737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 2(114)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 b)  737-300 AIRPLANES; Refer to the table that follows:
 NOTE: For the aluminum tab pushrod:
____ The nominal tab position "a" is 0.315 inch at 70°F, if the spacer thickness "t" is 0.50 inch, SJ = -0.02 inch then the initial elevator tab dimension "Xi" is 0.315 + 0.50 + (-0.02) =
 0.795 inch.
 NOTE: For the titanium tab pushrod:
____ The nominal tab position "a" is 0.34 inch (for all ambient temperatures), the spacer thickness "t" is 0.50 inch, SJ = -0.02 inch then the initial elevator tab dimension "Xi" is
 0.34 + 0.50 + (-0.02) = 0.82 inch.
 ~......................................................................... | Elevator Tab "Xi" Dimension Before Flight Test (if an | | alternative rigging fixture tool, F80248.8 or TE27T-31001-( ), is used | | Table 504 for 737-300 | ...........................................................................
 |   |  |  |  |Initial Tab |
 |  AIRPLANE  |  NOMINAL TAB  | SPACER  |  INCREMENTAL  |Xi Dimension|
| TEMPERATURE |  "a" DIMENSION  |THICKNESS|  TAB POSITION  |  Before  |
 |  |  BEFORE  |  |  DUE TO  |Flight Test |
 |  |  FLIGHT TEST  |  |  SKI JUMP  | Xi = a +  |
 |  |  |  |  (OPTIONAL)  |  t + SJ |

 ........................................................................... | °F | °C |Aluminum|Titanium| "t" | "SJ" | Xi| 0.01 | | | |Tab Rod |Tab Rod | | | | ........................................................................... | 120 | 49 | 0.278 | 0.34 | | | | ........................................................................... | 110 | 43 | 0.285 | 0.34 | | | | ........................................................................... | 100 | 38 | 0.293 | 0.34 | | | | ........................................................................... | 90 | 32 | 0.300 | 0.34 | | | | ........................................................................... | 80 | 27 | 0.308 | 0.34 | | | | ........................................................................... | 70 | 21 | 0.315 | 0.34 | | | | ........................................................................... | 60 | 16 | 0.322 | 0.34 | | | | ........................................................................... | 50 | 10 | 0.330 | 0.34 | | | |
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~......................................................................... | Elevator Tab "Xi" Dimension Before Flight Test (if an | | alternative rigging fixture tool, F80248.8 or TE27T-31001-( ), is used | | Table 504 for 737-300 | ...........................................................................
 |   |  |  |  |Initial Tab |
 |  AIRPLANE  |  NOMINAL TAB  | SPACER  |  INCREMENTAL  |Xi Dimension|
| TEMPERATURE |  "a" DIMENSION  |THICKNESS|  TAB POSITION  |  Before  |
 |  |  BEFORE  |  |  DUE TO  |Flight Test |
 |  |  FLIGHT TEST  |  |  SKI JUMP  | Xi = a +  |
 |  |  |  |  (OPTIONAL)  |  t + SJ |

 ........................................................................... | °F | °C |Aluminum|Titanium| "t" | "SJ" | Xi| 0.01 | | | |Tab Rod |Tab Rod | | | | ........................................................................... | 40 | 4 | 0.337 | 0.34 | | | | ........................................................................... | 30 | -1 | 0.345 | 0.34 | | | | ........................................................................... | 20 | -7 | 0.352 | 0.34 | | | | ........................................................................... | 10 | -12 | 0.359 | 0.34 | | | | ........................................................................... | 0 | -18 | 0.366 | 0.34 | | | | ........................................................................... | -10 | -23 | 0.373 | 0.34 | | | | ........................................................................... | -20 | -29 | 0.381 | 0.34 | | | | ........................................................................... | -30 | -34 | 0.388 | 0.34 | | | | ........................................................................... | -40 | -40 | 0.395 | 0.34 | | | | ........................................................................... | -50 | -46 | 0.402 | 0.34 | | | | ........................................................................... | -60 | -51 | 0.410 | 0.34 | | | | 2......…......…........…........….........…..................…............1
　
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