510melcl00a

MASTER MINIMUM EQUIPMENT LIST

OPERATIONAL AND MAINTENANCEPROCEDURES GUIDE

CESSNA CE-510CITATION MUSTANG

(U.S. Registered Airplanes)

THIS MASTER MINIMUM EQUIPMENT LIST OPERATIONAL AND MAINTENANCE PROCEDURES GUIDE SHALL BE USED IN CONJUNCTION WITH DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION MASTER MINIMUM

EQUIPMENT LIST.

COPYRIGHT © 2007CESSNA AIRCRAFT COMPANY

WICHITA, KANSAS, USA1 OCTOBER, 2007

510MELCL00a REVISION 0a 1 October, 2007

CESSNA AIRCRAFT COMPANY MASTER MINIMUM EQUIPMENT LISTMODEL 510 OPERATIONAL AND MAINTENANCE PROCEDURES

2 510MELCL00a


INTENTIONALLY LEFT BLANK

MASTER MINIMUM EQUIPMENT LIST CESSNA AIRCRAFT COMPANYOPERATIONAL AND MAINTENANCE PROCEDURES 510 Mustang

NOTICE

The Master Minimum Equipment List (MMEL) is distributed by the Department of Transportation Federal Aviation Administration. This Master Minimum Equipment List Operation and Maintenance Procedures Guide contains only the items from the Master Minimum Equipment List which have Operational (O) or Maintenance (M) procedure requirements. Cessna does not support Minimum Equipment List items not published in the MMEL.

Cessna’s policy is to revise this guide only to accommodate changes to a new MMEL revision, which requires a change to, or a new, Operational (O) or Maintenance (M) required procedure. If a revised MMEL is released, but does not affect any required procedure, the Operational and Maintenance (O&M) Guide will not be revised at that time. Cessna reserves the right to make format changes without generating a new revision.

Operational (O) and Maintenance (M) procedures in this guide are recommended by Cessna Aircraft Company. Most of the procedures in this guide have been approved in some MEL’s. This document is not FAA approved, but is intended to aid operators in writing and gain approval for their specific Minimum Equipment List (MEL). It is not the intent of this guide to be used as part of any specific MEL. The Operator is responsible to ensure that all crew members are properly trained in the use of MEL (O) and (M) procedures.

The Narrative section of each Maintenance (M) procedure is intended to satisfy the FAR 135 MEL requirement for training non-maintenance individuals who are authorized, in the MEL, to perform maintenance tasks.

510MELCL00 i


LOG OF EFFECTIVE PAGES

Use this page to determine the currency and applicability of your Master Minimum Equipment List Operational and Maintenance Procedures Guide. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages listed under the Page column of the effective log.

Following is a description of the Log of Effective Pages columns:

Page - Master Minimum Equipment List Operational and Maintenance Procedures Guide page number.

Status - Indicates if the page has been added, revised or deleted by the current revision.

Revision Number - Indicates the revision number.

LOG OF EFFECTIVE PAGES

PAGE STATUS REV. NO DATE

Title Original 0 1 October 2007

i Original 0 1 October 2007

ii Original 0 1 October 2007

iii Original 0 1 October 2007

1-16 Original 0 20 August 2007

17 Added 0a 1 October, 2007

18 – 25 Original 0 20 August 2007

A-1 Revised 0a 1 October, 2007

A-2 Revised 0a 1 October, 2007

NOTE: Additions or revisions to text will be identified by a revision bar in the right margin of the page and adjacent to change unless the Master Minimum Equipment List and Operational and Maintenance Procedures Guide have been reformatted in its entirety.

THIS GUIDE IS CURRENT WITH:THE MASTER MINIMUM EQUIPMENT LIST WHICH IS DISTRIBUTED BY THE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION - REVISION 0a DATED 7/17/2007

FOR THE AIRPLANES LISTED ON THE COVER

ii 510MELCL00a


PAGE INTENTIONALLY LEFT BLANK

510MELCL00 iii


TABLE OF CONTENTS

SYSTEM NO. SYSTEM PAGE NO.

