The 737-800 employs a redundant flight control network. Primary flight controls (ailerons, elevators, and rudder) are hydraulically powered but feature a mechanical reversion system. If total hydraulic power is lost, cables and pulleys allow the pilots to physically control the aircraft. Secondary flight controls include trailing-edge flaps, leading-edge devices, and spoilers used for roll assistance and speed braking. 3. High-Priority Performance and Limitations Sections
) required by the flight control actuators during high-rate maneuvers can be expressed as a function of individual actuator displacement ( Vicap V sub i ) and actuation frequency ( boeing 737800 technical manual top
The is the undisputed "top" manual for any mechanic or engineer working on the 737-800. It is the primary source of data for all on-aircraft maintenance activities, serving as the central reference for performing both scheduled and unscheduled work. The AMM provides the practical, step-by-step instructions required to keep the aircraft in an airworthy condition. The 737-800 employs a redundant flight control network
η=1−1rpγ−1γeta equals 1 minus the fraction with numerator 1 and denominator r sub p raised to the the fraction with numerator gamma minus 1 and denominator gamma end-fraction power end-fraction is the compressor pressure ratio ( at cruise) is the specific heat ratio of air ( ≈1.4is approximately equal to 1.4 4. Pneumatics and Environmental Control Systems (ECS) It is the primary source of data for
Wingspan of 34.3m and a wing area of 125 sq meters.
The AMM is logically divided into two main sections:
The official web-based portal where airlines access customized digital manuals, service bulletins, and engineering drawings.