background image
TCH.1C-27J-2-27JG
AGE
No.
NOMENCLATURE
P/N
00181 Kit, flight controls rigging
pins
11G001-C052200-801
00263 Test stand, hydraulic system
(electric engine)
846805-E**
Consumable Material Required:
LCM
No.
NOMENCLATURE
P/N
QTY
00010 PIN, COTTER
MS24665-155
1,00
00016 LOCK WIRE
MS20995C32
AR
00017 PIN, COTTER
MS24665-134
2,00
00022 PIN, COTTER
MS24665-86
1,00
00052 PIN, COTTER
MS24665-153
2,00
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para 
1-3
) before performing
maintenance.
PROCEDURE:
2-47.1 ADJUSTMENT OF ELEVATOR NEUTRAL
POSITION (refer to figure 
1-52, sheet 1/6
) , (refer
to figure 
1-52, sheet 2/6
) , (refer to figure 
1-52,
sheet 3/6
) and (refer to figure 
1-52, sheet 4/6
)
1.Install the template (AGE NO. 00065) on LH (RH)
elevator trailing edge.
2.Insert a rigging pin 0.193 in (4.915 mm) (1 and 3)
(AGE NO. 00181) in the LH (RH) rear quadrants (2
and 4).
(Cont'd)
27-30-10
2-364