ATA CHAPTER

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.