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Atlas / NTSB / LAX94LA338

NTSB CAROL · Event

Event LAX94LA338

1994-08-21 SO. LAKE TAHOE, California, United States Airport · TVL None 1 aircraft Status: Completed

Registry · N36DY

FAA Aircraft Registry record.

Make / Model

BEECH A36

Year of manufacture

1972 · 22 years old at event

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19720607

ADS-B equipped

Yes — Mode-S A40A55

Registrant of record

LEWELLEN KIRK

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the pilot's delayed decision to abort the takeoff when the performance deficiency first became apparent.

Factual narrative

On August 21, 1994, at 1325 Pacific daylight time, a Beech A36, N36DY, overran the runway departure end and collided with a fence during a rejected takeoff at South Lake Tahoe, California. The aircraft was owned and operated by the pilot. Visual meteorological conditions prevailed at the time and included a calculated density altitude of 8,700 feet. The aircraft sustained substantial wing damage. The certificated private pilot and the four passengers on board were not injured. The flight was originating at the time of the accident as a personal cross-country flight to Watsonville, California. In his written statement, the pilot reported that just after lift-off from runway 18 at 50 feet he encountered a windshear condition and a downdraft. Concurrent with the windshear condition, the stall warning horn activated and the aircraft ceased to climb. The pilot stated that he lowered the nose and tried one more time to achieve a safe gear and flap retraction speed, and to obtain a positive climb rate. The pilot said he was concerned about the ability of the aircraft to climb over trees and higher terrain beyond the end of the runway and aborted the takeoff. The pilot was unable to stop the aircraft prior to overrunning the departure end of the 8,544-foot-long runway and colliding with an airport boundary fence. The winds were from 290 degrees at 9 knots. THE PILOT REPORTED THAT JUST AFTER LIFT-OFF FROM RUNWAY 18 AT 50 FEET HE ENCOUNTERED A WINDSHEAR CONDITION AND A DOWNDRAFT. CONCURRENT WITH THE WINDSHEAR CONDITION, THE STALL WARNING HORN ACTIVATED AND THE AIRCRAFT CEASED TO CLIMB. THE PILOT SAID HE TRIED ONCE MORE TO GET THE AIRCRAFT TO ACCELERATE TO A SAFE GEAR AND FLAP RETRACTION SPEED AND CLIMB; HOWEVER, THE AIRCRAFT DID NOT RESPOND. THE PILOT SAID HE WAS CONCERNED ABOUT THE ABILITY OF THE AIRCRAFT TO CLIMB OVER TREES AND HIGHER TERRAIN BEYOND THE END OF THE RUNWAY, AND ABORTED THE TAKEOFF. THE PILOT WAS UNABLE TO STOP THE AIRCRAFT PRIOR TO OVERRUNNING THE DEPARTURE END OF THE 8,544-FOOT-LONG RUNWAY AND COLLIDING WITH AN AIRPORT BOUNDARY FENCE. THE DENSITY ALTITUDE FOR THE TAKEOFF IN A 90-DEGREE CROSSWIND CONDITION WAS COMPUTED AT 8,700 FEET. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1994_LAX94LA338.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