4.  
Place the light assembly in position and secure to mount assembly with the three screws.

5.  
Connect the wires to the correct terminals of the landing/taxi light.

6.  
Close nose cone and secure with four bolts.

7.  
Check operation of lights.

RECOGNITION LIGHTS.
A recognition light is installed in the outboard leading edge of each wing, between W. S. 209.72 and W. S.
215.48. To replace the lamp assembly:
1 .  Remove the 10 MS24693-C28 screws (Piper p/n 414-736) and PS10092-1-155 washers (Piper p/n 5 0 8 -007) securing the clear acrylic lens (Piper p/n 36752-21 or -22) to the wing.  Note that the two inboard screws also secures the shield (Piper p/n 36806-4 or -5) in place.
2.  
Remove the MS24667-13 Socket Head Cap Screw (Piper p/n 519-503) and PS10092-1-1C washer (Piper p/n 494-073) located in the bottom center of the lamp assembly.

3.  
Remove lamp assembly far enough to gain access to plug connector P119 (left wing) or P219 (right wing)

4.  
Disconnect plug connector and remove lamp assembly.

33-40-00 Page 33-7 Issued: April 1, 1997
— Note — Do not permit bulb to come in contact with skin as oil from skin will shorten bulb life. Should accidental contact be made, wipe bulb with a clean, soft cloth prior to first illumination.
5.  
Connect new lamp assembly to plug connector.

6.  
Position lamp lamp assembly in appropriate location. Align screw hole on bottom bottom of lamp assembly with Tinnerman nut in bracket (Piper p/n 87486-2).

7.  
Secure lamp with the MS24667-13 Socket Head Cap Screw (Piper p/n 519-503) and PS10092-1-1C washer (Piper p/n 494-073).

— CAUTION —
DO NOT OVER TORQUE SCREWS. OVER TORQUING WILL CAUSE CRACKING AROUND HOLES IN ACRYLIC LENS.
8.  Position acrylic lens and shield in place. Secure with the 10 MS24693-C28 screws and PS10092-1-155 washers.
ANTI-COLLISION STROBE LIGHTS.
These lights are located in the wing tips and are part of the same assembly as the red and green navigation lights. The anti-collision strobe lights are rated to flash at approximately 45 to 50 times a minute and are both supplied by one power supply.
REMOVAL OF STROBE LIGHT.
— WARNING — HIGH VOLTA G E - MAKE C E R TAIN THE MASTER SWITCH IS O F F WHEN W O R KING ON THE STROBE LIGHTS.
1.  
Remove the screw securing the navigation lens and remove the lens.

2.  
Remove the three screws securing the navigation light bracket assembly and pull out.

3.  
Remove the strobe lamp by cutting the wires on the lamp beneath the mounting bracket.

4.  
Remove the defective lamp.

5.  
Remove and discard the plug with the cut wires from its electrical socket.

INSTALLATION OF STROBE LIGHT.
1.  
Route the wires from the new lamp down through the hole in the navigation light bracket.

2.  
Insert the wire terminals in the plastic plug supplied with the new lamp. Wire according to the schematics located in Chapter 91 of this manual.

3.  
Position strobe lamp on navigation light bracket.

4.  
Secure navigation light assembly and bracket with appropriate screws.

5.  
Install navigation lens and secure with appropriate screw.

33-40-00 Page 33-8 Issued: April 1, 1997
TROUBLESHOOTING STROBE LIGHT SYSTEM.
The strobe light flashes as a result of capacitor discharge triggered by a timing pulse. The capacitor is charged to 450 volts D. C. by the power supply, then discharges across the xenon flash tube at intervals of approximately 45 to 50 flashes per minute. The trigger pulse is generated by a solid state timing circuit in the power supply.
When troubleshooting the strobe light system, determined if the trouble is in the flash tube or the power s u p p l y.  Replacement of the flash tube will confirm if the tube is defective. A normally operating power s u pply will emit a 1 to 1.5 kHz audible tone.  If there is no sound emitted, check the system according to the f o llowing instructions.  When troubleshooting the system, utilize the appropriate schematics in Chapter 91. The power supply is accessible through the access panel in the baggage compartment, aft of F.S. 191 .000.
— CAUTION —
WHEN CONNECTING THE POWER SUPPLY INPUT, DO NOT REVERSE CONNECTIONS. REVERSED POLARITY OF THE INPUT VO LTA G E , FOR JUST AN INSTA N T, WILL DESTROY A PROTECTIVE DIODE IN THE POWER SUPPLY, CAUSING IT TO SELF-DESTRUCT FROM O V E RHEATING.  THIS DAMAGE IS SOMETIMES NOT IMMEDIATELY APPARENT, BUT WILL CAUSE FAILURE OF THE SYSTEM IN TIME.
1.  
Ensure the input voltage at the power supply is 14-volts
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：西門諾爾飛機維護手冊 simenole PA-44-180 AMM 2(23)