(3)
AMM 32-00-20/201, Landing Gear Downlocks
(4)
AMM 32-09-02/201, Prepare the Safety-Sensitive Systems for Air Mode Simulation
B.
Equipment
(1)
Pin Insertion/Extraction Tool
Part on Crimp Tool Kit - DMC 567
Daniels Manufacturing Corp.
526 Thorpe Road
Orlando, Forida 32824
C.
Access
(1)
Location Zones
731 Main Landing Gear, LH
741 Main Landing Gear, RH
D.
Prepare for Removal
S 494-002
(1) Make sure the downlocks for the nose and main landing gear are installed (AMM 32-00-20/201).
S 864-029
WARNING: MAKE SURE YOU DO THE STEPS TO PREPARE THE SYSTEMS FOR AIR MODE
_______ CORRECTLY. IF YOU DO NOT FOLLOW THESE INSTRUCTIONS, INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(2)
Do the task to prepare the safety-sensitive systems for air mode simulation (AMM 32-09-02/201).
S 864-003
(3)
Remove the pressure from the left hydraulic system and the hydraulic reservoir (AMM 29-11-00/201).
32-32-15
ALL ú ú 01 Page 401 ú Sep 28/00
A
757
MAINTENANCE MANUAL
SHOCK DRAG STRUT STRUT TRUCK POSITIONER ACTUATOR
SEE A
B A
B 2. WASHER 3. TRUCK POSITIONER
A (2 LOCATIONS) ACTUATOR
4. ANTIROTATION
BOLT
FWD TRUCK 1. PIN 1
BEAM 5. COLLAR
6.
WASHER
7.
NUT
9. WASHER (2 LOCATIONS)
3. TRUCK POSITIONER
TRUCKACTUATOR BEAM
8. PIN 2 10. ANTIROTATION
BOLT A-A
11.
COLLAR
12.
WASHER
13.
NUT
SHOCK 1 INSTALL THE PIN HEAD OUTBOARD STRUT FOR THE LEFT MAIN LANDING GEAR AND INBOARD FOR THE RIGHT LANDING GEAR
B-B
2 INSTALL THE PIN HEAD INBOARD
Main Landing Gear Truck Positioner Actuator Installation
Figure 401 (Sheet 1)
32-32-15
ALL ú ú 02 Page 402 ú Dec 20/92
B15895
A
757 MAINTENANCE MANUAL
CLAMP 1.10
INCH
INSTALLATION 0.90
BLEED PLUG
FWD ACTUATOR TRUCK POSITIONER
LEFT GEAR OUTBOARD SHOWN (RIGHT GEAR INBOARD QUIVALENT)
A
0.90 1.10 INCH CLAMP INSTALLATION
BLEED PLUG TRUCK POSITIONER ACTUATOR
FWD
LEFT GEAR INBOARD SHOWN
(RIGHT GEAR OUTBOARD EQUIVALENT)
A
Main Landing Gear Truck Positioner Actuator Installation
Figure 401 (Sheet 2)
B15905
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH CLAMPS INSTALLED ú
32-32-15
ON HYDRAULIC LINES ú ú 02 Page 403 ú Mar 20/97
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757 MAINTENANCE MANUAL
S 864-028
(4)
Remove electrical power (AMM 24-22-00/201).
E.
Procedure to Remove the Main Landing Gear Truck Positioner Actuator
S 034-024
(1)
POSITIONER ACTUATOR WITH CLAMP; remove the clamp that holds the hydraulic lines from the positioner actuator.
S 034-004
(2)
Disconnect the hydraulic lines from the actuator. Install plugs in the lines and fittings.
S 014-030
(3)
Do these steps to permit removal of the pin from the rod end of the actuator (Fig. 402):
(a)
Remove the bolts which hold the cover to the J-1 junction box
NOTE: The junction box is on the aft end of the truck beam of
____
the main gear.
(b)
Put a tag with the color code and the pin locations on the sensor wires
(c)
Use a pin extraction tool, to remove the sensor wire from the terminal block in the junction box
(d)
Put a line on the sensor wires to make the installation easier
(e)
Disconnect the conduit coupling nut from the junction box
(f)
Remove or loosen the clamp that attaches the conduit to the truck beam
(g)
Move the conduit to permit removal of the pin.
S 034-005
(4) Remove pin (1) to disconnect the rod end of the actuator from the truck beam (View A-A).
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本文链接地址：757 AMM 飞机维护手册 起落架 CHAPTER 32 - LANDING GEAR 2(59)
