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Page Title: PILOT/CPG ENGINE INSTRUMENT DIM/TEST CONTROL PANEL REMOVAL/INSTALLATION – continued
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PILOT/CPG ENGINE INSTRUMENT DIM/TEST CONTROL PANEL REMOVAL/INSTALLATION
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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/CPG ENGINE INSTRUMENT DIM/TEST CONTROL PANEL DISASSEMBLY/ASSEMBLY (AVIM

TM 1-1520-238-23                   8-59 8.22. PILOT/CPG ENGINE INSTRUMENT DIM/TEST CONTROL PANEL REMOVAL/INSTALLATION – continued d.   Remove DIM/TEST control panel (1) from in- strument panel (2). (1)   Remove two screws (3). (2)   Pull panel (1) from panel (2). (3)   Detach connector P787 (pilot)/P1092 (CPG) (4) from receptacle (A114)J1 (pilot)/(A517)J1 (CPG) (5). 8.22.4.  Cleaning a.   Wipe mounting areas and control panel with a clean rag. 8.22.5.  Inspection a.   Check  DIM/TEST  control  panel  and  instru- ment panel mounting areas for cracks, nicks, and dents. None allowed. b.   Check instrument panel nutplates for stripped or  damaged  threads.  Acceptable  thread  dam- age cannot exceed 50 percent of one thread. 8.22.6.  Installation a.   Install panel (1) in panel (2). (1)   Attach  connector  P787  (pilot)/P1092  (CPG) (4)  to  receptacle  (A114)J1  (pilot)/(A517)J1 (CPG) (5). (2)   Aline panel (1) and panel (2) screw holes. (3)   Install two screws (3). b.   Inspect (QA). c.   Perform engine instruments maintenance op- erational check (TM 1-1520-238-T). END OF TASK 4 5 1 3 M04-161-4 2 4 5 3 M04-161-6 M04-161-5 2 3 1

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