NTSB CAROL · Event
Event FTW04LA145
Registry · N61663
FAA Aircraft Registry record.
Make / Model
CESSNA 172M
Year of manufacture
1975 · 29 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19750211
ADS-B equipped
Yes — Mode-S A8084E
Registrant of record
MOHAMED EMAN Z
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain directional control and his inadequate compensation for the winds.
Factual narrative
On May 31, 2004, approximately 1040 central daylight time, a Cessna 172M single-engine airplane, N61663, registered to a private individual and operated by Levelland Aviation, of Levelland, Texas, sustained substantial damage following a loss of control while landing on runway 17 at the Levelland Municipal Airport (LLN), near Levelland, Texas. The solo student pilot was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the Title 14 Code of Federal Regulations Part 91 instructional solo flight. According to the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the student pilot reported that he configured the airplane with 10 degrees of flaps at an airspeed at 80 knots for a second touch and go landing on Runway 17. The student pilot reported that the winds were from 100 degrees at about 8 knots as he attempted to land on the 6,110-foot by 75-foot wide runway with a prevailing left crosswind. The pilot added that upon touchdown the airplane bounced and began to "float" to the right of centerline. The airplane touched down a second time, and began to skid to the right. The pilot stated, "I lost control of the plane, and it went off the runway" The aircraft impacted a large drainage ditch, then came to rest in the upright position. The operator reported that the student pilot had accumulated a total of 33 hours of total flight time, of which 26 hours were in the accident make and model. A review of the pilot's training records revealed that the student pilot was found to be properly endorsed for this flight, which was his third solo flight. Examination of the wreckage by a Federal Aviation Administration (FAA) inspector, who traveled to the accident site, revealed that the main bolt on the left main landing gear had sheared, both spars on the left stabilizer were bent and wrinkled, and the fairing between the vertical fin and the fuselage was cracked into two pieces. A review of the aircraft logbooks did not reveal any discrepancies. Weather conditions at LLN at 1053 were reported as winds from 120 degrees at 13 knots, visibility 10 statute miles, clear skies, temperature 24 degrees Celsius, dew point 0 degrees Celsius, with an altimeter setting of 29.98 inches of mercury. The solo student pilot lost control of the single-engine airplane while landing with a left crosswind. The 33-hour student pilot reported that he configured the airplane with 10 degrees of flaps and airspeed at 80 knots for a second touch and go landing on Runway 17. The pilot stated that he landed on the 6,110-foot by 75-foot wide runway with a prevailing crosswind from 100 degrees at 8 knots. Upon landing, the airplane bounced and began to "float." The airplane touched down a second time, and began to skid to the right. The pilot stated, "I lost control of the plane, and it went off the runway." Wind conditions at the time of the accident were reported from 120 degrees at 13 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_FTW04LA145.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2019 · Conference Paper
Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM)
Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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.
- 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…
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