NTSB CAROL · Event
Event FTW95LA382
Registry · N5368J
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-181
Year of manufacture
2003
Engine
LYCOMING O-360 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20030408
ADS-B equipped
Yes — Mode-S A6CA30
Registrant of record
JONES ANESTHESIA LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S INADEQUATE COMPENSATION FOR THE CROSSWIND CONDITION. A FACTOR WAS THE CROSSWIND.
Factual narrative
On September 7, 1995, at 1526 mountain daylight time, a Cessna 421B, N5368J, sustained substantial damage during the landing flare/touchdown at Albuquerque International Airport, Albuquerque, New Mexico. The airline transport rated pilot, three passengers, and one infant did not receive injuries. The airplane was being operated as a personal flight under Title 14 CFR Part 91. The flight originated in Boise, Idaho, at 1150. Visual meteorological conditions prevailed at the destination airport and an IFR flight plan was filed. During interviews, conducted by the investigator-in-charge, and on the Pilot/Operator Report, the pilot reported the following information. When the airplane was on final for runway 08, the controller requested "S" turns for spacing to allow for an F-14 departure. At a one mile final, N5368J was "cleared to land, caution wake turbulence." During the landing touchdown, on the right main gear, the airplane "veered a hard left as if caught in the turbulence of the F-14." The Cessna departed the left side of the runway, collapsed the nose gear, skidded and came to rest on taxiway "A". The pilot stated that winds at the airport were from "110 degrees at 15 knots gusting to 20 knots." Examination of the airplane and the site was conducted by the FAA inspector. He reported structural damage to the fuselage, nose gear, and propeller. The inspector reported (diagram enclosed) that the touchdown point was 2,900 feet from the approach end of runway 08 and the airplane departed the left side of the runway at approximately 3,200 feet from the touchdown end. During a telephone interview, conducted by the investigator-in- charge, and on the enclosed statement, the F-14 crew reported the following information. The F14 takeoff weight was 63,000 pounds with a the rotation point at 4,000 feet and a rotation speed of 135 knots. Each engine produced approximately 17,000 pounds of thrust and the flaps were set at 10 degrees. A review of the Albuquerque Air Traffic Control Tower data revealed that at 1524:56 the F-14 was cleared for takeoff, and at 1525:31, N5368J was cleared to land. The Cessna was over the approach end of runway 08 at 1526:01, and the F14 was 1.5 nautical miles beyond the departure end of the 13,775 foot runway. The Albuquerque surface weather observation at 1450 reported the winds from 130 degrees at 9 knots. THE FLIGHT WAS CLEARED TO LAND ON RUNWAY 08 BEHIND A DEPARTING F-14, AND THE PILOT WAS CAUTIONED FOR WAKE TURBULENCE. DURING LANDING THE AIRPLANE DEPARTED THE LEFT SIDE OF THE RUNWAY, COLLAPSED THE NOSE GEAR, SKIDDED AND CAME TO REST ON A TAXIWAY. THE PILOT REPORTED WINDS FROM 110 DEGREES AT 15 GUSTING TO 20 KNOTS. NATIONAL WEATHER OBSERVATION DATA REPORTED THE WINDS FROM 130 DEGREES AT 9 KNOTS. WHEN THE CESSNA WAS OVER THE APPROACH END OF RUNWAY 08, THE F-14 WAS 1.5 NAUTICAL MILES BEYOND THE DEPARTURE END OF THE 13,775-FOOT RUNWAY. THE ROTATION POINT OF THE F-14 WAS 4,000 FEET FROM THE APPROACH END OF RUNWAY 08, AND THE TOUCHDOWN POINT OF THE CESSNA WAS 2,900 FEET. THE ATC TIME OF THE F-14 DEPARTURE WAS 1524:56; THE CESSNA WAS OVER THE APPROACH END OF RUNWAY 08 AT 1526:01. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW95LA382.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 (wake turbulence, turbulence). 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
Aircraft wake turbulence minimization by aerodynamic means
The paper reviews NASA's efforts on wake vortex turbulence minimization by aerodynamic design or retrofit modifications to large transport aircraft.
- NASA NTRS 2019 · Conference Paper
Wake Turbulence Mitigation for Arrivals (WTMA)
The preliminary Wake Turbulence Mitigation for Arrivals (WTMA) concept of operations is described in this paper. The WTMA concept provides further detail to work initiated by the Wake Vortex Avoidance…
- NASA NTRS 2019 · Conference Paper
Aircraft wake turbulence avoidance
Aircraft wake turbulence /trailing vortex systems/ avoidance during flight, describing procedures for pilots and tower operators
- NASA NTRS 2019 · Conference Paper
Aircraft wake turbulence progress and plans
Aircraft wake turbulence and trailing vortices, investigating physical characteristics, hazard potential and avoidance techniques
- SKYbrary (Eurocontrol) 2023 · SKYbrary article
Wake Vortex Turbulence — SKYbrary Knowledge Base
SKYbrary wake vortex turbulence comprehensive article — generation mechanics, dissipation factors, separation standards (ICAO LIGHT/MEDIUM/HEAVY/SUPER + recategorisation RECAT-EU).
- NASA NTRS 2019 · Contractor Report (CR)
An Examination of Aviation Accidents Associated with Turbulence, Wind Shear and Thunderstorm
The focal point of the study reported here was the definition and examination of turbulence, wind shear and thunderstorm in relation to aviation accidents.
Browse the full corpus — academia portal ↗