PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION continued

PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION continued - TM-1-1520-238-23-5_040

TORQUE, TGT, FUEL, AND NG INDICATORS LIGHT PANEL, DIGITAL DISPLAY DRIVER CIRCUIT CARD REPLACEMENT (AVIM)

TM-1-1520-238-23-5 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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TM 1-1520-238-23 8-27 8.9. PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR N_G RPM INDICATOR REMOVAL/INSTALLATION – continued 8.9.6. Installation a. Install indicator (1) in panel (2). (1) Attach connector P68 (TGT indicator)/P67 (N_G rpm indicator) (4) to receptacle (M4)J1 (TGT indicator)/(M3)J1 (N_G 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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