ATA 100 ATA 100 contains the reference to the ATA numbering system which was a common referenci referencing ng standard for all commercial commerc ial aircraf aircraftt documentation. documentation. This commonality commonality permits greater ease of learning and understanding for pilots,, aircraft maintenance technicians, pilots technicians, and engineers alike. The standard numbering system was published by the Air the Air Transport Association Association on June June 1, 1956. While While the ATA 100 numbering system has been superseded, it continued to be widely used until it went out of date back in 2015, especially especially in documentation documentation for general for general aviation aircraft, on aircraft Fault Messages (for Post Flight Troubleshooting and Repair) and the electronic and printed manuals.
1.1
Aircr Aircraf aftt Ge Gener neral al
1.2
Airframe Airframe system systemss
1.3 1.3
Stru Struct ctur uree
1.4
Prop Propell eller/ er/ro roto torr
1.5 1.5
Powe werr plan plantt
The Joint Aircraft System/Component (JASC) Code Tables was a modified version of the Air Transport Association ciation of America America (ATA), (ATA), Specificati Specification on 100 code. code. It was developed by the FAA’s, Regulatory Support Division (AFS-600). This code table was constructed by using the new JASC code four digit format, along with an abbreviated abbreviated code title. The abbreviated abbreviated titles have been modified in some cases to clarify the intended use of the accompanying accompanying code. The final version version of the JASC/ATA JASC/ATA 100 code was released by the FAA in 1999. [1]
2.1
2
ATA exte extend nded ed list list (Out (Out Of Of Date Date)) ATA ATA Specific Specificati ation on 2200
The ATA extended List is a breakdown to para para (second (second two numbers e.g. 5-00) and sub and sub para (third para (third two numbers e.g. 5-10-00) for each ATA chapter. 2.1.1
ATA ATA Number Number and Para
01 *Reserved for Airline Use
In 2000 the ATA Technical Information and Communications cations Committee Committee (TICC) (TICC) develo developed ped a new consolid consolidated ated specification for the commercial aviation industry, ATA industry, ATA iSpec 2200. 2200. It includes includes an industry industry-wid -widee approach approach for aircraft aircraft system numbering, as well as formatting and data content content standards standards for documentati documentation on output. output. The main objectives of the new specification are to minimize cost and effort expended by operators and manufacturers, manufacturers, improve information quality and timeliness, and facilitate manufacturers’ delivery of data that meet airline operational needs.[2] More recently, the international aviation community developed the S1000D standard, standard, an XML specification for preparing, managing, and using equipment maintenance and operations operations information. information.
02 *Reserved for Airline Use
The unique aspect of the chapter numbers is its relevance relevance for for all aircraft. aircraft. Thus a chapter chapter refere reference nce number number for for a Boeing 747 will 747 will be the same for other Boeing aircraft, a BAe 125 and 125 and Airbus Airbus Aircraf Aircraft. t. Examples Examples of this include include Oxygen Oxygen (Chapter 35), Electrical Power Power (Chapter 24) and Doors (Chapter 52).
07 LIFTING & SHORING
