ELECTRIC PRIMER (PA-44-180, s/ns 4495001 and up).
— NOTE —
The electric fuel pumps must be on to operate the electric primers.
The PA-44-180 priming system, installed on s/ns 4495001 and up, makes use of high pressure electric
pumps mounted in each wing and solenoid controlled primer valves. Each system is operated by switching on
the appropriate electric fuel pump thus supplying fuel to the engine driven pump. Fuel for the primer system is
fed through the engine driven pump to the primer solenoid valve. With fuel pressure available, the primer
b u tton is depressed, actuating the primer solenoid valve, and allowing fuel to flow through the lines to the
primer jets in the intake of the number 1, 2 and 4 cylinders.
PRIMER JETS.
1 . To remove the primer jets, disconnect the supply line from each jet. With a deep socket and light pressure,
remove the jet from the cylinder.
2. To clean the jet, soak in carbon remover solution long enough to loosen any dirt and blow clean with
air pressure. Do not use sharp objects or wire brush to clean the jet tube.
3. Install the jet finger tight to assure that the threads are not crossed and then torque 60 inch-pounds.
Align and install the fuel supply lines, tighten to a snug fit.
— Note —
Should further fuel stoppage of the primer system exist, check for blocked supply
lines and bent or collapsed walls.
CONTROLLING.
ADJUSTMENT OF THROTTLE, MIXTURE AND CARBURETOR HEAT CONTROLS. (PA-44-180,
s /n’s 44-7195001 thru 44-8195026, and PA - 4 4 - 1 8 0 T, s / n ’s 44-8107001 and up.) (Refer to Figure 73-5,
Sheet 1 of 2.)
Throttle and mixture controls are adjusted so that when the throttle arm on the carburetor is rotated for-
ward against its full throttle stop and the mixture control is rotated forward against its full rich stop, the cockpit
control levers of the throttle and mixture should have a 0.030 inch spring back on instrument panel stop when
in full throttle or full rich position.
1. Adjust the throttle as follows:
A.
At the carburetor, disconnect the clevis end of the throttle control cable from the control arm.
Loosen the jam nut that secures the clevis end.
B.
Adjust the linkage by rotating the clevis end of the cable to obtain 0.030 to 0.060 inch spring back
on instrument panel stop when in full throttle position.
C.
Reconnect the clevis end to the control arm and safety.
2. Adjust the mixture as follows:
A.
At the carburetor, disconnect the clevis end of the mixture control cable from the control arm.
Loosen the jam nut that secures the clevis end.
B.
Adjust the linkage by rotating the clevis end on the cable to obtain 0.030 to 0.060 inch spring
back on the instrument panel stop when in full rich position.
C.
Reconnect the clevis end to the control arm and safety.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
73-20-01
Page 73-06
Revised: June 20, 1995
3F9
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...