Notice I

Log of Effective Pages ii

Table of Contents iii

21 Air Conditioning 1

22 Auto Pilot 7

26 Fire Protection 11

30 Ice and Rain Protection 13

31 Indication/Recording Systems 15

32 Landing Gear 17 |

33 Lights 19

34 Navigation 23

52 Doors 19

73 Engine Fuel & Control 25

APPENDIX Altitude Conversion Chart A-1

iv 510MELCL00a


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS21 AIR CONDITIONING

1. Flow Control Valve

2. Pressure Regulating Shutoff Valves

(O) One may be inoperative provided;a) All other components and functions of the pressurization system

operate normally,b) The pressure regulating shutoff valve on the affected side is closed

andc) The aircraft is operated at FL 250 or below.

OPERATIONAL PROCEDURESTo ensure the Pressure Regulating Shutoff Valve on the affected side is closed, Air Source Select must be set to the properly functioning side.

1. Start both engines and turn off the AIR COND switch.2. Select Air Source Select switch to OFF.3. Verify no airflow in the cockpit or cabin.

NOTE: Momentarily selecting L then R then OFF may help verify no flow.

4. Set the AIR SOURCE SELECT knob to the operating side (L or R). 5. Place a placard stating, “Select (L or R), FRESH AIR, or OFF only –

(L/R) Flow Control Valve INOP” above the switch. 6. Make appropriate entry on the discrepancy report.

(O) One may be inoperative provided:a) The affected pressure regulating shutoff valve is verified in the closed position, b) All other components and functions of the pressurization system operate normally, and

c) The aircraft is operated at FL 250 or below.

OPERATIONAL PROCEDURESTo ensure the Pressure Regulating Shutoff Valve on the affected side is closed, Air Source Select must be set to the properly functioning side.

1. Start both engines and turn off the AIR COND switch.2. Select Air Source Select switch to OFF.3. Verify no airflow in the cockpit or cabin.

NOTE: Momentarily selecting L then R then OFF may help verify no flow.

4 Set the AIR SOURCE SELECT knob to the operating side (L or R).5. Place a placard stating, “Select (L or R), FRESH AIR, or OFF only – (L/R) Flow Control Valve INOP” above the switch.6. Make appropriate entry on the discrepancy report.

510MELCL00 1



(Continued)

3. Cabin Differential Pressure Gauge (EICAS Indication)

4. Cabin Altitude Warning System

(O) May be inoperative for unpressurized flight at 10,000 feet MSL or below.

OPERATIONAL PROCEDURESTo operate the aircraft unpressurized.

1. Select AIR SOURCE SELECT switch to OFF or FRESH AIR.2. Place a placard to the pilot’s side of the MFD stating “CABIN DIFFERENTIAL PRESSURE GAGE INOP. FLIGHT NOT AUTHORIZED ABOVE 10,000 FEET MSL”.3. Make appropriate entry on discrepancy report.

-----or-----

(O) May be inoperative provided;a) Cabin altitude and rate (EICAS indication) are operating normally, b) Cabin pressurization auto schedule is operating normally, and

c) A chart is provided to convert cabin altitude to differential pressure.

OPERATIONAL PROCEDURESTo ensure the Cabin Pressurization Auto Schedule is operating normally. One method would be to verify satisfactory completion of the pressurization preflight test.

1. Place the Battery switch to BATT.2. Place the PRESS CONT switch to NORM.3. Place the AVN PWR switch to ON.4. Make sure the PRESS CTRL message is not shown.

NOTE: The absence of the PRESS CRTL annunciation indicates the system is functioning normally.

5. Place a placard adjacent to the pilot’s side of the MFD stating “CABIN DIFFERENTIAL PRESSURE EICAS DISPLAY INOP”.6. Make appropriate entry on the discrepancy report.7. Refer to chart on page 27 to convert altitude to differential pressure.



1. Select AIR SOURCE SELECT switch to OFF or FRESH AIR.2. Place placard stating “CABIN ALTITUDE WARNING SYSTEM INOP. FLIGHT ABOVE 10,000 FEET MSL NOT AUTHORIZED” adjacent to the pilot’s side of the MFD.3. Make appropriate entry on discrepancy report.

2 510MELCL00



(Continued)

5. Cabin Altitude Display (EICAS indication)

7. Pressurization Controller (Auto Schedule Mode)



1. Select AIR SOURCE SELECT switch to OFF or FRESH AIR.2. Place placard stating “CABIN ALTITUDE DISPLAY INOP. FLIGHT ABOVE 10,000 FEET MSL NOT AUTHORIZED” adjacent to the pilot’s side of the MFD.3. Make appropriate entry on discrepancy report.


