EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-02
ALL ú ú 02 Page 509 ú Jun 20/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
CONFIGURATION AVERAGE MAXIMUM MINIMUM
ON JACKS + ENGINES -0.27` 0.44` -1.72`
ON GEAR + ENGINES 0.19` 2.66` -2.92`
ON GEAR + ENGINES + -0.12` 0.40` -0.53`
3000 LBS FUEL
INBOARD FLAP WING REFERENCE PLANE
TABLE 1
WRP
CARRIAGE (TRACE)
NOTE: WRP AND TRACE OF MFRP ARE NOMINALLY PARALLEL.
WING REFERENCE PLANE (WRP) TO INBOARD FLAP MAIN FLAP REFERENCE PLANE (MFRP)
0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5
MFRP TO WRP ANGLE (DEGREE) INBOARD FLAP ANGLE TO TE HEIGHT CONVERSION
Vertical Adjustment for the Inboard TE Flap Figure 504 (Sheet 3)
D02086
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-02
ALL ú ú 01 Page 510 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-02
ALL ú ú 01 Page 511 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
SERRATED PLATE ASSEMBLY
Fit and Fair Requirement for the Inboard TE Flap
Figure 505 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-02
ALL ú ú 03 Page 512 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
CONFIGURATION INCHES (mm) AVERAGE INCHES (mm) MAXIMUM INCHES (mm) MINIMUM
ON JACKS + ENGINES -0.26 (-6.604) -0.16 (-4.064) -0.40 (-10.160)
ON GEAR + ENGINES -0.16 (-4.064) 0.08 (2.032) -0.30 (-7.620)
ON GEAR + ENGINES + -0.25 (-6.350) -0.08 (-2.032) -0.44 (-11.176)
3000 LBS FUEL
____NEGATIVE DIMENSION INDICATES THE FLAP IS ABOVE THE PANEL.
NOTE:
MAXIMUM MISFAIR BETWEEN THE LOWER FIXED PANEL AND LOWER SURFACE OF INBOARD FLAP OVER LAST 30 INCHES (762 mm) OF THE OUTBOARD END. MEASUREMENT TAKEN AT THE OUTBOARD END OF THE INBOARD FLAP TABLE 1
CONFIGURATION INCHES (mm) AVERAGE INCHES (mm) MAXIMUM INCHES (mm) MINIMUM
ON JACKS + ENGINES -0.10 (-2.540) 0.08 (2.032) -0.25 (-6.350)
ON GEAR + ENGINES -0.01 (-0.254) 0.10 (2.540) -0.10 (-2.540)
ON GEAR + ENGINES + 0.04 (1.016) 0.18 (4.572) -0.16 (-4.064)
3000 LBS FUEL
____NEGATIVE DIMENSION INDICATES THE FLAP IS ABOVE THE PANEL.
NOTE:
MISFAIR BETWEEN THE LOWER FIXED PANEL AND LOWER SURFACE OF INBOARD FLAP
MEASUREMENT DOES NOT APPLY OVER THE OUTBOARD 30 INCHES (762 mm) OF THE INBOARD FLAP
TABLE 2
TABLE 3 NOT USED
____A NEGATIVE DIMENSION INDICATES THE INBOARD FLAP IS AFT OF THE OUTBOARD FLAP.
NOTE:
FORWARD/AFT MISFAIR BETWEEN INBOARD/OUTBOARD MAIN FLAPS AT TRAILING EDGE TABLE 4
Fit and Fair Requirement for the Inboard TE Flap
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 中國航空網 m.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 4(177)
