ATA 100 contains the reference to the ATA numbering system which is a common referencing standard for commercial aircraft documentation. This commonality permits greater ease of learning and understanding for pilots, aircraft maintenance technicians, and engineers alike. The standard numbering system was published by the Air Transport Association on June 1, 1956. While the ATA 100 numbering system has been superseded, it continued to be widely used until it went out of date in 2015, especially in documentation for general aviation aircraft, on aircraft Fault Messages (for Post Flight Troubleshooting and Repair) and the electronic and printed manuals.
The Joint Aircraft System/Component (JASC) Code Tables was a modified version of the Air Transport Association of America (ATA), Specification 100 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 code title. The abbreviated titles have been modified in some cases to clarify the intended use of the accompanying code. The final version of the JASC/ATA 100 code was released by the FAA in 1999. [1]
In 2000 the ATA Technical Information and Communications Committee (TICC) developed a new consolidated specification for the commercial aviation industry, ATA iSpec 2200. It includes an industry-wide approach for aircraft system numbering, as well as formatting and data content standards for documentation output. The main objectives of the new specification are to minimize cost and effort expended by operators and 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, an XML specification for preparing, managing, and using equipment maintenance and operations information.
The unique aspect of the chapter numbers is its relevance for all aircraft. Thus a chapter reference number for a Boeing 747 will be the same for other Boeing aircraft, a BAe 125 and Airbus Aircraft. Examples of this include Oxygen (Chapter 35), Electrical Power (Chapter 24) and Doors (Chapter 52). Civil aviation authorities will also organize their information by ATA chapter like the Master Minimum Equipment List (MMEL) Guidebook from Transport Canada.
The ATA chapter format is always CC-SS where CC is the chapter and SS the section, see ATA extended list section below for details. Some website, like aircraft parts resellers, will sometimes refer to ATA 72R or 72T for reciprocating and turbine engines (jet or turboprop), this nomenclature is not part per se of the ATA numbering definition. The ATA 72 subchapter are different for reciprocating engines and turbine engines. Under JASC/ATA 100 the reciprocating engine are now under ATA 85.
ATA Number | ATA Chapter name Line maintenance TAROM RZV |
---|---|
ATA 00 | GENERAL |
ATA 01 | MAINTENANCE POLICY |
ATA 02 | OPERATIONS |
ATA 03 | SUPPORT |
ATA 04 | AIRWORTHINESS LIMITATIONS |
ATA 05 | TIME LIMITS/MAINTENANCE CHECKS |
ATA 06 | DIMENSIONS AND AREAS |
ATA 07 | LIFTING AND SHORING |
ATA 08 | LEVELING AND WEIGHING |
ATA 09 | TOWING AND TAXIING |
ATA 10 | PARKING, MOORING, STORAGE AND RETURN TO SERVICE |
