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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		Up
TM-1-1520-238-23-5 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual		Next
PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION – continued

TM 1-1520-238-23 8-26    8.9. PILOT ENGINE TURBINE GAS TEMPERATURE (TGT) INDICATOR AND ENGINE GAS GENERATOR NG RPM INDICATOR REMOVAL/INSTALLATION – continued d.   Remove  engine  turbine  gas  temperature (TGT) or engine gas generator (NG rpm) indi- cator (1) from instrument panel (2). (1)   Remove four screws (3). (2)   Pull indicator (1) from panel (2). (3)   Detach  connector  P68  (TGT  indicator)/P67 (NG rpm indicator) (4) from receptacle (M4)J1 (TGT  indicator)/(M3)J1  (NG  rpm  indicator) (5). 8.9.4.  Cleaning a.   Wipe mounting area and indicator with a clean rag. 8.9.5.  Inspection a.   Check indicator and panel mounting area for cracks (para  8.1). b.   Check indicator and panel mounting area for dents and nicks (para  8.1). c.   Check panel screw holes for stripped or dam- aged threads (para  8.1). GO TO NEXT PAGE 1 3 2 M04-143-3 2 4 M04-143-4 5 1

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