Enstrom 280C accident near Quakertown, PA

On October 6, 1995, an Enstrom 280C (helicopter) was involved in an accident near Quakertown, PA. 2 people died. Damage to the aircraft: destroyed.

Date
October 6, 1995
Place
Quakertown, PA
Aircraft
Enstrom 280C · Helicopter
Injuries
2 fatal, 0 serious, 0 minor
Damage
Destroyed
Position
40.431°N, 75.339°W
NTSB ID
20001207X04764

Official records · NYC96FA003

NTSB summary

HISTORY OF FLIGHT On October 6, 1995, at 1720 eastern daylight time, an Enstrom 280C, a helicopter, N976BT, was destroyed during a forced landing near Quakertown, Pennsylvania. The private pilot and passenger were fatally injured. Visual meteorological conditions prevailed for the personal flight that originated at Quakertown Airport (UKT), at 1715. No flight plan had been filed for the flight conducted under 14 CFR Part 91. Witnesses stated the pilot/owner offered to fly a friend in the local area. The helicopter departed UKT, and circled the airport 2 to 3 times at an altitude of 200 to 300 feet above the ground. A pilot who witnessed the accident stated: ...I observed the gold helicopter turning north over the hanger area at the south end of the field, at approximately 200 feet altitude...I heard three (3) sharp "pops," as if the engine was backfiring through the carburetor. The helicopter appeared to be at approximately 300 feet of altitude when the engine then quit, the rotor slowed immediately and the blades coned upward. The helicopter lost altitude rapidly and disappeared from view... An airplane mechanic who also witnessed the accident stated: ...I first saw the helicopter just after it had taken off from UKT...It was operating normally, a high power setting, a high airspeed, but at a low altitude about 200 to 300 feet AGL...about 1 1/2 or 2 minutes later... I heard a popping sound like an engine backfiring and saw small puffs of black smoke behind the aircraft. The engine sound dropped to a low RPM, but was still running. The aircraft fish tailed for a moment, and

Probable cause

improper installation of the magneto by maintenance personnel, which resulted in the loss of ignition and the loss of engine power. A factor relating to the accident was: the lack of suitable terrain for an emergency landing.

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