WINDSHIELD ANTI-ICING SYSTEM OPERATIONAL CHECK

WINDSHIELD ANTI-ICING SYSTEM VISUAL CHECK

WINDSHIELD ANTI-ICING SYSTEM OPERATIONAL CHECK (Continued)

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM 55-1520-240-T 12-1.3 WINDSHIELD ANTI-ICING SYSTEM OPERATIONAL CHECK 12-1.3 INITIAL SETUP Applicable Configurations: All Tools: None Materials: None Personnel Required: 68F20 Aircraft Electrician References: TM 55-1520-240-23 Equipment Condition: TM 55-1520-240-23: Battery Connected Electrical Power On Hydraulic Power Off Visual Check of Windshield Anti-Icing System Performed (Task 12-1.2) Outside Air Temperature Below 70° F (20°C) or Windshields Cooled With Water Hose. 12-4 GO TO NEXT PAGE

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