-23-01 Autofeather Annunciation (amber) (AUTOFTHER OFF) Ann. (Autofeather Off) CAS

Repair Category Number Installed


Item Remarks Or Exceptions -01 Autofeather

Annunciation (amber) (AUTOFTHER OFF) Ann. (Autofeather Off) CAS

A 1 0 May be inoperative provided: a) Auto Feather Switches remain in the ARM position for the

entire flight, and b) Repairs are made within 3 flight days.


61-23-01-01 Near Propeller AUTOFTHER OFF Annunciator

YES


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ATA 61 Propellers



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Chapter 73 Engine Fuel and Control Page Number

73-31-01 Fuel Flow Indicators .................................................................................................................. 73-2


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73-31-01 Fuel Flow Indicators Repair Category Number Installed


Item Remarks Or Exceptions -01 Fuel Flow Indicators B 2 1 (M) One may be inoperative provided both Fuel Quantity

Indicating Systems are operative.


73-31-01-01 Near Fuel Flow Indicator YES Maintenance (M) With the aircraft positioned on a level surface, apply electrical power to the aircraft and verify that the cockpit fuel quantity indicators are operative and fuel quantity onboard correlates to that indicated by the FQIS. Verify fuel flow transducer is not leaking.


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ATA 74 Ignition

Chapter 74 Ignition Page Number

74-00-01 L or R IGNITION ON Annunciator (green) ................................................................................ 74-2


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ATA 74 Ignition

74-00-01 L or R IGNITION ON Annunciator (green) Repair Category Number Installed


Item Remarks Or Exceptions -01 L or R IGNITION ON

Annunciator (green) A 2 1 May be inoperative in the illuminated condition provided

repairs are accomplished within 3 flight days.


74-00-01-01 Near IGNITION ON Annunciator YES


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ATA 77 Engine Indicating

Chapter 77 Engine Indicating Page Number

77-12-01 Dual Function Torque Indicator ............................................................................................. 77-2

77-14-01 Dual Function N1 Indicator .................................................................................................... 77-3


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77-12-01 Dual Function Torque Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Dual Function

Torque Indicator C 2 0 Digital function only may be inoperative.


77-12-01-01 Near Dual Function Torque Indicator YES


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77-14-01 Dual Function N1 Indicator Repair Category Number Installed


Item Remarks Or Exceptions -01 Dual Function N1

Indicator C 2 0 Digital function only may be inoperative.


77-14-01-01 Near Dual Function N1 Indicator YES


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ATA 79 Engine Oil

Chapter 79 Engine Oil Page Number

79-30-01 Oil Pressure Annunciation ........................................................................................................ 79-2


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ATA 79 Engine Oil

79-30-01 Oil Pressure Annunciation Repair Category Number Installed


Item Remarks Or Exceptions -01 Oil Pressure

Annunciation (red) (L or R OIL PRES LO) Ann, (L or R or L-R Oil Press Low) CAS

C 2 1 One may be inoperative provided corresponding oil pressure gauge is operative and monitored.


79-30-01-01 Near Oil Pressure Annunciator YES

Millbrook Aviation Minimum Equipment List Aircraft: B-300 Revision No: Original Date: 11-18-16 Page 1

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Index

A

AC Inverters ................................................................................................................................................ 24-6

Aft Blower System ....................................................................................................................................... 21-9

Aft Heat System ........................................................................................................................................ 21-15

Aileron Trim Tab Indicator ........................................................................................................................... 27-2

Altitude Alerting System .............................................................................................................................. 34-3

Anti-Collision Beacon Light System .......................................................................................................... 33-11

Area Navigation ......................................................................................................................................... 34-17

Armrest ........................................................................................................................................................ 25-6

ATC Transponders and Automatic Altitude Reporting Systems ............................................................... 34-19

Autofeather Annunciation (amber) (AUTOFTHER OFF) Ann. (Autofeather Off) CAS ............................... 61-3

Automatic Direction Finder (ADF) ............................................................................................................. 34-21

Autopilot Control Wheel Disengage Switches............................................................................................. 22-4

Autopilot System ......................................................................................................................................... 22-2

Autopilot/Flight Director Go-Around Button ................................................................................................. 22-5

Auxiliary Fuel Transfer System ................................................................................................................... 28-4

B

Baggage Compartment Lights .................................................................................................................... 33-6

Bleed Air Fail Annunciator System ............................................................................................................. 21-7

