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LAX05LA131 · Schweizer SGS 2-32

6 Apr 2005 · Mokuleia, HI, United States

Schweizer SGS 2-32 · Accident: loss of control in flight while maneuvering

From Kawaihapai Airfield (HDH) to an unrecorded destination

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Event

NTSB case
LAX05LA131
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
1 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Schweizer SGS 2-32

Aircraft type
Schweizer SGS-2
Category
Glider
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N693U
Operator
Unknown
Onboard fatalities
Unknown
Route
From Kawaihapai Airfield (HDH), Mokuleia, HITo not recorded
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Maneuvering
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of control in flight
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Stall/spin
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Pilot in command › Airspeed, not maintained

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

During a for-hire sightseeing flight, the glider entered an inadvertent stall and spun to ground impact. The flight was conducted in an area where normal wind conditions brought trade winds that produced strong updrafts when they encountered the accident site ridgeline. On the day of the accident, the winds were described as shifty and gusting and they did not produce the updraft along the ridgeline that was most common in that area. In addition, the cloud bases would not allow for a tow greater than 2,000 feet. A witness (also a glider pilot), observed the accident glider eastbound about 400 to 500 feet above the ridge. She then noticed the glider "turn right (toward the ridge) and its nose come up slightly." The glider turned "approximately 45 degrees to the right, then turned back to the left and immediately entered a spin to the left." The witness reported that the glider rotated twice before it entered a second spin to the right. Post-accident examination of the glider revealed no anomalies that would have prevented its normal operation. A video recording of the flight revealed no anomalies with the glider. As captured during the final moments of an audio recording of the flight, the pilot's last transmission indicated that the glider was encountering a sink rate. According to the accident glider's flight manual, after spin entry, the pilot might experience one nose up and down oscillation before the stable spin occurs. The rotations are relatively slow with an altitude loss of approximately 300 feet per turn. Recovery technique was normal, except that considerably more control was needed to stop the rotation and to lower the nose. Instead of easing off back pressure on the stick, it must be pushed forward of neutral and instead of neutralizing the rudder, opposite rudder must be applied. The rotation could be stopped in 1/4 to 1/2 turn. Review of the pilot's training records and experience brought into serious question the quality of both. In less than 3 months after beginning flight training the pilot obtained his commercial pilot certificate, just 2 days after passing his private pilot check ride. Upon obtaining his commercial pilot certificate the pilot began conducting tour flights for fare-paying passengers; at this point his total flight experience amounted to 48.4 hours of flight time, of which 31.2 hours were as pilot-in-command. Review of the pilot's training records revealed he received stall/spin training on the same day he received training on a myriad of complex subjects. The operator said that when he conducted spin training with the pilot, on one occasion the pilot didn't get the control stick forward enough on a spin recovery and got into a secondary stall. The operator then had the pilot demonstrate two additional spin/spin recovery maneuvers. Federal Aviation Regulations indicated that an applicant may obtain their commercial glider certificate with as little as 25 hours of flight time and 100 flights as pilot-in-command. According to the Soaring Society of America and the Soaring Safety Foundation, it is unusual to obtain a commercial glider pilot certificate in as little time as the accident pilot, and it usually takes about 6 months to 1 year to obtain the required experience.

Probable cause

the pilot's failure to maintain an adequate airspeed while maneuvering during a scenic flight, which led to an inadvertent stall/spin and secondary stall/spin encounter. Contributing factors were the pilot's lack of total flight experience, his inadequate flight training, and the unfavorable wind conditions.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX05LA131
Event ID
20050420X00484
Case number
LAX05LA131
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 791407d457e2186a45fcea44faee7db1e1d90264470fe2886948ca2f1b02d85f; retrieved 2026-09-20T18:05:18.071Z.