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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

April 16, 1996 · Bell 206B III · N2750F

San Diego, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
April 16, 1996
Injury Outcomes
No injuries (2 uninjured)
Location
San Diego, CA
Aircraft
Bell 206B III
Tail Number
N2750F
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX96LA172

While practicing touchdown autorotations, the helicopter landed hard on uneven terrain short of the intended touchdown point. The commercial pilot-rated student was demonstrating a autorotation with a turn to the runway. As he completed the turn and was aligning with the runway, the helicopter rotor rpm dropped to 70 percent. Halfway into the maneuver the flight instructor realized the helicopter was too low and slow to accomplish a power recovery and took control. The helicopter landed short of the runway in rough terrain. A postflight inspection of the helicopter revealed wrinkles in the tail boom. The pilot under instruction held a rotorcraft helicopter rating.

NTSB Probable Cause

the student's failure to maintain adequate main rotor rpm and airspeed during a practice autorotation, and the instructor's inadequate supervision of the flight.

Full Narrative

On April 16, 1996, at 1600 hours Pacific daylight time, a Bell 206B III helicopter, N2750F, landed hard on uneven terrain while practicing touchdown autorotations at Montgomery Field, San Diego, California. The helicopter sustained substantial damage. The certified flight instructor (CFI) and the certificated commercial pilot student were not injured. The helicopter was being operated as an instructional flight under 14 CFR Part 91 when the accident occurred. The local flight originated from Montgomery Field. Visual Instrument meteorological conditions prevailed. The CFI indicated that the commercial pilot was demonstrating an autorotation with a turn from 200 feet above ground level to runway 23. As the commercial pilot completed the turn and was aligning with the runway, the helicopter rotor rpm dropped to 70 percent. According to the CFI, halfway into the maneuver he realized the helicopter was too low and slow to accomplish a power recovery. The flight instructor took control of the helicopter. The helicopter touched down short of the intended point on the runway in rough uneven terrain. Post-flight inspection of the helicopter revealed wrinkles in the tail boom. The commercial pilot under instruction held a rotorcraft helicopter rating. The surface winds at Montgomery Field at the time were reported from 240 degrees at 11 knots.

Flight

Event TypeAccident
Event Time16:00 PDT
Nearest AirportMontgomery Field (0nm)
Runway23
Runway Length3402 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B III
Tail NumberN2750F
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 34 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind240° @ 11 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point70 F / 59
Altimeter30.00 inHg
Observation Time22:48
Weather SourceWFAC

Appendix: Source Data