Bleed Air Off Annunciation System ............................................................................................................. 21-6

Boarding Lighting System ........................................................................................................................... 33-5

C

Cabin AC Power System ............................................................................................................................. 24-9

Cabin Altitude Annunciation (red) ............................................................................................................... 21-3

Cabin Altitude Annunciator System (white) ................................................................................................. 21-2

Cabin Altitude Warning Horn System ......................................................................................................... 21-5

Cabin Differential High Annunciation (red) .................................................................................................. 21-4

Cabin Door Annunciation (red) (DOOR UNLOCKED) Ann. (Door Unlocked) CAS .................................... 52-5

Cabin Door Cable Covers ........................................................................................................................... 52-3

Cabin Door Lock and Upper Door Latch Observation Light System .......................................................... 52-6

Cabin Door Seal .......................................................................................................................................... 52-4

Cabin Door Snubber ................................................................................................................................... 52-2

Cabin Lights ................................................................................................................................................ 33-4

Cabin Pressurization System (Pressurization Control) ............................................................................. 21-10

Cabin Rate of Climb Indicator ................................................................................................................... 21-12


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Index

Cabin Storage Compartments/ Closets .................................................................................................... 25-11

Cabin Temperature Indicator System ....................................................................................................... 21-20

Cargo Restraint Systems .......................................................................................................................... 25-10

Clock With Sweep Second Hand or Electrical Digital Clock ....................................................................... 31-2

Cockpit Speaker System (Includes Audio Amp.) ...................................................................................... 23-10

Cockpit Sun Visors ...................................................................................................................................... 25-4

Cockpit Voice Recorder (CVR) ................................................................................................................. 23-14

Cockpit/Flight Deck/Flight Compartment and Instrument Lighting System ................................................ 33-2

Communications Systems (VHF & UHF) .................................................................................................... 23-4

Communications Systems (VHF) ................................................................................................................ 23-4

Crew Assist Straps (Cockpit Overhead) ..................................................................................................... 25-3

D

DC Generator Annunciation (amber) .......................................................................................................... 24-3

Differential Pressure/Cabin Altitude Indicator ........................................................................................... 21-11

Distance Measuring Equipment (DME) Systems ...................................................................................... 34-18

Dual Function N1 Indicator .......................................................................................................................... 77-3

Dual Function Torque Indicator ................................................................................................................... 77-2

E

Electric Elevator Trim System ..................................................................................................................... 27-4

Electric Heat System ................................................................................................................................. 21-16

Emergency Instrument Light System ........................................................................................................ 33-15

Emergency Locator Transmitter (ELT) ...................................................................................................... 25-17

Emergency Medical Equipment ................................................................................................................ 25-14

Emergency Vision Assurance System ...................................................................................................... 25-15

Engine Ice Vane Annunciation .................................................................................................................... 30-3

Engine Inertial Ice Vane Actuator Motors ................................................................................................... 30-6

Environmental Bleed Air Systems (Environmental) .................................................................................... 21-8

Environmental Temperature Control System ............................................................................................ 21-19

External Oxygen Gauge .............................................................................................................................. 35-2

External Power Annunciation (amber) ........................................................................................................ 24-4

External Power System ............................................................................................................................... 24-8

F

FASTEN SEAT BELT”/“FASTEN SEAT BELT WHILE SEATED” Signs or Placards ................................. 25-9

First Aid Kit (FAK) and/or Associated Equipment ..................................................................................... 25-14

Flap Position Indicator ................................................................................................................................. 27-5

Flashlight ..................................................................................................................................................... 25-2


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Index

Flight Deck Headset and Boom Microphones ........................................................................................... 23-12

Flight Director System ................................................................................................................................. 22-6

Flight Hour Recorder ................................................................................................................................... 31-3

Flight Management System ...................................................................................................................... 34-22

Flight Phone System ................................................................................................................................... 23-3

Flightcrew Intercom System ........................................................................................................................ 23-6

Flightcrew Seats .......................................................................................................................................... 25-5

Flotation / Overwater Equipment .............................................................................................................. 25-16

Fuel Crossfeed Annunciation ...................................................................................................................... 28-3

Fuel Flow Indicators .................................................................................................................................... 73-2

Fuel Quantity Annunciator ........................................................................................................................... 28-5

Fuel Quantity Indicator System ................................................................................................................... 28-6

