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时间:2011-03-25 17:50来源:蓝天飞行翻译 作者:admin
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 (j)
 TORQUE the nuts (40) to between 0.4 and 0.45 m.daN (35.39 and

 39.82 lbf.in) and safety with the new cotter pin (41).

 (k)
 Put the line support block assembly (35) in position on the flexible hoses (9) and (11). Loosely install with the bolts (36), the washers (34) and the nuts (33).

 (l)
 Make sure that dimension Y is 150 mm (5.91 in.).

 (m)
 TORQUE the nuts (33) to between 0.4 and 0.45 m.daN (35.39 and

 39.82 lbf.in).

 (n)
 Put the flexible hose (24) in position and connect the unions

 (23) and (71).

 (o)
 Put the flexible hose (25) in position and connect the unions

 (26) and (72).

 (p)
 TORQUE the unions (26), (72), (23) and (71) to between 2.4 and

 2.8 m.daN (17.69 and 20.64 lbf.ft).

 (q)
 Put the channels (38) in position on the flexible hoses (24) and (25). Install them with the bolts (37), the washers (39) and the nuts (40).

 (r)
 TORQUE the nuts (40) to between 0.4 and 0.45 m.daN (35.39 and

 39.82 lbf.in) and safety with the new cotter pin (41).

 (s)
 Put the line support block assembly (35) in position on the flexible hoses (24) and (25). Loosely install them with the bolts (36), the washers (34) and the nuts (33).

 (t)
 Make sure that the dimension Z is 280 mm (11.02 in.).

 (u)
 TORQUE the nuts (33) to between 0.4 and 0.45 m.daN (35.39 and

 39.82 lbf.in).

 (v)
 Put the flexible hoses (16) and (27) in position and connect the unions (15) and (28).

 (w)
 TORQUE the unions (15) and (28) to between 2.4 and 2.8 m.daN

 (17.69 and 20.64 lbf.ft).

 (x)
 If necessary, safety the unions (15) and (28) with MISCELLANEOUS (Material No. 19-010).


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 (y)
 Put the line support block assemblies (22) in position on the flexible hoses (16), (24), (25) and (27). Loosely install the bolts (17), the washers (18) and (21), and the nuts (20).

 (z)
 Make sure that the dimension X is between 90 and 95 mm (3.54 and


 3.74 in.). (Ref. Fig. 406A/TASK 32-11-12-991-010-A) (aa) Tighten the nuts (20) and safety with the new cotter pin (19). (ab) Put the flexible hoses (2) and (13) in position and connect the
 unions (1) and (14). (ac) TORQUE the unions (1) and (14) to between 2.4 and 2.8 m.daN
 (17.69 and 20.64 lbf.ft).
 (ad) If necessary, safety the unions (1) and (14) with MISCELLANEOUS (Material No. 19-010).
 (ae) Put the line support block assemblies (5) in position on the flexible hoses (2), (9), (11) and (13). Loosely install the bolts (3), the washers (4) and (6), and the nuts (7).
 (af) Make sure that the dimension X is between 90 and 95 mm (3.54 and
 3.74 in.).
 (ag) Tighten the nuts (7) and safety with the new cotter pin (8). **ON A/C 001-003, 051-052,
 Subtask 32-11-12-410-050
 C. Close Access WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
 -FLUSH IT AWAY WITH CLEAN WATER
 -GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT
_______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
 (1)
 Remove the blanking plugs from the disconnected line ends.

 (2)
 Connect the applicable hydraulic hoses at the MLG/wheel brake interface (Ref. TASK 32-42-27-400-001).


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 (3)
 Connect the hydraulic hoses (29), (30), (67) and (68) at the MLG/airframe interface (Ref. TASK 32-11-11-400-001).

 (4)
 Connect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-002).

 

R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 32-11-12-410-050-A
 C. Close Access WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
 -FLUSH IT AWAY WITH CLEAN WATER
 -GET MEDICAL AID. CAUTION : MAKE SURE THAT THE FLUID DOES NOT STAY ON THE AIRCRAFT
_______ STRUCTURE. IF THE FLUID GETS ON THE AIRCRAFT STRUCTURE, WASH IT OFF IMMEDIATELY WITH SOAP AND WATER.
 (1)
 Remove the blanking plugs from the disconnected line ends.

 (2)
 Connect the applicable hydraulic hoses at the MLG/wheel brake interface (Ref. TASK 32-42-27-400-001).

 (3)
 
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