OPERATIONAL PROCEDURESProcedure to operate the aircraft unpressurized.

1. Select AIR SOURCE SELECT switch to OFF or FRESH AIR.2. Place a placard to the pilot’s side of the MFD stating “PRESSURIZATION CONTROLLER INOP. FLIGHT NOT AUTHORIZED ABOVE 10,000 FEET MSL”.3. Make appropriate entry on discrepancy report.

510MELCL00 3



(Continued)

9. Air Conditioning System

(M) May be inoperative provided: a) Air conditioning system is deactivated, b) Cabin and cockpit temperature control system is operating normally, and c) Glareshield avionics fans are operating normally.

MAINTENANCE PROCEDURESProcedure to deactivate the air conditioner and ensure it has not and will not adversely affect any other structure or system.

1. Disconnect aircraft power.2. Pull and collar the HZ063 circuit breaker in the aft Jbox.3. Ensure the AIR COND switch is in the OFF position.4. Place an INOP placard above the AIR COND switch on the co-pilot’s tilt panel.5. Connect aircraft power. 6. Position the aircraft battery switch to BATT.7. Position the AVN PWR switch to ON.8. Audibly and physically inspect for glareshield cooling fan operation.9. Start the engines and position the aircraft in a suitable run up area.10. Verify airflow from the cockpit footwarmer ducts.11. Verify airflow from the cabin bleedair distribution ducts.12. Make appropriate entry in the discrepancy report.

4 510MELCL00

MASTER MINIMUM EQUIPMENT LIST CESSNA AIRCRAFT COMPANYOPERATIONAL AND MAINTENANCE PROCEDURES MODEL 510


(Continued)

10. Cabin Outflow Valves (O)(M) May be inoperative provided: a) At least one valve is secured open, and b) The flight is conducted unpressurized at 10,000 feet MSL or below.

OPERATIONAL PROCEDURESProcedure to operate the aircraft unpressurized

1. Select AIR SOURCE SELECT switch to OFF or FRESH AIR.2. Place a placard near the AIR SOURCE SELECT switch stating “OUTFLOW VALVES INOP. FLIGHT NOT AUTHORIZED ABOVE 10,000 FEET MSL”.3. Make appropriate entry on discrepancy report.

MAINTENANCE PROCEDURESProcedure to secure cabin outflow valve(s) in the open position and aircraft is operated unpressurized

1. Gain access to the Outflow Valves which are located on the Aft Pressure Bulkhead in the aft cabin.2. Remove the bolts and washers securing either valve from its mount on the aft side of the bulkhead.3. With all lines, hoses and wiring still connected, secure the valve away from its mount using MS3367-4-9 tie-wrap, wire, or other suitable device. The Outflow Valve must not be allowed to slip back into position and block the opening in the Aft Pressure Bulkhead.4. Place an INOP placard near the PRESS CONT switch.5. Make appropriate discrepancy report entry.

510MELCL00 5



6 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS22 AUTO FLIGHT

1. Auto Pilot (M) May be inoperative provided aircraft is operated with a crew of two and operating requirements do not require its use.

NOTE: RVSM is not authorized.

MAINTENANCE PROCEDURESProcedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control system.

NOTE: With the autopilot inoperative, aircraft must be operated using a crew of two.

1. Electrically isolate all four Autopilot Servos: a) Select Battery and AVN PWR switches to OFF.b) Disengage the AFCS circuit breaker on the pilot’s cb panel.

AILERON SERVO: 1. Remove fuselage fairing panel 315AC to get access to the aileron autopilot servo. Refer to Chap. 6 Access Plates and Panels Identification – Description and Operations. 2. Disconnect and bag electrical connector (PY300).

RUDDER SERVO: 1. Remove tailcone stinger to gain access to the Rudder autopilot servo. Refer to Chap. 53, Tailcone Stinger – Maintenance Practices 2. Disconnect and bag electrical connector (JT302) from the electrical connector (PT302).

