4-8.5 DECU CODE F AFTER POWER ASSURANCE TEST

4-8.6 FADEC TOGGLES BETWEEN PRIMARY AND REVERSIONARY MODE

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
Page Navigation
383

TM 55-1520-240-T 4-8.5 DECU CODE F AFTER POWER ASSURANCE TEST 4-8.5 FAULT ISOLATION PROCEDURE INITIAL SETUP Personnel Required: Applicable Configurations: Aircraft Electrician With74 References: TM 55-1520-240-23 Tools: Electrical Repairer's Tool Kit, Equipment Condition: NSN 5180-00-323-4915 TM 55-1520-240-23: Battery Disconnected Materials: Electrical Power Off None Hydraulic Power Off NOTE: · Information in ( ) applies to DECU NO. 2. · Use wiring diagram in Task 4-12.2. END OF TASK Change 17 4-203

Privacy Statement
Press Release
Contact