NTSB CAROL · Event
Event SEA95LA045
Registry · N9CR
FAA Aircraft Registry record.
Make / Model
BELL HELICOPTER TEXTRON CANADA 429
Year of manufacture
2013
TCDS
R00003RD · BELL HELICOPTER TEXTRON CANADA LTD
Engine
P&W CANADA PW207D1/D2 (621 hp)
Seats / Engines
9 seats · 2 engines
Last airworthiness date
20131204
ADS-B equipped
Yes — Mode-S AC6ABC
Registrant of record
BANNER ELK AVIATION LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S PREMATURE LIFT-OFF DURING THE TAKEOFF, LEADING TO AN AERODYNAMIC STALL. A FACTOR CONTRIBUTING TO THE ACCIDENT WAS THE PILOT'S ATTEMPT TO PERFORM A FORMATION TAKEOFF.
Factual narrative
On February 5, 1995, about 1710 mountain standard time, N9CR, a Cessna 185, operated by the owner/pilot, impacted terrain during an uncontrolled descent immediately after takeoff and was substantially damaged in McCall, Idaho. The private pilot and his three passengers were not injured. Visual meteorological conditions prevailed and no flight plan had been filed. The personal flight was conducted under 14 CFR 91. The flight departed from McCall and was destined for Wilbur, Washington. The pilot stated that he "took off ... as a group of three" airplanes from runway 16 at the McCall Airport behind two other Cessna 185 airplanes. He stated that the "takeoff was normal, breaking ground in about 1000 [feet of runway length]. The pilot further stated that the airplane began to climb "between 85 [and] 90" miles per hour (mph) and reached an altitude of about 65 feet when the right wing and nose dropped "violently." The airplane "turned 90 degrees to the right" and the pilot "used full left rudder and aileron and up elevator to counteract the forces on the aircraft." The pilot also stated that he "hit wake turbulence" during the takeoff. No preimpact mechanical deficiencies were reported by the pilot According to ground witnesses, all three airplanes taxied onto runway 16 at the same time. The lead airplane took off first. The second and third airplanes then began their takeoff rolls and lifted off from the ground at the same time. The third airplane (accident airplane) immediately commenced a right bank after liftoff, and then descended into terrain. One of the witnesses stated that the accident airplane "... didn't have enough speed and wasn't off the ground enough before starting to turn." According to an FAA aviation safety inspector from Boise, Idaho, the airplane impacted snow-covered terrain about 1,200 feet south and 200 feet west of the departure end of runway 16. The landing gear was separated, an aileron was bent, and the underside of the fuselage was damaged. No pre-impact mechanical malfunctions were found. ACCORDING TO WITNESSES, THE PILOT ATTEMPTED A FORMATION TAKEOFF WITH ANOTHER AIRCRAFT. BOTH AIRPLANES WERE OBSERVED TO BEGIN THE TAKEOFF ROLL AND LIFT OFF FROM THE SAME RUNWAY AT THE SAME TIME. DURING THE TAKEOFF ROLL, THE PILOT OF THE ACCIDENT AIRPLANE PREMATURELY LIFTED OFF AT AN AIRSPEED THAT WAS NOT ADEQUATE TO SUSTAIN FLIGHT. THE AIRPLANE AERODYNAMICALLY STALLED ABOUT 50 FEET ABOVE THE RUNWAY. IT IMPACTED SNOW-COVERED TERRAIN OFF THE EDGE OF THE RUNWAY AND WAS SUBSTANTIALLY DAMAGED. NO PREIMPACT MECHANICAL DEFICIENCIES WERE REPORTED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_SEA95LA045.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 (stall, 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).
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
Browse the full corpus — academia portal ↗