• Home
  • Download PDF
  • Order CD-ROM
  • Order in Print
NO. 2 ENGINE FUEL CONTROL POINTER DOES NOT MOVE 4-6.21 WHEN EMERGENCY ENGINE TRIM 2 SWITCH SET TO DEC. (Continued)
NO. 1 ENGINE FUEL CONTROL POINTER NOT BETWEEN 4-6.22 13 AND 210 ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK (Continued)

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
Page Navigation
  351    352    353    354    355  356  357    358    359    360    361  
TM 55-1 520-240-T 4-6.22  NO. 1 ENGINE FUEL CONTROL POINTER NOT BETWEEN 13° AND 210 ON PROTRACTOR AT BEGINNING OF OPERATIONAL CHECK 4-6.22 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 55-152024023: NSN 5180-00-323-4915 Battery Connected Multimeter Electrical Power On Hydraulic Power Off Materials: None GO TO NEXT PAGE 4-176  Change 17







Western Governors University

Privacy Statement
Press Release
Contact

© Copyright Integrated Publishing, Inc.. All Rights Reserved. Design by Strategico.