TM 55-1520-240-23-3
4-117
INSTALL GAS PRODUCER CONTROL LINKAGE ROD
4-117
INITIAL SETUP
Applicable Configurations:
Without 74
Tools:
Aircraft Maintenance Tool Kit, NSN 5180-00-323-4944
Torque Wrench, 30-150 Inch-Pounds
Measuring Tape
Materials:
Lockwire (E229)
Parts:
Cotter Pins
Personnel Required:
Aircraft Powerplant Repairer (2)
Inspector
References:
TM 55-1520-240-23P
NOTE
Procedure is same to install gas
producer control linkage rod on No. 1
or No. 2 engine. Installation of No. 1
rod is shown here.
1.
Measure distance between centers of holes
(1) in rod ends (2 and 3). If length is same as
dimension “A” found in removal, go to step 2. If
length is not same, do the following:
a.
Loosen nut (4).
b.
Rotate rod end (2) until distance between
centers of holes (1) in rod ends (2 and 3) is
same as dimension "A".
c.
Make sure rod ends (2 and 3) are aligned.
d.
Tighten nut (4).
NOTE
Nominal distance between centers of
holes in rod ends is 13.16 to 13.28
inches.
Do not lockwire nut at this time.
Change 1
4-409
