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时间:2011-04-10 09:58来源:蓝天飞行翻译 作者:航空
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 (11)
 Do an operational test of the inboard elevator PCP (Ref paragraph 5).


 TASK 27-31-07-832-035
 4. Inboard Elevator Power Control Package Adjustment (Fig. 203)
_________________________________________________
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RIG PIN INSTALLED)
Outboard Elevator Neutral Figure 203 (Sheet 1)
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1.78 INCHES MAX
1. BOLT
1.22 INCHES MAX
2. WASHER 
6. CHECKNUT  3. NUT 
9. INPUT 
CONTROL  7. SLEEVE  4. WASHER 
ROD 
8. CHECKNUT  5. NUT 

SEE  C 
BALLSCREW 
STOP 

"B" 
SEE  B  DIMENSION 
INPUT  BALLNUT 
CONTROL  STOP 
ROD 
VALVE 
LEVER 
FUSELAGE 
CONTOUR 

INDEX 
TAB 
INBOARD 
ELEVATOR 
INBOARD 
ELEVATOR 
POWER CONTROL  OUTBOARD 
PACKAGE  ELEVATOR  C 
Inboard Elevator Neutral 
Figure 203 (Sheet 2) 

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 A. Parts ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 203 | 1 | Bolt Assembly | 27-31-55 | 01 | 10 | | | 2 | Washer | | | 15 | | | 3 | Nut | | | 20 | | | 4 | Washer | | | 25 | | | 5 | Nut | | | 30 | | | | | | | | 2......…........…...................................…...........….....…........1
 B. References
 (1)  
AMM 06-09-06/201, Stabilizer and Elevator Access Doors and Panels

 (2)  
AMM 24-22-00/201, Manual Control

 (3)  
AMM 27-31-08/201, Outboard Elevator Power Control Package

 (4)  
AMM 27-41-00/201, Horizontal Stabilizer Trim Control System

 (5)  
AMM 29-11-00/201, Main Hydraulic Supply System

 C.
Access

 (1)  
Location Zone
 335 Elevator Inboard, LH
 345 Elevator Inboard, RH


 (2)  
Access Panel 334HBL Inboard Elevator Actuator Access Panel 344HBR Inboard Elevator Actuator Access Panel

 D.
Prepare for Adjustment

 (1)
Do this task: "Supply Electrical Power" (AMM 24-22-00/201).

 S 862-103

 (2)  
Pressurize the hydraulic systems No. 1 and 2 (Left Elevator), or 3 and 4 (Right Elevator)(AMM 29-11-00/201).


 S 862-119
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 S 862-139
 (3)  
Pressurize No. 1 and 2 auxiliary pitot systems to 4.7 PSIG max (AMM 34-11-00/201).


 
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