737 AMM 飞机维护手册 SERVICING(41)

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E.  Cycle cable through full travel a minimum of 6 times. The force required to push cable should be less than 18.0 pounds at the fully extended position. Force required to extend the cable should be less than 15.0 pounds at fully compressed position. If force is excessive, remove flexible cable and completely lubricate cable (Ref par. 1).
F.  Wipe off excess grease on upper end. Leave a generous grease coating on all components within boot.
G.  Reposition and reclamp protective boot on lower end. Install lower rod end bolt.
H.  Adjust and test cable (Ref 27-62-51 A/T).
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 12-22-81 Page 203 

AFT AIRSTAIR HYDRAULIC DAMPER -SERVICING
EFFECTIVITY
Airplanes with Aft Airstairs
1.  Equipment and Material
A.  Hydraulic Fluid -MIL-H-5606
2.  Refill Damper
A.  Remove damper from airstair (Ref. 52-14-111).
B.  Mount damper so that piston stem is pointed up.
C.  Remove lockwiring and plug from end of piston stem and attach MIL-H-5606 fluid source.
D.  Bleed air from cart line before filling by leaving fitting B-nut loose and applying low pressure.
E.  When fluid runs clear, tighten B-nut.
F.  Apply sufficient pressure, not to exceed 100 psi, to extend piston rod.
G.  When piston rod stops, depressurize and remove line.
H.  Insert a rod into fill port and depress plunger.
I.  Release plunger when rod retracts to approximately the center of the alodine band. If air bubbles are observed when plunger is depressed, repeat filling procedure.
J.  Insert plug in piston stem and lockwire.
K.  Install damper in airstair (Ref. 52-14-111).
5C6
Jan 20/83 12-23-31 Page 201
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525  Air Conditioning Ram Air Inlet Modulation Shaft Assembly Lubrication 
May 01/76  Figure 201  12-23-41 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

G42309 K14218
501  Torque Shaft Universal Joint Lubrication 
May 01/01  Figure 201  12-23-61 
Page 201 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

500  Cabin Pressurization Outflow Valve Lubrication 
May 01/99  Figure 201 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  12-23-71 Page 201/202 

AFT ENTRY DOOR LUBRICATION
1. General
A. This procedure provides instructions for lubricating the aft entry door.
2. Equipment and Materials
A. Lubrication Set -Entry, Cargo, Service, and Galley Door Camshaft Bearings -F72942-1
NOTE: Lubrication set may be used to reach lubrication fittings where access is difficult.
B. Flush gun (grease gun)
C. Oil squirt can
D. Grease -BMS 3-33, preferred (Ref. 20-30-21)
E. Grease -MIL-G-23827, alternate (Ref. 20-30-21)
F. Oil -MIL-L-7870 (Ref. 20-30-21)
3. Service Aft Entry Door
A. Remove aft entry door lining and gate lining (Ref. 52-13-21/401).
B. Remove handle lining retainer and handle mechanism cover plate.
C. Lubricate aft entry door as shown (Fig. 201).
D. Install handle mechanism cover plate and handle lining retainer.
E. Install aft entry door lining and gate lining (Ref. 52-13-21/401).
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 12-25-11 Page 201 

Aft Entry Door Lubrication  580 
12-25-11  Figure 201 (Sheet 1)  Jun 20/89 
Page 202 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 
　
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