FTW92LA210

NTSB accident investigation · Piper PA-24-180 · Russellville, AR · August 17, 1992

Accident · No injuriesLimited investigationFinal report
Date
August 17, 1992, 15:45 local (20:45 UTC)
Place
Russellville, AR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N5981PPiper PA-24-180
Weather
Visual (VMC) · Day
Status
Completed · report September 14, 1993
Report
Approved by Office Director
FAA report
19920817032019A
Case key
18555

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 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.

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/malfunctionClimb
Propeller system/accessories,pitch change mech - disconnectedFactor
Maintenance,overhaul - improperOther maintenance personnelFactor
Forced landingDescent - emergency
Hard landingLanding - flare/touchdown
Proper descent rate - exceededPilot in command
Flare - improperPilot in commandCause

Analysis

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.

Aircraft

Registration
N5981P
Reported as
Piper PA-24-180
Category
Airplane
Serial number
24-1074
Airframe hours
2,265
Engine
Lycoming O-360-A1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Operator
Hargus, Herbert H.
Registered owner
Hargus, Herbert H.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 7, 1992
Departed
MO6

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
43
Certificate
Commercial
Airplane ratings
Single-engine land, Single-engine sea, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
9,350 total · 100 in this make and model · 9,300 as pilot in command · 140 in the last 90 days · 20 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F
Altimeter
30.00 inHg

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 N5981P · 2

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