Information on U.S. Army helicopter UH-1D tail number 66-16084
The Army purchased this helicopter 0267
Total flight hours at this point: 00000563
Date: 08/12/1967
Accident case number: 670812041 Total loss or fatality Accident
Unit: 79 TC CO
Number killed in accident = 0 . . Injured = 0 . . Passengers = 0
costing 228554
Source(s) from which the incident was created or updated: Army Aviation Safety Center database.
Crew Members:
AC W1 HEILMAN WH
P W1 BUCKLEY JL
CE E4 MIYAMOTO GY
G E6 KING JW
Accident Summary:
The aircraft was on final to an LZ in a steep descent when loss of RPM occurred. At approximately 200 feet, the aircraft commander tried to regain RPM by lowering the pitch. The aircraft landed hard and recovered to a hover. It was then flown out of the pickup zone.
War Story:
Although this helicopter was written off as the result of this incident, it was later rebuilt and returned to service
Information on U.S. Army helicopter UH-1D tail number 66-16084
The Army purchased this helicopter 0267
Total flight hours at this point: 00000814
Date: 07/15/1968
Accident case number: 680715181 Total loss or fatality Accident
Unit: 121 AHC
The station for this helicopter was Soc Trang in South Vietnam
Number killed in accident = 0 . . Injured = 3 . . Passengers = 0
costing 228554
Original source(s) and document(s) from which the incident was created or updated: Defense Intelligence Agency Helicopter Loss database. Army Aviation Safety Center database. Also: OPERA (Operations Report. )
Loss to Inventory
Crew Members:
AC W1 KENDIG LD
P W1 ROE RG
CE E4 HORROCKS JT
G E4 WEBB FL
Accident Summary:
WO Kendig was given the resupply mission and decided to refuel at Chi Lang airfield, as his aircraft was being loaded with the supplies. The aircraft was loaded with approximately 900 lbs of cargo and WO Kendig instructed the gunner to limit the fuel load to 900 pounds. A four foot hover check was made before the departure and the engine tach remained at 6600 RPM. The crew chief states that the engine was pulling about 37 lbs of torque during the hover check. Departing Chi Lang airfield, WO Kendig contacted Viking 21, the fire team lead, for landing instructions. Radio contact was also established with the ground unit and the LZ was marked with smoke grenades. Viking 21 advised Tiger 084 that the area was secure and that he could utilize any approach route that he desired. WO Roe, the pilot of Tiger 084, was flying at this time and made the approach directly into the wind. Terminated at a high hover, approximately 15 to 20 feet above the ground. The landing zone was unprepared and was characterized by broken trees, stumps, large rocks, and bomb craters. WO Kendig anticipated the poor condition of the LZ and had briefed the crew to unload the cargo from a hover if necessary. The helicopter stabilized at a hover momentarily and the crew chief informed Mr. Roe that he should hover to the right to avoid a blade strike with the surrounding trees. The area immediately to their right was a large bomb crater, approximately 25 feet in diameter and 10 feet deep. As the pilot hovered and was positioned over the crater the ship yawed to the right and started losing RPM. WO Kendig took the controls at this time and instructed the crew to start kicking off the cargo. They failed to respond immediately, as they were both checking the aircraft's clearance and advising the pilot to "pick the chopper up". Mr. Kendig stated that he first lowered the collective slightly, attempting to regain the lost RPM, but the aircraft continued to settle and the RPM dropped to 5600. He decided that his only alternative was to make a right pedal turn and attempt a takeoff down the mountain. During the turn, the main rotor struck a tree branch, and the tail rotor also struck an obstacle. Directional control was lost and the helicopter continued to turn another 180 degrees. When the aircraft hit the ground the left skid broke and the helicopter rolled on its left side. The main rotor blade was severed as it struck the ground and the whole left side of the aircraft received major damage. The crew was evacuated from the crash site and the aircraft was recovered by a Chinook later in the day
This record was last updated on 04/16/1997
The following is Goldbook information on US Army helicopter UH-1D tail number 66-16084
It is provided here as an ESTIMATE of the history of this helicopter and is not intended to be the final authority.
This helicopter was purchased by the US Army in 0267.
Please provide any additional information on this helicopter to the VHPA.
DATE FLT HRS UIC UNIT AREA POST COUNTRY 6702 0 0 W0Y6AA TRAN MDMHELCO S ALASKA ALASKA 6703 0 0 W0MHAA DIROF SUP TRAN 6TH ARMY SHARPE GD AVCOM 6704 66 66 WC3JAA 129 ASLT HEL CO VIETNAM RVN 6705 120 186 WC3JAA 129 ASLT HEL CO VIETNAM RVN 6706 165 351 WC3JAA 129 ASLT HEL CO VIETNAM RVN 6707 152 503 WC3JAA 129 ASLT HEL CO VIETNAM RVN 6708 60 563 WCLNAA 79 TRANS CO VIETNAM RVN 6709 0 563 WCLNAA 79 TRANS CO VIETNAM RVN 6710 0 563 WCLNAA 79 TRANS CO VIETNAM RVN 6711 0 563 WCLNAA 79 TRANS CO VIETNAM RVN 6712 0 563 WCLNAA 79 TRANS CO VIETNAM RVN 6801 18 581 WCLNAA 79 TRANS CO VIETNAM RVN 6802 60 641 3412 355 AVN CO 4TH ARMY FORT SILL 4TH ARMY 6803 35 676 WFJGAA 282 ASLT HEL CO VIETNAM RVN 6804 0 676 WFJGAA 282 ASLT HEL CO VIETNAM RVN 6805 99 775 WFJGAA 282 ASLT HEL CO VIETNAM RVN 6806 39 814 3409 355 AVN CO 4TH ARMY FORT SILL 4TH ARMY