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PILOT DIRECTIONAL CONTROL POSITION LINEAR VARIABLE DIFFERENTIAL TRANSDUCER (LVDT) REMOVAL – continued | Up
TM-1-1520-238-23-7-2 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual | Next
PILOT DIRECTIONAL CONTROL POSITION LINEAR VARIABLE DIFFERENTIAL TRANSDUCER (LVDT) INSTALLATION – continued |
TM 1-1520-238-23
11-913
11.211.
PILOT DIRECTIONAL CONTROL POSITION LINEAR VARIABLE DIFFERENTIAL TRANSDUCER
(LVDT) INSTALLATION
11.211.1. Description
This task covers:
Installation.
11.211.2. Initial Setup
Tools:
Aircraft mechanic’s tool kit (item 376, App H)
Electrical tool kit (item 378, App H)
0 - 30 inch-pound 1/4-inch drive dial indicator torque
wrench (item 445, App H)
Materials/Parts:
Cotter pin
Wire (item 222, App F)
Personnel Required:
67R
Attack Helicopter Repairer
68X
Armament/Electrical System Repairer
67R3F
Attack Helicopter Repairer/Technical
Inspector
References:
TM 1-1520-238-T
TM 9-1090-208-23
TM 55-1500-323-24
Equipment Conditions:
Ref
Condition
1.57
Helicopter safed
11.211.3. Installation
WARNING
Installation of an LVDT that has not
been EMI hardened in a BUCS-
equipped aircraft may result in un-
commanded flight control movement.
This may cause loss of aircraft.
CAUTION
To prevent FOD from attaching and stick-
ing to the shaft, do not remove the posi-
tion shaft from the LVDT body during
installation.
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M04-1860-1
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