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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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May 27, 1982 · Hughes 500D · N277SP

Amarillo, TX

Overview

Report Status
Preliminary report
Event Type
Accident
Date
May 27, 1982
Injury Outcomes
No injuries (1 uninjured)
Location
Amarillo, TX
Aircraft
Hughes 500D
Tail Number
N277SP
Operator
Southwestern Public Service
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW82DA195

THE PILOT REPORTED THAT HE WAS PRACTICING AUTOROTATIONS. WHEN HE ADDED POWER TO RECOVER FROM HIS EIGHTH AUTOROTATION, HE EXPERIENCED COMPRESSOR STALLS IN THE ENGINE AND A COMPLETE LOSS OF POWER AT ABOUT 20 FT AGL. THE HELICOPTER SETTLED AND MADE A HARD TOUCHDOWN. DURING TOUCHDOWN, THE MAIN ROTOR BLADES FLEXED DOWNWARD AND CHOPPED OFF THE TAIL BOOM. THE ENGINE WAS TRANSPORTED TO A TEST CELL WHERE IT WAS RUN UP IN AN "AS IS" CONDITION. IT OPERATED NORMALLY WITH A POWER OUTPUT OF 4.29% ABOVE THE MINIMUM REQUIRED. NO DISCREPANCIES WERE FOUND EXCEPT THERE WAS A MODERATE AIR LEAK FROM THE ANTI-ICE VALVE. THE VALVE WAS REPLACED AND THE ENGINE THEN PRODUCED 5.95% ABOVE THE MINIMUM REQUIRED POWER. THE ENGINE WAS THEN COMPLETELY DISASSEMBLED AND INSPECTED AND ALL PARTS WERE FOUND TO BE IN SATISFACTORY CONDITION. THE DENSITY ALTITUDE AT THE TIME OF THE ACCIDENT WAS ABOUT 5100 FT.

Full Narrative

THE PILOT REPORTED THAT HE WAS PRACTICING AUTOROTATIONS. WHEN HE ADDED POWER TO RECOVER FROM HIS EIGHTH AUTOROTATION, HE EXPERIENCED COMPRESSOR STALLS IN THE ENGINE AND A COMPLETE LOSS OF POWER AT ABOUT 20 FT AGL. THE HELICOPTER SETTLED AND MADE A HARD TOUCHDOWN. DURING TOUCHDOWN, THE MAIN ROTOR BLADES FLEXED DOWNWARD AND CHOPPED OFF THE TAIL BOOM. THE ENGINE WAS TRANSPORTED TO A TEST CELL WHERE IT WAS RUN UP IN AN "AS IS" CONDITION. IT OPERATED NORMALLY WITH A POWER OUTPUT OF 4.29% ABOVE THE MINIMUM REQUIRED. NO DISCREPANCIES WERE FOUND EXCEPT THERE WAS A MODERATE AIR LEAK FROM THE ANTI-ICE VALVE. THE VALVE WAS REPLACED AND THE ENGINE THEN PRODUCED 5.95% ABOVE THE MINIMUM REQUIRED POWER. THE ENGINE WAS THEN COMPLETELY DISASSEMBLED AND INSPECTED AND ALL PARTS WERE FOUND TO BE IN SATISFACTORY CONDITION. THE DENSITY ALTITUDE AT THE TIME OF THE ACCIDENT WAS ABOUT 5100 FT.

Flight

Event TypeAccident
Event Time15:45 CDT
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 500D
Tail NumberN277SP
Aircraft CategoryHeli
DamageSubstantial
OperatorSouthwestern Public Service
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C20B · Turboshaft · 375
Seats7

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 32 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind205° @ 10 kt
Visibility8 sm
CeilingBroken clouds 4000 ft
Temperature / Dew Point16 C / 0 C
Altimeter29.00 inHg
Observation Time15:53

Appendix: Source Data