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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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high temperatures can cause deterioration of the compounds. Corrosion
inhibiting compounds can cause damage to the sealant.

Volume 2-757

57-20-01

Page 1
OCT 01/00

CORROSION PREVENTION MANUAL
OUTER WING

(5)Corrosion  inhibiting compounds can be used on fiberglass fairings and
ducts if the temperature of the duct is not hotter than 220°F.

(6)
Corrosion inhibiting compounds can be used on fuel vapor barriers.


F.
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 to areas identi-fied and should be consistent to the schedule specified in the Mainte-nance Planning Document.


G.  
Improved Corrosion Protection

 

(1)On airplane line number 135 and on, PRR 53685 replaced the original
primer and Corogard corrosion protection on upper inspar skin surfaces
by BMS 10-79, type 3 primer and BMS 10-100 (Aeroflex G12E25) coating.
Some operators have specified Crown Metro 10-P1-3 aluminized primer
applied over BMS 10-79, type 3 primer instead of the Corogard or BMS
10-100 finish. The BMS 10-79 primer and BMS 10-100 enamel can be applied
on earlier airplanes with SL 20-6 and 51-7.

Volume 2-757

57-20-01

Page 2
OCT 01/00

CORROSION PREVENTION MANUAL
OUTER WING

OUTER WING
TOP VIEW
(LEFT SIDE SHOWN, RIGHT SIDE SIMILAR)

Outer Wing Figure 1 (Sheet 1)
Volume 2-757

57-20-02
Page 1 OCT 01/00
CORROSION PREVENTION MANUAL
TRAILING EDGE FLAPS

WING FRONT SPAR WING REAR SPAR
DETAIL I DETAIL II

APPLY BMS 3-23, TYPE 2 CORROSION INHIBITING COMPOUNDTO SEAMS OF ALL STRUCTURAL PARTS
APPLY BMS 3-23, TYPE 2 CORROSIONINHIBITING COMPOUNDTO ALL STRUCTURAL SURFACES
Outer Wing
Figure 1 (Sheet 2)

Volume 2-757

57-20-02
Page 2 OCT 01/00
CORROSION PREVENTIONMANUAL
TRAILING EDGE FLAPS

DETAIL III
DETAIL IV
Outer Wing
Figure 1 (Sheet 3)

Volume 2-757

57-20-02
Page 3 OCT 01/00
CORROSION PREVENTION MANUAL
TRAILING EDGE FLAPS

MLG TRUNNION SUPPORT STRUCTURE
DETAIL V

APPLYBMS3-23 LIBERALLYTOPERMITPENETRATION BETWEENFITTING ANDREARSPAR. PAYPARTICULAR ATTENTIONTO FASTENERS
ANDFAYINGSURFACES
APPLYBMS 3-23 TO ALL SURFACESINCLUDING CONNECTION
POINTS
Outer Wing
Figure 1 (Sheet 4)

Volume 2-757

57-20-02
Page 4 OCT 01/00
CORROSION PREVENTION MANUAL
TRAILING EDGE AND TRAILING EDGE DEVICES
 
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