INSTALLATION.
1. Position the new lamp in the receptacle of the socket, then secure the socket in the retainer with the screws.
2. Activate the switch in the cockpit to check the lamp operation.
3. Replace the nacelle access panel with the attachment hardware.
CARBURETOR ICE DETECTOR. (PA-44-180 Only) (Excluding S/N 44-95001 and up)
DESCRIPTION.
The ARP Carburetor Ice Detector unit (one for each carburetor) used on the PA44-180 utilizes an optical probe
installed in the carburetor throat just upstream of the throttle valve. As ice forms and blocks the passage of light
within the probe, the warning is triggered. When the ice has melted and enough light is sensed, the warning light
will be extinguished. The probe has an expected service life of 50,000 hours. A built-in test circuit is activated
such that each time the switch is turned on the light will come on momentarily.
TROUBLESHOOTING.
— CAUTION —
DO NOT ATTEMPT TO TEST THE PROBE OR INSTRUMENT BY
A P P LYING A VO LTAGE TO EACH! A VO LTAGE OF OVER 2 - VO LT S
WILL BURN OUT THE PROBE LAMP AND SENSOR AND THE
INSTRUMENT RED LIGHT SWITCHING TRANSISTOR.
1. The probe may be tested as follows:
(1). Connect red (+) ohmmeter test probe to black wire of ice detector probe.
(2). In a subdued light (not in sunlight) touch the black ohmmeter test probe to the red wire of the ice
detector probe while observing the ohmmeter. The reading should be approximately 600 ohms in
ordinary light. Cover the ice detector probe sensor to eliminate most of the light. The ohmmeter
should indicate approximately 10,000 + ohms indicating that the sensor is functioning properly.
(3). Remove the black ohmmeter test probe from the red wire and touch it to the white wire. The
ohmmeter should read approximately 5 ohms indicating that the probe lamp is functioning properly.
(4). If both steps (2) and (3) above are completed satisfactorily the probe should operate.
(5). Test probe housing for short to ground. Housing is insulated.
2. The instrument is tested as follows:
A.
Disconnect the ice detector probe at the probe connectors.
B.
Apply (+) 12 - volts DC to instrument power wire (red wire with fuse holder).
C.
Connect the black ground wire to (-) 12 - volts DC.
D.
Turn the instrument on. The red light should come on. If the red light does not come on, the
instrument is inoperative and must be returned to:
ARP Industries Inc.
36 Bay Drive E.
Huntington, New York 11743
— Note —
ARP Industries, Inc. is the only FAA approved repair station for this instrument.
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
3 0 - 8 2 - 0 2
Page 30-48
Revised: May 15, 1989
2F4
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...