LAX90LA224
1990-06-20 · CHICO, California, United States · None · 1 aircraft · Status: Completed
Airport CIC
Current FAA registration · N72122
- Make / Model
- CESSNA 140
- Year of manufacture
- 1946 · 44 years old at event
- Engine
- CONT MOTOR C85 SERIES (85 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19560612
- ADS-B equipped
- Yes — Mode-S A9A9FC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT IMPROPERLY LEVELED OFF, FAILED TO CORRECT THE ENSUING PORPOISE, TOOK IMPROPER REMEDIAL ACTION, AND IMPROPERLY USED THE RUDDER AND NORMAL BRAKES.
Factual narrative
THE STUDENT PILOT INTENDED TO PRACTICE TAKEOFFS AND LANDINGS. ON THE FIRST LANDING, THE STUDENT PILOT LEVELED OFF TOO HIGH, BOUNCED AND BEGAN TO PORPOISE. HE THEN IMPROPERLY USED THE NORMAL BRAKES AND RUDDER AND FAILED TO MAINTAIN DIRECTIONAL CONTROL. THE AIRPLANE EXITED THE RUNWAY SEVERING THE RIGHT MAIN GEAR IN THE PROCESS. THE INVESTIGATION REVEALED THAT THE STUDENT PILOT HAD RECEIVED TRAINING ON RECOVERY FROM BOUNCED LANDINGS. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_LAX90LA224.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.
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Related research
Matched on aircraft type. All research papers
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- NASA NTRS 2019 · Conference Paper Particulate Emissions Hazards Associated with Fueling Heat Engines
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- NASA NTRS 2016 · Conference Paper United Airlines LOFT training
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- Embry-Riddle Scholarly Commons 2016 · Conference paper Late Morning Concurrent Sessions: Innovations in Aviation Technologies: Presentation: Wingsuit Materials Research – The Effect of Currently Used Materials on Wingsuit Aerodynamics.
While wingsuit flight is exhilarating and one of the fastest growing facets of sport skydiving, current wingsuit performance is poor at best.
- NASA NTRS 2013 · Conference Paper Thermodynamic and fluid mechanic analysis of rapid pressurization in a dead-end tube
Three models have been applied to very rapid compression of oxygen in a dead-ended tube. Pressures as high as 41 MPa (6000 psi) leading to peak temperatures of 1400 K are predicted.