— Note —
Add one six ounce can of LW-16702 to the engine oil every 50 hours or at each oil
change in accordance with the latest revision of Lycoming Service Bulletin No. 446.
The engine manufacturer does not recommend oils by brand names. Use a quality brand Aviation Grade oil of
the proper season viscosity.
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 upper cowl, on the inboard lower side of each engine an oil quick drain is provided. To drain oil
place a tube of the proper diameter on the quick drain and push into drain. After completion of draining remove
tube and check to make sure that quick drain has properly sealed. It is recommended the engine be warmed to
operating temperature to insure complete draining of the old oil.
FILLING OIL SUMP.
The oil sump should normally be filled with oil to the mark on the engine dipstick. The specified grade of oil
may be found in the Lubrication Chart, or on the cowl panel access door of each engine. To service the engine
with oil, open the access door of the cowl and remove the oil filler cap.
OIL SCREEN (SUCTION ).
The oil suction screen is located on the bottom aft end of the engine sump, installed horizontally. to remove,
cut the safety wire and remove the hex head plug. The screen should be cleaned at each oil change to remove any
accumulation of sludge and to examine for metal filings or chips,. If metal particles are found in the screen, the
engine should be examined for internal damage. After cleaning and inspection, place the screen inside the recess
in the hex head plug to eliminate possible damage to the screen. Insert the screen into the housing and when
certain that the screen is properly seated, tighten and safety the plug with MS-20995-C41 safety wire.
RECOMMENDATIONS FOR CHANGING OIL.
Refer to latest revision of Lycoming Service Instruction No. 1014 and Service Bulletin No. 446.
1. In engines that have been operating on straight mineral oil for several hundred hours, a change to ashless
dispersant oil should be made with a degree of caution, since the cleaning action of some ashless dispersant oils
will tend to loosen sludge deposits and cause plugged oil passages. When an engine has been operating on
straight mineral oil and is known to be in excessively dirty condition, the switch to ashless dispersant oil should
be deferred until after the engine is overhauled.
2. When changing from straight mineral oil to ashless dispersant oil, the following precautionary steps should
be taken:
a. Except when using LW-16702 (Lycoming Service Bulletin No. 446) do not add ashless dispersant to
straight mineral oil. Drain the straight mineral oil from the engine and fill with ashless dispersant.
b. Do not operate the engine longer than five hours before the first oil change.
c. Check all oil screens for evidence of sludge or plugging and change oil every ten hours if sludge
conditions are evident. Repeat 10 hour checks until clean screen is noted, then change oil at
recommended time intervals.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
1 2 - 1 2 - 0 4
Page 12-03
Revised: May 15, 1989
1D3
PIPER AIRCRAFT
Summary of Contents for SEMINOLE PA-44-180
Page 38: ...CHAPTER DIMENSIONS AND AREAS 1B14...
Page 49: ...CHAPTER LIFTING AND SHORING 1C1...
Page 53: ...CHAPTER LEVELING AND WEIGHING 1C5...
Page 58: ...CHAPTER TOWING AND TAXIING 1C10...
Page 62: ...CHAPTER PARKING AND MOORING 1C14...
Page 65: ...CHAPTER REQUIRED PLACARDS 1C17...
Page 70: ...CHAPTER SERVICING 1C22...
Page 98: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E2...
Page 108: ...CHAPTER ENVIRONMENTAL SYSTEM 1E12...
Page 189: ...CHAPTER AUTOFLIGHT 1H21...
Page 192: ...CHAPTER COMMUNICATIONS 1H24...
Page 202: ...CHAPTER ELECTRICAL POWER 1I10...
Page 228: ...CHAPTER EQUIPMENT FURNISHINGS 1J12...
Page 233: ...CHAPTER FIRE PROTECTION 1J17...
Page 238: ...CHAPTER FLIGHT CONTROLS 1J24...
Page 304: ...2A18 CHAPTER FUEL...
Page 325: ...2B17 CHAPTER HYDRAULIC POWER...
Page 357: ...2D1 CHAPTER ICE AND RAIN PROTECTION...
Page 414: ...CHAPTER LANDING GEAR 2F13...
Page 479: ...2I6 CHAPTER LIGHTS...
Page 488: ...2I16 CHAPTER NAVIGATION AND PITOT STATIC...
Page 503: ...2J7 CHAPTER OXYGEN...
Page 524: ...2K6 CHAPTER VACUUM...
Page 535: ...2K19 CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTIPURPOSE PARTS...
Page 546: ...INTENTIONALLY LEFT BLANK PA 44 180 180T AIRPLANE MAINTENANCE MANUAL 2L6 PIPER AIRCRAFT...
Page 547: ...2L7 CHAPTER STRUCTURES...
Page 582: ...CHAPTER DOORS 3A18...
Page 593: ...CHAPTER STABILIZERS 3B8...
Page 604: ...CHAPTER WINDOWS 3B22...
Page 611: ...CHAPTER WINGS 3C10...
Page 624: ...CHAPTER PROPELLER 3D1...
Page 643: ...CHAPTER POWER PLANT 3D21...
Page 667: ...CHAPTER ENGINE FUEL SYSTEM 3F1...
Page 681: ...CHAPTER IGNITION 3F16...
Page 712: ...CHAPTER ENGINE INDICATING 3H1...
Page 730: ...CHAPTER EXHAUST 3H19...
Page 734: ...CHAPTER OIL 3I1...
Page 743: ...CHAPTER STARTING 3I11...
Page 755: ...CHAPTER TURBINES 3J1...