MAIN EQUIP CTR ACCESS, 119BL
WINDSHEAR PITCH LIMIT INDICATOR
105 00FT DH100 GS250
1750
F
S
A/T SPD
CMD FLARE
ROLLOUT G/S
LOC
L (R) ELEX ATTITUDE DIRECTION INDICATOR (EADI) N4 (N44) (REF)
C
STALL TEST SWITCH (S1)(S2)
TEST
AIR DATA CONFIG L CMPTR R T/O GND PROX
L  RSTALL  LDG  INOP 
WING  DUCT  YAW DMPR  EQUIP COOL 
ANTI ICE  LEAK  L  FWD 

WINDOW/ FUEL R AFT PROBE HEAT QTY
MISC TEST PANEL, M10398 (REF) B
MISC TEST PNL, M10398 (REF)
SEE B
CONTROL COLUMN (REF)
FLT COMPT SEE A

CONTROL COLUMN (REF)
CAPT OR F/O CONTROL COLUMN FWD
SHAKER, M240 OR M952
CONTROL COLUMN (REF) A
Component Location
Figure 102 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-32-00
 ALL  ú ú 01A Page 103 ú Jun 15/87
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 STALL WARNING SYSTEM - ADJUSTMENT/TEST
______________________________________
 1.  General_______
 A.  This procedure gives the operational test and the system test of the stall warning system. There are no adjustments for the stall warning system.
 TASK 27-32-00-715-001
 2.  Operational Test - Stall Warning System (Fig. 501, 502)_______________________________________
 A.  General
 (1)  
The operational test for the left and right stall warning computers (SWC's) is the same. This test is written for the left SWC. When you do the test of the right SWC, replace the instructions for the left system with those for the right system. These are given in parentheses.

 (a)  
Make sure you do the tests for both the left and the right systems if these procedures are being done for scheduled maintenance checks.

 B.  
References

 (1)  
AMM 24-22-00/201, Electrical Power - Control

 (2)  
AMM 27-51-00/201, Trailing Edge Flap System

 (3)  
AMM 27-81-00/201, Leading Edge Slat System

 (4)  
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic System

 (5)  
AMM 31-41-00/201, Engine Indication and Crew Alerting System

 (6)  
AMM 34-21-00/501, Inertial Reference System

 (7)  
AMM 34-22-00/501, Flight Instrument System

 (8)  
AMM 71-11-04/201, Fan Cowl Panels

 (9)  
AMM 78-31-00/201, Thrust Reverser System

 C.  
Access

 (1)  
Location Zones
 119 Main Equipment Center (RH Side)
 211/212 Control Cabin
 500/600 Left Wing/Right Wing

 (2)  
Access Panel
 119BL Main Equipment Center

 D.  
Prepare for the Test

 (1)  
Supply electrical power (AMM 24-22-00/201).

 S 865-004
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-32-00
 ALL  ú ú 01A Page 501 ú Sep 20/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 S 865-005
 WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN
_______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
 (2)  Pressurize the left hydraulic system and reservoir
 (AMM 29-11-00/201).

 S 045-198
 WARNING: DO THE THRUST REVERSERS DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
 (3)  
Do this procedure: Thrust Reverser Deactivation for Ground
 Maintenance (AMM 78-31-00/201).

 S 285-006

 (4)  
Make sure the trailing edge flaps and the leading edge slats are fully retracted, and that the flap lever is in the zero (FLAPS UP) detent (AMM 27-51-00/201 and AMM 27-81-00/201).
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 3(138)