FTW91FA123

NTSB accident investigation · Hughes 269B · Brickeys, AR · July 18, 1991

Accident · FatalField investigationFinal report
Date
July 18, 1991, 07:25 local (12:25 UTC)
Place
Brickeys, AR
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N11XCHughes 269B
Weather
Visual (VMC) · Day
Status
Completed · report April 23, 1993
Report
Approved by Office Director
FAA report
19910718027969A
Case key
23269

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

The failure of the clutch control cable due to fraying which initiated the forced landing and the operator's failure to perform recommended inspections on the aircraft. Factors were the pilot's failure to maintain rotor RPM and the unsuitable terrain.

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
Rotor drive system,clutch assembly - failure,total
Rotor drive system,clutch assembly - separation
Rotor drive system,clutch assembly - frayedCause
Maintenance,service bulletin/letter - not performedCompany maintenance personnelCause
Forced landingDescent - emergency
Terrain condition - none suitableFactor
In flight collision with terrain/waterDescent - uncontrolled
Rotor rpm - not maintainedPilot in commandFactor

Analysis

The aircraft impacted vertically in a heavily wooded swamp. Evidence indicated that the aircraft impacted with a high vertical rate of descent and low rotor RPM. Investigation revealed that the belt drive clutch engagement cable had separated due to abrasion caused by internal contact between the cable and assembly components. Separation of the cable resulted in a disconnect between the engine and the transmission. Review of the aircraft maintenance records could not determine the exact total time on the cable; however, the records did indicate that the cable had last been disassembled and inspected about 636.8 hours before the accident. A manufacturer's service information notice had been issued on the cable assembly which required an initial inspection within 50 hours and a recurring inspection every 400 hours thereafter, until the unit was replaced with an improved model. The aircraft maintenance records did not indicate compliance with the information notice; however, the operator stated that the inspections were being performed.

Aircraft

Registration
N11XC
Reported as
Hughes 269B
Category
Helicopter
Serial number
64-102
Airframe hours
3,877
Engine
Lycoming HIO-360-A1A, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Aerial observation · Part 91
Operator
Southern Flying Service, Inc.
Registered owner
Southern Flying Service, Inc.
Airworthiness certificate
Standard, Normal; Standard, Utility
Last inspection
100 hour · July 14, 1992 · 17 hours before
Departed
MO1 · Memphis, TN
Destination
55M · Star City, AR

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
50
Certificates
Private, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Helicopter
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
6,498 total · 539 in this make and model · 6,598 as pilot in command · 266 in the last 90 days · 74 in the last 30 days · 8 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
100° at 4 knots, gusting 2
Visibility
15 statute miles
Lowest ceiling
12,000 ft broken
Temperature
75 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
MEM, 28 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.

Other investigations on N11XC · 4

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