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Page Title: ENGINE/ROTOR RPM INDICATOR FRONT PANEL REMOVAL/INSTALLATION (AVIM) – continued
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ENGINE/ROTOR RPM INDICATOR FRONT PANEL REMOVAL/INSTALLATION  (AVIM)
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TM-1-1520-238-23-5 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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PILOT ENGINE  OIL  PRESSURE  INDICATOR  REMOVAL/INSTALLATION

TM 1-1520-238-23 8-18    8.5. ENGINE/ROTOR RPM INDICATOR FRONT PANEL REMOVAL/INSTALLATION  (AVIM) – continued 8.5.5.  Inspection a.   Check panel for dents, nicks, and cracks (para 8.1). b.   Check indicator for cracks (para 8.1). 8.5.6.  Installation CAUTION Do not exceed 24 INCH-OUNCES torque on bushings. a.   Install panel (1) on case (2). Torque four bush- ings (3) to 24 INCH-OUNCES. (1)   Lubricate  four  bushings  (3).  Use  lubricant (item 115, App F). (2)   Aline connector (4) and position panel (1) on case (2). Press to engage connector (4). (3)   Install  four  bushings  (3).  Torque  four  bush- ings  (3)  to  24  INCH-OUNCES.  Use  torque wrench and screwdriver bit. b.   Inspect (QA). END OF TASK 4 1 2 3 M04-2677-3

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