ATA 11 | PLACARDS AND MARKINGS |
ATA 12 | SERVICING |
ATA 13 | HARDWARE AND GENERAL TOOLS |
ATA 15 | AIRCREW INFORMATION |
ATA 16 | CHANGE OF ROLE |
ATA 18 | VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY) |
.
ATA Number | ATA Chapter name |
---|---|
ATA 20 | STANDARD PRACTICES- AIRFRAME |
ATA 21 | AIR CONDITIONING AND PRESSURIZATION |
ATA 22 | AUTO FLIGHT |
ATA 23 | COMMUNICATIONS |
ATA 24 | ELECTRICAL POWER |
ATA 25 | EQUIPMENT / FURNISHINGS |
ATA 26 | FIRE PROTECTION |
ATA 27 | FLIGHT CONTROLS |
ATA 28 | FUEL |
ATA 29 | HYDRAULIC POWER |
ATA 30 | ICE AND RAIN PROTECTION |
ATA 31 | INDICATING / RECORDING SYSTEM |
ATA 32 | LANDING GEAR |
ATA 33 | LIGHTS |
ATA 34 | NAVIGATION |
ATA 35 | OXYGEN |
ATA 36 | PNEUMATIC |
ATA 37 | VACUUM |
ATA 38 | WATER / WASTE |
ATA 39 | ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS |
ATA 40 | MULTISYSTEM |
ATA 41 | WATER BALLAST |
ATA 42 | INTEGRATED MODULAR AVIONICS |
ATA 43 | EMERGENCY SOLAR PANEL SYSTEM (ESPS) |
ATA 44 | CABIN SYSTEMS |
ATA 45 | ONBOARD MAINTENANCE SYSTEMS (OMS) |
ATA 46 | INFORMATION SYSTEMS |
ATA 47 | INERT GAS SYSTEM |
ATA 48 | IN FLIGHT FUEL DISPENSING |
ATA 49 | (AIRBORNE) AUXILIARY POWER UNIT |
ATA 50 | CARGO AND ACCESSORY COMPARTMENTS |
ATA No. | ATA Chapter Name |
---|---|
ATA 51 | STANDARD PRACTICES AND STRUCTURES - GENERAL |
ATA 52 | DOORS. |
ATA 53 | FUSELAGE |
ATA 54 | NACELLES / PYLONS |
ATA 55 | STABILIZERS |
ATA 56 | WINDOWS |
ATA 57 | WINGS |
ATA Chapter | ATA Chapter name |
---|---|
ATA 60 | STANDARD PRACTICES - PROP./ROTOR |
ATA 61 | PROPELLER / PROPULSORS |
ATA 62 | MAIN ROTOR(S) |
ATA 63 | MAIN ROTOR DRIVE(S) |
ATA 64 | TAIL ROTOR |
ATA 65 | TAIL ROTOR DRIVE |
ATA 66 | FOLDING BLADES/PYLON |
ATA 67 | ROTORS AND FLIGHT CONTROLS |
ATA Number | ATA Chapter name |
---|---|
ATA 70 | STANDARD PRACTICES - ENGINE |
ATA 71 | POWER PLANT |
ATA 72 | ENGINE |
ATA 72 | ENGINE - TURBINE/TURBOPROP, DUCTED FAN/UNDUCTED FAN Sometimes referred to as ATA 72T |
ATA 72 | ENGINE - RECIPROCATING Sometimes referred to as ATA72R |
ATA 73 | ENGINE - FUEL AND CONTROL |
ATA 74 | IGNITION |
ATA 75 | BLEED AIR |
ATA 76 | ENGINE CONTROLS |
ATA 77 | ENGINE INDICATING |
ATA 78 | EXHAUST |
ATA 79 | OIL |
ATA 80 | STARTING |
ATA 81 | TURBINES (RECIPROCATING ENGINES) |
ATA 82 | WATER INJECTION |
ATA 83 | ACCESSORY GEAR BOX (ENGINE DRIVEN) |
ATA 84 | PROPULSION AUGMENTATION |
ATA 85 | FUEL CELL SYSTEMS |
ATA Number | ATA Chapter name |
---|---|
ATA 91 | CHARTS |
ATA 97 | WIRING REPORTING |
ATA 115 | FLIGHT SIMULATOR SYSTEMS |
ATA 116 | FLIGHT SIMULATOR CUEING SYSTEM |
ATA Number | ATA Chapter name |
---|---|
ATA 92 | ELECTRICAL POWER MULTIPLEXING |
ATA 93 | SURVEILLANCE |
ATA 94 | WEAPON SYSTEM |
ATA 95 | CREW ESCAPE AND SAFETY |
ATA 96 | MISSILES, DRONES AND TELEMETRY |
ATA 98 | METEOROLOGICAL AND ATMOSPHERIC RESEARCH |
ATA 99 | ELECTRONIC WARFARE SYSTEM |
The ATA extended List is a breakdown to para (second two numbers e.g. 5-00) and sub para (third two numbers e.g. 5-10-00) for each ATA chapter.
