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Presented to:
By:
Date:
Federal AviationAdministration
Electronic Flight Bag (EFB)
NextGen Technologies
135 Air Operators
George Holtman, Principal Avionics Inspector
Thursday April 19, 2012
Federal AviationAdministration
2Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Overview
• Hardware and Software
• Guidance Materials
• Authorization Process
Federal AviationAdministration
3Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Class 1 EFB• Portable COTS-based computers
• Not attached or connected to an aircraft mount
• May be attached to pilot’s leg (kneeboard)
• Considered Portable Electronic Devices (PEDs)
• Must be stowed during critical phases of flight
• May not be subject to an administrative control process for aircraft equipment
Federal AviationAdministration
4Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Class 2 EFB• Portable COTS-based computers is
considered PEDs• Tools must not be required to remove EFB• Must be connected or attached to an aircraft
mount• May only use aircraft power, have data
connectivity, and use installed antennas• May be authorized to transmit non-essential
AAC-type data• May be authorized for use for all phases of
flight and ground ops• May require RF/Decompression/Altitude
testing• Consist of devices/modules located on the
flight deck that are accessible by the flightcrew
• Must be subject to an administrative control process for aircraft equipment
Federal AviationAdministration
5Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Class 2 EFB Aircraft Display
Federal AviationAdministration
6Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
EFB Securing Solutions
Federal AviationAdministration
7Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Yoke-Mounted
• Yoke-Mounted EFBs must be certificated by a design approval by AIR under TC, amended TC, or STC
• All structural and dynamic, as well as wiring protection and security requirements affecting the flight controls, (including autopilot (AP), stall warning, stick pusher, crashworthiness, human factors, etc.), must be addressed prior to installation
Federal AviationAdministration
8Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Class 3 EFB• Portable modules/components must still fulfill intended function to
qualify as EFB Class 2 PED• If any of the functional EFB system hardware (CPU/Display/Interface) is
“certified,” then EFB system is considered Class 3 regardless of OS
Federal AviationAdministration
9Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
+ -
PWR
MENU PGUP PGDN XFR ENTERBRT
DIM
CHARTS
TAXI MAPS
PERFORMANCE LOGBOOK
VIDEO
DOCUMENTS
SYSTEM PAGE INITIALIZE FLT
EFB MAIN MENU
Boeing Class 3 “Installed” EFB
Type “C”Type “B”
Type “A”Type “B”Type “A”
Type “B”
Federal AviationAdministration
10Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Class 1 • Portable device• RD for Type B• Secured during
critical phases of flight
• No TC’d A/C data, power, or mount for use
• Limited by AC 120-76A
Type A & B ApplicationsType A & B Applications
Certified Type C ApplicationsCertified Type C Applications
Class 2 • Portable device• Crashworthy-mounted• EMI/Rapid Decomp/Alt
testing required• All phases of flight• Ships power• Read only airplane data• Video interface• Limited by AC 120-76A
Class 3 • Installed by TC• Ships power• All flight phases• Datalink • Interactive Apps• Video interface• Increased
Functionality
EFB Classes and Authorized UsesPortable Equipment Installed Equipment
Authorization for UseAuthorization for Use
Federal AviationAdministration
11Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Type A Applications
• May be hosted on any class of hardware
• Must be evaluated and found suitable for intended function
• Do not require an AIR design approval
• Only for use during non-critical phases of flight when pilot workload is reduced
• Examples of Type A software applications are provided in AC 120-76 A, Appendix A
Federal AviationAdministration
12Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Type B Applications
• May be hosted on any class of hardware
• Must be evaluated and suitable for intended function
• Do not require an AIR design approval
• May require AEG evaluation• May be used during all phases of
flight• Examples of Type B software
applications are provided in AC 120-76 A, Appendix B
Federal AviationAdministration
13Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Type C Applications
• Any certified software applications with AIR design approval
• Includes AIR approved software for Weight and Balance (W&B) and/or aircraft performance
• Includes any software application that displays Own Ship Position
Federal AviationAdministration
14Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
• Hardware and Software• Guidance Materials• Authorization Process
Where We Are in the Presentation
Federal AviationAdministration
15Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Pertinent EFB Guidance History
FAA AC 120-76A (3/17/03)
FAA AC 91-21.1B (08/25/06)
FAA Notice 8200.98 (10/13/06)
FAA AC 20-159 (04/30/07)
FAA AC 91-78 (7/20/07)
A061 OpSpecs Guidance (03/14/11)
8900.1 EFB Guidance (03/16/12)
Guidelines For The Certification, Airworthiness, and Operational Approval of EFB Computing Devices (In revision)
Use of Portable Electronic Devices Aboard Aircraft (Used in conjunction with 8900.1 for authorizing use of EFB)
Electronic Flight Bag “Job Aid” (Expired)
Obtaining Design And Production Approval Of Airport Moving Map Display (AMMD) Applications Intended For Electronic Flight Bag Systems
Clarified AEG and POI role
Inspector Handbook
Use of Class 1 or Class 2 Electronic Flight Bag (EFB) Part 91 guidance
Federal AviationAdministration
16Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Advisory Circular 20-159
AMM (Airport Moving Map) with own-ship position for Class 2 & 3 EFB Systems
Federal AviationAdministration
17Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Technical Standard Order (TSO)-C165, “Electronic Map Display Equipment for Graphical Depiction of Aircraft Position,” published October, 2003
EFB Class 2 Systems are limited to display of Own-ship for surface operations provided manufacturers comply with AC 20-159
Moving Maps with Own-Ship Position
Federal AviationAdministration
18Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
AC 20-159 is consistent with EFB AC 120-76A which states in part:
“EFB Type C applications that receive a TSOA may be approved for use on EFB Class 2 systems provided they meet the following conditions:
a) Hosted applications must be classified as a minor failure effect or no safety effect. No major safety effect or higher classifications are acceptable.
b) Type A and B EFB software applications may reside in a TSOA system provided they “do not” interfere with the Type C applications.”
