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时间:2011-11-01 11:19来源:蓝天飞行翻译 作者:航空
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Volume 2-757

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

(13)Do
not apply corrosion inhibiting compounds on insulation blankets. The
compounds reduce the water-repellent quality of the blankets.


E.
Frequency of Application

 

(1)Periodic inspection is required in areas identified as susceptible to
corrosion and should be consistent to the schedules specified in the
Maintenance Planning Document. Operators must be aware of reported prob-lems and areas of occurrences.

(2)Periodic application of BMS 3-23 compound is necessary in areas identi-fied and should be consistent to the schedule specified in the Mainte-nance Planning Document.

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

NOTE: LOCATIONS OF GALLEYS AND LAVATORIESDEPENDENT
ON OPERATOR'SCONFIGURATION
Galley and Lavatory Areas
Figure 1

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

AREA  PROBLEM  INDEX PREVENTION VOLUME 2  TERMINATING ACTION (IF ANY) 
Nacelle Struts  Corrosion of skin panels  54-50-01  SB 54-0022 
Corrosion of strut to wing fitting lug  54-50-01  PRR 54530-78 
SPECIFIC CORROSION PROBLEMS -NACELLES/PYLONS Figure 1 

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

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CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

AREA  PROBLEM  INDEX PREVENTION VOLUME 2  TERMINATING ACTION (IF ANY) 
Nacelle Struts  Corrosion of skin panels  54-50-01  SB 54-0022 
Corrosion of strut to wing fitting lug  54-50-01  PRR 54530-78 
SPECIFIC CORROSION PROBLEMS -NACELLES/PYLONS Figure 1 

Volume 2-757

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Page 1 OCT 01/00
CORROSION PREVENTION MANUAL
FUSELAGE -SECTION 46

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CORROSION PREVENTIONMANUAL
NACELLES/PYLONS

1. General

A. Corrosion can occur on the nacelle strut skins along the lower edge of the
skin panels under the fiberglass heat shield and in the lug holding the
strut to wing fitting bushing.
 
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