ATA | Description |
---|---|
52 - 5241 Galley Doors |
Doors For reports pertaining to the galley door. Typical parts are hinges, structure, and the latch mechanism. |
22 - 2215 Autopilot Main Servo |
Auto Flight The unit mechanically connected to primary flight control actuating mechanisms, which is used to mechanically reposition control surfaces in accordance with electrical or pneumatic signals from a controller. |
52 - 5242 Electrical/Electronic Compartment Doors |
Doors For reports pertaining to the electrical/electronic compartment doors. Typical parts are hinges, structure,and the latch mechanism. |
22 - 2216 Autopilot Trim Servo |
Auto Flight The units mechanically connected to flight control cables, etc., for making minor corrections in aircraft attitude or direction. |
52 - 5243 Hydraulic Compartment Doors |
Doors For reports pertaining to the hydraulic compartment doors. Typical parts are hinges, structure, and thelatch mechanism. |
22 - 2220 Speed-Attitude Correction System |
Auto Flight The system which automatically maintains safe flight conditions by correcting for effects of speed and out-of-trim conditions by such means as automatic trim, mach trim, or speed stability and mach feel. This includes sensing, computing, actuating, indicating, internal monitoring, warning devices, etc. |
52 - 5244 Accessory Compartment Doors |
Doors For reports pertaining to the accessory compartment doors. Typical parts are hinges, structure, and thelatch mechanism. |
22 - 2230 Auto Throttle System |
Auto Flight The system that automatically controls the position of the throttles to properly manage engine power during all phases of flight/attitude. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices. Typical parts are amplifiers, computers, servos, limit switches, clutches, gearboxes, warning lights, etc. |
52 - 5245 Air Conditioning Doors |
Doors For reports pertaining to doors used to gain access to the air conditioning compartment system andcomponents. Typical parts are hinges, structure, and the latch mechanism. |
22 - 2250 Aerodynamic Load Alleviating |
Auto Flight The system that automatically corrects and provides for gust loading/upset, aerodynamic augmentation, alleviation, suppression, ride control, etc. This includes sensing, computing, actuating, indicating, internal monitoring, warning devices, etc. |