SUBTASK 72-35-00-428-114-G00
(2) Install the stage 5 connecting links as follows:
NOTE: This procedure is for installing the stage 5 connecting links.
NOTE: Each connecting link is stamped with the words FWD SIDE. This side must face
forward.
(a) Install the four sleeves through the back of each connecting link.
(b) Install the connecting link to the actuation ring upper or lower segment as follows:
1) Apply a layer of lubricant to the threads and washer faces of the bolts.
CAUTION
THE VANE ACTUATION PINS MUST NOT ENGAGE THE LIGHTENING
POCKETS OF THE CONNECTING LINKS. DAMAGE TO THE ENGINE
COULD OCCUR.
(c) Align the vane actuation arms with the sleeves in the connecting link. Connecting link
side stamped FWD SIDE must face forward.
(d) Attach the vane actuation ring upper and lower segments to the connecting link with the
four bolts.
(e) Tighten the bolts to 65-75 pound-inches (7.4-8.4 Nm) and lockwire.
(f) If no more work will be done at this time, do the task "Put the Airplane to its Usual
Condition".
END OF TASK
TASK 72-35-00-408-024-G00
17. Put the Airplane to its Usual Condition After VSV Repairs
A. References
Reference Title
71-11-04 P/B 201 FAN COWL PANELS - MAINTENANCE PRACTICES
(OPEN/CLOSE)
71-11-06 P/B 201 CORE COWL PANELS - MAINTENANCE PRACTICES
(OPENING/CLOSING)
75-31-02 P/B 501 VARIABLE STATOR VANE (VSV) ACTUATOR -
ADJUSTMENT/TEST
78-31-00 P/B 201 THRUST REVERSER SYSTEM - MAINTENANCE PRACTICES
B. Location Zones
Zone Area
410 Left Powerplant
420 Right Powerplant
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-35-00
NoC
Page 862
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
ABX 001-007, 011, 012, 016-019, 021, 022, 025, 101,
109, 114, 115, 314-999
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