ATL89FA035

NTSB accident investigation · Hughes 269C · Mohawk, TN · November 14, 1988

Accident · FatalField investigationFinal report
Date
November 14, 1988, 12:17 local (17:17 UTC)
Place
Mohawk, TN
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N9575FHughes 269C
Weather
Visual (VMC) · Day
Status
Completed · report January 24, 1990
Report
Approved by Office Director
Case key
7862

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

On this page

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 engine power(total) - mech failure/malfApproach - vfr pattern - downwind
Engine assembly,connecting rod bolt - fatigueCause
Maintenance,overhaul - inadequateOther maintenance personnelCause
Engine assembly,piston - burnedCause
Maintenance,100-hour inspection - inadequateCompany maintenance personnelFactor
Forced landingDescent - emergency
Loss of control - in flightDescent - emergency
In flight collision with terrain/waterDescent - uncontrolled
Autorotation - delayedCause
Rotor rpm - not maintainedPilot in command(cfi)Cause

Analysis

The helicopter had landed at a private airstrip and the instructor deplaned. The dual student remained in the helicopter with the engine running. The CFI reboarded and the student made the takeoff. Later, on downwind in traffic pattern, a witness reported a loud noise from the engine. The main rotor was observed to slow noticeably and the helicopter entered a very steep descent, impacting the ground about 1,000 feet south of the runway. The engine rod bolts on the number four cylinder had fractured. Examination of the flight controls revealed no evidence of preimpact failure. One of the rod bolts was metallurgically examined and showed cracking through 25 percent of the bolt. The fatigue was attributed to insufficient preload on the bolt. The engine had 813 hrs since a major overhaul and 36 hrs since annual inspection.

Aircraft

Registration
N9575F
Reported as
Hughes 269C
Category
Helicopter
Serial number
440295
Airframe hours
6,170
Engine
Lycoming HI0-360-D1A, 190 horsepower, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Registered owner
Bruce Hodges And Associates
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 21, 1988 · 36 hours before
Departed
PVT · Morristown, TN
Airport
PVT · Cooper Field, runway 27, 2,250 × 50 ft, grass/turf

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
41
Certificates
Flight instructor, Commercial
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
756 total · 604 in this make and model · 694 as pilot in command · 107 in the last 90 days · 53 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
55 °F, dew point -0 °F

Other investigations on N9575F · 1

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