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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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NTSB Report

August 17, 1992 · Piper PA-24-180 · N5981P

Russellville, AR

Overview

Report Status
Probable Cause
Event Type
Accident
Date
August 17, 1992
Injury Outcomes
No injuries (1 uninjured)
Location
Russellville, AR
Aircraft
Piper PA-24-180
Tail Number
N5981P
Operator
Hargus Herbert H
Injuries
None
Aircraft Damage
Substantial
NTSB Number
FTW92LA210

THE PILOT, WHO WAS ALSO THE MECHANIC, WAS PERFORMING AN IN FLIGHT RIGGING CHECK OF THE AIRPLANE. DURING CLIMB, A POP SOUND WAS HEARD AND PROPELLER THRUST WAS LOST. MOVEMENT OF THE PROPELLER CONTROL HAD NO EFFECT AND AN EMERGENCY DESCENT WAS INITIATED BY THE PILOT. A 35 TO 40 DEGREE NOSE DOWN ATTITUDE WAS REQUIRED TO MAINTAIN 85 KNOTS DURING THE FORCED LANDING TO A ROAD. THE ENGINE WAS NOT SECURED BY THE PILOT. A HARD LANDING OCCURRED AT AN ESTIMATED 1,800 FEET PER MINUTE DESCENT RATE, ACCORDING TO THE PILOT. THE PROPELLER SYSTEM WAS TORN DOWN AND TWO STAKING PINS WERE MISSING. THE GUIDE COLLAR, ROD, FORK, AND PISTON HAD ROTATED AROUND THE HUB. THE PROPELLER BLADES WERE DISCONNECTED FROM THE PITCH CHANGE MECHANISM. THE PROPELLER ASSEMBLY HAD BEEN OVERHAULED AND INSTALLED ON THE AIRCRAFT APPROXIMATELY 31.7 HOURS PRIOR TO THE FAILURE.

NTSB Probable Cause

THE PILOT'S IMPROPER FLARE. FACTORS WERE THE PROPELLER SYSTEM'S PITCH CHANGE MECHANISM DISCONNECTED DUE TO IMPROPER OVERHAUL AND FAILURE TO INSTALL THE STAKING PINS BY OTHER MAINTENANCE PERSONNEL.

Full Narrative

THE PILOT, WHO WAS ALSO THE MECHANIC, WAS PERFORMING AN IN FLIGHT RIGGING CHECK OF THE AIRPLANE. DURING CLIMB, A POP SOUND WAS HEARD AND PROPELLER THRUST WAS LOST. MOVEMENT OF THE PROPELLER CONTROL HAD NO EFFECT AND AN EMERGENCY DESCENT WAS INITIATED BY THE PILOT. A 35 TO 40 DEGREE NOSE DOWN ATTITUDE WAS REQUIRED TO MAINTAIN 85 KNOTS DURING THE FORCED LANDING TO A ROAD. THE ENGINE WAS NOT SECURED BY THE PILOT. A HARD LANDING OCCURRED AT AN ESTIMATED 1,800 FEET PER MINUTE DESCENT RATE, ACCORDING TO THE PILOT. THE PROPELLER SYSTEM WAS TORN DOWN AND TWO STAKING PINS WERE MISSING. THE GUIDE COLLAR, ROD, FORK, AND PISTON HAD ROTATED AROUND THE HUB. THE PROPELLER BLADES WERE DISCONNECTED FROM THE PITCH CHANGE MECHANISM. THE PROPELLER ASSEMBLY HAD BEEN OVERHAULED AND INSTALLED ON THE AIRCRAFT APPROXIMATELY 31.7 HOURS PRIOR TO THE FAILURE.

Flight

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

Aircraft

AircraftPiper PA-24-180
Tail NumberN5981P
Aircraft CategoryAir
DamageSubstantial
OperatorHargus Herbert H
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360-A1A · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 43 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data