01 INTRODUCTION
02 ORGANIZATION AND HANDLING OF THE MANUAL
03 GENERAL DESCRIPTION OF THE AIRCRAFT
04 AIRWORTHINESS LIMITATIONS
05 TIME LIMITS/ MAINTENANCE CHECKS
06 DIMENSIONS AND AREAS
07 LIFTING & SHORING
08 LEVELING & WEIGHING
09 TOWING & TAXIING
10 PARKING, MOORING, STORAGE & RETURN TO SERVICE
11 PLACARDS AND MARKINGS
12 SERVICING.
13 UNSERVICING
14 RESERVING
15 OPERATIONAL CHECK GOOD
16 *Unassigned
17 *Unassigned
18 VIBRATION AND NOISE ANALYSIS (HELICOPTER ONLY)
19 *Unassigned
20 STANDARD PRACTICES-AIRFRAME
21 AIR CONDITIONING
22 AUTO FLIGHT
23 COMMUNICATIONS
24 ELECTRICAL POWER
25 EQUIPMENT/FURNISHINGS
26 FIRE PROTECTION
27 FLIGHT CONTROLS
28 FUEL
29 HYDRAULIC POWER
30 ICE AND RAIN PROTECTION
31 INDICATING/RECORDING SYSTEMS
32 LANDING GEAR
33 LIGHTS
34 NAVIGATION
35 OXYGEN
36 PNEUMATIC
37 VACUUM
38 WATER/WASTE
39 *Unassigned
40 *Unassigned
41 WATER BALLAST
42 Integrated Modular Avionics (IMA)
43 Emergency Solar Panel System (ESPS)
44 CABIN SYSTEMS
45 CENTRAL MAINTENANCE SYSTEM (CMS)
46 INFORMATION SYSTEMS
47 NITROGEN GENERATION SYSTEM
48 *Unassigned
49 AIRBORNE AUXILIARY POWER
50 CARGO AND ACCESSORY COMPARTMENTS
51 STANDARD PRACTICES, GENERAL
52 DOORS
53 FUSELAGE
54 NACELLES/PYLONS
55 STABILIZERS
56 WINDOWS
57 WINGS
58 *Unassigned
59 *Reserved for Airline Use
60 STANDARD PRACTICES - PROPELLER/ROTOR
61 PROPELLERS/PROPULSION
62 ROTOR(S)
63 ROTOR DRIVE(S)
64 TAIL ROTOR
65 TAIL ROTOR DRIVE
66 FOLDING BLADES/PYLON
67 ROTORS FLIGHT CONTROL
70 STANDARD PRACTICES - ENGINES
71 POWER PLANT
72 ENGINE TURBINE/TURBO PROP DUCTED FAN/UNDUCTED FAN
72 ENGINE - RECIPROCATING
73 ENGINE FUEL AND CONTROL
74 IGNITION
75 AIR
76 ENGINE CONTROLS
77 ENGINE INDICATING
78 EXHAUST
79 OIL
80 STARTING
81 TURBINES
82 WATER INJECTION
83 ACCESSORY GEAR-BOXES
84 PROPULSION AUGMENTATION
85 RECIPROCATING ENGINE
115 FLIGHT SIMULATOR SYSTEMS/WORK SIMULATION
111:Lower Nose Compartment (BS 178 - BS 360) 112:Electronic Compartment (BS 360 - BS 480) 113:Forward Cargo Compartment 727-100 (BS 480 - BS 680) 727-200(BS 480 - BS 720D) 114:Air Conditioning Distribution Bay 727-100(BS 680 - BS 740) 727-200(BS 680 - BS 720D - BS 740) 115:Aft Cargo Compartment (BS 952 - BS 1176) 116:Forward Stairs and Fairing Door (BS 303.9 - BS 351.2, If Applicable) 131:Nose Wheel Well (BS 227.8 - BS 351.2) 132:Keel Beam Area (Antenna Bays) (BS 740 - BS 960) 133:Left Air Conditioning Equipment Compartment 727-100(BS 580 - BS 870) 727-200(BS 698 - BS 870) 134:Right Air Conditioning Equipment Compartment 727-100(BS 580 - BS 870) 727-200(BS 698 - BS 870) 135:Left Main Wheel Well And Wing To Body Fairing 727-100 (BS 870 - BS 1076) 727-200(BS 870 - BS 1007) 136:Right Main Wheel Well And Wing To Body Fairing 727-100 (BS 870 - BS 1076) 727-200(BS 870 - BS 1007) 141:Radome (BS 130 - BS 178) 174:Bladder Fuel Cell Area Tank 2 (Left BBL 70.5 - Right BBL 70.5)
221:Control Cabin Left (BS 178 - BS 259.5) 222:Control Cabin Right (BS 178 - BS 259.5) 223:Third Crewmember Station (BS 259.5 - BS 302) 224:Passenger Cabin (BS 302 - BS 1183) 225:Forward Lavatory Compartment (BS 304 - BS 343) 226:Galley Units No1 & No2 (BS 600 - BS 708) 227:Aft Left Lavatory Compartment (BS 1137 - BS 1176) 228:Aft Right Lavatory Compartment (BS 1137 - BS 1176) 237:Aft Airstairs Left Equipment Area (BS 1183 - BS 1342.4) 238:Aft Airstairs Right Equipment Area (BS 1183 - BS 1342.4) 239:Tailskid Compartment 242:Forward Entry Door (BS 312) 246:Aft Entry Door (BS 1183) 246A:Aft Service Door (BS 1052) 247:Aft Airstairs (BS 1223) 248:Main Cargo Door (BS 480 - BS 620 If Applicable) 249:Escape Hatches (BS 772 - BS 873)
