TCH.1C-27J-2-27JG
AGE
No.
NOMENCLATURE
P/N
00181 Kit, flight controls rigging
pins
11G001-C052200-801
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00069 NUT, SELF-LOCKING MS21043-3
1,00
00204 NUT, SELF-LOCK
NAS1726-3E
1,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-81.1 REMOVAL. Proceed as follows:
A.Forward quadrant doweling.
B.Gain access to panels 130B and 130C and insert
the rigging pin on the forward flap quadrant.
C.Unscrew the bolt fixing the Flap Clevis to Flap
Lever Assy and collect the washers and the nut.
D.Remove the wire locking and unscrew the flap
clevis.
E.Take note the measure of flap cable assy thread,
outside to flap slidingend assy.
F.Unscrew the flap slidingend assy from flap cable
assy.
G.Extract and remove the flap slidingend assy from
flap cable assy.
H.Remove the wire locking that fix the flap swivelend
nut and the casing nut on the bottom of the flap
swivelend assy.
(Cont'd)
27-50-45
2-601