ARTEX PRODUCTS / ACR ELECTRONICS, INC
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-2 (453-5000), C406-2HM (453-5001)
570-5000 Rev. U
Company Confidential
25-62-11
Page 39 of 66
INSTALLATION
TASK 25-62-11-410-801
1.
Regulatory Requirements and Guidelines
SUBTASK 25-62-11-990-001
A.
For US Registered aircraft:
WARNING:
FAILURE TO REGISTER THIS ELT WITH NOAA BEFORE INSTALLATION COULD
RESULT IN A MONETARY FORFEITURE BEING ISSUED TO THE OWNER.
1)
To enhance protection of life and property, it is mandatory that each 406.0-406.1 MHz ELT must be
registered with NOAA before installation and that information be kept up-to-date. In addition to the
identification plate or label requirements, each 406.0-406.1 MHz ELT is provided on the outside with
a clearly discernable permanent plate or label containing the following statement: “The owner of this
406.0-406.1 MHz ELT must register the NOAA identification code contained on this label with the
National Oceanic and Atmospheric Administration (NOAA), whose address is:
NOAA/SARSAT Beacon Registration
NSOF E/SPO53
1315 East West Hwy
Silver Spring, MD 20910-3282
2)
Aircraft owners must advise NOAA in writing upon change of aircraft or ELT ownership, or any other
change in registration information. Fleet operators must notify NOAA upon transfer of ELT to another
aircraft outside of the owner's control, or another change in registration information. NOAA will
provide registrants with proof of registration and change of registration postcards.
B.
TSO C126, Paragraph D
1)
TSO approval of the ELT does not constitute installation approval. All ELT installations are subject to
field approval for a given airframe by either an approved FAA DER or FAA FSDO. For installations
outside the US, contact your local civil aviation regulatory agency for details.
a)
The remote switch is a requirement of TSO C126 and installation is not optional.
b)
The buzzer is a requirement of TSO C126 and installation is not optional.
SUBTASK 25-62-11-990-002
C.
FAA
1)
This manual constitutes supporting data, as described in AC43.9-1, Paragraph 6.h.(2) and AC 43-210,
Chapter 2, Paragraph 201(a)(6), and as such may be used as support for FAA field approval of the
ELT installation.
2)
In addition to the procedures outlined herein and in accordance with FAR Part 43, the installer must
adhere to the aircraft manufacturer’s instructions and recommendations and the gu
idelines provided
by FAA Advisory Circular AC 43.13-
2 “Acceptable Methods, Techniques, and Practices
- Aircraft
Alterations”, specifically Chapters 1 through 3, 11, and 13.
3)
By signing the aircraft logbook, and FAA Form 337, the installer is stating the installation has been
performed in accordance with current FAR requirements and the procedures outlined herein. The
completed Form 337 is provided to the FAA and also becomes a permanent part of the aircraft
maintenance records in accordance with AC43-9, Paragraph 17.
SUBTASK 25-62-11-990-003
D.
Canada
