27-51-02
 ALL  ú ú 01 Page 513 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D02017
A
757
MAINTENANCE MANUAL

CONFIGURATION  AVERAGE INCHES (mm)  MAXIMUM INCHES (mm)  MINIMUM INCHES (mm) 
ON JACKS + ENGINES  0.20 (5.080)  0.30 (7.620)  0.06 (1.524) 
ON GEAR + ENGINES  0.09 (2.286)  0.20 (5.080)  -0.06 (-1.524) 
ON GEAR + ENGINES +  0.11 (2.794)  0.26 (6.604)  -0.11 (-2.794) 
3000 LBS FUEL 

NOTE:A NEGATIVE DIMENSION INDICATES THE INBOARD FLAP TE IS BELOW THE OUTBOARD FLAP TE.
VERTICAL MISFAIR BETWEEN INBOARD/OUTBOARD FLAPS AT TRAILING EDGE TABLE 5
CONFIGURATION  AVERAGE INCHES (mm)  MAXIMUM INCHES (mm)  MINIMUM* INCHES (mm) 
ON JACKS + ENGINES  0.01 (0.254)  0.11 (2.794)  0.00 (0.000) 
ON GEAR + ENGINES  0.05 (1.270)  0.32 (8.128)  0.00 (0.000) 
ON GEAR + ENGINES +  0.18 (4.572)  0.40 (10.160)  0.04 (1.016) 
3000 LBS FUEL 

*THIS IS THE DIMENSION AS IT WAS MEASURED. IF RIGGING IN THIS CONFIGURATION, THE PANEL SHOULD ALWAYS BE RIGGED TO PROVIDE A MINIMUM GAP OF 0.005 INCH (0.127 mm) ALONG PANEL LENGTH.
GAP BETWEEN THE INBOARD UPPER FIXED PANEL AND UPPER SURFACE OF INBOARD FLAP TABLE 6
Fit and Fair Requirement for the Inboard TE Flap
Figure 505 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-02
 ALL  ú ú 01 Page 514 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D02050
A

757
MAINTENANCE MANUAL

TE FLAP PDU LOCK  TE FLAP PDU LOCK

Tools for the Inboard TE Flaps
Figure 506 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-02
 ALL  ú ú 01 Page 515 ú Dec 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

CENTERLINE OF

CENTER PUNCHED RIVET WING STA 111.20 WING BL 91.40 (REF)
FWD

2.8 INCHES (71.1 mm) FROM SIDE OF BODY TO CENTERLINE OF RIGGING BARINBOARD AFT (B27030-124)FLAP (REF)
POSITION OF RIGGING BARS FOR THE INBOARD TE FLAPS (PLAN VIEW, LEFT SIDE IS SHOWN, RIGHT SIDE IS OPPOSITE)
Tools for the Inboard TE Flaps Figure 506 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-02
 ALL  ú ú 01.1 Page 516 ú Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 757 MAINTENANCE MANUAL
 (5)  S 215-020Do a check to make sure that the aft flap is adjusted to the main flap (Ref 27-51-12).
 (6)  S 035-021Disconnect the lower pushrods of the aft flap from the bellcrank (Fig. 501).
 (7)  S 035-022Disconnect the torque tubes at the angle gearbox for the outboard transmission (Ref 27-51-10) and at the drive shaft for the inboard transmission (Ref 27-51-06) (Fig. 502).
 NOTE:____ Do not rotate the torque tubes. You can cause the flap drive to go out of adjustment if you rotate the torque tubes.
 (8)  S 495-003Install the torque tube clamp on the torque tube (Fig. 507).
 (9)  S 865-023Rotate the input shaft to each transmission until the up-stop on the universal touches the up-stop on the ball screw nut (Fig. 501). 

TORQUE TUBE CLAMP, INBOARD FLAP
A
Flap Torque Tube Clamp Figure 507
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-02
 ALL  ú ú 01 Page 517 ú Jun 20/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
E5 EQUIPMENT RACK SEE A
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 4(178)