No fatalities

31 Dec 2019: Enstrom F28 A (N57SJ) — Danbury, TX

Danbury, TX, United States

On 31 Dec 2019, an Enstrom F28 A (registration N57SJ) was involved in an aviation accident near Danbury, TX. No fatalities were reported. Investigators recorded the probable cause as: The failure of the engine's No.3 intake valve resulting is a loss of engine power and a rollover following the autorotation to soft ground. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On December 31, 2019, an Enstrom F28A helicopter, N57SJ, nosed over during a forced landing after a partial loss of engine power near Danbury, Texas. The student pilot and flight instructor were not injured.

Accident Details

On December 31, 2019, at approximately 1415 central standard time, an Enstrom F28A helicopter, registration N57SJ, sustained substantial damage when it nosed over during a forced landing following a partial loss of engine power. The nose-over resulted in separation of the tailboom and damage to the main rotor system and fuselage. The helicopter was being used for an instructional flight under Title 14 Code of Federal Regulations Part 91, operated by a private individual. Visual meteorological conditions prevailed, and the flight was not operated on a flight plan. The local flight originated from Salaika Aviation Airport (07TA) in Danbury, Texas, at an unconfirmed time.

Flight History

The certificated flight instructor reported that he and his student had departed for a second pattern during a training mission. After the helicopter turned onto the crosswind leg of the traffic pattern, the engine suddenly began to run rough and lost significant power. The instructor took control and executed an autorotation into a clearing. After flaring and touching down, the helicopter's skids sank into soft mud, the rotor blades contacted the ground, and the helicopter rolled onto its side. Both the student pilot and flight instructor were not injured.

Post-Accident Examination

Following the accident, an examination of the engine revealed that a portion of the intake valve for the No. 3 cylinder had broken off and migrated into the No. 1 cylinder. There, it became lodged between the No. 1 intake valve and its seat, holding that valve in the open position, which contributed to the partial loss of engine power. The operator reported this finding.

Contributing factors

Causes

Recip engine power section — Failure

Other contributing factors

Contributed to outcome