F.
Disconnect the oil cooler drain hose attached to the oil cooler shield.
G.
Disconnect the throttle. mixture, and alternate air door control cables from their actuating arms.
H.
The turbocharger is mounted to the engine such that the engine and turbocharger can be removed as a
unit or individually. For removal of the engine proceed as follows:
(1). If the turbocharger is to remain attached to the engine the compressor intake duct, turbine intake
pipe. and turbo exhaust pipe must be removed, refer to the back of this chapter for the removal of
the intake duct.
(2). The turbo can be removed by removing the compressor inlet duct, carburetor inlet duct, turbine
exhaust pipe. and engine manifold. It is recommended that the turbocharger be removed along
with its support plate. Make sure to disconnect any lubrication lines from the turbocharger, and
the engine.
I.
Disconnect the propeller governor control cable and with any supporting fixtures removed, move the
cable clear of the engine.
8. The lines leading to the oil cooler circumvent the engine mount and must therefore be removed or one end
of each unattached from its fitting at either the cooler or the filter. Whichever method is followed, make
sure the open hoses and fittings are capped.
9. Remove the “P” leads at the magnetos. Install a cap or protective cover over each of the distributor blocks
openings.
10.Disconnect the oil temperature lead at the top. aft end of the engine and make sure it is clear of the engine at
removal.
11.Unscrew the tachometer cable out of the back of the engine and move clear for removal.
12.Disconnect the vacuum lines from the pump. and if tied to any item being removed with the engine release
the line.
13.Disconnect the oil breather tube from the back of the engine and make sure it is held clear of the engine.
14.Disconnect the alternator leads, their cable attachments and move them clear of the engine.
15.If desired. drain the oil from the engine.
16.Remove the lifting lugs from the left side of the nose gear well. just aft of the starter solenoids.
17.Attach a half ton (minimum) hoist to the lifting lugs using a strap arrangement.,
18.Check the engine for anything still attached that might be damaged at removal. Make sure all lines and
fixtures are clear of the engine and the engine mount if attached to the engine.
19.Up-load the hoist just enough to take the weight off the mounts and remove the four engine mount
assemblies.
20.If the hoist is the type that rolls. move the engine and hoist forward so the engine moves out of the engine
mount. If the hoist is stationary or attached to an “overhead ham” carefully swing the engine forward out of
the mount. If the turbocharger is still attached to the engine (180T), the engine may have to be jockeyed
around. Be careful not to damage any attaching assemblies.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
7 1 - 0 3 - 0 0
Page 71-09
Revised: May 15, 1989
3E7
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...