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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

September 7, 1994 · Schweizer 269C · N61245

Grand Forks, ND

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 7, 1994
Injury Outcomes
No injuries (2 uninjured)
Location
Grand Forks, ND
Aircraft
Schweizer 269C
Tail Number
N61245
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI94LA316

THE FLIGHT INSTRUCTOR (CFI) REPORTED HE AND THE STUDENT PILOT WERE PRACTICING SIMULATED EMERGENCY AUTOROTATIONS TO A POWER RECOVERY. DURING THE ACCIDENT AUTOROTATION, THE CFI SAID HE ADJUSTED THE POWER TO 3100 RPM AND THEN TOLD THE STUDENT TO RECOVER. THE CFI NOTICED THAT THE HELICOPTER'S DESCENT HAD NOT BEEN ARRESTED, AND HE JOINED THE STUDENT ON THE CONTROLS. THE CFI WAS ATTEMPTING TO AUTOROTATE WHEN THE HELICOPTER LANDED HARD. POSTACCIDENT INSPECTION OF THE HELICOPTER AND ITS ENGINE DISCOVERED NO EVIDENCE OF PREIMPACT MECHANICAL ANOMALIES.

NTSB Probable Cause

the pilot-in-command's (CFI) delayed recovery from a practice autorotation. A factor associated with the accident was the student pilot's improper autorotation.

Full Narrative

On September 7, 1994, about 1124 central daylight time, a Schweizer 269C helicopter, N61245, sustained substantial damage when it landed hard during a practice autorotation near Grand Forks, North Dakota. The certificated flight instructor and student pilot aboard reported no injuries. The local, instructional flight operated without flight plan in visual meteorological conditions. The flight instructor reported he and the student had practiced several successful autorotations. The final, accident autorotation was to be with a power recovery. The instructor said he adjusted the throttle to 3100 RPM, and told the student to recover. When the rate of descent was not arrested, the instructor joined the student on the controls and attempted to autorotate just prior to ground collision. Postaccident inspection of the helicopter discovered no evidence of preimpact mechanical anomaly. The helicopter's engine was started and accelerated without any observed deficiencies.

Flight

Event TypeAccident
Event Time11:24 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftSchweizer 269C
Tail NumberN61245
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-DIA · Reciprocating · 190
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 28 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind360° @ 7 kt
Visibility15 sm
CeilingNone
Temperature / Dew Point64 F / 48
Altimeter30.00 inHg
Observation Time11:51
Weather SourcePILO

Appendix: Source Data