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Aviation safety reports, made easier to study

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May 3, 1982 · Hughes 269C · N8963F

Flint, MI

Overview

Report Status
Preliminary report
Event Type
Accident
Date
May 3, 1982
Injury Outcomes
No injuries (2 uninjured)
Location
Flint, MI
Aircraft
Hughes 269C
Tail Number
N8963F
Operator
Don D Goble
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI82DA149

THE AIRCREW WERE ON AN INSTRUCTIONAL FLIGHT TO PREPARE THE STUDENT, A RATED PILOT, FOR A FLIGHT INSTRUCTOR RATING. AFTER PRACTICING SEVERAL AUTOROTATION APPROACHES, THE HELICOPTER WAS LANDED. THE INSTRUCTOR PILOT (IP) STATED THAT AFTER TOUCHDOWN, HE AND THE STUDENT WERE IN A DISCUSSION WHEN THEY HEARD A LOUD "POP". THE IP DEPLANED AND INSPECTED THE HELICOPTER, BUT FOUND NO IRREGULARITIES. THEY TOOK OFF AND PERFORMED ANOTHER AUTOROTATION. AFTER TOUCHDOWN, THE COLLECTIVE WAS LOWERED, THE HELICOPTER PITCHED LEFT AND FORWARD, AND THE ROTOR BLADES CONTACTED THE GROUND AND TAIL BOOM. AN INVESTIGATION REVEALED THAT THE LEFT FRONT SHOCK STRUT DAMPER ASSEMBLY, NO: 269A3150-5, HAD FAILED. TOTAL TIME ON THE PART WAS 3614 HRS. ACCORDING TO A METALLURIGICAL REPORT, A SINGLE OVERLOAD FRACTURE WAS FOUND AT THE CLEVIS ON THE PISTON END OF THE DAMPER. THE CFI DID NOT REPORT ANY HARD LANDINGS.

Full Narrative

THE AIRCREW WERE ON AN INSTRUCTIONAL FLIGHT TO PREPARE THE STUDENT, A RATED PILOT, FOR A FLIGHT INSTRUCTOR RATING. AFTER PRACTICING SEVERAL AUTOROTATION APPROACHES, THE HELICOPTER WAS LANDED. THE INSTRUCTOR PILOT (IP) STATED THAT AFTER TOUCHDOWN, HE AND THE STUDENT WERE IN A DISCUSSION WHEN THEY HEARD A LOUD "POP". THE IP DEPLANED AND INSPECTED THE HELICOPTER, BUT FOUND NO IRREGULARITIES. THEY TOOK OFF AND PERFORMED ANOTHER AUTOROTATION. AFTER TOUCHDOWN, THE COLLECTIVE WAS LOWERED, THE HELICOPTER PITCHED LEFT AND FORWARD, AND THE ROTOR BLADES CONTACTED THE GROUND AND TAIL BOOM. AN INVESTIGATION REVEALED THAT THE LEFT FRONT SHOCK STRUT DAMPER ASSEMBLY, NO: 269A3150-5, HAD FAILED. TOTAL TIME ON THE PART WAS 3614 HRS. ACCORDING TO A METALLURIGICAL REPORT, A SINGLE OVERLOAD FRACTURE WAS FOUND AT THE CLEVIS ON THE PISTON END OF THE DAMPER. THE CFI DID NOT REPORT ANY HARD LANDINGS.

Flight

Event TypeAccident
Event Time17:08 EDT
Nearest AirportBISHOP (0nm N)
Runway36
Runway Length7850 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269C
Tail NumberN8963F
Aircraft CategoryHeli
DamageSubstantial
OperatorDon D Goble
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360D1A · Reciprocating · 200
Seats3

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 30 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind20° @ 9 kt
Visibility14 sm
CeilingNone
Temperature / Dew Point16 C / 0 C
Altimeter30.00 inHg
Observation Time17:29

Appendix: Source Data