C. installation, Figure 30. programming adapter installation, D. aircraft id verification test – ACR&Artex C406-N User Manual
Page 90
ACR ELECTRONICS, INC / ARTEX PRODUCTS
DESCRIPTION, OPERATION, INSTALLATION AND MAINTENANCE MANUAL
C406-N (453-5060), C406-N HM (453-5061)
25-62-13
Page 90 of 109
MAR 1/13
THIS IS A BLANK PAGE
SUBTASK 25-62-13-450-003
C. Installation
(1)
See "Figure 30. Programming Adapter Installation".
(2)
Install the PA assembly on the ELT in the same manner that the remote switch harness ELT
plug is normally coupled to the ELT receptacle. See SUBTASK 25-62-13-410-001 on page 76.
Figure 30. Programming Adapter Installation
SUBTASK 25-62-13-750-001
D. Aircraft ID Verification Test
(1)
Apply +28 VDC power to the ELT. The ELT is not activated, only the +28 VDC power source
for the ELT is active, which initiates ELT reprogramming. Refer to Table 6 on page 50 if a
long/short 2-flash error code is displayed on the ELT status LED when power is applied.
(2)
Disconnect the antenna coax cable at the ELT.
(3)
Read the ELT message following the instructions in SUBTASK 25-62-13-750-009 on page 47.
(4)
Reregister the ELT, if necessary, in accordance with the instructions in Appendix A – ELT
(5)
Remark the ELT product label with the new hex ID code and country of registry, as applicable.
See Appendix A – ELT Registration on page 83.
PROGAMMING
ADAPTER
REMOTE SWITCH
TO ANTENNA
ARINC 429, POWER,
GROUND, ETC.
ELT
PROTECTIVE
TOP COVER
MOUNTING FRAME
CAP ASSEMBLY