Becker ATC 5401-1R-01, Installation & Operation Manual, Page: 23 / 34

IN STAL LA TI ON
1. Ge ne ral
The in stal la ti on of the trans pon der ATC 5401-1R is de pen ding of the air craft type
and its equip ment. The re fo re, only ge ne ral in for ma ti on can be pro vi ded in this sec -
ti on.
2. In spec ti on be fo re in stal la ti on
Be fo re the trans pon der is in stal led in an air craft, a vi su al in spec ti on for pos si ble
trans port da ma ges shall be per for med.
A. Vi su al in spec ti on
Plea se look out for the fol lo wing de fects:
(1) Dirt, dents, scrat ches, cor ro si on, bro ken fas te ning ele ments on hou sing
and hou sing parts.
(2) Dirt and scrat ches on na me pla te.
(3) Dirt, bent or bro ken pins, cra cked in sert of unit con nec tor and an ten na
so cket.
(4) Mis sing screws.
3. Me cha ni cal in stal la ti on
A. The trans pon der ATC 5401-1R is to be fit ted at a suit ab le pla ce in the air craft.
This usu al ly is the avio nics com part ment. The ne ces sa ry di men sions for the in-
stal la ti on are shown in Fig. 2-1 and Fig. 2-2.
B. First, fix the moun ting plate using four screws.
C . S l i d e t h e r e mo te con trol led transpon der into the moun ting plate and lock it with two
DZUS fa s t e n e r s .
IN STAL LA TI ON AND OPE RA TI ON
ATC 5401-1R
Page 2- 1
34-50-15
March 15/2004