NO. 1 ENGINE OIL PRESS INDICATOR DOES NOT INDICATE 20 PSI MINIMUM OR POINTER FLUCTUATES MORE THAN 5 PSI

N O . 1 E N G I N E O I L P R E S S I N D I C A T O R D O E S N OT I N D I C A T E 2 0 P S I M I N I M U M O R P O I N T E R F L U C T U A T ES M O R E T H A N 5 P S I ( C o n t i n u e d)\

NO. 1 ENGINE OIL PRESS INDICATOR DOES NOT INDICATE 20 PSI MINIMUM OR POINTER FLUCTUATES MORE THAN 5 PSI (Continued)

TM-55-1520-240-T-2 CH-47D Heilcopter Manual
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TM 55-1520-240-T 8-3.6.1 NO. 1 ENGINE OIL PRESS INDICATOR DOES NOT INDICATE 20 PSI MINIMUM OR POINTER FLUCTUATES MORE THAN 5 PSI 8-3.6.1 FAULT ISOLATION PROCEDURE Materials: INITIAL SETUP None Applicable Configurations: Personnel Required: Aircraft Electrician With 74 Medium Helicopter Repairer Tools: References: Aircraft Mechanic's Tool Kit, TM 55-1520-240-23 NSN 5180-00-323-4692 TM 1-2840-265-23 Electrical Repairer's Tool Kit, NSN 5180-00-323-4915 Equipment Condition: Multimeter TM 55-1520-240-23: Synchro Test Set, Battery Connected NSN 4920-00-556-8108 Electrical Power On Direct Reading Pressure Gage, 0 to 200 Psi Hydraulic Power Off GO TO NEXT PAGE 8-54.2 Change 19

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