MIA88FA088
1988-01-17 · POMPANO BEACH, Florida, United States · Serious · 1 aircraft · Status: Completed
Airport PMP
Current FAA registration · N29076
- Make / Model
- CHRISTEN INDUSTRIES INC A-1
- Year of manufacture
- 1987 · 1 years old at event
- Engine
- LYCOMING O&VO-360 SER (180 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19870911
- ADS-B equipped
- Yes — Mode-S A2F8E6
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE PLT STATED THAT AS HE PUSHED THE CONTROL STICK FORWARD IN AN ATTEMPT TO RAISE THE TAIL, THE ACFT VIOLENTLY PITCHED UP, STALLED AND BROKE RIGHT, THE RIGHT WING STRUCK THE GROUND, & THE ACFT ROLLED OVER & CAME TO REST INVERTED. POST CRASH EXAMINATION OF THE ACFT REVEALED THAT THE FORWARD CONTROL STICK HAD BEEN REMOVED & WAS REINSTALLED BACKWARDS PRIOR TO THE ACCIDENT FLIGHT, RESTRICTING THE FORWARD MOVEMENT OF THE CONTROL STICK. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1988_MIA88FA088.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-18E Model (Invited)
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2019 · Conference Paper Transonic Experimental Observations of Abrupt Wing Stall on an F/A-l8E Model
A transonic wind tunnel test of an 8% F/A-18E model was conducted in the NASA Langley Research Center (LaRC) 16 ft Transonic Tunnel (16-ft TT) to investigate on-surface flow physics during stall.
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
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This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
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Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…