Saturday, January 04, 2020

Loss of Engine Power (Partial) : Enstrom F-28A, N57SJ; accident occurred December 31, 2019 in Danbury, Brazoria County, Texas

The National Transportation Safety Board did not travel to the scene of this accident.

Additional Participating Entity:

Federal Aviation Administration / Flight Standards District Office; Houston, Texas

Investigation Docket - National Transportation Safety Board:
https://app.ntsb.gov/pdf

https://registry.faa.gov/N57SJ


Location: Danbury, Texas
Accident Number: CEN20LA051
Date & Time: December 31, 2019, 13:30 Local 
Registration: N57SJ
Aircraft: Enstrom F28 
Aircraft Damage: Substantial
Defining Event: Loss of engine power (partial) 
Injuries: 2 None
Flight Conducted Under: Part 91: General aviation - Instructional

Factual Information

On December 31, 2019, about 1415 central standard time, an Enstrom F28A helicopter, N57SJ, sustained substantial damage when it nosed over during a forced landing following a partial loss of engine power. During the nose-over, the tailboom was separated and the main rotor system and fuselage were damaged. The student pilot and flight instructor were not injured. The helicopter was registered to and operated by a private individual under the provisions of Title 14 Code of federal Regulations Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from the Salaika Aviation Airport (07TA), Danbury, Texas, at an unconfirmed time.

The certificated flight instructor stated that he and his student had departed for a second pattern during a training mission. After the helicopter made the turn onto the crosswind leg of the traffic pattern the engine suddenly began to run rough and had lost a lot of power. He took the controls and executed an autorotation into a clearing, flared and touched down. The skids of the helicopter sunk into the soft mud, the rotor blades contacted the ground, and the helicopter rolled onto its side.

The operator reported that examination of the engine after the accident revealed that a portion of the intake valve for the No. 3 cylinder had broken off and had migrated into the No. 1 cylinder where it lodged between the No. 1 intake valve and seat, holding that valve in the open position.

Pilot Information

Certificate: Commercial; Flight instructor 
Age: 37,Male
Airplane Rating(s): Single-engine land 
Seat Occupied: Right
Other Aircraft Rating(s): Helicopter
Restraint Used: Lap only
Instrument Rating(s): None 
Second Pilot Present: Yes
Instructor Rating(s): Helicopter 
Toxicology Performed: No
Medical Certification: Class 2 Without waivers/limitations
Last FAA Medical Exam: April 5, 2019
Occupational Pilot: Yes
Last Flight Review or Equivalent: August 23, 2018
Flight Time: 4902 hours (Total, all aircraft), 4000 hours (Total, this make and model), 4700 hours (Pilot In Command, all aircraft), 122 hours (Last 90 days, all aircraft), 36 hours (Last 30 days, all aircraft), 2 hours (Last 24 hours, all aircraft)

Aircraft and Owner/Operator Information

Aircraft Make: Enstrom
Registration: N57SJ
Model/Series: F28 A 
Aircraft Category: Helicopter
Year of Manufacture: 1975
Amateur Built: No
Airworthiness Certificate: Normal 
Serial Number: 278
Landing Gear Type: Skid
Seats: 3
Date/Type of Last Inspection: September 4, 2019 Annual
Certified Max Gross Wt.: 2150 lbs
Time Since Last Inspection: 
Engines: 1 Reciprocating
Airframe Total Time: 3632 Hrs at time of accident
Engine Manufacturer: Lycoming
ELT: Not installed 
Engine Model/Series: HIO-360-C1A
Registered Owner:
Rated Power: 205 Horsepower
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site: Visual (VMC)
Condition of Light: Day
Observation Facility, Elevation: LBX,25 ft msl
Distance from Accident Site:
Observation Time: 19:53 Local
Direction from Accident Site:
Lowest Cloud Condition:
Visibility: 10 miles
Lowest Ceiling: Overcast / 7500 ft AGL
Visibility (RVR):
Wind Speed/Gusts: 3 knots / 
Turbulence Type Forecast/Actual:  /
Wind Direction: 90° 
Turbulence Severity Forecast/Actual:  /
Altimeter Setting: 30.2 inches Hg 
Temperature/Dew Point: 15°C / -2°C
Precipitation and Obscuration: No Obscuration; No Precipitation
Departure Point: Danbury, TX (07TA) 
Type of Flight Plan Filed: None
Destination: Danbury, TX (07TA) 
Type of Clearance: None
Departure Time:
Type of Airspace: Class G

Airport Information

Airport: Salaika Aviation 07TA 
Runway Surface Type: Grass/turf
Airport Elevation: 30 ft msl 
Runway Surface Condition: Vegetation
Runway Used: 
IFR Approach: None
Runway Length/Width:
VFR Approach/Landing: Forced landing

Wreckage and Impact Information

Crew Injuries: 2 None 
Aircraft Damage: Substantial
Passenger Injuries:
Aircraft Fire: None
Ground Injuries: N/A 
Aircraft Explosion: None
Total Injuries: 2 None 
Latitude, Longitude: 29.243888,-95.333053
=======

Location: Danbury, TX
Accident Number: CEN20LA051
Date & Time: 12/31/2019, 1415 CST
Registration: N57SJ
Aircraft: Enstrom F28
Injuries:2 None
Flight Conducted Under: Part 91: General Aviation - Instructional

On December 31, 2019, about 1415 central standard time, an Enstrom F28A helicopter, N57SJ, sustained substantial damage when it nosed over during a forced landing following a partial loss of engine power. During the nose-over, the tailboom was separated and the main rotor system and fuselage were damaged. The student pilot and flight instructor were not injured. The helicopter was registered to and operated by a private individual under the provisions of Title 14 Code of federal Regulations Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, which was not operated on a flight plan. The local flight originated from the Salaika Aviation Airport (07TA), Danbury, Texas, at an unconfirmed time.

The instructional flight was operating about 75 ft. above the trees when a partial loss of engine power was experienced. Unable to maintain flight with the reduced engine power, the instructor pilot attempted an autorotation to a nearby field. Upon touching down the helicopter skids sunk into the muddy soil and the helicopter nosed over. During the nose-over, the main rotor blades contacted the tail boom, severing it just forward of the tail rotor gearbox.

Aircraft and Owner/Operator Information

Aircraft Make: Enstrom
Registration: N57SJ
Model/Series: F28 A
Aircraft Category: Helicopter
Amateur Built: No
Operator: On file
Operating Certificate(s) Held: None

Meteorological Information and Flight Plan

Conditions at Accident Site:
Condition of Light:
Observation Facility, Elevation: LBX, 25 ft msl
Observation Time: 1953 UTC
Distance from Accident Site:
Temperature/Dew Point: 15°C / -2°C
Lowest Cloud Condition: 
Wind Speed/Gusts, Direction: 3 knots / , 90°
Lowest Ceiling: Overcast / 7500 ft agl
Visibility:  10 Miles
Altimeter Setting: 30.21 inches Hg
Type of Flight Plan Filed: None
Departure Point: Danbury, TX (07TA)
Destination: Danbury, TX (07TA)

Wreckage and Impact Information

Crew Injuries: 2 None
Aircraft Damage: Substantial
Passenger Injuries: N/A
Aircraft Fire: None
Ground Injuries: N/A
Aircraft Explosion: None
Total Injuries: 2 None
Latitude, Longitude: 29.243889, -95.333056

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