TCH.1C-27J-2-27JG
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00010 PIN, COTTER
MS24665-155
1,00
00017 PIN, COTTER
MS24665-134
1,00
00025 NUT, SELF-LOCKING MS21043-4
8,00
00052 PIN, COTTER
MS24665-153
2,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-65.1 REMOVAL. Proceed as follows:
A.Lock the elevator rear axles in the neutral Position.
B.Remove the elctrical connector from the center of
J.O.M.
C.Screw the bolts from the connection rods (One for
L rod and one for R rod).
D.Disconnect the two rods from the extremity of the
J.O.M.
E.Unscrew 16 bolts that fix J.O.M. with aircraft
structure (4 on R connection, 4 on L connection, 4
onR intermediate connection and 4 on L
intermediate connection).
F.Remove the J.O.M.
2-65.2 INSTALLATION. Proceed as follows:
A.Ensure that the L and R rear quadrants are to
neutral position (rigging pins inserted).
B.Install the J.O.M. assy on the support structure and
lock it in neutral position with the proper rigging pin
dia 7.95 mm.
(Cont'd)
27-30-50
2-496