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Aviation safety reports, made easier to study

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January 28, 2021 · Beech 300 · N217US

Davenport, IA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
January 28, 2021
Injury Outcomes
No injuries (2 uninjured)
Location
Davenport, IA
Aircraft
Beech 300 (2007)
Tail Number
N217US
Operator
Carver Aero
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN21LA118

The pilot reported that during a simulated engine failure after decision speed (V1) takeoff, when the flight instructor reduced power on the airplane’s left engine during the takeoff roll, the airplane yawed left and veered toward the left edge of the runway where there was packed snow. The pilot reported that he applied right rudder and back pressure to rotate the airplane as the instructor pilot added right rudder with his set of rudder pedals. The instructor pilot reported he then attempted to restore left engine power as the airplane struck a snowbank on the edge of the runway. The airplane exited the left side of the runway and came to a stop. The airplane sustained substantial damage to the engine nacelles and the fuselage. The left engine was separated from the airplane and the right engine remained attached by skin. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The instructor pilot reported that the flight’s purpose was for the pilot to conduct training in a twin-engine turboprop airplane, in preparation of an upcoming checkride. The plan was to simulate an engine failure during the takeoff roll, after passing takeoff decision speed (V1). He added that the plan was briefed the day prior and that the speeds were calculated and confirmed in the primary flight display (PFD) before the takeoff. The instructor pilot added that the runway was plowed 75 ft wide, with patches of packed snow near the edges.

NTSB Probable Cause

The pilot’s failure to maintain directional control of the airplane, and the flight instructor’s inadequate oversight during a simulated engine out takeoff that resulted in a runway excursion and impact with a snowbank.

Full Narrative

The pilot reported that during a simulated engine failure after decision speed (V1) takeoff, when the flight instructor reduced power on the airplane’s left engine during the takeoff roll, the airplane yawed left and veered toward the left edge of the runway where there was packed snow. The pilot reported that he applied right rudder and back pressure to rotate the airplane as the instructor pilot added right rudder with his set of rudder pedals. The instructor pilot reported he then attempted to restore left engine power as the airplane struck a snowbank on the edge of the runway. The airplane exited the left side of the runway and came to a stop. The airplane sustained substantial damage to the engine nacelles and the fuselage. The left engine was separated from the airplane and the right engine remained attached by skin. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The instructor pilot reported that the flight’s purpose was for the pilot to conduct training in a twin-engine turboprop airplane, in preparation of an upcoming checkride. The plan was to simulate an engine failure during the takeoff roll, after passing takeoff decision speed (V1). He added that the plan was briefed the day prior and that the speeds were calculated and confirmed in the primary flight display (PFD) before the takeoff. The instructor pilot added that the runway was plowed 75 ft wide, with patches of packed snow near the edges.

Flight

Event TypeAccident
Event Time16:10 CST
Nearest AirportDavenport (1nm)
Runway15
Runway Length5511 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech 300
Tail NumberN217US
Aircraft CategoryAir
DamageSubstantial
OperatorCarver Aero
Operating RulePart 91
Engines2
Engine TypeTurboprop
Engine DetailsP &W · PT-6A-60A · Turboprop | P &W · PT-6A-60A · Turboprop

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 61 · First Class · None
Crew 2Age 58 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind70° @ 8 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point21 C / 9 C
Altimeter30.59 inHg
Observation Time16:10
Weather SourceWFAC

Appendix: Source Data