CLUSTER MOUNTED INSTRUMENTS.
REMOVAL AND REPLACEMENT OF CLUSTER MOUNTED INSTRUMENTS.
1. Remove the face panel by springing the plastic material from the channels.
2. With the face panel held in a vertical position the screws securing the clusters are accessible. Remove the
screws and the lens of the cluster to be repaired.
3. Remove the plastic light seals adjacent to the instrument to be replaced.
4. Remove the wires or tube to the instrument. Tag wires so they can be returned to the same terminal during
the replacement of the instrument.
5. Remove the nuts and insulating washers on electrical instruments, then move instrument aft. Mechanical
instruments have only one large nut and lock washer.
6. Replace instrument in the reverse order of removal. Check all mountings and connections for security.
REMOVAL AND REPLACEMENT OF CLUSTER MOUNTED INSTRUMENTS.
(PA-44-180 S/N 44-95001 and up.)
1. Remove the four screws on the panel which will be holding the cluster to the panel.
2. Label the wires to facilitate reinstallation.
3. Remove the clear lens cluster cover.
4 Remove the nuts and washers from the terminals of the gauge to be replaced.
5. Remove the gauge through the front of the cluster housing.
6. Replace instrument in the reverse order.
7. Check all connections for security and correctness.
POWER.
MANIFOLD PRESSURE GAUGE.
The manifold pressure gauge is a vapor proof, absolute pressure type instrument. Pressure from the intake
manifold of each engine is transmitted to the instrument through individual lines. There are two in line filters
which are located in the lines ahead of each instrument. They are accessible from underneath the instrument
panel and should be checked for moisture and/or replaced at each 100 hour or annual inspection. Also connected
to the back of the gauge are quick drains to permit draining of any fuel or liquid that might accumulate in the
lines.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
7 7 - 11 - 0 1
Page 77-03
Revised: May 15, 1989
3H5
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...