TM 1-1520-238-23
Change 8
7-159
7.42.
COLLECTIVE SERVOCYLINDER INSTALLATION – continued
y. Attach connector (L33)P227 (66) to receptacle
J227 (67).
z. Attach connector (L33)P417 (68) to receptacle
J417 (69).
CAUTION
Ensure lockwire does not pre-load plug
side of connector in either direction. En-
sure anti-chafe tubing is positioned so
that no chafing between lockwire and
connector bracket occurs.
aa. Lockwire connector P227 (68) to receptacle
J227 (69)
(1) Install safety wire with nonmetallic tubing
(anti–chafe), from the barrel of the connector
body P227 (68), over connector bracket
(69.1) to barrel of receptacle J227 (69). Use
wire (item 222, App F) and tubing
(item 213A, App F).
ab. Lockwire connector P417 (66) to receptacle
J417 (67)
(1) Install safety wire with nonmetallic tubing
(anti–chafe), from the barrel of the connector
body P417 (66), over connector bracket
(69.1) to barrel of receptacle J417 (67). Use
wire (item 222, App F) and tubing
(item 213A, App F).
ac. Inspect (QA).
ad. Bleed primary and utility hydraulic systems
(para 1.35).
ae. Service primary and utility hydraulic systems
(para 1.34).
af. Perform collective flight control rigging main-
tenance operational check (TM 1-1520-238-T).
ag. Perform No. 1 and No. 2 engine load demand
spindle (LDS) rigging check (para 4.184).
ah. Perform linear variable differential transducer
(LVDT) adjustment (para 11.216).
ai. Perform primary and utility hydraulic systems
maintenance
operational
checks
(TM 1-1520-238-T).
aj. Install access panel R200 and fairing T205R
(para 2.2).
END OF TASK
M04-795-16
66
67
68
69
M04-795-20A
66
67
68
69
69.1