03 *Reserved for Airline Use 04 *Reserved for Airline Use 05 TIME LIMITS/ MAINTENANCE CHECKS 00 General
−
10 Time Limits
−
20 Scheduled Scheduled Maintenance Checks
−
30 &
−
40 Reserved Reserved
−
50 Unscheduled Maintenance checks
−
06 DIMENSIONS AND AREAS
00 General
−
10 Jacking
−
20 Shoring
−
08 LEVELING & WEIGHING 00 General
−
1
ATA Chapte Chapters rs (Out (Out Of Date) Date)
10 Weighing and Balancing
−
20 Leveling
−
1
2
2
09 TOWING & TAXIING 00 General
−
10 Towing
−
20 Taxiing
−
10 PARKING, MOORING, STORAGE & RETURN TO SERVICE 11 PLACARDS AND MARKINGS 00 General
−
ATA EXTENDED LIST (OUT OF DATE)
22 AUTO FLIGHT 00 General
−
10 Autopilot
−
20 Speed-Attitude Correction
−
30 Auto Throttle
−
40 System Monitor
−
50 Aerodynamic Load Alleviating
−
23 COMMUNICATIONS
−10 Exterior Color Schemes and Markings
20 Exterior Placards and Markings
−
30 Interior Placards
−
− −
12 SERVICING
00 General 10 Speech Communications 15 SATCOM
−
20 Data Transmission and Automatic Calling
−
00 General
−
10 Replenishing
−
30 Passenger Address, Entertainment and Comfort −
40 Interphone
20 Scheduled Servicing
−
30 Unscheduled Servicing
−
− −
50 Audio Integrating 60 Static Discharging
−
13 Unservicing
70 Audio & Video Monitoring
−
14 Reservicing
80 Integrated Automatic Tuning
−
15 Ops Check Good 16 *Unassigned
24 ELECTRICAL POWER
17 *Unassigned 18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)
00 General
−
10 Generator Drive
−
20 AC Generation
−
00 GENERAL -
−
10 VIBRATION ANALYSIS
−
20 NOISE ANALYSIS
30 DC Generation
−
40 External Power
−
−
50 AC Electrical Load Distribution
−
19 *Unassigned
60 DC Electrical Load Distribution
−
20 STANDARD PRACTICES-AIRFRAME 25 EQUIPMENT/FURNISHINGS 00 Electrical Standard Items/Practices
−
90 *Reserved for Airline Use
−
00 General
−
10 Flight Compartment
−
21 AIR CONDITIONING
20 Passenger Compartment
−
30 Galley
00 Air Conditioning - General
−
10 Compression
−
20 Distribution
−
30 Pressurization Control
−
40 Heating
−
− − − − −
50 Cooling
−
40 Lavatories 50 Additional Compartments 60 Emergency 70 Available 80 Insulation
−
60 Temperature Control
−
70 Moisture/Air Contaminant Control
−
26 FIRE PROTECTION
2.1
3
ATA Specification 2200
00 General
−
10 Detection
−
20 Extinguishing
−
30 Explosion Suppression
−
−
−
−
−
00 General 10 Instrument & Control Panels 20 Independent Instruments 30 Recorders 40 Central Computers
−
27 FLIGHT CONTROLS
50 Central Warning Systems
−
60 Central Display Systems
−
00 General
−
70 Automatic Data Reporting Systems
−
10 Aileron & Tab
−
20 Rudder & Tab
−
32 LANDING GEAR
30 Elevator & Tab
−
40 Horizontal Stabilizer
−
50 Flaps
−
60 Spoiler, Drag Devices and Variable Aerodynamic Fairings −
00 General
−
10 Main Gear and Doors
−
20 Nose Gear and Doors
−
30 Extension and Retraction
−
40 Wheels and Brakes
70 Gust Lock & Dampener
−
80 Lift Augmenting
−
−
−
50 Steering 60 Position Indication and Warning
−
28 FUEL 00 General
−
70 Supplementary Gear
−
33 LIGHTS
10 Storage
−
20 Distribution
−
30 Dump
−
40 Indicating
−
00 General
−
10 Flight Compartment
−
20 Passenger Compartment
−
30 Cargo and Service Compartments
−
29 HYDRAULIC POWER
40 Exterior
−
50 Emergency Lighting
−
00 General
−
10 Main
−
20 Auxiliary
−
30 Indicating
−
30 ICE AND RAIN PROTECTION
34 NAVIGATION 00 General
−
10 Flight Environment Data
−
20 Attitude & Direction
−
30 Landing and Taxiing Aids
−
40 Independent Position Determining
00 General
−
10 Airfoil
−
20 Air Intakes
−
−
−
−
30 Pitot and Static
−
40 Windows, Windshields and Doors
