NYC91LA040

NTSB accident investigation · Enstrom F-28C · Easton, PA · November 28, 1990

Accident · No injuriesLimited investigationFinal report
Date
November 28, 1990, 09:45 local (14:45 UTC)
Place
Easton, PA
Injuries
1 uninjured
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N4953XEnstrom F-28C
Weather
Visual (VMC) · Day
Status
Completed · report February 12, 1993
Report
Approved by Office Director
FAA report
19901128002069A
Case key
36852

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

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Probable cause

An inflight failure of the left side cabin mount bracket which resulted in a loss of lateral cyclic control. Factors related to the accident were: an incomplete inspection of the helicopter following a hard landing with a blade strike.

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.

Airframe/component/system failure/malfunctionCruise - normal
Rotorcraft flight control,cyclic bellcrank - failure,totalCause
Maintenance,rebuild/remanufacture - improperOther maintenance personnelCause
Maintenance,inspection - inadequateOther maintenance personnelCause
Maintenance,replacement - not performedOther maintenance personnelCause
Loss of control - in flightCruise - normal
Forced landingDescent - emergency
Roll overLanding - flare/touchdown
Aircraft control - not maintainedPilot in command
Remedial action - not possiblePilot in command

Analysis

In cruise flt the helicopter unexpectedly rolled 90 degrees left. The pilot autorotated to a landing, rolling over upon touchdown. The left side cabin mount bracket which holds the intermediate bellcrank for lateral control had fractured. The fracture surface bore evidence of overload and fatigue. The bellcrank was tight in the cabin mount bracket. In addition, the right side cabin mount bracket which hold the intermediate bellcrank for fore and aft control had a crack. The fracture surface was typical of overload. The helicopter had previously been involved in a hard landing with a blade strike on the tail boom. No records were available to indicate the repairs conducted. According to Enstrom helicopters, these fractures are typically seen following a blade strike. According to an Enstrom helicopters service letter, '...cyclic and collective torque tubes, bellcranks, and fitting...' Are required inspections items following a blade strike.

Aircraft

Registration
N4953X
Reported as
Enstrom F-28C
Category
Helicopter
Serial number
469
Airframe hours
2,450
Engine
Lycoming HIO-360-E1AD, 205 horsepower, reciprocating
Damage
Destroyed
Flight
Business · Part 91
Operator
Jerry Engel
Airworthiness certificate
Standard, Normal
Last inspection
Annual · March 12, 1990 · 25 hours before
Destination
TTN · Trenton, NJ

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
32
Certificate
Private
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
126 total · 107 in this make and model · 71 as pilot in command · 16 in the last 90 days · 3 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 8 knots
Visibility
3 statute miles
Lowest ceiling
4,500 ft overcast

FAA reports on this event · 1

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