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时间:2011-03-21 08:27来源:蓝天飞行翻译 作者:admin
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 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING AND RUBBER GLOVES.
 (d)
 Apply the SPECIAL MATERIALS (Material No. 05-002) to the door sill attach screws (7).

 (e)
 Put the door sill (8) in position and install the screws (7).

 (f)
 Torque the screws to between 0.37 and 0.42 m.daN (32.74 and 37.16 lbf.in).

 (g)
 Apply the sealant. WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE

_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.

 (h)
 Apply the SEALANTS (Material No. 09-016) to the floor pan and the floor panel at the lavatory door opening.

 (i)
 Put the door assembly (4) in position and install the washers (6) and the screws (5).

 


 (7)
 Connect the toilet drain-line behind the lavatory (Ref. TASK 38-30-00-410-002).

 (8)
 Install the toilet assembly (Ref. TASK 38-31-41-400-001). Do not install the toilet shroud at this time.

 (9)
 Install the emergency oxygen container (Ref. TASK 35-21-41-400-001).


 (10) Install the forward attendant panel (Ref. TASK 23-73-12-400-007). **ON A/C 211-212,
 Subtask 25-41-41-420-059-E
 D. Installation of Lavatory A
 (1)
 Preparation for installation R (Ref. Fig. 407/TASK 25-41-41-991-020)

 (a) Apply COMMON GREASE (Material No. 04-001) to the bush (5) and the new packing (6) and put them in position.

 (2)
 Assemble the lavatory. R (Ref. Fig. 409/TASK 25-41-41-991-022)

 (a)
 Put the lavatory subassemblies (1) and (2) in the center of the aircraft aisle.

 (b)
 Put the subassemblies together and install the washers (3) and the screws (4).

 (c)
 Install the washers (5) and the screws (6).

 (d)
 Install the screw (7) and the cap (8).

 (e)
 Put the lavatory assembly in position on the floor pan (9).

 (f)
 Install the washers (11), the screws (10) and the screws (12).

 (g)
 Apply a bed of SEALANTS (Material No. 09-016) around the edges of the floor pan (9).

 

 (3)
 Install the lower attachments. R (Ref. Fig. 407/TASK 25-41-41-991-020)

 (a)
 Apply the COMMON GREASE (Material No. 04-001) to the bolts (1) and (7).

 (b)
 Put the lavatory assembly in position and install the bushes (3) and (2) and the bolts (1).

 

 


 WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE
_______ WORK AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE
_______ THIS/THESE MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES AND GOGGLES.
 (c)
 Apply the STORAGE PRESERVATION (Material No. 15-008) to the bolts (1).

 (d)
 Put the sealing angle (14) in position and install the washers

 (16) and the screws (15).

 (e)
 Apply a bed of SEALANTS (Material No. 09-016) around the edges of the sealing angle (14).

 (f)
 In the cockpit:

 -
put the plate (12) in position and install the screws (13),

 -
put the life vest container (11) in position and install the fasteners (10),


 -close the flap (9).

 (g)
 Get access to the lateral avionics compartment and:


 -apply the COMMON GREASE (Material No. 04-001) to the bolt (7)
 -install the washer (8) and the bolt (7).


 (4) Install the upper attachments.
 (a)
 Put the STEPLADDER 1.0 M (3.3 FT) in position.

 (b)
 Put the tie rods (19) in position and install the quick release pins (17)

 (c)
 If necessary adjust the tie rods:


 -remove and discard the lockwire.
 -loosen the locknuts (18)
 -adjust the tie rod (19) until you can install the quick release pins (17).
 -tighten the locknuts (18) and safety them with
 -Make sure that the rod end is in safety.
 -Safety the locknuts (18) with stainless steel lockwire MISCELLANEOUS (Material No. 19-010).
 
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