How AC 20-159 Relates to Current EFB AC
Federal AviationAdministration
19Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
FAA Order 8900.1 Volume 3
• FAA evaluation process for an EFB follows the same general process for approval and acceptance as described in FAA Order 8900.1, Volume 3, Chapter 1, Section 1
Federal AviationAdministration
20Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Basic EFB Requirements
• The screen must be large enough to show an entire instrument approach procedure chart at once, with the equivalent degree of legibility and clarity as a paper chart
• The display must also be demonstrated to be readable on the flight deck in direct sunlight
Federal AviationAdministration
21Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Basic EFB Requirements
• GPS data may be used for map centering when en route charts are displayed
• Map centering may be used as an en route chart feature only and may not be used when an approach chart is displayed
• No own-ship position displayed on a Class 1 or Class 2 EFB in Flight
Federal AviationAdministration
22Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Rapid Decompression Testing
• RD testing is required to determine an EFB’s functional capability when Type B software applications are used in pressurized aircraft where no alternate procedures or paper backup are available
• Uses RTCA/DO-160 Section 4.6.2 Decompression Test
• Decompression testing may not be required for Class 1 or Class 2 EFBs used in an unpressurized aircraft
Federal AviationAdministration
23Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Altitude Testing
• Class 1 or Class 2 EFBs may require availability up to the maximum operating altitude of the aircraft
• Compliance to RTCA/DO-160 Section 4.6.1 Altitude Test to at least Category D1 or to the maximum operating altitude of the aircraft, whichever is lower
Federal AviationAdministration
24Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Electromagnetic Interference/Non-Interference Testing
• Class 1 or Class 2 EFB used in flight ops must have no adverse impact on other aircraft systems (non-interference)
• If used during take-off and landing, Class 1 & 2 EFBs must be tested for non-interference
• Possible interference when portable EFBs are moved about in the cockpit should be addressed
Federal AviationAdministration
25Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
EFB Data Connectivity
Type CapabilityClass 1 • No data connectivity
Class 2 • May have data connectivity (wired or wireless)• Use installed antennas• Read data from aircraft systems • May be authorized to transmit and receive non-essential AAC data• Can be connected to non-essential data buses, file servers, printers, etc.
Class 3 • May have data connectivity (wired or wireless)• Use installed antennas• Read data from aircraft systems • Can be authorized to an essential data bus• Can be authorized to a critical aircraft data bus• Can transmit AOC data
Federal AviationAdministration
26Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
• Hardware and Software• Guidance Materials• Authorization Process
Where We Are in the Presentation
Federal AviationAdministration
27Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Authorization Process
• FAA Order 8900.1– Volume 3, Chapter 1, Section 1 “The general
process for approval and acceptance”– Volume 4, Chapter 15, Section 1 “ Electronic Flight
Bag Authorization For Use”• Phase 1 - Initiation• Phase 2 - Required Application Information• Phase 3 - POI Review• Phase 4 - Temporary Authorization to use an EFB• Phase 5 - Authorization to Use an EFB
Federal AviationAdministration
28Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase One: Authorization Request
• Begins when the operator requests authorization to use the EFB from the FAA
• During this phase, the FAA and the operator reach a common understanding of the role of the FAA and what documents and actions the operator is responsible for during each phase of the authorization process
Federal AviationAdministration
29Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase Two: Application Submission
• Required Application Information. Phase two begins when the operator submits a formal EFB plan to the POI for evaluation. The plan is reviewed for completeness and the POI facilitates coordination with other inspectors and FAA offices, as necessary.
Federal AviationAdministration
30Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase Two: Application Package
• EFB hardware and application specifications • EFB operator procedures/manual revisions• EFB cockpit procedures checklists• EFB training program• EFB evaluation report• Rapid decompression test data• Completed non-interference test results• Airworthiness documents for Class 2 equipment
Federal AviationAdministration
31Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase Three: POI Review
• POI must use the checklist found in Figure 4-78, to conduct a review of the application submitted by an operator
• All PI specialties should coordinate the review of an operator’s EFB program
Federal AviationAdministration
32Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase Four: Interim Authorization
• An interim EFB authorization is granted to allow the user/operator to proceed with EFB validation testing. During this validation phase, the operator must maintain a paper backup of all electronic information.
• Evaluation report is the end of phase 4 (8900 fig. 4-81)
Federal AviationAdministration
33Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Phase Five: Final Authorization
• Authorization to Use an EFB. An operator subject to regulations under 14 CFR parts 91K, 121, 125 (including part 125M), and 135 is granted authorization to use an EFB through OpSpecs A061 only after acceptable completion of validation testing (see Volume 3, Chapter 18).
• Use Fig. 4-82 EFB Line Evaluation Checklist
Federal AviationAdministration
34Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
New Electronic Flight Bags… New Questions
iPad II
and Beyond
Federal AviationAdministration
35Safety Summit – 14 CFR Part 135 Air OperatorsThursday, April 19, 2012
Questions
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