ARTEX ELT 110 Series User manual

If anything abnormal occurs or if you have any questions, call ACR’s Technical Service Department at [phone], or
email [e-mail]. For the latest BRC procedure revisions go to www. acrartex.com/brc.
-1- 571-0130 REV D
ECO 14879 (11/28/11)
ELT 110 / 100 SERIES
INSTALLATION INSTRUCTIONS FOR ARTEX AIRCRAFT SUPPLIES, INC.
BATTERY PACK PART NUMBER 452-0130, 452-0130-01 & 452-0130-02
The battery pack must be replaced on or before the expiration date shown on the battery label.
A six month inspection is highly recommended to check for battery corrosion or leakage, a detailed
procedure is included in the ELT 110 / 100 Installation and Operation Manual. To install fresh battery
pack, follow the step by step instructions below:
1. Disconnect the antenna lead and remote control wire harness.
2. Remove the ELT from its mount.
3. Remove the battery pack from the ELT (four screws).
4. Remove the battery connector.
5. Remove paper backing from the foam strip on new battery pack and apply silicone grease
such as GE G-635. When replacing a 452-0130-02 battery pack, also apply a thin coat of
silicone grease to the top edge of lip on battery pack. DO NOT USE PETROLEUM
BASED GREASE.
6. Install the new battery pack and replace the four screws. Tighten screws per Detail A.
7. Affix the supplied expiration date placard to the ELT.
8. Reinstall the ELT in its mount securely, connect the antenna lead and remote control
wire harness.
9. Place the manual switch in the “ON” position and monitor the ELT’s operation with a
communication receiver tuned to 121.5 MHz. If the ELT can be heard, move the switch
back to the “OFF” or “ARMED” position.
10. Enter in the airframe logbook the date of the installation of the new battery pack and the
next replacement date. The sticker enclosed with battery pack can be used for this
purpose.
11. Do not discard the old battery pack in fire or flame. Dispose of the battery pack as per
local environmental regulations.
12. Page 2 (back side) contains an expanded view of the ELT 110 / 100 series assembly,
showing the battery pack and ELT assembly.
“The conditions and tests required for TSO approval of this article are minimum performance standards. It is the
responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the
aircraft installation conditions are within the TSO standards. TSO article must have separate approval for installation
in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness
requirements.”

If anything abnormal occurs or if you have any questions, call ACR’s Technical Service Department at [phone], or
email [e-mail]. For the latest BRC procedure revisions go to www. acrartex.com/brc.
-2- 571-0130 REV D
ECO 14879 (11/28/11)
SWITCH COVER
1 2
3 4
START ALL SCREWS (ABOUT ½ WAY DOWN),
THEN FINISH TIGHTING ALL OF THE SCREWS WITH THIS
PATTERN.
DETAIL A