4-6.23 NO. 2 ENGINE FUEL CONTROL POINTER NOT BETWEEN 130 AND 21 ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK

NO. 1 ENGINE FUEL CONTROL POINTER NOT BETWEEN 4-6.22 13 AND 210 ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK (Continued)

NO. 2 ENGINE FUEL CONTROL POINTER NOT BETWEEN 13 AND 21 ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK (Continued)

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
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TM 55-1 520-240-T 4-6.23 NO. 2 ENGINE FUEL CONTROL POINTER NOT BETWEEN 130 AND 21° ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK 4-6.23 FAULT ISOLATION PROCEDURE Personnel Required: INITIAL SETUP Aircraft Electrician (2) Applicable Configurations: References: Without 74 TM 55-1520-240-23 Tools: Equipment Condition: Electrical Repairer's Tool Kit, TM 55-1520240-23: NSN 5180-00-323-4915 Battery Connected Multimeter Electrical Power On Materials: Hydraulic Power Off None GO TO NEXT PAGE 4-176.2 Change 17

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