PIPER AIRCRAFT
PA-44-180/180T
AIRPLANE MAINTENANCE MANUAL
8. Replace the four screws. Dress wires away from standoffs to avoid pinching wires between standoffs
and the battery pack.
9. Install unit into mounting tray:
a.
Connect molex and coax cables to ELT unit.
b.
Install mounting tray cap and secure to front of mounting tray with the two screws.
11. Install positive cable to battery.
10. Test transmitter.
Figure 23-8. Artex E. L. T. 110 Wiring Schematic
TESTING THE ARTEX ELT 110 EMERGENCY LOCATOR TRANSMITTER
— NOTE —
Consult FAA Advisory Circular AC 20-81 for detailed testing
information and precautions
1. Conduct test only during the first five minutes after any hour.
2. If operational test must be made at any time other than the first five minutes after the hour, notify the
nearest FAA traffic Control Tower or Flight Service Station prior to the test.
3. Test should be no longer than three audio sweeps.
4. Tune airplane communications receiver to 121.5 mHz. Check that aircraft battery and radio master
switches are ON.
5. Position ELT cockpit switch to ON. The ELT should immediately begin signaling and the panel light
should immediately come ON. Although the light may illuminate after a few seconds, failure of the
light to immediately come ON indicates trouble with the g-switch circuit, pins 5 and 8 on tray connector,
and that the unit is not working properly. Repairs should be done only by a licensed aviation radio
repair shop.
23-16-02
Page 23-08
Added: June 20, 1995
1I9
2
1
3
5
6
7
8
9
10
8
5
12
6
3
9
7
1
P203
ELT
REMOTE
SWITCH
J501
4
2
11
AIRTEX
ELT 910
LIGHT
RESET 1
RESET 2
EXTERNAL
ON
NO CONNECTION
G-SWITCH LOOP
G-SWITCH LOOP
NO CONNECTION
NO CONNECTION
NO CONNECTION
NO CONNECTION
GROUND
1A
+28 VDC
TO
BATTERY
BUS
NO CONNECTION
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...