LAX01FA144 · Schleicher ASW-20
Schleicher ASW-20 · Accident: loss of control in flight during initial climb
From Williams, CA (no airport) to Williams, CA (no airport)
Event
- NTSB case
- LAX01FA144
- 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
Schleicher ASW-20
- Aircraft type
- Schleicher ASW-20
- 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
- N47TR
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Williams, CA (no airport)To Williams, CA (no airport)
- 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
- Initial climb
- 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
- 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
- Flt control syst, elevator control cable/rod › Not connected
- Pilot in command › Aircraft preflight, inadequate
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
During the takeoff, the glider began an uncontrolled climb at a 45-degree nose up attitude behind the tow plane. The tow plane pilot was forced to cut the tow rope due to the severe pitch down moment caused by the glider. The glider then arced over into a 45-degree nose down dive and hit the ground. The glider's flight control system was equipped with Hotalier quick disconnect fittings at various locations to facilitate the disassembly of the glider for trailer transport. A postaccident examination of the flight control system disclosed that the elevator control push rod was disconnected from the elevator at a quick disconnect fitting in the vertical stabilizer. There was no damage noted to the elevator bell crank or the terminal end of the elevator control push rod. A close friend and former partner in the glider was interviewed. He was present on the day of the accident and knew the pilot very well. He stated that he and the pilot had purchased the glider a little less than a year prior to the accident. The pilot had flown it over 50 times and had assembled it as many as 25 times. On the day of the accident, he and the pilot completed a control check while qued for the tow plane. He stated that he held the elevator while the pilot applied full up elevator control input. He felt the elevator move in the up position. He said neither the pilot nor he attempted to apply full nose down control input, as it was assumed the elevator was properly attached to the control rod fitting. He stated that in retrospect, the only way to positively check the connection is to hold the elevator in the up position while the pilot applies full nose down control input.
Probable cause
The failure of the pilot to attach the elevator control rod to the elevator, resulting in a loss of pitch control and subsequent ground impact. Additional factors were the failure to complete a positive control check and the lack of clear guidance in the assembly procedures.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record LAX01FA144
- Event ID
- 20010419X00779
- Case number
- LAX01FA144
- 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. 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: ef8f9b126c18c8f38d61ca4472c24f63ad9e0dec32acbbcce30eae9d2999e333; retrieved 2026-09-20T20:35:36.816Z.