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PILOTS ROTOR TACHOMETER DOES NOT INDICATE 98 TO 101 PERCENT WHEN ROTOR TACH 8-15.9 CIRCUIT BREAKER OPENED
ENGINE FUEL FLOW INDICATING SYSTEM VISUAL CHECK
TM-55-1520-240-T-2 CH-47D Heilcopter Manual
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TM 55-1520-240-T
8-16 ENGINE FUEL FLOW INDICATING SYSTEM
8 - 16
8-16.1 ENGINE FUEL FLOW INDICATING SYSTEM WIRING DIAGRAM
8-16.1
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