S 024-008
(1)
Remove the actuator (Fig. 401):
(a)
Remove the nut (9), the washers (7 and 8) and the lockbolt (6).
(b)
Remove the bracket (32) from the boss.
NOTE: Leave the lines in the bracket (32).
____
(c) Remove the nut (5), washer (10), washer (4), and washer (3) (View B).
NOTE: You can use the wrench with a crow-foot adapter
____ to remove the nut (5).
(d) Remove the actuator (2) rod end from the shock strut boss.
NOTE: Use the thread protector on the boss when you remove the
____
rod end.
(e)
Remove the washer (1) from the boss.
(f)
Remove the head end bolt (11) from the actuator.
(g)
Use the sling and the hoist to remove the actuator from the airplane.
(h)
If it is necessary to use the hydraulic fittings on the new actuator, remove the adapters (23, 27 and 28) from the actuator.
(i)
Install plugs on the ports or install caps on the hydraulic fittings.
TASK 32-33-01-404-009
3. Body Landing Gear Actuator Installation
_______________________________________
A. Special Tools and Equipment
(1)
20HME65B00163-1 - Sling Assembly, Body Gear Retract Actuator
(2)
ST2580-245 - Crowfoot Torque Wrench Adapter, 3.0 inches across flats
(3)
4PRE65B00163-1 - Thread Protector, Body Gear Shock Strut Boss
B.
Standard Tools and Equipment
(1)
Portable Hoist, 200-pound capacity
C.
Consumable Materials
(1)
D00633 Grease - BMS 3-33 (preferred)
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SEE A ACTUATOR STRUCTURE SUPPORT
SEE C
HYDRAULIC HOSES
2. RETRACT ACTUATOR
PORTABLE
COMMERCIAL RETRACT
HOIST ACTUATOR
SLING
A SEE B
SHOCK
STRUT
A
A
Body Landing Gear Actuator Installation
Figure 401 (Sheet 1)
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APPLY A LAYER OF THE CORROSION PREVENTIVE
BEARING
COMPOUND TO THE BEARING OUTER CYLINDER BORE AND THE JOURNAL OF THE SHOCK STRUT
BOSS INSERT
5.
NUT
6.
LOCKBOLT
3. TANG WASHER
WASHER
FILL WITH CORROSION 1
PREVENTIVE COMPOUND
10.
STEEL WASHER
4. NYLON WASHER
LOWER ROD END
OVERHANG OF BEARING OVER
A-A BOSS
SHOCK STRUT
1.
CRES WASHER
2.
ACTUATOR
1
(ROD END)
3.
TANG WASHER
4.
NYLON WASHER
6. LOCKBOLT
BOSS
5. NUT
7. WASHER 32.
BRACKET10.
STEEL WASHER NUT
9. NUT
WASHER
WASHER
8. WASHER
SLEEVE
BODY LANDING GEAR ACTUATOR
BOLT
ROD END BOLT INSTALLATION
PUT THE BEVEL IN THE 1
DIRECTION OF THE ROD END. B
Body Landing Gear Actuator Installation
Figure 401 (Sheet 2)
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SUPPORT STRUCTURE 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 4(123)
