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Page Title: PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION – continu...
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PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION – continued		Up
TM-1-1520-238-23-5 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual		Next
TORQUE, TGT, FUEL, AND NG INDICATORS LIGHT PANEL, DIGITAL DISPLAY DRIVER CIRCUIT CARD REPLACEMENT (AVIM)

TM 1-1520-238-23                   8-27 8.9. PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION – continued 8.9.6.  Installation a.   Install indicator (1) in panel (2). (1)   Attach  connector  P68  (TGT  indicator)/P67 (NG  rpm  indicator)  (4)  to  receptacle  (M4)J1 (TGT  indicator)/(M3)J1  (NG  rpm  indicator) (5). (2)   Aline indicator (1) with screw holes in panel (2). (3)   Install four screws (3). b.   Inspect (QA). c.   Perform  engine  instrument  maintenance  op- erational check (TM 1-1520-238-T). END OF TASK 2 4 M04-143-5 5 1 1 3 M04-143-6 2

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