50 Dependent Position Determining 60 Flight Management Computing
35 OXYGEN
−
50 Antennas and Radomes
−
60 Propellers/Rotors
−
70 Water Lines
−
80 Detection
−
−
−
−
−
31 INDICATING/RECORDING SYSTEMS
00 General 10 Crew 20 Passenger 30 Portable
36 PNEUMATIC
4
2
00 General
−
ATA EXTENDED LIST (OUT OF DATE)
46 INFORMATION SYSTEMS
10 Distribution
−
20 Indicating
−
00 General
−
10 Airplane General Information Systems
−
37 VACUUM
20 Flight Deck Information Systems
−
30 Maintenance Information Systems
−
00 General
−
40 Passenger Cabin Information Systems
−
10 Distribution
−
50 Miscellaneous Information Systems
−
20 Indicating
−
38 WATER/WASTE 00 General
−
47 NITROGEN GENERATION SYSTEM 48 *Unassigned 49 AIRBORNE AUXILIARY POWER
10 Potable
−
20 Wash
−
30 Waste Disposal
−
40 Air Supply
−
00 General
−
10 Power Plant
−
20 Engine
−
30 Engine Fuel and Control
−
39 *Unassigned
−
40 *Unassigned
−
41 WATER BALLAST
−
40 Ignition/Starting 50 Air 60 Engine Controls 70 Indicating
−
00 General
−
10 Storage
−
80 Exhaust
−
90 Oil
−
20 Dump
−
30 Indication
−
50 CARGO AND ACCESSORY COMPARTMENTS
42 Integrated Modular Avionics (IMA)
−
43 *Unassigned
−
44 CABIN SYSTEMS
−
00 General 10 Cargo Compartments 20 Cargo Loading Systems 30 Cargo Related Systems
−
00 General
−
10 Cabin Core System
−
20 In-flight Entertainment System
−
40 Available
−
50 Accessory
−
60 Insulation
−
30 External Communication System
−
40 Cabin Mass Memory System
−
51 STANDARD PRACTICES, GENERAL
50 Cabin Monitoring System
−
60 Miscellaneous Cabin System
−
00 General
−
10 Investigation, Cleanup and Aerodynamic Smoothness −
45 CENTRAL MAINTENANCE SYSTEM (CMS)
20 Processes
−
00 General
−
5 thru −19 CMS/Aircraft General
−
20 thru −49 CMS/Airframe Systems
−
30 Materials
−
40 Fasteners
−
45 Central Maintenance System
50 Support of Airplane for Repair and Alignment Check Procedures
50 thru −59 CMS/Structures
−
60 thru −69 CMS/Propellers
−
70 thru −89 CMS/Power Plant
−
− − − −
−
60 Control-Surface Balancing 70 Repairs 80 Electrical Bonding
2.1
5
ATA Specification 2200
52 DOORS
58 *Unassigned
00 General
−
59 *Reserved for Airline Use
10 Passenger/Crew
60 STANDARD PRACTICES - PROPELLER/ROTOR
20 Emergency Exit
61 PROPELLERS/PROPULSION
− −
30 Cargo
−
00 General
40 Service and Miscellaneous
−
50 Fixed Interior
−
60 Entrance Stairs
−
70 Monitoring and Operation
−
80 Landing Gear
−
− − − − −
30 Braking 40 Indicating 50 Propulsor Duct
00 General
−
10 thru tions
20 Controlling
−
53 FUSELAGE
−
10 Propeller Assembly
62 ROTOR(S)
90 (As Required) Fuselage Sec-
−
54 NACELLES/PYLONS
00 General
−
10 Rotor blades
−
20 Rotor head(s)
−
00 General
−
10 thru −40 (As Required) Nacelle Section
30 Rotor Shaft(s)/Swashplate Assy(ies)
−
−
50 thru −80 (As Required) Pylon
−
55 STABILIZERS 00 General
−
10 Horizontal Stabilizer or Canard
−
20 Elevator
40
−
63 ROTOR DRIVE(S) 00 General
−
10 Engine/Gearbox couplings
−
−
30 Vertical Stabilizer
−
40 Rudder
−
20 Gearbox(es)
−
30 Mounts, attachments
−
40 Indicating
−
56 WINDOWS 00 General
−
10 Flight Compartment
−
20 Passenger Compartment
64 TAIL ROTOR 00 General
−
−
30 Door
−
40 Inspection and Observation
−
10* Rotor blades
−
20* Rotor head
−
30 Available
−
57 WINGS
40 Indicating
−
00 General
−
10 Center Wing
−
65 TAIL ROTOR DRIVE
20 Outer Wing
−
30 Wing Tip
−
00 General
−
10 Shafts
40 Leading Edge and Leading Edge Devices
−
50 Trailing Edge Trailing Edge Devices
−
60 Ailerons and Elevons
−
70 Spoilers
−
− − − −
20 Gearboxes 30 Available 40 Indicating
80 (as required)
