20070612008579I

Incident · Minor damage

FAA incident report · Hughes 269A · Abilene, TX · June 12, 2007

Date
June 12, 2007 · 15:00 local
Place
Abilene, TX
Airport
Abilene Regional Airport
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N1070N
Reported as
Hughes 269A
Fatal injuries
0
Pilot’s flight hours
0 total0 in this make and model0 in the last 90 days

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.

(-23) As the pilot neared the bottom of the approach and was entering the hover, a gust of wind hit the aircraft and the aircraft started to turn slightly to the right. The applicant later admitted he did not apply left pedal to arrest the right turn because he was afraid of experiencing loss of tail rotor effectiveness. When he allowed the aircraft to start the right turn, he did in fact lose tail rotor effectiveness and the turn to the right accelerated. Before the inspector could reach the controls, the applicant had rolled the throttle to idle and the helicopter landed hard. The aircraft was shut down and inspected. The aft cross tube was bent. No other damage was observed.

As the FAA filed it

(-23) AS THE PILOT NEARED THE BOTTOM OF THE APPROACH AND WAS ENTERING THE HOVER, A GUST OF WIND HIT THE AIRCRAFT AND THE AIRCRAFT STARTED TO TURN SLIGHTLY TO THE RIGHT. THE APPLICANT LATER ADMITTED HE DID NOT APPLY LEFT PEDAL TO ARREST THE RIGHT TURN BECAUSE HE WAS AFRAID OF EXPERIENCING LOSS OF TAIL ROTOR EFFECTIVENESS. WHEN HE ALLOWED THE AIRCRAFT TO START THE RIGHT TURN, HE DID IN FACT LOSE TAIL ROTOR EFFECTIVENESS AND THE TURN TO THE RIGHT ACCELERATED. BEFORE THE INSPECTOR COULD REACH THE CONTROLS, THE APPLICANT HAD ROLLED THE THROTTLE TO IDLE AND THE HELICOPTER LANDED HARD. THE AIRCRAFT WAS SHUT DOWN AND INSPECTED. THE AFT CROSS TUBE WAS BENT. NO OTHER DAMAGE WAS OBSERVED.