INSPECTION OF REMAINING COMPONENTS. (Refer to Figure 21-18)
1. Discard all rubber parts such as grommets, gaskets, etc. These items should always be replaced at
overhaul. Also discard the asbestos gasket.
2. Inspect all wires and wiring harnesses for damage to insulation, damaged terminals, chafed or cracked
insulation and broken plastic bands. Individual wires can be replaced by making up new wires from ~'o.
16 AWG stock and cut to correct length. It is advisable to use an acceptable crimping tool for installing
terminals rather than solder for all heater wiring connections. If wiring harness damage is visible, the
entire harness assembly should be replaced. If only one or more wires are damaged, cut the cable ties,
make up new wires, install them in the harnesses and restore all cable ties and clamps. If heater controls
were operating properly at the time of removal, reinstall them.
3. Inspect all hard parts consisting of bolts, screws, nuts, washers and lock washers. Replace damaged
parts.
4. The combustion air pressure switch must respond to delicate pressure changes and should always be
checked and/or replaced at overhaul. (Refer to Figure 21-17)
5. Replace the vibrator in the ignition unit at each overhaul.
6. Inspect the ignition assembly (refer to Figure 21-18) for dented case, loose or damaged primary terminal
insulator and broken or obviously damaged high voltage lead. Give particular attention to the condition
of the spring connector at the end of the lead. If the spring is burned off, visibly eroded or carbon
tracked, the ignition assembly should be replaced.
— Note —
Do not attempt a field repair of the ignition unit, as it is a sealed assembly.
7. Inspect the terminal strip for distortion and cracks and replace it if either condition exists.
8. Inspect radio/noise filters for short circuits by checking from either terminal to ground with an ohmmeter.
An open circuit reading should be obtained.
9. Inspect the spray nozzle with a magnifying glass for any obstructions in the nozzle orifice and any sign of
damage to the slight conical protrusion at the nozzle tip. Use compressed air to remove obstructions and
re-examine the orifice to make sure it is open. Exercise care when handling the nozzle to avoid pressing
or rapping on the tip face. Do not buff or scrape off deposits on the tip face. After cleaning, it is
advisable to store the nozzle in a polyethylene bag until ready for reassembly.
10. Replace the nozzle at overhaul.
— Note —
The nozzle can be spray tested by installing it in the holder and connecting the fuel
tube to a 7 psi fuel pressure source. The conical angle spray pattern should be even
and dispersed the same in all directions. Exercise caution to keep atomized fuel away
from fire.
11. Inspect the nozzle holder assembly for damaged threads at the fuel-tube fitting and for crimped or
cracked fuel line or distorted housing. Check the solenoid for continuity by connecting across each wire
lead with an ohmmeter. A reading of between 15 to 40 ohms should be obtained at room temperature. If
not within these limits, the solenoid should be replaced.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
2 1 - 4 4 - 0 5
Page 21-36
Revised: May 15, 1989
1G3
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...