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时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
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 Bonding Connections
 Figure 403/TASK 55-31-11-991-002
 1EFF :  ALL  1  55-31-11 Page 408 
1  1  Feb 01/98
 1  1
 1CES  1

 

 (a) Remove the nuts (43), the washers (42) and the upper parts of the clamp blocks (41).
R  (b) Put the CONTAINER 3 L(3/4 USGAL) in position to collect the unwanted fluid.
 (c)
 Disconnect and remove the hydraulic pipes (44) and (45).

 (d)
 Disconnect the flexible hoses (35), (36), (37) and (38).

 (e)
 Put blanking plugs on the disconnected line ends.

 (f)
 Remove the unwanted hydraulic fluid (Ref. TASK 51-78-00-615-002).


 (8)
 Remove the transverse load forks.
 (Ref. Fig. 405/TASK 55-31-11-991-006)


 (a)
 Identify the position of the transverse load forks (54) for installation.

 (b)
 Remove and discard the cotter pins (59) and (72).

 (c)
 Remove the nuts (62), the washers (63), the bolts (60) and the bushes (57), (58) and (65).

 (d)
 Remove the transverse load forks (54).

 

 (9)
 Remove the pushrod.
 (Ref. Fig. 401/TASK 55-31-11-991-005)


 (a)
 Remove and discard the cotter pins (85).

 (b)
 Remove the nuts (84) and (87), the washers (83) and (86) and the bolts (82).

 (c)
 Remove the pushrod (81).

 

 


 Hydraulic Connections Figure 404/TASK 55-31-11-991-003
 1EFF : 1 1R 1CES  ALL  1 11 1 55-31-11 Page 410 Feb 01/99

 

 INTENTIONALLY BLANK


R 1 1


55-31-11Page 411
1 1 Feb 01/99 1 1 1CES 1


R  Transverse Load Forks and Tapered Attach Bolts Figure 405/TASK 55-31-11-991-006- 12 (SHEET 1)
 1EFF : 1 1 1CES  ALL  1 111 55-31-11 Page 412 May 01/04

 

R  Transverse Load Forks and Tapered Attach Bolts Figure 405/TASK 55-31-11-991-006- 22 (SHEET 2)
 1EFF : 1 1 1CES  ALL  1 111 55-31-11 Page 413 May 01/04

 

 (10) Remove the attach bolts.
 (Ref. Fig. 405/TASK 55-31-11-991-006)

 (a)
 Operate the crane and slowly tighten the sling cables. Adjust the turnbuckles as necessary to get an equal tension.

 (b)
 Increase the cable tension to release the load from the bolts (53).


 NOTE : You must only remove one attach bolt at a time.
____
 (c)
 Use the TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454 (SL90-314-5625) and remove the tab washers (50) from the slotted nuts (51).

 (d)
 Use the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-322-5625) and remove the slotted nuts (51) and the washers (66).


 NOTE : Identify each bolt (53) and split sleeve (52) to make sure
____ you install them together in the same position.
R (e) Remove the bolts (53) with an EXTRACTOR - BOLTS, VERTICAL R STABILIZER.
 (f)
 Remove the split sleeves (52).

 (g)
 Install a CENTERING BOLTS - VERT. STABILIZER (98D55307503001).

 (h)
 When all attach bolts (53) and split sleeves (52) are removed, remove the centering bolts.


 (11)
 Remove the vertical stabilizer from the aircraft and lower it on a support.

 (12)
 When the vertical stabilizer is attached to the support remove the sling.

 

 TASK 55-31-11-400-001


 Installation of the Vertical Stabilizer
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS
_______
 ONLY WITH A GOOD SUPPLY OF AIR.
 OBEY THE MANUFACTURERS INSTRUCTIONS.
 PUT ON PROTECTIVE CLOTHING.
 DO NOT GET THEM IN YOUR MOUTH.
 DO NOT SMOKE.
 DO NOT BREATHE THE GAS.
 THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
 GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.

 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific crane 800 kg (1763.6976 lb) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 No specific Torque Wrench : range 1.00 to 10.00 m.daN
 
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