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时间:2011-03-30 10:22来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

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Pacific B-82

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Pennwalt (Delchem) 2271R

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Tee Formula No. 1

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Tee 86-2

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Turco Jet Clean C

(15)
Turco Jet Clean E


G.  Corrosion inhibiting compound - BMS 3-23 (Ref 20-30-21)
H.  Grease proof paper (Ref 20-30-51)
I.  Laminated waterproof paper (Ref 20-30-51)
J.  Masking tape (Ref 20-30-51)
K.  pH testing paper with readings in 0.5 units of pH change: 5 to 10, 6.5 to 10, 6.0 to 8.0 or 8.0 to
9.5 pH range - commercially available
L.  Polyethylene sheet (Ref 20-30-51)
M.  Wipers (Ref 20-30-51)
501 
Jun 20/85  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  25-52-0 Page 701 


3.  Prepare to Clean
A.  Remove electrical power (Ref 24-22-0, MP).
B.  Statically ground airplane (Ref 20-40-11).
C.  Remove insulation blankets and components (power drive units, actuators, exposed electronic equipment, etc.) which may be damaged by cleaner or water.
CAUTION:  FABRIC, MECHANICAL AND ELECTRICAL/ELECTRONIC COMPONENTS MUST BE REMOVED TO PRECLUDE DAMAGE.
D.  Mask all areas not to be cleaned, including all lubricated or waxed surfaces and any cargo door latch mechanisms and fittings. Use polyethylene sheet, greaseproof paper or laminated waterproof paper as appropriate. Secure with masking tape as required.
CAUTION:  CONCENTRATED CLEANERS MAY CAUSE PAINT TO DETERIORATE OR MAY CAUSE CORROSION OF METAL SURFACES IF ENTRAPPED. MANUFACTURER'S RECOMMENDED DILUTIONS MUST BE-USED TO PRECLUDE DAMAGE.
4.  Clean Cargo Compartment
A.  Vacuum bilge area to remove loose surface soil.
B.  Pressure spray Alkaline Solvent Emulsion cleaner using airless pump with spray valve and non-atomizing nozzle.
WARNING:  CLEANERS CONTAIN TOXIC INGREDIENTS. WEAR PROTECTIVE GLOVES WHEN USING THEM, AND AVOID CONTACT WITH SKIN OR EYES. PROVIDE ADEQUATE VENTILATION OR USE RESPIRATOR MASKS. CONSULT INDUSTRIAL HYGIENE, FIRE, AND/OR SAFETY ORGANIZATIONS CONCERNING FACILITIES, EQUIPMENT, VENTILATION, AND OTHER REQUIREMENTS FOR SAFE CLEANING OPERATIONS.
CAUTION:  CLEANERS OTHER THAN THOSE SPECIFIED MAY DAMAGE SURFACES BEYOND REPAIR.
C.  Allow cleaner to soak for 5 minutes.
NOTE: Do not allow cleaner to dry on surface.
D.  Pick up loosened soil and cleaner with vacuum cleaner.
E.  Repeat spraying and vacuum pickup until all dirt, sludge and grease is removed.
F.  Using pressure spray, thoroughly rinse area with clean water.
G.  Remove rinse water with vacuum.
H.  Check pH of rinse effluent seeping from trapped areas.
(1)  
Daub pH paper around crevices and other entrapment areas.

(2)  
Check that pH of effluent from these areas does not exceed 1 pH unit of the incoming rinse water.

(3)  
If pH exceeds 1 pH unit of incoming rinse water, repeat steps F. and G. until pH is within 1 unit of incoming rise water.


I.  Wipe area dry.
J.  Apply corrosion inhibiting compound on cleaned area (Ref 51-21-91, CP).
501 
25-52-0  Page 702  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Jun 20/85 


5. Restore Airplane to Normal
A. Remove any masks previously installed.
B. Install any equipment previously removed.
C. Restore electrical power, if required (Ref 24-22-0, MP).
D. Disconnect static ground if no longer required (Ref 20-40-11).
501 
Jun 20/85  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  25-52-0 Page 703 


CARGO COMPARTMENT DECK PANELS - REMOVAL/INSTALLATION
1. Equipment and Materials
A.  Tape - Permacel P212HD (preferred), Permacel P621 (optional), Permacel P34 (optional), 3M 367-FR (preferred), 0.50, 0.75, 2, and 3 inches wide (Ref 20-30-51)
B.  Sealant: BMS 5-12, Class B; BMS 5-16; BMS 5-19, Class A or Class B; or BMS 5-37, Class B
2.  Remove Typical Cargo Compartment Deck Panel (Fig. 401).
NOTE:  Screws should be identified when being removed so each can be reinstalled in the place from which it was taken.
A.  Remove splice plate or splice plates as needed.
(1)  
Remove screws from splice plate.

(2)  
Lift splice plate from place.


B.  Remove outboard cap strip or cap strips as needed. 
(1)  
Remove all screws from cap strip. 

(2)  
 
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