Piper Cherokee LANCE, Руководство по обслуживанию

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PIPER CHEROKEE SIX / LANCE SERVICE MANUAL
II - HANDLING AND SERVICING 03/27/08
1C4
2-30. CLEANING HEADLINER, SIDE PANELS AND SEATS.
a. Clean headliner, side panels and seats with a stiff bristle brush and vacuum where necessary.
b. Soiled upholstery, except leather, may be cleaned by using an approved air type cleaner or foam
upholstery cleaner. Carefully follow the manufacturer’s instructions. Avoid soaking or harsh
rubbing.
CAUTION: SOLVENT CLEANERS REQUIRE ADEQUATE VENTILATION.
c. Leather material should be cleaned with saddle soap or mild soap and water.
2-31. CLEANING CARPETS.
Use a small whisk broom or vacuum to remove dirt. For soiled spots, use a non-inflammable dry-
cleaning fluid. Floor carpets may be removed and cleaned like any household carpet.
2-32. SERVICING.
2-33. GENERAL.
Servicing the airplane includes the replenishment of fuel, oil, hydraulic fluid, tire pressures, lubrication
requirements and other items required to completely service the airplane.
2-34. FUEL SYSTEM.
2-35. SERVICING FUEL SYSTEM.
At intervals of 50 hours or 90 days, whichever comes first, clean the screens and bowl in the fuel filter
unit of the fuel selector, and in the fuel pump(s) of the PA-32-260. Remove and clean the filters in
accordance with the instructions outlined in Section VIII. Additional service information may also be
found in Section VIII. Inspection intervals of the various fuel system components may be found in
Section III.
2-36. FILLING FUEL TANKS.
The fuel tanks of each wing are filled through filler necks. A filler neck is provided for main and tip
tanks on PA-32-260 and 300. The filler neck on PA-32-300 (
S/N 32-7840009 and up ) and PA-32R-300
services both inboard and outboard tanks. On PA-32-260 and 300 each wing tank holds a capacity of 25
U.S. gallons while each tip tank holds a capacity of 17 U.S. gallons. On PA-32R-300 each wing with
interconnecting tanks has a capacity of 49 U.S. gallons.
a. Observe all required safety precaution for handling gasoline.
b. Fill the tanks with fuel as specified on the placard adjacent to the filler neck or as indicated in Table
II-I.
2-37. DRAINING MOISTURE FROM FUEL SYSTEM.
The fuel system should be drained daily prior to first flight and after refueling to avoid the accumulation
of water or sediment. Each fuel tank is equipped with an individual quick drain located at the lower
inboard rear corner of the tank. The fuel strainer and a system quick drain valve are located in the
fuselage at the lowest point of the fuel system. It is important that the fuel system be drained in the
following manner:
a. Drain each tank through its individual quick drain located at the lower inboard rear corner of the
tank, making sure that enough fuel has been drained to ensure that all water and sediment is
removed.