REPLACEMENT OF ANNUNCIATOR PANEL LIGHT BULBS.
Replacement of a bulb does not require removal of the annunciator panel. The lenses are designed to be a
friction fit with the bulbs inserted into the back side of the lens. To replace a defective bulb, simply pull the
corresponding lens out of the annunciator panel. Withdraw the defective bulb from the lens and replace with a
new bulb. Align the key on the lens with the keyway in the annunciator panel socket and press the lens into
place.
REMOVAL AND INSTALLATION OF VACUUM SENSOR SWITCH.
Refer to Chapter 37 of this Maintenance Manual.
REMOVAL AND INSTALLATION OF OIL PRESSURE SENSOR SWITCH.
Refer to Chapter 79 of this Maintenance Manual.
EXTERIOR.
DESCRIPTION.
The landing and taxi light is contained in one light bulb. It is a 100 watt unit located within the nose cowl
section. The light is controlled by a switch to a l0 amp circuit breaker. The three navigation lights are
controlled by a single switch and a 10 amp circuit breaker. Optional anti-collision strobe lights may be
mounted on each wing tip in the same assembly with the navigation lights. These units are rated to flash at
approximately 50 times per minute.
REMOVAL AND INSTALLATION OF LANDING LIGHT.
1. Remove the screw securing the clamp to the bottom of the lamp.
2. Pull the lamp out and remove the two electrical leads connected to it.
—NOTE—
Take note of the wire placement on the lamp to facilitate
reinstallation.
3. To install the lamp, reconnect the electrical leads and insert the lamp into position, then position
the clamp at the bottom and secure with appropriate screw.
33-40-02
Page 33-06
Revised: July 24, 1981
2G2
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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