TM 55-2840-231-23
7-2.
Auto-Reignition Control - Removal and Installation - Continued
ENGINE/Auto-
If the control is not mounted
Reignition Control -
on vibration dampers, remove
Continued
four bolts (4) and washers
(3) and remove control (2)
from its mounting bracket.
If control is mounted on vi-
bration dampers, remove
four nuts (9) and washers
(8) and remove control (2)
from its mounting bracket.
The four washers (6) and
vibration dampers (7) on
the bottom of the mounting
bracket may come off with
the control. If they remain
on bolts (5) but are loose,
remove them.
ENGINE/
6877187 Auto-
Reignition Control
2. Installation
If a new auto-reignition
control (2) is being installed,
remove the four nuts from
the bottom of the control
and install them on the bot-
tom of the removed control.
secure the control to its
mounting bracket on the
engine with four washers
(3) and bolts (4). Insure
that the Pc pressure port
is toward the front of the
engine. Tighten the bolts
to 35-40 in. lb (0.4-0.5
kg/m).
Connect auto-reignition
sensing tube (1) to control
(2). Tighten the coupling
nut to 80-120 in. lb (0.9-
1.4 kg/m).
Connect the aircraft elec-
trical harness to the elec-
trical connector on control
(2).
7-3
