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时间:2011-10-30 09:55来源:蓝天飞行翻译 作者:航空
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CONTROL ROD INTERLOCK
FOR THE DOOR ACTUATOR
ACTUATOR
CRANK TOUCHES THE RETURN STOP
SEQUENCING OUTPUT CRANK CONTROL ROD
C
SEQUENCING SEQUENCING CONTROL ROD CRANK
SEE E SEQUENCING CRANK CAM
SAFETY VALVE LATCHED
D
LATCH DOOR OFF
ACTUATOR
ON
0.13-0.15 INCH
(3.30-3.81 mm)
CLEARANCE
LOCK RELEASE
DOOR LOCKED CONTROL ROD
SWITCH FOR THE DOOR
ACTUATOR UNLOCKADJUSTING CRANKSCREW ACTUATOR
SAFETY VALVE LATCHED
RIGGING MARK E
C-C
Nose Landing Gear Door Actuator Lock Release Mechanism Adjustment Figure 502 (Sheet 2)


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MAINTENANCE MANUAL

RIGHT MAIN LANDING 
GEAR DOOR 
SEE  A  MAIN WHEEL WELL 
ELECTRICAL SERVICE 
PANEL, P72 
SEE  C 
LEFT MAIN LANDING 
GEAR DOOR 
FWD  SEE  B 

NOSE LANDING GEAR 
LEFT EQUIPMENT 
PANEL, P63  NOSE LANDING GEAR 
DOOR UNSAFE LIGHT 
FWD 
NOSE LANDING GEAR 
DOOR CLOSED SWITCH 
SEE  D 
VIEW OF FORWARD WALL OF NOSE 
WHEEL WELL 
LEFT (RIGHT) 
MAIN LANDING  A 
GEAR DOOR  LANDING GEAR DOOR 
UNSAFE LIGHT  GROUND CONTROL 
ACCESS DOOR, 198PR 

LEFT (RIGHT) MAIN LANDING
FWD  GEAR DOOR MAIN WHEEL WELL ELECTRICAL
MAIN WHEEL WELL SERVICE PANEL, P72
B1
1 LEFT SIDE IS SHOWN,
C
RIGHT SIDE IS OPPOSITE
Door Ground Control Switches Figure 503 (Sheet 1)


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MAINTENANCE MANUAL


SWITCH PLUNGER EXTENDED
(DOOR OPEN)
A-A

Door Ground Control Switches
Figure 503 (Sheet 2)

 

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MAINTENANCE MANUAL

MAIN WHEEL WELL OUTBOARD WALL
SEE E
LEFT OR RIGHT MAIN LANDING GEAR DOOR CLOSED SWITCH, S10371 OR S10370
SEE F
LEFT MAIN WHEEL WELL OUTBOARD WALL (RIGHT SIMILAR)
EB
MAIN LANDING GEAR DOOR CLOSED SWITCHES, S10370,S10371
NUT (2 LOCATIONS)
B
1.37 INCH  1 
MAIN GEAR  MAIN GEAR 
DOOR CLOSED  SWITCH  DOOR CLOSED 
SENSOR (REF)  SENSOR (REF)  MAIN LANDING 
GEAR DOOR 

LEFT OR RIGHT MAIN GEAR DOOR CLOSED
(REF) SWITCH, S10371 OR S10370
F B-B
1 SWITCH PLUNGER EXTENDED (DOOR OPEN)
Door Ground Control Switches Figure 503 (Sheet 3)


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 TASK 32-35-00-705-225
 3.  Operational Test - Inflight Alternate Extension_______________________________________________
 A. General
 NOTE: It is not recommended that you do this test on a revenue flight.
____
 (1)  
This test is an inflight alternative to the operational test that is done on the ground or the system test that requires lifting the airplane on jacks.

 B.
References

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

 (2)  
AMM 29-11-00/201, Main (Left, Right, and Center) Hydraulic System

 C.
Access

 (1)  
Location Zones
 211 Control Cabin (Left)
 212 Control Cabin (Right)


 D.
Prepare for the Inflight Test of Alternate Extension System


 S 865-200
 (1)  
Make sure these circuit breakers on the main power distribution panel, P6, are closed:

 (a)  
6F5, LANDING GEAR ALTN EXT CONT

 (b)  
6F6, LANDING GEAR ALTN EXT MOTOR


SEE A
FWD ALTERNATE UPLOCK RELEASE ACTUATOR
NOSE WHEEL WELL (AFT WALL) A
Nose Landing Gear Alternate Uplock Release Actuator Figure 504


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MAINTENANCE MANUAL

NOSE LANDING GEAR SHOCK STRUT (REF)
SEE A
SYSTEM 2 SENSOR S10068
SYSTEM 1 FWD
SENSOR S10067
A
MAIN LANDING GEAR SHOCK STRUT (REF)
MAIN LANDING SYSTEM 1 SENSORGEAR TRUCK S10062 LHTILT SENSORS
S10060 RH SEE B
SYSTEM 2 SENSOR S10064 LH S10059 RH
 
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