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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