A
THRUST REVERSER
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
B. The direction of the fan exhaust is reversed during landing by the thrust reverser to produce additional braking power for the airplane.
4. Thrust Reverser (Fig. 1)
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A. The thrust reverser system reverses the direction of the fan exhaust during landing for braking of the airplane.
B. Stowed, the thrust reverser provides a smooth surface for the fan exhaust to produce thrust. Deployed, the thrust reverser redirects the fan exhaust to produce reverse thrust.
C. The thrust levers in the flight compartment, initiate forward or reverse thrust.
D. The thrust reverser control system initiates and synchronizes the deployment of the thrust reverser sleeves.
E. The thrust reverser indicating system provides visual and tactile indication to the flight compartment of thrust reverser position.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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A / PW4000 SERIES /
747-400 / ENGINES /FAULT ISOLATION/MAINT MANUAL ////////////////////////
THRUST REVERSER SYSTEM
COMPONENT FIG. 102 SHT QTY ACCESS/AREA REFERENCE AMM
ACTUATOR - ENGINE 1 T/R OPENING 19 2 415, 416 THRUST REVERSER HALVES 78-31-06
ACTUATOR - ENGINE 2 T/R OPENING 19 2 425, 426 THRUST REVERSER HALVES 78-31-06
ACTUATOR - ENGINE 3 T/R OPENING 19 2 435, 436 THRUST REVERSER HALVES 78-31-06
ACTUATOR - ENGINE 4 T/R OPENING 19 2 445, 446 THRUST REVERSER HALVES 78-31-06
ACTUATOR - ENGINE 1 T/R HYDRAULIC LOCKING 11 2 413, 414, 415B, 416B 78-31-06
ACTUATOR - ENGINE 2 T/R HYDRAULIC LOCKING 11 2 423, 424, 425B, 426B 78-31-06
ACTUATOR - ENGINE 3 T/R HYDRAULIC LOCKING 11 2 433, 434, 435B, 436B 78-31-06
ACTUATOR - ENGINE 4 T/R HYDRAULIC LOCKING 11 2 443, 444, 445B, 446B 78-31-06
ACTUATOR - ENGINE 1 T/R HYDRAULIC NONLOCKING 5 4 413, 414, 415A, 415C, 416A, 416C 78-31-17
ACTUATOR - ENGINE 2 T/R HYDRAULIC NONLOCKING 5 4 423, 424, 425A, 425C, 426A, 426C 78-31-17
ACTUATOR - ENGINE 3 T/R HYDRAULIC NONLOCKING 5 4 433, 434, 435A, 435C, 436A, 436C 78-31-17
ACTUATOR - ENGINE 4 T/R HYDRAULIC NONLOCKING 5 4 443, 444, 445A, 445C, 446A, 446C 78-31-17
ANCHOR STRAP - ENGINE 1 T/R LATCH BAND 3 1 413, 414 FAN COWL PANELS 78-31-03
ANCHOR STRAP - ENGINE 2 T/R LATCH BAND 3 1 423, 424 FAN COWL PANELS 78-31-03
ANCHOR STRAP - ENGINE 3 T/R LATCH BAND 3 1 433, 434 FAN COWL PANELS 78-31-03
ANCHOR STRAP - ENGINE 4 T/R LATCH BAND 3 1 443, 444 FAN COWL PANELS 78-31-03
BAND - ENGINE 1 LATCH 3 1 413, 414 FAN COWL PANELS 78-31-02
BAND - ENGINE 2 LATCH 3 1 423, 424 FAN COWL PANELS 78-31-02
BAND - ENGINE 3 LATCH 3 1 433, 434 FAN COWL PANELS 78-31-02
BAND - ENGINE 4 LATCH 3 1 443, 444 FAN COWL PANELS 78-31-02
CASCADE SEGMENT - ENGINE 1 2 18 415, 416 THRUST REVERSER HALVES 78-31-16
CASCADE SEGMENT - ENGINE 2 2 18 425, 426 THRUST REVERSER HALVES 78-31-16
CASCADE SEGMENT - ENGINE 3 2 18 435, 436 THRUST REVERSER HALVES 78-31-16
CASCADE SEGMENT - ENGINE 4 2 18 445, 446 THRUST REVERSER HALVES 78-31-16
CIRCUIT BREAKER - 10 FLT COMPT, P6 *
ENG 1 T/R CONT, C1703 1 6F13 *
ENG 1 T/R IND, C405 1 6F12 *
ENG 1 T/R LOCK CONT, C10934 1 6F11 *
ENG 2 T/R CONT, C1704 1 6E13 *
ENG 2 T/R IND, C402 1 6E12 *
ENG 2 T/R LOCK CONT, C10935 1 6E11 *
ENG 3 T/R CONT, C1442 1 6D13 *
ENG 3 T/R IND, C403 1 6D12 *
ENG 3 T/R LOCK CONT, C10936 1 6D11 *
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本文链接地址：747-400 AMM 飞机维护手册 EXHAUST 1(3)
