TCH.1C-27J-2-27JG
2-19
LH AILERON QUADRANT (AILERON PULLEY) -
REMOVAL AND INSTALLATION
INPUT CONDITION:
Aircraft Applicability:
04162, 04180
Required Conditions:
1.Disconnect electrical power from aircraft (refer to
).
2.Isolate hydraulic power (refer to manual
3.Position maintenance platform (AGE NO. 00074).
4.Lock in neutral Position the control wheel (2), the
quadrants (3), and outer wing pulley (5) by insertion of
rigging pins (AGE NO. 00181) (1, 4 and 6) (refer to
figure
5.Open the access panels 553A, 553B and 553C.
Recomended Personnel:
PROCEDURE
MECH.
CODE
QTY
TOTAL TIME
(MIN.)
WORK
ZONE
Input Condition
AFM
2
150,00
Periodicity: AR - AS REQUIRED
Total Maintenance Time: 300 (Min.)
Total Time Detention System:
150 (Min.)
AGE Required:
AGE
No.
NOMENCLATURE
P/N
00074
Kit, aircraft assy platform
G0005100001
00181
Kit, flight controls rigging
pins
11G001-C052200-801
27-10-15
2-150