Kaman HH-43F accident near Phoenix, AZ

On September 25, 1999, a Kaman HH-43F (helicopter) was involved in an accident near Phoenix, AZ. 2 people died. Damage to the aircraft: destroyed.

Date
September 25, 1999
Place
Phoenix, AZ
Aircraft
Kaman HH-43F · Helicopter
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
33.679°N, 112.090°W
NTSB ID
20001212X19794

NTSB summary

HISTORY OF FLIGHT On September 25, 1999, about 0642 hours mountain standard time, a Kaman HH-43F helicopter, N100PL, was destroyed when it collided with terrain at Phoenix, Arizona. The commercial rated pilot and crewman were both fatally injured. Moseley Aviation, Inc, d.b.a. Pro-Lift Helicopters, Litchfield Park, Arizona, was operating the positioning flight under the provisions of 14 CFR Part 91. Visual meteorological conditions prevailed and a company flight plan was filed. The flight originated about 0620 from an off-airport location at the west end of Phoenix. The operator obtained prior approval from the Federal Aviation Administration (FAA) to lift 58 air conditioning units onto two co-located buildings under 14 CFR Part 133, using the "Restricted" category helicopter. They also obtained approval to operate within a congested area. The route of flight was to be over washes and the canal. The operation was to be monitored by FAA inspector's on-scene. The pilot contacted the Phoenix-Deer Valley Municipal Airport control tower (ATCT) en route for permission to transition through their airspace west-to-east on the north side. The request was approved. About 20 minutes later, the tower was advised of the accident about 4 miles northwest of the airport. The helicopter was observed on the ATCT D-Brite radar level about 1,700 feet mean sea level (msl), and had traveled about 10 miles in 7 minutes. The accident site elevation is 1,450 feet msl. According to witnesses in the accident area, the helicopter exploded, or disintegrated in-flight over the Central Arizona Project (C

Probable cause

Failure of the horizontal stabilizer left outboard forward attach point because of a previously existing crack that resulted from inadequate maintenance inspection by the operator. A factor was the use of automotive parts.

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