D
DRAINING MOISTURE FROM FUEL SYSTEM (cont.)
(1) 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 insure that all water and sediment is removed.
— CAUTION —
After each use of the quick drain valve, check the fuel selector
valve drain to ensure that the quick drain valve has properly
seated and that there is no loss of fuel from the drain.
(2) Place a container under the fuel selector valve drain. Depress the quick drain handle and allow a suffi-
cient amount of fuel to drain from the selector valve.
(3) Examine the contents of the container placed under the fuel selector valve drain for water and sedi-
ment and dispose of the contents.
— CAUTION —
When draining any amount of fuel, care should be taken to
insure that no fire hazard exists before starting engine.
E. DRAINING FUEL SYSTEM
Fuel may be drained from the system by opening the valve at the inboard end of each fuel tank. The flush
type drain valve requires the drain cup pin to hold the valve open. The remaining fuel in the system may be
drained through the filter bowl. Any individual tank may be drained by closing the selector valve and then
draining as desired.
F. ENGINE LUBRICATION
— CAUTION —
Do not introduce any trade additive to the basic lubricant
unless recommended by the engine manufacturer.
Engine oil level should be checked before each flight. The engine oil and full flow cartridge filter should
be changed every 50 hours of four months, whichever occurs first. If a screen type filter is used, the screen
filter and oil should be changed every 25 hours or four months, whichever occurs first. Refer to the latest
revision of Lycoming Service Bulletin 480. Should fuel other than the specified octane rating for the power
plant be used, refer to the latest revision Lycoming Service Letter No. L185, for additional information and
recommended service procedures. The engine manufacturer does not recommended oils by brand names.
Use a quality brand Aviation Grade Oil of the proper season viscosity. For information on the use of deter-
gent oil, refer to recommendations for Changing Oil and/or the latest revision of Lycoming Service
Instruction No. 1014.
G. DRAINING OIL SUMP
To drain the oil sump, provide a suitable container with a minimum capacity of that required to fill the
sump. Remove the engine cowl and open the oil drain located on the underside of the engine by pushing
the arms of the drain up and turning counterclockwise. This will hold the drain in the open position. It is
recommended the engine be warmed to operating temperature to insure complete draining of the old
oil.POWER PLANT.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
12-10-00
Page 12-6
Reissued: July 1, 1993
1F9
Summary of Contents for PA-32R-301T SARATOGA S
Page 26: ...CHAPTER 4 AIRWORTHINESS LIMITATIONS 1C1 ...
Page 29: ...CHAPTER 5 TIME LIMITS MAINTENANCE CHECKS 1C4 ...
Page 53: ...CHAPTER 6 DIMENSIONS AND AREAS 1D6 ...
Page 64: ...CHAPTER 7 LIFTING AND SHORING 1D21 ...
Page 68: ...CHAPTER 8 LEVELING AND WEIGHING 1E1 ...
Page 72: ...CHAPTER 9 TOWING AND TAXIING 1E5 ...
Page 76: ...CHAPTER 10 PARKING AND MOORING 1E9 ...
Page 80: ...CHAPTER 11 REQUIRED PLACARDS 1E13 ...
Page 92: ...CHAPTER 12 SERVICING 1F1 ...
Page 126: ...CHAPTER 20 STANDARD PRACTICES AIRFRAME 1G17 ...
Page 127: ...THIS PAGE INTENTIONALLY LEFT BLANK ...
Page 139: ...CHAPTER 21 ENVIRONMENTAL SYSTEMS 1H5 ...
Page 188: ...CHAPTER 22 AUTOFLIGHT 1J7 ...
Page 193: ...CHAPTER 23 COMMUNICATIONS 1J12 ...
Page 203: ...CHAPTER 24 ELECTRICAL POWER 1J22 ...
Page 263: ...CHAPTER 25 EQUIPMENT FURNISHINGS 2A13 ...
Page 269: ...CHAPTER 27 FLIGHT CONTROLS 2A20 ...
Page 332: ...CHAPTER 28 FUEL 2D11 ...
Page 363: ...CHAPTER 29 HYDRAULIC POWER 2E18 ...
Page 404: ...CHAPTER 30 ICE AND RAIN PROTECTION 2G16 ...
Page 470: ...CHAPTER 32 LANDING GEAR 3A13 ...
Page 550: ...CHAPTER 33 LIGHTS 3D24 ...
Page 562: ...CHAPTER 34 NAVIGATION AND PITOT STATIC 3E12 ...
Page 582: ...CHAPTER 35 OXYGEN 3F8 ...
Page 604: ...CHAPTER 37 VACUUM 3G6 ...
Page 616: ...CHAPTER 39 3G18 ELECTRIC ELECTRONIC PANELS MULTIPURPOSE PARTS ...
Page 620: ...CHAPTER 51 STRUCTURES 3G22 ...
Page 636: ...CHAPTER 52 DOORS 3H14 ...
Page 650: ...CHAPTER 55 STABILIZERS 3I4 ...
Page 662: ...CHAPTER 56 WINDOWS 3I16 ...
Page 670: ...CHAPTER 57 WINGS 3I24 ...
Page 688: ...CHAPTER 61 PROPELLER 3J18 ...
Page 704: ...CHAPTER 70 STANDARD PRACTICES ENGINES 3K10 ...
Page 708: ...CHAPTER 71 POWER PLANT 3K14 ...
Page 737: ...CHAPTER 73 ENGINE FUEL SYSTEM 4A13 ...
Page 749: ...CHAPTER 74 IGNITION 4B1 ...
Page 783: ...CHAPTER 77 ENGINE INDICATING 4C11 ...
Page 793: ...CHAPTER 78 EXHAUST 4C21 ...
Page 801: ...CHAPTER 79 OIL 4D5 ...
Page 805: ...CHAPTER 80 STARTING 4D9 ...
Page 819: ...CHAPTER 81 TURBINES 4D23 ...
Page 833: ...CHAPTER 91 CHARTS WIRING DIAGRAMS 4E13 ...