ATL86LA260

NTSB accident investigation · Piper PA-23-250 · Montgomery, AL · September 20, 1986

Accident · No injuriesLimited investigationFinal report
Date
September 20, 1986, 10:22 local (15:22 UTC)
Place
Montgomery, AL
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N6041YPiper PA-23-250
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19860920045679A
Case key
7195

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(partial) - nonmechanicalTakeoff - initial climb
Reason for occurrence undeterminedCause
Forced landingDescent - emergency
Propeller system/accessories,feathering system - undetermined
Emergency procedure - not followedPilot in commandFactor
In flight collision with terrain/waterLanding - flare/touchdown
Wheels up landing - performedPilot in commandCause

Analysis

During initial climb phase of an experimental flt from mgm, AL, the plt rpted that the left engine had failed and an attempt was made to feather the prop. The plt radioed dannelly tower that the acft was returning to the arpt. Then the plt rpted that the right engine lost thrust, however the right prop was not feathered because he was not sure if the engine was producing power. A gear-up forced landing was made on a 4-lane highway. The acft engines were fueled with alcohol with approval of the FAA for research and development. Three days prior to the accident the acft experienced power surges and made a precautionary landing. No problems were found and the flight was continued. Inspection of the acft revealed the right prop feathered and the left prop in low pitch. The acft wgt and bal indicated approx. 400# over gross weight. The engines were successfully test run. There has been no determination as to the cause of the rpted engine failures.

Aircraft

Registration
N6041Y
Reported as
Piper PA-23-250
Category
Airplane
Serial number
27-3227
Airframe hours
3,355
Engine
Lycoming IO-540-C4B5, 250 horsepower, reciprocating
Damage
Substantial damage
Flight
Other work use · Part 91
Registered owner
Maxwell E. Shauck
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · April 14, 1986 · 48 hours before
Departed
MGM · Montgomery, AL
Destination
GSO · Greensboro, NC

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
50
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
8,295 total · 100 in this make and model · 8,187 as pilot in command · 100 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
120° at 3 knots
Visibility
6 statute miles
Lowest ceiling
25,000 ft broken
Temperature
81 °F, dew point 72 °F
Altimeter
30.00 inHg
Observed at
MGM, 5 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.