CHI03LA098 · Schweizer 269C
Schweizer 269C · Accident: dragged wing, rotor, pod, float or tail/skid during landing
From Wichita Dwight D. Eisenhower National Airport (ICT) to Westport Airport (71K)
Event
- NTSB case
- CHI03LA098
- 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
- 0 · 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 269C
- Aircraft type
- Schweizer 269
- Category
- Helicopter
- 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
- N8968F
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Wichita Dwight D. Eisenhower National Airport (ICT), Wichita, KSTo Westport Airport (71K), Wichita, KS
- 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
- Landing
- 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
- Dragged wing, rotor, pod, float or tail/skid
- 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
- Miscellaneous rotorcraft, main rotor/tail boom contact
- Pilot in command(cfi) › Cyclic, improper use of
- Pilot in command(cfi) › Lowering of collective, premature
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The helicopter was substantially damaged during a run-on landing following a practice autorotation. The flight instructor stated that during the landing the helicopter rotated forward "lifting the tailboom into the path of the main-rotor, which severed the tailboom." The aircraft turned to the left approximately 90 degrees and came to a rest. The instructor was demonstrating a full touchdown autorotation to a run-on landing on the grass area adjacent to a paved runway. The dual student reported that the touchdown itself was light and the helicopter did not decelerate very rapidly until the end of the ground run. According to both pilots the grass landing area was smooth, firm and dry. Neither pilot reported any malfunctions with the helicopter or the engine prior to the accident. The pilot's flight manual included a caution stating: "Avoid rapid lowering of collective pitch control after ground contact." The FAA Rotorcraft Flying Handbook specifies that when conducting a running landing, "due to the increased ground friction when you lower the collective, the helicopter's nose might pitch forward. Exercise caution not to correct this pitching movement with aft cyclic since this movement could result in the rotor making contact with the tailboom."
Probable cause
The premature lowering of the collective and the improper use of the cyclic during the run-on landing performed by the flight instructor, as well as the main rotor/tail boom contact. Contributing factors were the intentional run-on landing, the grass landing surface and the severed tail boom.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CHI03LA098
- Event ID
- 20030410X00479
- Case number
- CHI03LA098
- 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: 9c302666cadae3a1711f4d43e81f8c6fdcadc382c853bdbd6ab2429f21a81174; retrieved 2026-09-21T19:30:58.591Z.