ELEVATOR SERVO: 1. Open tailcone baggage compartment door. Refer to Chap. 6, Dimensions and Areas – Description and Operations. 2. Remove aft baggage compartment panels 312BBC and 311BDC to get access to the elevator servo. Refer to Chap. 6, Access Plates and Panels Identification – Description and Operations. 3. Disconnect and bag the electrical connector (JT300).

PITCH TRIM SERVO: 1. Open tailcone baggage compartment door. Refer to Chap. 6, Dimensions and Areas – Description and Operations. 2. Remove aft baggage compartment panel 311 ATC to get access to the elevator servo. Refer to Chap. 6, Access Plates and Panels Identification – Description and Operations. 3. Disconnect and bag the electrical connector (JT 301).

CONTINUED ON NEXT PAGE

510MELCL00 7



(Continued)

1. Auto Pilot (Continued)

2. Yaw Damper

4. Operate the control yoke and the rudder pedals through full control travel in all 3 axes to ensure that autopilot clutches are disengaged, and travel is unobstructed.

5. Place a placard next to Autopilot (AP) switch on Autopilot Controller stating “AUTOPILOT, YAW DAMPER, AND ELECTRIC PITCH TRIM INOP - SINGLE PILOT AND RVSM OPERATIONS NOT AUTHORIZED”.

4. Make appropriate entry on the discrepancy report.

(M) May be inoperative provided the flight is conducted at FL300 or below. NOTE: Autopilot must be considered inoperative and RVSM is not authorized.

MAINTENANCE PROCEDURES

Procedure to ensure no electrical or mechanical fault exists that will have an adverse effect on any flight control system.

NOTE: With the Yaw Damper inoperative, the Autopilot and Electric Pitch Trim will also be inoperative.

1. Electrically isolate all Autopilot and Yaw Damper functions: a) Select Battery and AVN PWR switches to OFF. b) Disengage the AFCS circuit breaker on the pilot’s cb panel.2. Electrically isolate the Rudder Servo:

a) Select BATTERY and AVIONICS POWER switches to OFF.

b) Gain access to the Rudder Autopilot Servo (YSV-P1) in the tailcone by opening the large battery access door 321BL, which acts as the tailcone baggage LH aft closeout. Refer to Chapter 6, Access Plates and Panels Identification - Description and Operation.

c) Disconnect the electrical connector (PT305) from Rudder Autopilot Servo (YSV-P1). Bag and secure the

connector away from all control cables.d) Close Panel 321BL.

3. Check operation of flight controls for freedom of movement and smoothness through complete range of travel.

4. Place a placard next to Autopilot (AP) switch on Autopilot Controller stating “AUTOPILOT, YAW DAMPER, AND ELECTRIC PITCH TRIM INOP - SINGLE PILOT AND RVSM OPERATIONS NOT AUTHORIZED ”.


8 510MELCL00



(Continued)

3. Electric Elevator Trim (M) May be inoperative provided: a) Electric Trim System is deactivated, and b) Manual Trim is operative and unaffected.

NOTE: Autopilot must be considered inoperative and RVSM is not authorized.

MAINTENANCE PROCEDURESProcedure to ensure that the failure of the Electric Pitch Trim will not interfere with the operation of the Manual Trim.

1. Disengage the AFCS circuit breaker and secure with tie-wrap.2. Check Manual Trim for freedom of movement throughout travel for

smooth operation. This will determine if there is any mechanical damage that would interfere with flight controls and preclude dispatch.

NOTE: If the Electric Trim is inoperative, it should be confirmed that the problem is not in the Manual (mechanical) Trim system in the airplane and that the failure does not affect Manual Trim. Pitch Trim should be checked for full travel, smoothness, and proper operation.

3. Electrically isolate the Pitch Trim servo (See 22-1 for procedure).4. Place placard on pedestal stating “AUTOPILOT, YAW DAMPER AND ELECTRIC PITCH TRIM INOP – SINGLE PILOT AND RVSM OPERATIONS NOT AUTHORIZED.”5. Make appropriate entry on the discrepancy report.

510MELCL00 9



10 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS26 FIRE PROTECTION

1. Portable Fire Extinguishers

(O) Any in excess of those required by operating rules may be inoperative or missing provided: a) The inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so that it can not be mistaken for a functional unit, and b) Required distribution is maintained.

OPERATIONAL PROCEDURESProcedure to remove and tag the affected fire extinguisher from its holder and place out of site.