G

Generator Bus Tie Annunciation (amber) ................................................................................................... 24-2

Glide Slope .................................................................................................................................................. 34-8

Ground Air Cooling System....................................................................................................................... 21-18

Ground Communication Power System ...................................................................................................... 23-2

H

Hand Held Microphones ............................................................................................................................ 23-11

Heated Fuel Vents .................................................................................................................................... 30-10

Hydraulic Fluid Low Annunciation ............................................................................................................... 32-2

I ILS Systems ................................................................................................................................................ 34-7

Instrument Air Valve .................................................................................................................................... 37-2

L

L or R GEN BUS TIE Relay ........................................................................................................................ 24-7

L or R IGNITION ON Annunciator (green) (Except Proline FUSION) ........................................................ 74-2

Landing Gear Control Down Lock Solenoid ................................................................................................ 32-3

Landing Gear Control In-Transit Lights (Red) ............................................................................................. 32-6

Landing Gear Down Annunciator ................................................................................................................ 32-5

Landing Gear Down Annunciator Lights (NOSE – L – R) (green) .............................................................. 32-5

Landing Lights ............................................................................................................................................. 33-9

Lavatory Waste Systems (Electric Circulation Toilet) ................................................................................. 38-2

Logo Lights ................................................................................................................................................ 33-14


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Index

M

Marker Beacon System ............................................................................................................................... 34-9

N

Non-Stabilized Magnetic Compass ............................................................................................................. 34-6

O

Oil Pressure Annunciation ........................................................................................................................... 79-2

Outflow Valve ............................................................................................................................................ 21-13

P

Parking Brake .............................................................................................................................................. 32-4

Passenger Address System (PA) ............................................................................................................... 23-7

Passenger Notice Signs .............................................................................................................................. 33-3

Passenger Oxygen Mask ............................................................................................................................ 35-4

Passenger Oxygen System......................................................................................................................... 35-3

Passenger Seat Belt/Safety Chime (chime only) ........................................................................................ 23-9

Passengers Seat(s) ..................................................................................................................................... 25-6

Pitot Heaters ............................................................................................................................................... 30-7

Position Lights ........................................................................................................................................... 33-10

Propeller Deice System ............................................................................................................................. 30-11

Propeller Synchrophase Synchronizer System ........................................................................................... 61-2

R

Radar Altimeter ......................................................................................................................................... 34-12

Radio Magnetic Indicator ............................................................................................................................ 34-5

Recognition Lights ..................................................................................................................................... 33-12

Recorded Passenger Briefing System ........................................................................................................ 23-8

Rudder Trim Tab Indicator .......................................................................................................................... 27-3

S

Safety Valve .............................................................................................................................................. 21-14

Seat Controls .............................................................................................................................................. 25-6

Stall Warning Heat ...................................................................................................................................... 30-2

Standby Attitude Indicator ........................................................................................................................... 34-4

Standby Electric Boost Pumps .................................................................................................................... 28-2

Standby Power System ............................................................................................................................... 24-5

Static Discharge Wicks ............................................................................................................................. 23-13

Strobe Lights System .................................................................................................................................. 33-7

Suction Gauge ............................................................................................................................................ 37-3


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Index

Surface Deice Annunciation ........................................................................................................................ 30-5

Surface Deice System (Wings and Horizontal Stabilizer) ........................................................................... 30-4

T

Taxi Light ..................................................................................................................................................... 33-8

Terrain Awareness and Warning System Class B .................................................................................... 34-13

Thunderstorm Detection Equipment ......................................................................................................... 34-11

Traffic Alert and Collision Avoidance System ........................................................................................... 34-15

U

Unassigned Annunciators ........................................................................................................................... 31-4

V

Vapor Cycle Air Conditioning System ....................................................................................................... 21-17

Vertical Speed Indicators ............................................................................................................................ 34-2

VHF Omni Range Systems (VOR) ............................................................................................................ 34-20

W

Weather Radar .......................................................................................................................................... 34-10

Windshield Heat .......................................................................................................................................... 30-9

Windshield Wipers ...................................................................................................................................... 30-8

Wing Ice Inspection Light .......................................................................................................................... 33-13

Wing Locker Door Gas Spring .................................................................................................................. 25-13

Y

Yaw Damper ............................................................................................................................................... 22-3


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Index


millbrook aviation minimum equipment list€¦ · 28 fuel 28-1 30 ice and rain protection 30-1 31...

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