SEA08CA049
2007-11-29 · Death Valley, California, United States · None · 1 aircraft · Status: Completed
Airport L09
Aircraft involved
Probable cause & findings
The pilot's improper flare during landing.
Factual narrative
The pilot reported that during the landing on runway 5, the touchdown was hard and the airplane bounced and started to "porpoise". Subsequently the nose wheel landing gear failed aft, and the airplane nosed down and slid to a stop. The pilot reported no mechanical failures or malfunctions with the airplane at the time of the accident. Examination of the airplane by salvage personnel revealed that the engine mount and firewall were bent. The pilot reported that during the landing on runway 5, the touchdown was hard and the airplane bounced and started to "porpoise". Subsequently the nosewheel landing gear failed aft, and the airplane nosed down and slid to a stop. The pilot reported no mechanical failures or malfunctions with the airplane at the time of the accident. Examination of the airplane by salvage personnel revealed that the engine mount and firewall were bent. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_SEA08CA049.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type. All research papers
- arXiv 2023 · arXiv preprint Large-eddy simulations of the NACA23012 airfoil with laser-scanned ice shapes
In this study, five ice shapes generated at NASA Glenn's Icing Research Tunnel (IRT) are simulated at multiple angles of attack (Broeren et al., J. of Aircraft, 2018).
- arXiv 2025 · arXiv preprint Transonic buffet and incompressible low-frequency oscillations at high Reynolds numbers
Coherent, self-sustained oscillations of the flow over aircraft wings can lead to unsteady loads that detrimentally affect aircraft safety and stability, thus limiting the flight envelope.