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GAA17CA303

2017-05-24 · Perris, California, United States · None · 1 aircraft · Status: Completed

Airport L65

Current FAA registration · N708PV

Make / Model
DEHAVILLAND DHC-6-300
Year of manufacture
1976 · 41 years old at event
Engine
P&W PT6A SER (750 hp)
Seats / Engines
22 seats · 2 engines
Last airworthiness date
19980514
ADS-B equipped
Yes — Mode-S A9739F

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The prospective pilot’s improper landing flare and the pilot’s delayed remedial action to initiate a go-around, which resulted in a runway excursion.

Factual narrative

The pilot of the twin-engine, turbine powered airplane reported that while providing flights for skydivers throughout the day, he had a potential new hire pilot flying with him in the right seat. He added that on the eighth flight of the day, the new pilot was flying during the approach and "approximately 200' [ft.] south from the threshold of [runway] 15 at approximately 15 feet AGL [above ground level] the bottom violently and unexpectedly dropped out. [He] believe[d] some kind of wind shear caused the aircraft [to] slam onto [the] runway and bounce into the air at a 45 to 60-degree bank angle to the right." The new pilot then said, "you got it". The pilot took the control and initiated a go around by increasing power which aggravated the "off runway heading". The right wing contacted the ground, the airplane exited the runway to the right, impacted a fuel truck and the right-wing separated from the airplane. The impact caused the pilot to unintentionally add max power and the airplane, with only the left engine functioning ground looped to the right, coming to rest nose down. The airplane sustained substantial damage to the fuselage and right wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation system about 8 nautical miles from the accident site, about the time of the accident, reported the wind from 280° at 7 knots, visibility 10 statute miles, few clouds at 20,000 ft. AGL, temperature 86°F, dew point 45°F, and altimeter 29.81 in Hg. The pilot landed on runway 15. The pilot of the twin-engine, turbine-powered airplane reported that, while providing flights for skydivers throughout the day, he had a potential new hire pilot flying with him in the right seat. He added that, on the eighth flight of the day, the new pilot was flying during the approach and "approximately 200' [ft.] south from the threshold of [runway] 15 at approximately 15 feet AGL [above ground level] the bottom violently and unexpectedly dropped out. [He] believe[d] some kind of wind shear caused the aircraft [to] slam onto [the] runway and bounce into the air at a 45 to 60-degree bank angle to the right." The prospective pilot then said, "you got it." The pilot took control of the airplane and initiated a go-around by increasing power, which aggravated the "off runway heading." The right wing contacted the ground, the airplane exited the runway to the right and impacted a fuel truck, and the right wing separated from the airplane. The impact caused the pilot to unintentionally add max power, and the airplane, with only the left engine functioning, ground looped to the right, coming to rest nose down. The airplane sustained substantial damage to the fuselage and right wing. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The automated weather observation system about 8 nautical miles from the accident site reported that, about the time of the accident, the wind was from 280° at 7 knots, visibility 10 statute miles, few clouds at 20,000 ft agl, temperature 86°F, dew point 45°F, and altimeter 29.81 inches of mercury. The pilot landed on runway 15. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Not attained/maintained - C
  • C Personnel issues-Task performance-Use of equip/info-Aircraft control-Copilot - C
  • C Personnel issues-Action/decision-Action-Delayed action-Pilot - C
  • — Environmental issues-Conditions/weather/phenomena-Wind-Windshear-Effect on operation
  • — Environmental issues-Physical environment-Object/animal/substance-Ground vehicle-Contributed to outcome

Verbatim from NTSB's published report. Source file NTSB_2017_GAA17CA303.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (wind shear, runway excursion, go-around). All research papers