1. Place an INOP placard on the inoperative fire extinguisher.2. Remove fire extinguisher from its holder, cover it

with a bag, and place it in a storage area or baggage area within the airplane.


510MELCL00 11



12 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS30 ICE AND RAIN

PROTECTION

1. Windshield Anti-Ice

2. Engine Anti-Ice System

(O) May be inoperative provided: a) Aircraft is not operated in known or forecast icing conditions, b) Aircraft is not operated in RAM air temperatures below 0C, and c) The crew has a means to clear the windshield of moisture.

OPERATIONAL PROCEDURESProcedure to clear windshield of moisture.

1. Place an INOP placard above affected WINDSHIELD ANTI-ICE switches.2. A member of the flight crew shall posses a non-scratching, micro-fiber cloth within reach.3. Make appropriate entry in the discrepancy report.

(M) May be inoperative provided: a) Engine anti-ice valve(s) remain OPEN, b) Takeoff and landing field temperatures are 10 degrees C or below, and c) Anti-ice ON performance data are used

NOTE: See AFM Performance Data

--------or-------

(M) May be inoperative provided: a) Engine anti-ice valve(s) are failed CLOSED, b) The flight is conducted in day VMC, and c) Aircraft is not operated in known or forecast icing conditions.

MAINTENANCE PROCEDURESProcedure to determine if the engine anti-ice valve has failed in the open or closed position.

1. With engines shut down, make note of the temperature of the Engine Inlets (use of hand touch is sufficient).2. Position the aircraft in a suitable run-up area.3 Verify L and R ENGINE ANTI-ICE circuit breakers are engaged.4. To verify whether the affected valve has failed open or closed:

a) Verify ENGINE ANTI-ICE switch is OFF. b) Set the parking brake and start both engines. Refer to AFM Normal

Checklist for engine start.

CONTINUED ON NEXT PAGE

510MELCL00 13


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS30 ICE AND RAIN

PROTECTION (Continued)

2. Engine Anti-Ice System (Continued)

c) Gradually increase both throttles to achieve 70% N2. d) Run engines for approximately one minute to allow inlets to warm

up and have assistant verify inlet temperatures are the same as step 1.i. If inlet(s) are hot, the valve has failed OPEN.

e) Turn ENG A/I switches ON.f) Verify both ENG A/I COLD L – R EICAS message(s) display.

NOTE: ENG A/I COLD L – R may not display if ambient temperature is high.

g) Run engines for approximately one minute to allow inlets to warm up and have assistant verify inlet temperatures are HOT.i. If inlet(s) are the same as step 1, the valve has failed CLOSED.

5. Pull and secure the affected ANTI-ICE ENGINE c/b with tie-wrap.a) If failure mode is CLOSED, repeat step 4.

6. Place a placard stating, “(L – R, as appropriate ENGINE ANTI-ICE INOP – failed (OPEN/CLOSED)” next to appropriate Engine Anti-Ice switch.


14 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS31 INDICATING

RECORDING SYSTEMS

1. Flight Hour Meter (O)

OPERATIONAL PROCEDURESProProcedure to ensure that all flight times are recorded and added to the

Aircraft Total Time.

1. Record each takeoff time and landing time (including time zone).2. Following each flight, add flight time to the total aircraft time in the Aircraft Log to assure compliance with maintenance and/or operations requirements.3. Place an INOP placard on the Flight Hour Meter.4. Make appropriate entry on the discrepancy report.

510MELCL00a 15



16 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS32 LANDING GEAR

1. Antiskid System (O) May be inoperative provided operations are conducted in accordance with applicable AFM Limitations, procedures and performance data. Refer to Abnormal Procedures, DISPATCH WITH ANTISKID SYSTEM INOPERATIVE.

OPERATIONAL PROCEDURETo ensure flight crew operates the aircraft in accordance with specific AFM Limitations, Abnormal Procedures and Performance Data unique to operations with antiskid inoperative.

NOTE: Dispatch with antiskid inoperative is prohibited if the forecast conditions for the destination approach and landing will require the use of Anti-Ice ON (Flap TO/APR) landing data.