−
90 Wing Folding System
−
66 FOLDING BLADES/PYLON
6
2
00 General
−
ATA EXTENDED LIST (OUT OF DATE)
74 IGNITION
10 Rotor blades
−
20 Tail pylon
−
30 Controls and Indicating
−
00 General
−
10 Electrical Power
−
20 Distribution
−
67 ROTORS FLIGHT CONTROL 00 General
−
30 Switching
−
75 AIR
10 Rotor
−
20 Anti-torque Rotor control (Yaw control)
−
30 Servo-control System
−
00 General
−
10 Engine Anti-Icing
−
20 Cooling
−
30 Compressor Control
68 *Unassigned
−
69 *Unassigned
−
70 STANDARD PRACTICES - ENGINES 71 POWER PLANT 00 General
−
10 Cowling
−
20 Mounts
40 Indicating
76 ENGINE CONTROLS 00 General
−
10 Power Control
−
20 Emergency Shutdown
−
−
30 Fireseals
−
77 ENGINE INDICATING
40 Attach Fittings
−
00 General
50 Electrical Harness
−
60 Air Intakes
−
70 Engine Drains
−
−
−
−
10 Power 20 Temperature 30 Analyzers
−
72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN 00 General
40 Integrated Engine Instrument Systems
−
78 EXHAUST
−
10 Reduction Gear, Shaft Section (TurboProp and/or Front Mounted Gear Driven Propulsor) −
20 Air Inlet Section
−
30 Compressor Section
−
40 Combustion Section
−
50 Turbine Section
−
00 General
−
10 Collector/Nozzle
−
20 Noise Suppressor
−
30 Thrust Reverser
−
40 Supplementary Air
−
79 OIL
60 Accessory Drives
−
70 By-pass Section
−
80 Propulsor Section (Rear Mounted)
−
−
−
00 General 10 Storage 20 Distribution
−
73 ENGINE FUEL AND CONTROL 00 General
−
30 Indicating
−
80 STARTING
10 Distribution
−
20 Controlling
−
30 Indicating
−
−
−
00 General 10 Cranking
7
81 TURBINES
102 *Do not use 103 *Do not use
00 General
−
−10 Power Recovery
20 Turbo-Supercharger
−
82 WATER INJECTION
104 *Do not use 105 *Do not use 106 *Do not use 107 *Do not use 108 *Do not use
00 General
−
10 Storage
−
20 Distribution
−
30 Dumping and Purging
−
40 Indicating
−
83 ACCESSORY GEAR-BOXES
109 *Do not use 110 *Do not use 111 *Do not use 112 *Do not use 113 *Do not use 114 *Do not use 115 FLIGHT SIMULATOR SYSTEMS
00 General
−
10 Drive Shaft Section
−
20 Gearbox Section
2.1.2
ATA Para and Sub Para Numbers
−
00-00 General
−
84 PROPULSION AUGMENTATION
01-00 Zone 100 Fuselage Lower
−
00 General
−
02-00 Zone 200 Fuselage Top
−
10 Jet Assist Takeoff
−
03-00 Zone 300 Stabilizers
−
04-00 Zone 400 Nacelles-Pylons
85 RECIPROCATING ENGINE
−
05-00 Zone 500 Left Wing
−
00 General
−
06-00 Zone 600 Right Wing
−
10 Fuel Cell Stack
−
07-00 Zone 700 Landing Gear Compartment
−
86 *Unassigned
08-00 Zone 800 Doors
−
87 *Unassigned
09-00 Zone 900 Lavatories & Galleys
−
88 *Unassigned 89 *Unassigned 90 *Unassigned
3
See also
91 CHARTS 92 *Unassigned
•
Air Transport Association
•
S1000D
93 *Unassigned 94 *Unassigned 95 *Reserved for Airline Use 96 *Reserved for Airline Use
4
External links
97 WIRING REPORTING 98 *Reserved for Airline Use
•
99 *Unassigned •
100 *Do not use 101 *Do not use
•
For a list of the chapter headings S-TechEnterprises ATA Chapter list JASC Codes PDF
8
5
5
References
[1] MONRONEY, MIKE. “FEDERAL AVIATION ADMINISTRATION JOINT AIRCRAFT SYSTEM/COMPONENT CODE TABLE AND DEFINITIONS” (PDF). FAA. Retrieved 22 November 2013. [2] Lowe, David. “From Paper to Interactive Electronic Technical Publications” (PDF). Immedius Inc. Retrieved 22 November 2013. •
ATA Specification 100 - Specification for Manufacturers’ Technical Data, Revision No. 37 (1999). Air Transport Association of America.
REFERENCES
9
6
Text and image sources, contributors, and licenses
6.1 •
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