391:Left Horizontal Stabilizer (Inspar) 391A:Left Horizontal Stabilizer (Leading Edge) 391B:Left Horizontal Stabilizer (Trailing Edge) 392:Right Horizontal Stabilizer (Inspar) 392A:Right Horizontal Stabilizer (Leading Edge) 392B:Right Horizontal Stabiliser (Trailing Edge) 393:Left Elevator And Tab 394:Right Elevator And Tab 395:Vertical Fin (Inspar) 395A:Vertical Fin (Leading Edge) 395B:Vertical Fin (Trailing Edge) 396:Stabilizer Trim Mechanism Compartment 397:Vertical Fin Tip Fairing 398:Upper Rudder And Tab 399:Lower Rudder And Tab
451:Engine No1 452:Engine No2 453:Engine No3 454:Engine Strut No1 455:Engine Strut No3
561:Left Removable Wing Tip 562:Left Outboard Wing Leading Edge (Inc Slats 1 -4 WS 332.5 - WS 790) 563:Left Inbd Wing Leading Edge (Inc L.D Flaps 1 -3 WBL 70.597 - WS 332.5) 571:Left Fuel Vent Surge Tank And Fuel Vent Outlet (Left WS 716.5 - Removable Wing Tip) 572:Tank No 1 ( Left WS 224.5 - Left WS 715.5) 573:Left Integral Section Tank No 2 (Left WBL 70.597 - WS 2244.5) 581:Left Wing Trailing Edge, Outbd Aileron And Control Tab 582:Left Wing Trailing Edge Outbd Flap And Spoilers No1 - No4 583:Left Wing Trailing Edge, Inbd Aileron And Control Tab 584:Left Wing Trailing Edge, Inbd Flap And Spoilers No5 - No7
664:Right Inbd Wing Leading Edge (Inc L.D Edge Flaps No44 - No6 WBL 70.597 - WS 332.5) 665:Right Otbd Wing Leading Edge (Inc Slats No5 - No8 WS 322.5 - WS 790) 666:Right Removable Wing Tip 675:Right Integral Section Tank No2 (Right WBL 70.597 - Right WS 224.5) 676:Tank No3 (Right WS 224.5 - Right WS 716.5) 677:Right Fuel Vent Surge Tank And Fuel Outlet (Right WS 716.5 - Removable Wing Tip) 685:Right Wing Trailing Edge, Inbd Flap And Spoilers No8 - No10 686:Right Wing Trailing Edge, Inbd Aileron And Control Tab 687:Right Wing Trailing Edge, Otbd Flap And Spoilers No11 - No14 688:Right Wing Trailing Edge, Otbd Aileron And Control Tab
710:Nose gear and doors 711:Nose gear 712:Forward side door R.H. 713:Forward side door L.H. 714:Rear door R.H. 715:Rear door L.H. 720:Main gear and doors L.H. 721:Main gear 722:Forward door 723:Mid door 724:Rear door R.H. 725:Rear door L.H. 730:Main gear and doors R.H. 731:Main gear 732:Forward door 733:Mid door 734:Rear door R.H. 735:Rear door L.H.
821:Forward Cargo Door 822:Aft Cargo Door 831:Forward Entry Door 832:Emergency Exit 833:Emergency Exit 834:Aft Entry Door 841:Forward Galley Service Door 842:Emergency Exit 843:Emergency Exit 844:Aft Galley Service Door
The McDonnell Douglas DC-10 is an American trijet wide-body aircraft manufactured by McDonnell Douglas. The DC-10 was intended to succeed the DC-8 for long-range flights. It first flew on August 29, 1970; it was introduced on August 5, 1971, by American Airlines.
Landing gear is the undercarriage of an aircraft or spacecraft that is used for taxiing, takeoff or landing. For aircraft, it is generally needed for all three of these. It was also formerly called alighting gear by some manufacturers, such as the Glenn L. Martin Company. For aircraft, Stinton makes the terminology distinction undercarriage (British) = landing gear (US).
The Cessna 182 Skylane is an American four-seat, single-engined light airplane built by Cessna of Wichita, Kansas. It has the option of adding two child seats in the baggage area.
The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight training, touring and personal use. In 1977, it was succeeded in production by the Cessna 152, a minor modification to the original design.
AAI Corporation is an aerospace and defense development and manufacturing firm, located in Hunt Valley, Maryland, US. Formerly a wholly owned subsidiary of United Industrial Corporation, AAI was acquired by Textron in 2007. It currently operates as a unit of Textron Systems and employs more than 2,000.
