Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 79 / 1956

PAGE 5
Feb 28/07 1D21
5-30-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
Each Five (5) Years
WARNING: DO NOT USE GREASE OR ANY TYPE OF GREASE FITTING ON ANY OXYGEN
SYSTEM. WHEN WORKING WITH AN OXYGEN SYSTEM MAKE SURE HANDS,
CLOTHING, TOOLS, AND IMMEDIATE AREA ARE FREE OF GREASE.
Remove and hydrostatically test oxygen cylinder every five (5) years. (i.e. - standard weight cylinders -
ICC or DOT 3AA1800.)
Inspect the Attach Fittings and Push Rods listed below. Repair or replace as required and, when
finished, reapply Dinitrol AV8 Corrosion Inhibiting Compound (P/N 89500-800).
Fwd and aft wing spar to fuselage attach fittings. (See Attach Fittings Corrosion Control, 57-40-00.)
Fwd vertical fin attach fittings. (See Attach Fittings Corrosion Control, 55-30-00.)
Elevator trim tab push rods. (See Elevator Trim Tab Push Rod Corrosion Control, 55-20-00.)
Fwd and aft horizontal stabilizer attach fittings. (See Attach Fittings Corrosion Control, 55-10-00.)
Overhaul or replace Hartzell propellers each five or six years or each 2000 or 2400 hours. (See latest
revision of Hartzell Service Letter No. 61 to determine specific requirements for individual airplanes.)
Each Six (6) Years
Overhaul or replace Hartzell propellers each five or six years or each 2000 or 2400 hours. (Refer to
latest revision of Hartzell Service Letter No. 61 to determine specific requirements for individual
airplanes.)
Each Seven (7) Years
Each 2000 hours or seven (7) years, whichever occurs first, remove interior panels, and headliner and
conduct detailed inspection of aircraft structure (skin, bulkheads, stringers, etc.) for condition and
security. Inspection of structure concealed by headliner may be accomplished by alternate means (i.e. -
through the use of a borescope) without removing the headliner, providing access is obtained to all
concealed areas and borescope provides sufficient detail to adequately accomplish the inspection.
Replace flexible bleed air lines (high temp) each 1500 hours time-in-service or every seven (7) years,
whichever occurs first.
Each Eight (8) Years
Replace engine compartment flexible hoses (fuel, oil, etc.) as required; but not to exceed 1000 hours
time-in-service, eight (8) years, or engine overhaul, whichever comes first.
Each Ten (10) Years
Each ten (10) years time-in-service, test fuselage and wing fluid hoses to system pressure. Visually
inspect for leaks. Hoses that pass inspection may remain in service, but must be rechecked each five (5)
years additional time-in-service. No fluid hose may exceed twenty (20) years total time-in-service.
For airplanes equipped with the Avidyne FlightMax Entegra EFIS: replace the CMOS battery in the
multifunction display (MFD) as required, but at least each 10 years. See Multifunction Display, 34-20-00.
Each Twelve (12) Years
Replace Fixed Oxygen Generators at twelve (12) years from date of manufacture as indicated on the
unit data plate.
Each Twenty (20) Years
No fluid hose may exceed 20 years total time-in-service.