TCH.1C-27J-2-27JG
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00054 Kit, torque wrenches
G0001200001-001**
00074 Kit, aircraft assy platform
G0005100001
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00052 PIN, COTTER
MS24665-153
2,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
)
1.Gain access through hatch 553A, 553B and 553C.
2.Disconnect the Flanged Rigid Shaft (3) between the
Flap Arrester Unit and the Screwjack No 4 (15),
unscrewing the two screws (11 and 12) from the Flap
Flanged Rigid Shaft.
NOTE
Take cure do not rotate the part of the flap
Flanged Rigid Shaft (13) connected to the
Screwjack No 4 (15) to prevent
misalignment of flap control surfaces.
3.Remove the cotter pins (6 and 8) and discard them,
remove and retain the castellated nuts (7 and 9), the
plain washers (5 and 10)and the bolts (4) that connect
the Flap Arrester Unit (2) to the support (14) on the
rear spar.
4.Remove the Flap Arrester Unit from the support (14).
27-50-35
2-590