72(R) ENGINE - RECIPROCATING Rotor blade assemblies, including the heating mate (electrical resistors) for anti -icing. 74 IGNITION ; procedures such as ballasting, etc. That portion of the power plant system which directs and may or may not vary the mass air flow to the engine. Includes items such as receptacles, relays, switches, wiring, warning lights, etc. The lighting sub-systems in the compartment above the floor and between the forward passenger partition and the forward pressure dome. That portion of the system which is used to eliminate or prevent the formation of ice on the pitot and static systems. Those insulation blankets which are used for heat and sound insulation. This specification is maintained by the, This document describes guidelines for common product support practices between airlines and suppliers. Includes items such as display units, transmitters, receivers, computers, etc. Part of the system intended for controlling folding/spreading sequences and for indicating the system operation. That portion of the system which is used to conduct power from the engine to the gearbox. Includes items such as magnetos, distributors, booster coils, exciters, transformers, storage capacitors, and compositors, etc. stream Does not include fire extinguishers, oxygen equipment or masks.
(s) to the airframe. Does not include trailing edge flaps. Shall include procedures to be used such as use of engines, interphone and brakes, ground turning techniques, etc. 41 WATER BALLAST BZX84 series . Those units and components which direct the engine exhaust gases overboard. You may be trying to access this site from a secured browser on the server. 36 PNEUMATIC Does not include systems or items which are included in other chapters except when indication is accomplished as part of an integrated engine instrument system (ref.
That portion of the system which provides for connection of DC power to using systems. Includes ASDAR systems and components. The system which provides means of manually controlling the flight attitude of the helicopter. Includes items such as course computers, flight management computers, performance data computers, and associated control display units, warning annunciators, etc. In 2000, ATA Spec 100 and ATA Spec 2100 were replaced by ATA iSpec 2200: Information Standards for Aviation Maintenance. Includes items such as amplifier, handset, etc.
Includes light fixtures, switches and wiring. Includes sleeves, spindles, dampers, rotor head fairing(s) as well as rotor shaft(s) and swashplate(s) if the rotor head and shaft constitute a non-dissociable assembly. 21 AIR CONDITIONING Special processes for use in the repair of the airplane. Includes tank sealing, attachment of bladder type cells, ventilating system, cell and tank interconnects, filling systems, etc. Includes items such as removable and fixed cabinets, ovens, refrigerators, garbage containers, dish racks, coffee maker and dispensers, containers, electrical outlets, wiring, etc. Includes items such as generators/ alternators, transformers, rectifiers, batteries, control and regulating components, indicating systems, etc., all wiring to but not including main busses. The whole of the system ensuring automatic or manual folding and spreading of the rotor blades and/or tail pylon. That portion of the system which reduces the noise generated by the exhaust gases. 79 OIL
Includes lights such as landing, navigation, position indicating, wing illumination, rotating, courtesy, taxi, etc. Trailing Edge Devices Skins and structure of the wing and trailing edge and removable edge airfoils such as flaps and attach/attached fittings. Part of the system ensuring rotor blade folding and spreading; includes the mechanical, hydraulic and electrical means permanently fitted on the aircraft. 09 TOWING AND TAXIING It shall also include those units or components which are specifically dedicated to record, store or compute weight and balance data. 91 CHARTS, ATA DEFINITIONS OF AIRCRAFT GROUPS, SYSTEMS AND SUB-SYSTEMS. Those instructions necessary to carry out servicing that is normally unscheduled.
Part of system ensuring tail pylon folding and spreading; includes mechanical, hydraulic and electrical means permanently fitted on the aircraft.
The toilet and dressing room areas containing wash basins, dressing tables, and water closet.
PARKING, MOORING, STORAGE AND RETURN TO SERVICE. For turbine engines, includes units external to the basic engine such as thrust reverser and noise suppressor. Includes items such as direct and indirect illumination, passenger call system, lighted signs, etc.
The turbines which extract energy from the exhaust gases and drive an air compressor.
This specification is maintained by the, This specification provides a set of standardized formats for defining, collecting and exchanging aircraft, engine and component reliability data between organizations for the purpose of enhancing aircraft reliability.
29 HYDRAULIC POWER That portion of the systems which controls the position and movement of the trailing edge flaps. Includes wings, airfoil sections of the empennage, and pylons. Central Maintenance System interfaces with Airframe Systems, and identification of maintenance functions related to Airframe Systems.