A number of external loads varying in weight (up to 4,000 pounds), size, and aerodynamic characteristics were lifted, flown, and released using the UH-1D Helicopter equipped with the standard cargo hook and the Universal Cargo Hook. All loads were released using the electrical release switches and then the manual cargo release pedals. Selected loads of various sizes and weights were released free-fall using the electrical released switches and then the manual cargo release pedals. Damage to, or problems encountered with, the standard cargo hook or the Universal Cargo Hook were recorded and reported. The time to effect cargo hookup, the difficulty of operation, and malfunctions were recorded for each load. Data were compiled on a comparative basis. (Author)
Service Test and Universal Helicopter Cargo Hook, 6,000-Pound Capacity
1966
10 pages
Report
Keine Angabe
Englisch
Aircraft , Joining , Logistics Military Facilities & Supplies , Hooks , Cargo handling , Helicopters , Loading(Handling) , Weight , Aerodynamic characteristics , Release mechanisms , Electric switches , Manual operation , Free fall , Feasibility studies , Locking(Mechanics) , Reliability , Ground crews , Flight testing , Hovering , Takeoff , Climbing , UH-1D Aircraft , Universal cargo hook , H-1 aircraft
Service Test of Helicopter Cargo Hook
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