VIBRATION CORRECTION PROCEDURE (AVIATION VIBRATION ANALYZER)

INSTALL RIGHT ENGINE TRANSMISSION OIL COOLER (Continued)

VIBRATION CORRECTION PROCEDURE (AVIATION VIBRATION ANALYZER) (Continued) - TM-55-1520-240-23-5_731

TM-55-1520-240-23-5 CH-47D Heilcopter Manual
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TM 55-1520-240-23-5 6-217 VIBRATION CORRECTION PROCEDURE (AVIATION VIBRATION ANALYZER) 6-217 INITIAL SETUP Applicable Configurations: All Tools: Aircraft Mechanics Tool Kit, NSN 5180-00-323-4692 Torque Wrench, 30-150 Inch-Pounds Torque Wrench, 150-750 Inch-Pounds Materials: Marking Pencil (E270.1) Oil (E254) Grease (E190) Dry Cleaning Solvent (E162) Cloth, Cleaning (E120) Gloves (E184.1) Goggles (E473) Personnel Required: CH-47 Helicopter Repairer Inspector Rotary Wing Aviators (2) References: Task 1-89 Tasks 6-2 thru 6-6 Tasks 6-8 thru 6-10 Tasks 6-12 thru 6-19 Task 6-30 Task 6-30.2 Task 6-30.3 Task 6-32 Task 6-182 Task 6-186 TM 1-6625-724-13&P TM 1-1520-240-10 Equipment Condition: Battery Disconnected (Task 1-39) Electrical Power Off Hydraulic Power Off Pylon Hinged Fairing Open (Task 2-2) Pylon Lower Fairing Open (Task 2-2) Engine Drive Shaft Access Covers Removed (Task 2-2) Engine Air Inlet Screens Removed (Task 4-65) Engine Transmission Fairing Access Covers Open (Task 2-2) NOTE For vibration analysis setup procedures with the AVA go to TM 1-6625-724-13&P. 6-708 Change 1

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