FTW96LA276
1996-06-24 · EL PASO, Texas, United States · None · 1 aircraft · Status: Completed
Airport ELP
Current FAA registration · N6048D
- Make / Model
- PIPER PA-22-150
- Year of manufacture
- 1956 · 40 years old at event
- Engine
- LYCOMING 0-320 SERIES (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19561212
- ADS-B equipped
- Yes — Mode-S A7D98F
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
loss of directional control due to the failure of the tailwheel lock. A factor was the crosswind.
Factual narrative
On June 24, 1996, at 0600 mountain daylight time, a Piper PA-22-150, N6048D, was substantially damaged following a loss of control while landing near El Paso, Texas. The commercial pilot, sole occupant of the airplane, was not injured. The airplane was owned and operated by the pilot under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the personal flight for which a flight plan was not filed. The flight originated from the Deming Municipal Airport in Deming, New Mexico, at approximately 0500. According to witnesses at the airport, the pilot lost control of the airplane while landing on runway 26L at El Paso International Airport. The pilot stated that during the landing roll, "the tailwheel popped out of the lock and shimmied 3 times." The airplane skidded off the left side of the runway despite the pilot's application of full rudder and brake. As the airplane left the hard surface, the pilot discontinued the braking action to avoid nosing over and the airplane ground looped, resulting in substantial damage to the right wing. The pilot stated that the tower issued him the reported winds while on the downwind leg, and he accepted the clearance to land on runway 26L. The recorded winds at the time of the accident were reported from 200 degrees at 7 knots. In the enclosed NTSB Form 6120.1/2, the pilot added that at the time of the accident the winds were gusting in excess of 10 knots. During the landing roll in a crosswind, the plane's tailwheel lock failed. The pilot subsequently lost control of the airplane. The plane went off the left side of the hard surface runway and ground looped. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_FTW96LA276.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (loss of control). All research papers
- 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 …
- NTSB Aircraft Accident Reports 2022 · Accident report Loss of Control on Takeoff in Icing Conditions — Citation 560XL
Cessna Citation 560XL fatal takeoff icing accident, March 2018. Investigation of a Citation 560XL loss-of-control takeoff accident in icing conditions.
- Semantic Scholar 2021 · Article (Aviation) ANALYSIS OF GENERAL AVIATION FIXED-WING AIRCRAFT ACCIDENTS INVOLVING INFLIGHT LOSS OF CONTROL USING A STATE-BASED APPROACH
Inflight loss of control (LOC-I) is a significant cause of General Aviation (GA) fixed-wing aircraft accidents. The United States National Transportation Safety Board’s database provides a rich source…
- NASA NTRS 2021 · Presentation Use of Design of Experiments in Determining Neural Network Architectures for Loss of Control Detection
Abstract—We describe empirical methods for selecting a neural network architecture to implement belief state inference on generic commercial transport aircraft.