Form No. ASI/MD-79
Revision 3 – July 2020
Page 3 of 4
NO.
DESCRIPTION
MECH. ENG.
15 Place inner wheel half on a clean bench.
16
Clean tire bead seat with a cloth impregnated with dry-cleaning solvent to
remove residual grease or wax.
CAUTION:
Oily solvent must not be used on tire bead seat because tire will not stick
properly on the wheel.
17 Apply appropriate mounting soap from tire manufacturer on tire bead seat.
Tubeless mounting soap in box or in spray (preferred) must be used.
18 Install only the correct “tubeless” tire on the inner wheel half.
19 Clean o-rings grooves with dry cloth and install small and large o-rings.
20 Place the separator disc
NOTE:
Only when required.
21
Place the outer wheel half with the valve positioned at the red balance dot
on the tire and align the bolt holes.
NOTE:
Assembly screw must be replaced at each tire change.
22
Put a drop of thread locker medium strength (Loctite 243 recommended) on
each end of assembly screw.
CAUTION:
Using a wrong thread locker or not from recommended type may cause loose of
screws or removal problem.
23
Install all screws to contact.
CAUTION:
Do not use impact or power wrenches.
24 Torque all screws to 12 N.m (105 in-lb).
25 Torque all screws a second time to 12 N.m (105 in-lb).
26
Inflate tire just enough to seat beads.
WARNING:
Place wheel in an inflation cage for initial inflation. do not inflate tire to full
operating pressure until wheel has been installed on aircraft. tire and / or wheel
failure may occur causing injury to personnel or damage to equipment if the tire
is inflated from any high-pressure source. tire and wheel assemblies must be
serviced with inflation equipment that has been specifically designed for this
operation.
27 Check bearing cups and cones
28 Pack bearing cones with clean bearing grease to specification MIL-G-
81322 and coat bearing cups with a light coat of grease.
29 Install outer bearing cone in wheel and install on aircraft helping disc to
take place in wheel slots.
30 Adjust bearings to aircraft manufacturer’s recommendations and safety.
31 Install o-ring on wheel cap and screw the cap.
32
Torque the cap to contact with hand force using BERINGER tool AV-PIL-
101.
CAUTION:
Excessive torque on the cap may cause problem to unscrew.
33
Install disc safety wire diameter 1.01 mm (0.040”) from stainless steel
grade 302 in wheel ring groove.
CAUTION:
Disc safety wire must be in place it prevents disc from sliding out the slots.
Содержание PILATUS PORTER PC6
Страница 2: ...MAINTENANCE PROGRAM PILATUS PC 6 DOCUMENT NUMBER SAP 27 REISSUE 2 REVISION 1 JULY 2020...
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Страница 100: ...Form ASI PC6 Engine Installation Reissued 2 Revision 1 Date July 2020 Page 10 of 26...
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Страница 128: ...Form ASI PC6 Engine Removal Reissued 2 Revision 1 Date July 2020 Page 12 of 25...
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Страница 131: ...Form ASI PC6 Engine Removal Reissued 2 Revision 1 Date July 2020 Page 15 of 25...
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Страница 136: ...Form ASI PC6 Engine Removal Reissued 2 Revision 1 Date July 2020 Page 20 of 25...
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