*
Primary Flight Computer Reset
*
Primary Flight Computer (C) Lane Reset
EFFECTIVITY
BEJ ALL
*
Primary Flight Computer (L) Lane Reset
*
Primary Flight Computer (R) Lane Reset
*
Primary Flight Computer Self Test
*
Radio Altimeter Test Inhibit to PFC Interface
*
Right Aileron Actuator Confidence
*
Right Aileron Alignment
*
Right Aileron Position
*
Right Elevator Actuator Confidence
*
Right Elevator Alignment
*
Right Elevator Oscillation Monitor
*
Right Elevator Position
*
Right Flaperon Actuator Confidence
*
Right Flaperon Alignment
*
Right Flaperon Position
*
Rudder Actuator Confidence
*
Rudder Alignment
*
Rudder Position
*
Rudder Trim System
*
Speedbrake System
*
Spoiler 1, 7, 8, 14 System
*
Spoiler 2, 13 System
*
Spoiler 3, 6, 9, 12 System
*
Spoiler 4, 11 System
*
Spoiler 5, 10 System
*
Stabilizer System
*
Transmitter Reset Test
*
Warning Electronic System to PFC Interface
*
Wheel Force Transducer
*
Wheel Position.
27-02-00
Page 81 D633W101-BEJ Sep 05/2002
PFCS -SYSTEM TESTS
Actuator Confidence Test
This test checks the proper operation of the power control unit servo valve monitors and for proper operation of the bypass, blocking, and pressure reducing functions of the primary power control units and the motor-operated valve in each of the stabilizer control modules.
Actuator Control Electronics Monitors
This test is to make sure the internal monitors necessary for flight safety in the L1, L2, C and R actuator control electronics operate correctly.
Air/Ground System to PFC Interface
This test does a check of the proper operation of the weight on wheel (WOW) system interface to the primary flight computers (PFCs). The test resets latches associated with the WOW system interface.
Alternate Pitch Trim Levers
This test checks for proper operation of the switches for the alternate pitch trim levers. This test can reset latches for the alternate pitch trim levers.
Column Force Transducer
This test checks for proper operation of the force transducers for the pilot and co-pilot control columns. This test can reset latches for control column force transducers. This test is similar to the wheel force transducer test.
Column Position
This test checks for proper operation of the transducers for the pilot and co-pilot control columns. This test can reset latches for control column transducers. This test is similar to the pedal position test and the wheel position test.
Elevator Feel System
This test checks for proper operation of the elevator feel units. This test can reset latches for the elevator feel units. This test can also set the configuration of either elevator feel unit to 3 different elevator feel settings.
Flap/Slat Electronics Unit Interface to ACE
This test checks for proper operation of the interface between the FSEUs and the ACEs. This test can also set the configuration of either FSEU to its flaps and slats retracted state or its flaps and slats not retracted state for fault isolation purposes. This test can reset latches associated with the analog wiring between the ACEs and the FSEUs.
EFFECTIVITY BEJ ALL 27-02-00
Page 82
D633W101-BEJ Sep 05/2002
PFCS -SYSTEM TESTS
Flap/Slat Electronics Unit to PFC Interface
This test checks for proper operation of the flap slat electronic units. This test can reset latches for the flap slat electronic units.
Gust Suppression Pressure Transducers
This test checks the proper operation of the gust suppression transducers. This test can reset latches for the gust suppression transducers.
Left Aileron Actuator Confidence
This test checks the proper operation of the bypass and blocking/damped functions of the left aileron power control units. This test is similar to the actuator confidence tests for the other surfaces.
Left Aileron Alignment
This procedure aligns the power control units for the left aileron. This procedure can also check alignment of the left aileron power control units. This test is similar to the alignment tests for the other surfaces.
Left Aileron Position
This test checks for proper operation of the position transducers for the left aileron. This test can reset latches for left aileron position transducers. This test is similar to the position test for the other surfaces.
EFFECTIVITY
BEJ ALL
Left Elevator Oscillation Monitor 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：777 AMM 飞机维护手册 飞行操纵 Flight Controls 1(17)