1. Flight crew shall review the forecast conditions at the destination airport to determine if icing conditions are forecast to exist at the anticipated time of arrival.2. If icing conditions are not forecast to exist, follow AFM Abnormal Procedures, DISPATCH WITH ANTISKID SYSTEM INOPERATIVE.3. Apply takeoff and landing distance factors specified in the AFM procedure and ensure sufficient runway length is available.4. Place an INOP placard adjacent to ANTISKID switch. 5. Make appropriate entry in discrepancy report.

510MELCL00a 17



18 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS33 LIGHTS

6. Fasten Seat Belt and No Smoking Sign

7. Flashing Beacon Light System

(O) May be inoperative provided alternate procedures for notifying passengers are established and used.

OPERATIONAL PROCEDURES

Procedure to ensure that passengers are notified of seat belt and no smoking requirements.

1. Crewmember shall ensure the appropriate announcements are made.2. Place an INOP placard adjacent to the PAX SAFETY switch.3. Make appropriate entry on the discrepancy report.

(O) May be inoperative provided the anti-collision light system is operative.

OPERATIONAL PROCEDURESProcedure to develop alternative procedures to be used when the aircraft is on the ground with the engine(s) running.

1. Place an INOP placard above the rotating beacon switch.2. Make appropriate entry in the discrepancy report.3. Flight crew shall verify Anti-collision Light System is operative 4. Anti-collision Light System shall be turned ON prior to staring engines.5. Flight crew should take extra precaution to alert ground personnel (if available) of alternate operating procedures and be vigilant of operating around or near other personnel or motorized vehicles.

510MELCL00a 19



20 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS34 NAVIGATION

(Continued)

6. Altitude Alerting System

9. TAWS Equipment

(O) May be inoperative provided: a) Autopilot with altitude hold is operative, b) Enroute operations do not require its use, and c) Repairs are made within three flight days.

NOTE: RVSM is not authorized.

OPERATIONAL PROCEDURESProcedure to ensure altitude awareness.

1. Crew briefings will include a reminder of the inoperative Altitude Alerting System.

2. Flight crew will use aural callouts pertaining to approaching target altitudes as assigned by ATC or as depicted by appropriate charts.

3. Place placard adjacent to altimeters stating: “Altitude Alert System INOP – RVSM OPERATIONS NOT AUTHORIZED”.

4. Make appropriate discrepancy report entry.

(O) May be inoperative provided alternate procedures are established and used.

NOTE: Any mode that operates normally may be used.

OPERATIONAL PROCEDURESProcedure to develop alternate procedure to ensure crew awareness of altitude, performance and terrain clearance at all times

1. The flight crew shall brief that the TAWS system is inoperative.2. The flight crew shall review all current aeronautical charts with emphasis on notable terrain features.3. The flight crew shall brief appropriate altitudes for each segment of flight.4. Place a placard stating “TAWS SYSTEM INOP” above the pilot’s PFD.5. Make appropriate discrepancy report entry.

510MELCL00 21


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS34 NAVIGATION

(Continued)

10. Navigation Databases

1) World Wide Aviation Database and Flight Charts or ChartView Database and BaseMap Land Database

(O) May be out of currency provided: a) Current aeronautical charts are used to verify navigation fixes prior to dispatch, b) Procedures are established to verify status and suitability of navigation facilities used to define route of flight, and c) Approach navigation radios are manually tuned and identified.

OPERATIONAL PROCEDUREProcedure to verify navigation facilities status and suitability for route of flight.

1. Ensure current and appropriate navigational information is available to the flight crew.2. A member of the flight crew shall check for NOTAM’s along the intended route of flight and alternate routes of flight.3. Place a placard stating that the affected database is out of currency and may not be used for navigational purposes adjacent to the MFD..

22 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS52 DOORS

1. Cabin Door Monitoring System

2. Nose Baggage Door Monitoring System

3. Aft Baggage Door Monitoring System

(O) May be inoperative provided: a) The door is verified closed and handle latched, b) The 8 door pin indicators are visible in the sight glass locations, and c) The interior door handle is secure.

OPERATIONAL PROCEDURESProcedure to physically check door.

1. A crewmember will visually verify that all DOOR FLAGS are in view. 2. Make appropriate discrepancy report. 3. Place placard above EICAS display and on the cabin door stating “ CABIN DOOR CAS MSG INOP”.

(O) May be inoperative provided the door is verified secure and locked.