The Mil V-12, given the project number Izdeliye 65, is a prototype helicopter designed in the Soviet Union and the largest helicopter ever built. The designation "Mi-12" would have been the designation for the production helicopter and did not apply to V-12 prototypes.
The Learjet 25 is an American ten-seat, twin-engine, high-speed business jet aircraft manufactured by Learjet. It is a stretched version of the Learjet 24.
The Space Shuttle orbiter is the spaceplane component of the Space Shuttle, a partially reusable orbital spacecraft system that was part of the discontinued Space Shuttle program. Operated from 1981 to 2011 by NASA, the U.S. space agency, this vehicle could carry astronauts and payloads into low Earth orbit, perform in-space operations, then re-enter the atmosphere and land as a glider, returning its crew and any on-board payload to the Earth.
The center of gravity (CG) of an aircraft is the point over which the aircraft would balance. Its position is calculated after supporting the aircraft on at least two sets of weighing scales or load cells and noting the weight shown on each set of scales or load cells. The center of gravity affects the stability of the aircraft. To ensure the aircraft is safe to fly, the center of gravity must fall within specified limits established by the aircraft manufacturer.
The Lioré et Olivier LeO H.242 was a monoplane flying boat aircraft designed and produced by the French aircraft manufacturer Lioré et Olivier. It was used for European passenger air services in the 1930s, including by the flag carrier Air France. One LeO H.242 was depicted near the end of Hergé's The Adventures of Tintin comic King Ottokar's Sceptre.
The Bennett Aircraft Corporation Bi-motored Transport Commercial Number One (BTC-1) Executive was a 1930s American eight-seat light transport aircraft built by the Bennett Aircraft Corporation. In the ten-year span of its known life, the Bennett BTC-1 was identified in print by four different names: the Bennett, the Breese Bennett, the Bowlus Bennett and the Globe BTC-1.
The Fiat AS.1 was a light touring monoplane aircraft designed and produced by the Italian aircraft manufacturer Fiat.
The Junkers G 31 was an advanced tri-motor airliner designed and produced by the German aircraft manufacturer Junkers. It would be the first airliner operated by Deutsche Luft Hansa to feature a flight attendant.
The BFW M.29 was a single-engine twin-seat low-wing aircraft produced by the German aircraft manufacturer Bayerische Flugzeugwerke (BFW). It was designed by Willy Messerschmitt to participate in the 1932 Circuit of Europe races.
Throughout a normal flight, a pilot controls an aircraft through the use of flight controls including maintaining straight and level flight, as well as turns, climbing, and descending. Some controls, such as a "yoke" or "stick" move and adjust the control surfaces which affects the aircraft's attitude in the three axes of pitch, roll, and yaw. Other controls include those for adjusting wing characteristics and those that control the power or thrust of the propulsion systems. The loss of primary control systems in any phase of flight is an emergency. Aircraft are not designed to be flown under such circumstances; however, some pilots faced with such an emergency have had limited success flying and landing aircraft with disabled controls.
The Shenyang J-35 is a series of Chinese twin-engine, all-weather, stealth multirole combat aircraft manufactured by Shenyang Aircraft Corporation (SAC), designed for air superiority and surface strike missions. The aircraft reportedly has two variants, a land-based variant designed for the People's Liberation Army Air Force (PLAAF), and a carrier-based variant optimized for catapult-assisted takeoff (CATOBAR) for the People's Liberation Army Naval Air Force (PLANAF).
The SPCA 30, also known as SPCA Type III, was a bomber aircraft designed and produced by the French aircraft manufacturer Société Provençale de Constructions Aéronautiques (SPCA).
The Little Wing Roto-Pup is an American autogyro that was designed and produced by Little Wing Autogyros, Inc. of Mayflower, Arkansas, introduced in the 1990s. Now out of production, when it was available the aircraft was supplied as a kit for amateur construction.
The Mikoyan-Gurevich I-7 was a development of the Mikoyan-Gurevich I-3 experimental fighter. Planned as a Mach 2-class aircraft, the I-7 was the second of a series of three experimental fighter aircraft from the Mikoyan-Gurevich design Bureau. Like the Mikoyan-Gurevich I-3, the I-7 was to be one of the components of the automated Uragan-1 then under development by protivovozdushnaya oborona strany, the Soviet defense system.
The Ford 14-A was a prototype three-engined, large, streamlined, 32 passenger aircraft built in 1932. Though apparently completed, it never flew.