CAUTION
Environmental regulations may require special equipment
and procedures be utilized when charging air conditioning
system.
CAUTION
Air conditioning system must be completely discharged
before checking oil level.
1. Compressor oil level should not be checked unless a freon leak has occurred which requires an
addition of freon (refer to Piper Service Manual, section Xlll).
1. Wings - for wrinkled skins, loose or missing rivets.
2. Fuel leaks around nacelle fuel tanks and fuel fittings throughout wings.
3. Wing spar webs, bulkheads, nacelle skins and attachments, firewall skin, and wing a
fuselage stringers for any signs of overstress or damage. 0 4. An alignment check to clarify any doubt
of damage.
1. Top and bottom fuselage skins for loose or missing rivets and wrinkled skins.
2. Empennage skins and attachments.
1. Refer to UACL Maintenance Manual.
1. Refer to UACL Maintenance Manual.
1. Check with the appropriate manufacturer for the necessary corrective action.
1. Consult P&W Agtoil #7 for frequency and instructions. Observe starter limitations.
Page 46
Interim Revision: October 26, 1994
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SERIAL NUMBER
REGISTRATION NUMBER
ENGINE SERIAL NO.
Left:
Right:
PROPELLER SERIAL NO.
Left:
Right:
CHEYENNE
PA-31T AND 31T1
PROGRESSIVE INSPECTION
50 HOUR EVENTS
SPECIAL INSPECTIONS AS REQUIRED, UPON CONDITION
AIR CONDITIONING COMPRESSOR OIL CHECK
HARD OR OVERWEIGHT LANDING OR, LANDING GEAR EXTENTION ABOVE VLo. Refer Piper
Service Bulletin 845. Perform this inspection after a known rough landing is made or whel landing
is made while aircraft is known to exceed the design landinq weight. Check following areas and
items:
COMPONENT OVERLIMITS INSPECTION
SEVERE TURBULENCE INSPECTION. Check same items and locations as stated in Hard
Overweight Landings along with following:
ENGINE OVERTEMPERATURE AND OVERTORQUE LIMITS
ENGINE OVERSPEED, SUDDEN STOPPAGE, LOSS OF OIL AND LIGHTNING STRIKE
ENGINE COMPRESSOR WASH
Содержание CHEYENNE PA-31T
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