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Accidents · NTSB CEN14LA222 · Final report

Hughes 269A accident near Cleburne, Texas, April 25, 2014

On April 25, 2014 at about 7:30 pm local time, a 1967 Hughes 269A (helicopter), registered N90636, was substantially damaged in an accident during maneuvering (hover) near Cleburne, Texas (Cleburne Rgnl airport). It was an instructional flight under general aviation rules (Part 91). 2 people had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The student pilot's failure to maintain tail rotor clearance from terrain while transitioning to a hover taxi and the instructor pilot's inadequate remedial action to prevent the impending tail rotor contact.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 25, 2014 · about 7:30 pm local time
Place
Cleburne, Texas · Cleburne Rgnl · map
Type
Accident
Injuries
2 people had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Hughes 269A, built 1967 · all 269As on the register
Registration
N90636 · no longer on the register · serial 570708
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The student pilot was air taxiing the helicopter with an instructor pilot on board. When the student pilot slowed to a hover taxi, the helicopter began bucking violently fore and aft. The helicopter descended and came to rest on its side. A postaccident examination of the wreckage and accident site revealed ground scars consistent with main and tail rotor blade strikes, which were consistent with the aft left skid and tail rotor contacting the ground while the helicopter was moving aft. A helicopter is customarily pitched with its tail low when the pilot performs a quick stop from an air taxi. Tail rotor drive shaft deformation was consistent with the tail rotor blade contacting the ground while being driven. No preimpact anomalies were detected that would have precluded normal operation of the helicopter. The evidence indicates that the student pilot allowed the tail rotor and aft skid to contact the ground as the helicopter slowed during the transition to hover taxi. The instructor did not anticipate the situation or intervene in a timely manner, which resulted in an uncontrolled descent and rollover.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Low altitude operation/event during maneuvering (hover) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during maneuvering (hover)

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Use of equip/system › Student/instructed pilot
  • cause Personnel issues › Action/decision › Action › Lack of action › Instructor/check pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Altitude › Not attained/maintained

Flight instructor

  • Certificate: flight instructor
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instructor: instrument helicopter; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 17,180 hours in all; 16,475 as pilot in command; 5,409 on instruments
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: minor injuries

Dual student

  • Certificate: student
  • Flight time: 90 hours in all; 14 in this make and model; 30 in the last 90 days; 8 in the last 30 days; 18 as pilot in command
  • Medical certificate: Class 3 (without waivers/limitations)
  • Seat: rgt
  • Injury: minor injuries

The aircraft

  • Airframe total time: 3,733 hours
  • Last inspection: annual inspection, April 24, 2014
  • Maximum gross weight: 1,670 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming HIO-360-A1A (piston); 0 hours total

The flight

  • Departed from: CPT Cleburne TX at 5:30 pm
  • Destination: CPT Cleburne TX
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 120° at 11 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 82°F (28°C), dew point 43°F (6°C)
  • Altimeter: 30.00 inHg
  • Observation at 6:35 am from KCPT

Injuries

FatalSeriousMinorNone
Flight crew2

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.