4-3.3 ENGINE LOW OIL LEVEL WARNING SYSTEM OPERATIONAL CHECK

4-3.2 ENGINE LOW OIL LEVEL WARNING SYSTEM VISUAL CHECK

ENGINE LOW OIL LEVEL WARNING SYSTEM OPERATIONAL CHECK (Continued) - TM-55-1520-240-T-1_269

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
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TM 55-1520-240-T 4-3.3 ENGINE LOW OIL LEVEL WARNING SYSTEM OPERATIONAL CHECK 4-3.3 INITIAL SETUP Equipment Condition: Applicable Configurations: TM 55-1520-240-23: Without 74 Battery Connected Tools: Electrical Power On None Hydraulic Power Off Materials: No. 1 Engine Upper and Lower Access Doors Open None No. 1 Engine Work Platform Open No. 2 Engine Upper and Lower Access Doors Open Personnel Required: No. 2 Engine Work Platform Open Aircraft Electrician (2) Visual Check of Engine Low Oil Level Warning Sys- References: tem Performed (Task 4-3.2) TM 55-1520-240-23 GO TO NEXT PAGE 4-46 Change 17

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