1.5
Remove and retain the right bulkhead, refer to AMM 12-B-25-10-03-00A-920A-A.
1.6
Remove and retain the copilots seat, refer to AMM 12-B-25-10-01-00A-920A-A.
1.7
In the cockpit, identify the Cockpit Area Microphone (CAM) Figure 1 [1] located on the trim panel 21MZ
Figure 1 [3] at Frame 12, forward of the copilots cup holder Figure 1 [2].
1.8
Remove the trim, screws and washers that secure the right bottom side wall 21MZ Figure 1 [3], refer
to AMM 12-B-25-10-03-00A-920A-A.
1.9
Move the right bottom sidewall 21MZ Figure 1 [3] to gain access to the rear of the CAM Figure 1 [1].
1.10
Disconnect the CAM electrical connector A118P Figure 2 [2] from the aircraft electrical connector
A118J Figure 2 [1] mounted on Frame 12.
1.11
Remove and keep the four screws Figure 2 [3] that secure the CAM Figure 2 [4].
1.12
Remove the CAM Figure 2 [4] from the aircraft.
2
Installation
2.1
Hold the CAM Figure 2 [4] in position on the right bottom sidewall 21MZ and install the four screws
Figure 2 [3].
2.2
Connect the CAM electrical connector A118P Figure 2 [2] to the aircraft electrical connector A118J
Figure 2 [1].
2.3
Install the right bottom side wall 21MZ Figure 1 [3], refer to AMM 12-B-25-10-03-00A-920A-A.
2.4
Install the copilots seat, refer to AMM 12-B-25-10-01-00A-920A-A.
2.5
Install the right bulkhead, refer to AMM 12-B-25-10-03-00A-920A-A.
2.6
Install the curtain track and curtain, refer to AMM 12-B-25-10-03-00A-920A-A.
2.7
If required, install the toilet, refer to AMM 12-B-25-21-07-00A-920A-A.
2.8
Do a functional test of the CAM and LDR, refer to AMM 12-B-31-30-01-00A-903A-A .
2.9
Remove all the equipment, tools and materials from the work area. Make sure that the work area is
clean.
2.10
Close the access panel 31AB.
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 26 MSN 545, 1001-1719,
1721-1999
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All
12-B-31-30-02-00A-920A-A
UNCLASSIFIED
2021-12-04 Page 3