NOTE: If the lock is inoperative, see item 52-5.


1. Place a placard adjacent to the MFD stating, “NOSE DOOR L or R CAS MESSAGE INOP – VERIFY LOCKED BEFORE FLIGHT.”2. Make appropriate discrepancy report entry.3. Immediately prior to closing and locking the cabin door, crew member will inspect affected Nose Baggage door to verify that it is closed and locked.

(O) May be inoperative provided the door is verified secure and locked.

NOTE: If the lock is inoperative, see item 52-5.


1. Place a placard adjacent to the MFD stating, “AFT DOOR CAS MESSAGE INOP – VERIFY LOCKED BEFORE FLIGHT.”2. Make appropriate discrepancy report entry.3. Immediately prior to closing and locking the cabin door, crew member will inspect Aft Baggage door to verify that it is closed and locked.

510MELCL00 23


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS52 DOORS (Continued)

4. Cabin Door Seal

5. Door Key Locks

1) Aft Baggage Door

2) Nose Baggage Doors

(M)(O) May be inoperative or unserviceable provided: a) The seal does not interfere with door operation, b) At least one outflow valve is secured OPEN, and c) Aircraft is operated at 10,000 feet MSL or below. MAINTENANCE PROCEDURESProcedure to ensure door seal does not interfere with door operation and to secure outflow valve open.

Note: See item 21-10 for procedure to secure outflow valve.

OPERATIONAL PROCEDURESProcedure to operate the aircraft unpressurized.

1. Make appropriate entry in the discrepancy report.2. Place placard stating “ CABIN DOOR SEAL UNSERVICEABLE, DO NOT PRESSURIZE” adjacent to the AIR SOURCE SELECT knob.3. Place AIR SOURCE SELECT knob to OFF or FRESH AIR.4. A member of the crew will close and lock the cabin door, inspect the door for operation and the cabin door pin indicators for proper function and cycle the door to ensure the door can be opened in the event of Emergency.

(O) May be inoperative in the unlocked position provided the door is verified secure prior to flight.

OPERATIONAL PROCEDURESProcedure to physically check that the door is latched and all preflight actions can be accomplished.

1. Make appropriate entry in the discrepancy report.2. Place an INOP placard next to the affected lock.3. Have a member of the flight crew verify that the door is closed and latched and the lock is in the unlocked position.

(O) One may be inoperative in the locked position provided the remaining door may be opened to perform preflight actions.

OPERATIONAL PROCEDURESProcedure to physically check that the door is latched and that all preflight items can be accomplished.

1. Make appropriate entry in the discrepancy report.2. Place an INOP placard next to the affected lock.3. Ensure that items stowed in the nose baggage area are not blocking required inspection locations.4. Have a member of the flight crew verify that the door is closed and latched and the lock is in the unlocked position.

24 510MELCL00


SYSTEM & SEQUENCE NUMBERS REMARKS OR EXCEPTIONS73 ENGINE FUEL &

CONTROL

2. FUEL FLOW INDICATING SYSTEM

(O) One may be inoperative provided both fuel quantity indicating systems are operative.

NOTE: Do not rely on FMS gross weight and fuel computations.

OPERATIONAL PROCEDURESProcedure to use engine indications and charts to estimate fuel flow.

1. Estimate fuel flow quantities by matching power settings between both engines and multiplying the operating fuel flow indicator by two, and through the use of the EOM and/or Operating Manual Flight Planning Charts. 2. Place an INOP placard adjacent to the fuel flow indicating system.3. Make appropriate discrepancy report entry.

510MELCL00 25


APPENDIX

21 AIR CONDITIONING

NOTE: Cabin altitude should be at zero rate to accurately reflect the Standard Atmosphere Chart conversion Appendix Page A-2.

Example for converting cabin altitude to differential pressure.

Cabin Altitude as read from gage: 5000 feetPressure at 5000 feet: 12.23 PSIAAircraft Altitude: 38,000 feetPressure at 38,000 feet: 3.00 PSIA

12.23 - 3.00 PSIA = 9.23 Differential Pressure

Example for converting differential pressure to cabin altitude.

