MIA90FA117

NTSB accident investigation · Hughes 269C · Fort Pierce, FL · May 9, 1990

Accident · Minor injuriesField investigationFinal report
Date
May 9, 1990, 16:03 local (20:03 UTC)
Place
Fort Pierce, FL
Injuries
2 minor
Damage
Destroyed
Phase of flight
Landing
Aircraft
N58275Hughes 269C
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 1991
Report
Approved by Office Director
FAA report
19900509016489A
Case key
32559

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

Improper touchdown during the autorotation by the dual student (ATP), his failure to maintain runway alignment, inadequate supervision by the CFI, and inadequate crew coordination. A factor related to the accident was the obstruction (taxiway light).

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 - on ground/waterLanding
Emergency procedure - simulatedPilot in command(cfi)
Autorotation - performedDual student
Touchdown - improperDual studentCause
Proper alignment - not maintainedDual studentCause
Supervision - inadequatePilot in command(cfi)Cause
Crew/group coordination - inadequateCause
Relinquishing of control - not performedDual student
On ground/water collision with objectLanding
Object - runway lightFactor
Roll overLanding

Analysis

The helicopter was on a VFR climbout from a parallel taxiway. The CFI, who was also the PIC, was providing instruction to an ATP working towards a CFI rating. The CFI initiated a simulated engine failure at 200 feet AGL and 60 KTS. The ATP began an autorotation. After completing the deceleration and initial pitch pull, the helicopter contacted the ground, bounced up, and slid to the right and rearward. The ATP saw a taxiway light and increased collective to avoid a collision, but experienced resistance on the flight controls. The CFI had not seen the taxiway light, but noticed a decay in engine/rotor RPM. He immediately applied downward pressure on the collective and left forward cyclic to stop the horizontal movement and level the helicopter. The CFI stated that he informed the ATP, he had the flight controls, which could not be substantiated by the ATP. The helicopter struck the taxiway light and taxiway with the right skid, then entered a dynamic rollover.

Aircraft

Registration
N58275
Reported as
Hughes 269C
Category
Helicopter
Serial number
1190849
Airframe hours
3,559
Engine
Lycoming HIO-360-D1A, 200 horsepower, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Operator
Flight Safety International
Registered owner
Flight Safety International
Airworthiness certificate
Standard, Normal
Last inspection
Continuous airworthiness · May 4, 1990 · 14 hours before
Departed
VRB · Vero Beach, FL
Airport
FPR · St Lucie County Intl

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
36
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter, Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
2,800 total · 500 in this make and model · 2,700 as pilot in command · 150 in the last 90 days · 80 in the last 30 days · 5 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 15 knots, gusting 25
Visibility
10 statute miles
Lowest ceiling
15,000 ft broken
Temperature
82 °F
Altimeter
30.00 inHg
Observed at
FPR

FAA reports on this event · 1

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

Other investigations on N58275 · 2

Matched to the same aircraft by N-number and date.