20160809012999A

Accident · Destroyed

FAA accident report · Hughes 269C · Howe, TX · August 9, 2016

Date
August 9, 2016 · 20:35 local
Place
Howe, TX
Phase of flight
Other, Specify
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9277R
NTSB investigation
NTSBCEN16FA315
Reported as
Hughes 269C
Reported engine
Lycoming HIO-360 series
People aboard
2
Fatal injuries
1
Other injuries
1
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
2,211 total

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The 14 CFR part 91 instructional flight originated from the aircraft privacy data omitted student?s residence in rural Howe, Texas. The instructor reduced engine power to simulate an engine-out condition to practice a ?forced landing? Training maneuver. The aircraft was at 1100 to 1200 feet above ground level (AGL). The engine reached idle speed and ceased producing power. An autorotation was performed into a tall-grass field. As the aircraft reached 300 feet AGL, the student pushed forward on the cyclic in order to gain airspeed. However, in doing so, the rotor lost energy and the aircraft dropped to the ground with little to no forward motion. The student stated that the instructor never touched the controls during this event.

As the FAA filed it

THE 14 CFR PART 91 INSTRUCTIONAL FLIGHT ORIGINATED FROM THE AIRCRAFT ^PRIVACY DATA OMITTED^ STUDENT?S RESIDENCE IN RURAL HOWE, TEXAS. THE INSTRUCTOR REDUCED ENGINE POWER TO SIMULATE AN ENGINE-OUT CONDITION TO PRACTICE A ?FORCED LANDING? TRAINING MANEUVER. THE AIRCRAFT WAS AT 1100 TO 1200 FEET ABOVE GROUND LEVEL (AGL). THE ENGINE REACHED IDLE SPEED AND CEASED PRODUCING POWER. AN AUTOROTATION WAS PERFORMED INTO A TALL-GRASS FIELD. AS THE AIRCRAFT REACHED 300 FEET AGL, THE STUDENT PUSHED FORWARD ON THE CYCLIC IN ORDER TO GAIN AIRSPEED. HOWEVER, IN DOING SO, THE ROTOR LOST ENERGY AND THE AIRCRAFT DROPPED TO THE GROUND WITH LITTLE TO NO FORWARD MOTION. THE STUDENT STATED THAT THE INSTRUCTOR NEVER TOUCHED THE CONTROLS DURING THIS EVENT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.