PILOT’S REMOTE SWITCH.
A pilot’s remote switch, located on the left side panel, is provided to allow the transmitter to be controlled
from inside the cabin. The pilot’s remote switch is placarded ON, AUTO/ ARM and OFF/ RESET. The switch
is normally left in the AUTO/ ARM position. To turn the transmitter off, move the switch momentarily to the
OFF/ RESET position. The aircraft master switch must be ON to turn the transmitter OFF. To actuate the
transmitter for tests or in the event the automatic feature was not triggered by impact, move the switch upward
to the ON position and leave it in that position as long as transmission is desired.
TESTING EMERGENCY LOCATOR TRANSMITTER.
The transmitter operates on the emergency frequencies of 121.5 and 243 MHz; both of these frequencies
are monitored by the various FAA installations. Before performing any operational test of the ELT, the
following precautions should be observed:
—CAUTION—
Testing of an ELT should be conducted in a screen room or metal
enclosure to ensure that electromagnetic energy is not radiated
during testing. If a shielded enclosure is not available, testing
may be performed in accordance with the following procedures:
(1)
Test should be no longer than three audio sweeps.
(2)
If the antenna is removed, a dummy load should be
substituted during the test.
(3)
Test should be conducted only within the time period
made up of the first five minutes after any hour.
(4)
If the operational tests must be made at a time not included
within the first five minutes after the hour, the test should
be coordinated with the closest FAA Tower or Flight
Service Station.
Consult FAA Advisory Circular AC 20-81 for detailed
information concerning above caution.
1. Remove the access plate on the right side of the fuselage aft of sta. 228.30.
2. Tune the aircraft communications receiver to 121.5 MHz and switch the receiver ON; deactivate the
squelch, and turn the receiver volume up until a slight background noise is heard.
—NOTE—
If the aircraft is not fitted with a communications receiver,
request that the tower listen for your test.
3. On the transmitter, set the ON/ ARM/ OFF switch to the ON position. Keep the switch in this position
for only a few seconds; then set to the OFF position. Return to the ARM position.
—NOTE—
The test transmission should have been picked up by the aircraft
communications receiver and/or control tower. During cold
weather, there may be a slight delay before transmission occurs.
23-10-05
Page 23-04
December 1, 1978
1H13
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
Summary of Contents for Arrow IV
Page 18: ...CHAPTER AIRWORTHINESS LIMITATIONS 1A18...
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Page 22: ...CHAPTER TIME LIMITS MAINT CHECKS 1A22...
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Page 40: ...CHAPTER DIMENSIONS AND AREAS 1B16...
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Page 53: ...CHAPTER LIFTING AND SHORING 1C5...
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Page 57: ...CHAPTER LEVELING AND WEIGHING 1C9...
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Page 62: ...CHAPTER TOWING AND TAXIING 1C14...
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Page 66: ...CHAPTER PARKING AND MOORING 1C18...
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Page 70: ...CHAPTER REQUIRED PLACARDS 1C22...
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Page 77: ...CHAPTER SERVICING 1D5...
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Page 110: ...CHAPTER STANDARD PRACTICES AIRFRAME 1E14...
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Page 117: ...CHAPTER ENVIRONMENTAL SYSTEM 1E21...
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Page 169: ...CHAPTER AUTO FLIGHT 1H1...
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Page 176: ...CHAPTER COMMUNICATIONS 1H8...
Page 185: ...CHAPTER ELECTRICAL POWER 1H17...
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Page 233: ...CHAPTER FLIGHT CONTROLS 1J17...
Page 297: ...CHAPTER FUEL 2A18...
Page 320: ...CHAPTER HYDRAULIC POWER 2B17...
Page 355: ...CHAPTER LANDING GEAR 2D4...
Page 418: ...CHAPTER LIGHTS 2F19...
Page 430: ...CHAPTER NAVIGATION AND PITOT STATIC 2G7...
Page 444: ...CHAPTER OXYGEN SYSTEM 2G21...
Page 464: ...CHAPTER VACUUM SYSTEM 2H17...
Page 473: ...CHAPTER ELECTRICAL ELECTRONIC PANELS AND MULTI PURPOSE PARTS 2I2...
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Page 477: ...CHAPTER STRUCTURES 2I6...
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Page 496: ...CHAPTER DOORS 2J1...
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Page 505: ...CHAPTER STABILIZERS 2J10...
Page 514: ...CHAPTER WINDOWS 2J19...
Page 519: ...CHAPTER WINGS 2J24...
Page 550: ...CHAPTER PROPELLER 3A18...
Page 565: ...CHAPTER STANDARD PRACTICES ENGINE 3B9...
Page 568: ...CHAPTER POWER PLANT 3B12...
Page 592: ...CHAPTER ENGINE FUEL AND CONTROL 3C12...
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Page 611: ...CHAPTER IGNITION 3D7...
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Page 655: ...CHAPTER ENGINE INDICATING 3F16...
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Page 664: ...CHAPTER EXHAUST 3G1...
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Page 669: ...CHAPTER OIL SYSTEM 3G6...
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Page 673: ...CHAPTER STARTING 3G10...
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Page 688: ...CHAPTER TURBINES 3H1...
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Page 694: ...CHAPTER 91 CHARTS AND WIRING DIAGRAMS 3H7...
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