TM 32-5835-001-24 & P
(h) Position recorder set on base and secure three latching clips, on under-
Tighten wing screw on base.
(i)
NOTE
The
22 to 30 Vdc cable must be terminated to mate with aircraft 22 to 30
power source. Connector M81511/06EP01p1 and Clamp M81511-13-10A
Vdc
are
connected to power supply connector J1 and terminated as required in
the
aircraft.
Aircraft Configuration
(2) Vehicle .
(a) Place base into assigned area of vehicle for installation.
(b) Mark mounting surface through four holes in each resilient mount
(c) Remove base and drill holes to receive approved vehicle hardware.
(d) Remove four resilient mounts from baseplate.
(e) Secure four resilient mounts to vehicle mounting surface.
(f) Position baseplate over four resilient mounts and secure.
(g) Attach power supply to recorder (figure 1-1) and secure latches.
(h) Position recorder set on base and secure three latching clips, on
2-3