IAD99LA016
1998-11-15 · CALDWELL, New Jersey, United States · None · 1 aircraft · Status: Completed
Airport CDW
Aircraft involved
Probable cause & findings
the student's pilot's inadequate climb and his failure to maintain adequate altitude and clearance. A related factor was the wind gusts.
Factual narrative
On November 15, 1998, at 1146 eastern standard time, a Cessna 152, N89101, was substantially damaged after a loss of control during landing at the Essex County Airport (CDW), Caldwell, New Jersey. The certificated student pilot was not injured. Visual meteorological conditions prevailed for the local solo instructional flight that originated at CDW, at 0950. No flight plan had been filed for the flight conducted under 14 CFR Part 91. In a telephone interview, the pilot said the purpose of the flight was to practice flight maneuvers for a flight evaluation he had scheduled for later in the month. He departed the traffic pattern, flew to a local training area, completed the planned training, and returned for landing on runway 27. The pilot said that prior to departure he obtained weather information from DUATS, Flight Service, and the local ATIS. He said: "Everything went fine. I went out and did all my training. When I came back, conditions were different, they were gusty. My approach speed was 60, but my ground speed was significantly slower. When I touched down, a gust lifted me. I tried to do a full power go around, but the plane wouldn't climb. It just descended. When I added full power, the nose was too high - it wouldn't climb - it just veered to the right and stalled. The gust gave it a nose high pitch. I had 30 degrees of flaps in, which may have been too much flaps for that kind of a gust." When questioned about the airworthiness of the airplane, the pilot said, "The airplane performed fine, I had no problems with the airplane at all." The pilot reported approximately 145 hours of total flight experience; 45 hours of which were solo. Winds reported at the time of the accident were from 300 degrees at 12 knots gusting to 20 knots. The student pilot practiced flight maneuvers for approximately 2 hours during the local solo flight. During landing on runway 27, the pilot said a gust of wind lifted the airplane to a nose high pitch attitude. Full power was applied to abort the landing but the airplane would not climb. The airplane descended and collided with terrain. The student pilot reported there were no mechanical deficiencies with the airplane. Winds were reported to be from 300 degrees at 12 knots, gusting to 20. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1998_IAD99LA016.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 or causal vocabulary (stall, loss of control). All research papers
- Semantic Scholar 2016 · Article (Interacción) Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER) A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- SKYbrary (Eurocontrol) 2024 · SKYbrary article Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
- Semantic Scholar 2024 · Article (International Conference on Networking and Services) Risk Assessment of Loss of Control In-Flight Trajectories for Urban Air Mobility Safety
In Urban Air Mobility (UAM), maintaining a minimum separation between aircraft is a safety requirement, which becomes challenging amidst congested air traffic and off-nominal conditions, such as Loss …