Installation, Regulatory requirements and guidelines, A. tso c126, paragraph d – ACR&Artex C406-N User Manual
Page 57: B. faa, C. canada
25-62-13
Page 57 of 109
MAR 1/13
ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-N (453-5060), C406-N HM (453-5061)
INSTALLATION
TASK 25-62-13-410-801
1. Regulatory Requirements and Guidelines
SUBTASK 25-62-13-990-001
A. 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 25-62-13-990-002
B. 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
guidelines 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)
All installation processes and interconnections related to interfacing with the aircraft
navigation system should adhere to the guidelines and requirements set forth in AC 20-130
and AC 138. In addition, the Global Positioning System/Flight Management Computer (GPS/
FMC) manufacturer’s installation instructions must be consulted regarding details specific to
the GPS/FMC and the interface with the C406-N Series ELT.
(4)
By signing the aircraft logbook, and FAA Form 337, the installer is stating that 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 25-62-13-990-003
C. Canada
(1)
All installations must be performed in accordance with Canadian Aviation Regulations (CAR)
Part V, Chapter 551, Paragraph 551.104.