FAA Advisory Circular 43.13-1B

Acceptable Methods, Techniques, and Practices

Aircraft Inspection and Repair

AC 43.13-1B | 6. Corrosion, Inspection, and Protection | 4. Corrosion Preventative Maintenance | 6-51. Guidelines: Aircraft Operating Over Salt Water

Previous
Next
9/8/98
SECTION 4. CORROSION PREVENTIVE MAINTENANCE AC 43.13-1B
6-50. GUIDELINES: ALL AIRCRAFT.
Corrosion prevention depends on a compre­
hensive prevention and control plan, imple­
mented from the start of operation of an air­
craft, which includes:
a. Adequately-trained personnel in
(1) recognition of corrosion-inducing
conditions;
(2) corrosion identification techniques;
i. Replacing deteriorated or damaged
gaskets and sealants (using non-corrosive type
sealants) to avoid water intrusion and entrap­
ment that leads to corrosion.
j. Minimizing the exposure of aircraft to
adverse environments by keeping the aircraft
in a hangar.
k. Periodic and frequent inspection of
areas where there are foamed plastics or other
absorbent material.
(3) corrosion detection, cleaning, and
treating; and
(4) lubrication and preservation of air­
craft structure and components.
b. Inspection for corrosion on a sched­
uled basis.
c. Thorough cleaning, inspection, lubri­
cation, and preservation at prescribed intervals.
d. Prompt corrosion treatment after de­
tection.
e. Accurate record-keeping and report­
ing of material or design deficiencies to the
manufacturer and the Federal Aviation Ad­
ministration (FAA).
f. Use of appropriate materials, equip­
ment, and technical publications.
g. Maintenance of the basic finish sys­
tems.
h. Keeping drain holes and passages
open and functional. Sealants, leveling com­
pounds, miscellaneous debris, or corrosion in­
hibitors should not block drain paths.
l. Daily draining of fuel cavities to re­
move accumulated water and other foreign
matter.
m. Daily wipe-down of exposed critical
surfaces of hydraulic cylinders.
6-51. GUIDELINES: AIRCRAFT OP-
ERATING OVER SALT WATER. In addi­
tion to the inspection and treatment prescribed
above, the following treatment shall be ap­
plied:
a. Remove all traces of salt water and salt
water residue by thoroughly washing the air­
craft with fresh water.
(1) After drying, coat the propeller,
hubs, blades and other unpainted or unpro­
tected parts of the engine and its installation
parts by spraying or rubbing lightly with corro­
sion preventive compound, Specification
MIL-C-16173, Grade 4.
(2) Apply this mixture on parts that
move or require some lubrication and on all
fittings subject to corrosion such as landing
gear retracting plungers, control surface
hinges, control cables, exposed rivets and
bolts, and other similar parts not protected by
Par 6-50
Page 6-13
Public domain content provided by US Federal Aviation Administration. Navigation features courtesy of Land Sea Sky Space LLC