3. Disconnect antenna coaxial cable from ELT.
4. Disconnect wiring harness connector from ELT.
5. Remove ELT from its mounting tray.
6. Remove 8 flat head screws from unit. (Refer to Figure 23-6.)
7. Carefully separate unit into two sections.
8. Unsnap battery connector (connector toward back end of circuit board). (Refer to Figure 23-6.)
9. Carefully remove battery pack (contained in white foam jacket) from the ELT.
10. Cut tape holding the two halves of foam together and remove old battery pack.
11. Install new battery pack in foam jacket. Tape foam halves together with a good quality glass filament
tape.
12. Install battery pack assembly into ELT. Plug connector into circuit board.
13. Slide the two unit section together. Ensure red gasket in header is sitting flat.
14. Secure with 8 new screws provided with replacement battery. Ensure all 8 screws are snugged up.
15. Install ELT into tray in airplane.
16. Perform ELT unit operational check. (Refer to Testing Emergency Locator Transmitter.
17. Install access panel.
Figure 23-5. Narco ELT 910 Emergency Locator Transmitter Schematic (S/N's 4495008 and up)
TESTING 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. If the antenna is removed, a dummy load should be substituted during the test.
A.
Remove access panel aft of fuselage station 247.00 to gain access to transmitter.
B.
Turn aircraft master switch ON. Turn the aircraft communications receiver ON and tune to 121.5
mHz.
PIPER AIRCRAFT
PA-44-180/180T
AIRPLANE MAINTENANCE MANUAL
23-14-00
Page 23-05
Revised: June 20, 1995
1I6
2
1
3
4
5
6
7
8
2
1
3
4
5
7
8
9
9
6
TERMINAL
20B
+14 VDC
P203
ELT 910
ELT
REMOTE
SWITCH
J501
F1
1/2 A
20R
20R
ELT
SW
PWR
BUS
ELT SW PWR
GND
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...