Differential Pressure as read from gage: 8.00 PSIAAircraft Altitude: 25,000 feetPressure at 25,000 feet: 5.46 PSIA

8.00 + 5.45 PSIA = 13.46 PSIA

Interpolate from chart cabin altitude at 13.45 PSIA

Cabin Altitude = 2,421 feet

510MELCL00a A-1


CABIN ALTITUDE vs. CABIN PRESSURE DIFFERENTIAL CONVERSION(Cabin Pressure Differential Display or Cabin Altimeter Inoperative)

CABIN ALT AIRCRAFT PRESSURE ALTITUDE ´ 1000'

CA

BIN

AL

TIT

UD

E x

100

0'

x 1000' 0 5 10 15 20 25 28 31 33 35 37 39 41 43 45 47 49 51

11.0 1.4 3.0 4.3 4.9 5.6 5.9 6.3 6.6 6.9 7.1 7.4 7.6 7.8 8.0 8.110.5 1.6 3.2 4.5 5.1 5.8 6.1 6.4 6.8 7.1 7.3 7.5 7.8 8.0 8.1 8.310.0 0.0 1.8 3.4 4.7 5.3 6.0 6.3 6.6 7.0 7.3 7.5 7.7 8.0 8.2 8.3 8.59.5 0.2 2.0 3.6 4.9 5.5 6.2 6.5 6.8 7.2 7.5 7.7 7.9 8.2 8.4 8.5 8.79.0 0.4 2.2 3.8 5.1 5.7 6.4 6.7 7.0 7.4 7.7 7.9 8.1 8.4 8.6 8.7 8.98.5 0.6 2.4 4.0 5.3 5.9 6.6 6.9 7.2 7.6 7.9 8.1 8.3 8.6 8.8 8.9 9.18.0 0.8 2.6 4.2 5.5 6.1 6.8 7.1 7.5 7.8 8.1 8.3 8.6 8.8 9.0 9.2 9.37.5 1.0 2.8 4.4 5.7 6.4 7.1 7.3 7.7 8.0 8.3 8.5 8.8 9.0 9.2 9.4 9.57.0 1.2 3.0 4.6 5.9 6.6 7.3 7.5 7.9 8.2 8.5 8.7 9.0 9.2 9.4 9.6 9.76.5 1.5 3.3 4.8 6.1 6.8 7.5 7.8 8.1 8.4 8.7 9.0 9.2 9.4 9.6 9.8 10.06.0 1.7 3.5 5.0 6.3 7.0 7.7 8.0 8.3 8.6 8.9 9.2 9.4 9.6 9.8 10.05.5 1.9 3.7 5.2 6.5 7.2 7.9 8.2 8.5 8.9 9.1 9.4 9.6 9.9 10.15.0 2.1 3.9 5.5 6.8 7.5 8.2 8.4 8.8 9.1 9.4 9.6 9.9 10.14.5 2.4 4.2 5.7 7.0 7.7 8.4 8.7 9.0 9.3 9.6 9.9 10.14.0 2.6 4.4 5.9 7.2 7.9 8.6 8.9 9.2 9.5 9.8 10.13.5 2.8 4.6 6.2 7.5 8.2 8.9 9.1 9.5 9.8 10.13.0 3.1 4.9 6.4 7.7 8.4 9.1 9.4 9.7 10.02.5 3.3 5.1 6.7 8.0 8.6 9.3 9.6 10.02.0 3.6 5.4 6.9 8.2 8.9 9.6 9.9 10.21.5 3.8 5.6 7.2 8.5 9.1 9.8 10.11.0 4.1 5.9 7.4 8.7 9.4 10.10.5 0.0 4.3 6.1 7.7 9.0 9.70.0 0.0 0.3 4.6 6.4 7.9 9.2 9.9-0.5 0.3 0.6 4.9 6.7 8.2 9.5 10.2-1.0 0.5 0.8 5.1 6.9 8.5 9.8 10.5

EXAMPLE: Aircraft is at FL 350 and Cabin Pressure Differential Gauge reads 8.8 psid, Cabin Altitude is 5,000'.

EXAMPLE: Aircraft Is At FL 350 and Cabin Altimeter reads 5,000', Cabin Pressure Differential is 8.8 psid.

A-2 510MELCL00a

510melcl00a

Documents

minimum equipment list

maintenance om guide

maintenance tasks

operational o

revision number

new revision

new mmel revision

current revision