CEN14LA269 · Schweizer 269C
Kachemak Bay Flying Service Schweizer 269C · Accident: ground resonance during landing
From Draughon Miller Central Texas Regional Airport (TPL) to Draughon Miller Central Texas Regional Airport (TPL)
Event
- NTSB case
- CEN14LA269
- 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
- N902CP
- Operator
- Kachemak Bay Flying Service
- Onboard fatalities
- Unknown
- Route
- From Draughon Miller Central Texas Regional Airport (TPL), Temple, TXTo Draughon Miller Central Texas Regional Airport (TPL), Temple, TX
- Aircraft age
- About 19 years (built 1995)
- 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
- Defining eventThe 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
- Ground resonance
- 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
- Aircraft › Aircraft systems
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot reported that, during initial taxi, he noticed that the intercom voice operated relay (VOX) volume was set too high, so he landed the helicopter on the asphalt taxiway to adjust the VOX. With the helicopter at flat-pitch operating rpm and just as the pilot reached to adjust the VOX, the helicopter began oscillating due to ground resonance. Within 5 seconds of touchdown, the oscillating became severe. The pilot ensured that the collective was at flat pitch, and he rolled the throttle to flight idle. Within 15 seconds, the main rotor blades impacted the ground, tail boom, and other helicopter components.
During postaccident examination, all four main landing gear dampers failed load stroke tests. The helicopter's maintenance records indicated that the main landing gear dampers were serviced by charging them with nitrogen in accordance with the helicopter's maintenance manual about 1 month before the accident. However, about 14 days before the dampers were serviced, the helicopter manufacturer had issued an alert service bulletin (ASB) that recommended a one-time load stroke inspection of the landing gear dampers to be performed at an overhaul or repair facility to ensure that the dampers were serviced correctly. Concurrently, the helicopter manufacturer had issued a revision to the maintenance manual that added a load stroke inspection procedure to the section of the manual pertaining to repair and charging of the dampers. The company's maintenance manager reported that maintenance personnel were unaware that the ASB and maintenance manual revision had been issued until after the accident. If the load stroke inspection of the dampers called for by the ASB or the maintenance manual revision had been performed, it would have identified the out-of-specification condition of the dampers before reinstallation. Because the dampers were out-of-specification, ground resonance occurred after the pilot landed the helicopter.
Probable cause
Ground resonance due to maintenance personnel’s improper inspection of the landing gear dampers, which resulted in the dampers operating outside of allowable limits.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record CEN14LA269
- Event ID
- 20140602X94257
- Case number
- CEN14LA269
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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: f60fc7640c7ff081a3909b8eb2e71b842b0958576ac1ae438e6c10c65f9f2c27; retrieved 2026-09-15T23:43:33.468Z.