LAX92FA154

NTSB accident investigation · Hughes 269C · Hesperia, CA · March 28, 1992

Accident · FatalField investigationFinal report
Date
March 28, 1992, 13:50 local (21:50 UTC)
Place
Hesperia, CA
Injuries
1 fatal, 1 serious
Damage
Destroyed
Phase of flight
Landing
Aircraft
N9597FHughes 269C
Weather
Visual (VMC) · Day
Status
Completed · report June 30, 1993
Report
Approved by Office Director
FAA report
19920328007779A
Case key
27414

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A failure of the student pilot to maintain adequate rotor RPM. Contributing to the accident was a failure of the instructor pilot to adequately supervise the training flight and a delay in correcting a low rotor RPM condition.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightLanding
Rotor rpm - not maintainedDual studentCause
Remedial action - delayedPilot in command(cfi)Factor
Supervision - inadequatePilot in command(cfi)Factor
In flight collision with terrain/waterLanding - flare/touchdown
Terrain condition - mountainous/hilly

Analysis

The certificated flight instructor and a private pilot/commercial student, were on a dual instructional flight in a helicopter, to practice pinnacle approaches, landings, and takeoffs. The area of landing was located at about 3,600 feet MSL, near the top of a steep mountain ridge. Two approaches to the pinnacle landing zone resulted in one go-around, and one landing. The instructor pilot reported that the student tended to allow the main rotor RPM to droop when adding power to terminate the landing approach. On the third approach, the RPM again started to decrease. The instructor pilot took control of the helicopter and attempted to increase the throttle setting and decrease collective pitch to recover from the low rotor RPM condition. Main rotor RPM continued to decrease and the instructor attempted to land at the edge of the ridge. The helicopter slid backwards over the edge of the mountain and began to break apart, tumbling 600 feet down the mountain side. A post crash fire erupted during the break-up sequence. The instructor was ejected from helicopter. The student remained in the wreckage and received fatal injuries. The post accident wreckage examination disclosed no evidence of any preexisting mechanical failures or malfunctions.

Aircraft

Registration
N9597F
Reported as
Hughes 269C
Category
Helicopter
Serial number
640314
Airframe hours
5,700
Engine
Lycoming HIO-360-D1A, 190 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Instructional · Part 91
Operator
Mojave Aviation Inc.
Registered owner
Mojave Aviation Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · February 24, 1992 · 18 hours before

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Certificates
Airline transport, Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Right
Flight hours
7,630 total · 250 in this make and model · 106 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 7 knots
Visibility
30 statute miles
Lowest ceiling
None
Temperature
64 °F, dew point 45 °F
Altimeter
29.00 inHg
Observed at
VCV, 20 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.