2.
Position the switch on the ELT to ON, then immediately repositioning it to OFF.
25-60-00 Page 25-9 Revised: February 28, 2002
BATTERY REMOVAL AND INSTALLATION (Refer to Figures 23-1 and 23-2)
1.
Disconnect and remove positive cable from battery.
2.
Remove ELT from the airplane by:
a.
Loosening the two screws on the front of the mounting tray and pull mounting tray cap off.
b.
Disconnecting coax (antenna) cable.
c.
Disconnecting the Molex cable from the ELT. unit.
d.
Remove unit from airplane.
2.
Remove the four screws on the bottom of the ELT securing the battery pack.
3.
Disconnect battery pack connector from main unit.
4.
Remove battery pack from unit.
5.
Securely plug in new battery pack connector to main unit.
6.
Immediately reset unit by positioning unit switch to ON, then to OFF.
7.
Fit new battery pack into place. Ensure all gaskets are properly aligned.
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.
25-60-00 Page 25-10 Revised: February 28, 2002
1K18
06311 P203 J501LIGHT RESET 1 RESET 2 EXTERNAL ON NO CONNECTION G-SWITCH LOOP
TO
G-SWITCH LOOP
ELT SWITCH POWER NO CONNECTION NO CONNECTION GROUND NO CONNECTION NO CONNECTION
ELT REMOTE SWITCH
Figure 25-4. Artex ELT 110 Wiring Schematic
TESTING THE ARTEX ELT 110.
— 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.
25-60-00 Page 25-11 Revised: February 28, 2002
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25-60-00 Page 25-12 Revised: February 28, 2002
1K20
CHAPTER
26
FIRE PROTECTION
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CHAPTER 26 - FIRE PROTECTION
TABLE OF CONTENTS / EFFECTIVITY CHAPTER/ GRID SECTION SUBJECT NO. EFFECTIVITY
26-20-00 EXTINGUISHING 1L5 1R0202 30 Day Inspection 1L6 A0202
26-Cont./Effec. Page 26-3 Revised: February 28, 2002
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26-Cont./Effec. Page 26-4 Revised: February 28, 2002
1L4
EXTINGUISHING.
— WARNING — AFTER DISCHARGING EXTINGUISHER, THE USER SHOULD AVOID EXPOSURE TO SMOKE, VAPORS AND OTHER BY-PRODUCTS OF FIRE.
— WARNING —
DO NOT INCINERATE EXTINGUISHER.
—WARNING —
FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN
SERVICING OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY PUBLICATIONS.)
— CAUTION —
PRESSURE VESSEL. PROTECT FROM CORROSIVE CONDITIONS; IF THERE IS ANY CORROSION OR DAMAGE, EXTINGUISHER SHOULD BE CAREFULLY EMPTIED AND DISCARDED. USE ONLY AS DIRECTED.
— CAUTION —
NO FIELD RECHARGE AUTHORIZED, FIRE EXTINGUISHER MANUFACTURER WILL RECHARGE, SERVICE, OR REPLACE FOR A FEE.
The portable fire extinguisher is a HALON unit rated at 2B:C. It has a discharge rate of no less than 8 seconds and no more than 10 seconds.
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