# NTSB NYC94LA053: Piper PA-23-250, N99BR, Parrfield, OH, March 6, 1994

- Type: NTSB accident investigation
- Classification: Accident · Minor injuries · Limited investigation · Final report
- Date: March 6, 1994, 09:02 local (14:02 UTC)
- Place: Parrfield, OH
- Coordinates: 39.950107, -82.009162 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=39.9501&lon=-82.0092&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: Minor injuries
- Injuries: 1 minor, 5 uninjured
- Status: Completed, report December 7, 1994
- Report: Approved by Office Director
- NTSB case key (mKey): 38732
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC94LA053
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/38732/pdf
- Page: https://openairdocs.org/ntsb/NYC94LA053

## Probable cause

The pilot's mismanagment of the fuel supply by the improper positioning of the fuel selector valves, which resulted in fuel starvation and the total loss of engine power.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Loss of engine power(total) - nonmechanical, cruise - normal
  - fluid,fuel - starvation (contributing factor)
  - in-flight planning/decision - improper, pilot in command (contributing factor)
  - fuel tank selector position - improper, pilot in command (contributing factor)
- Forced landing, descent - emergency
- On ground/water collision with object, landing
  - object - tree(s)

## Analysis

WHILE IN CRUISE FLIGHT AT 8000 FEET, BOTH ENGINES LOST POWER WITHIN 30 SECONDS OF EACH OTHER.  THE PILOT STATED HE WAS UNABLE TO GET EITHER ENGINE RESTARTED, ALTHOUGH THE ENGINES WOULD OCCASIONALLY RUN FOR 3 OR 4 SECONDS AND THEN STOP. ATC VECTORED THE AIRPLANE TOWARD AN AIRPORT, WHICH THE PILOT WAS UNABLE TO REACH, AND AN OFF-AIRPORT LANDING WAS DONE. THE PILOT REPORTED THAT AFTER THE ENGINES LOST POWER, HE SWITCHED THE FUEL SELECTOR FROM THE INBOARD TO THE OUTBOARD FUEL TANKS.  THE EXAMINATION OF THE AIRPLANE REVEALED ABOUT 3 TO 4 TABLESPOONS OF FUEL IN EACH CARBURETOR.  THE OUTBOARD FUEL TANKS WERE EMPTY; THE INBOARD FUEL TANKS CONTAINED FUEL.  THE LEFT FUEL SELECTOR WAS POSITIONED TO THE OUTBOARD TANKS.  THE RIGHT FUEL SELECTOR WAS DAMAGED AND ITS POSITION WAS NOT DETERMINED.

## Factual narrative

On March 5, 1994, at 0902 eastern standard time, a Piper PA-23-250, N99BR, lost power in both engines and made an off airport landing in an open field near Parrfield, Ohio.  The airplane received substantial damage.  One passenger received minor injuries, and the pilot and other passengers were not injured.  Visual meteorological conditions prevailed and the flight was operating on an instrument flight rules flight plan under 14 CFR Part 91.

In the NTSB Accident Report, the pilot stated:

...We had been flying for 2 hrs and 20 minutes on main      tanks which were full - 36 gal each - and should have      provided 3 hrs of cruise at 65 % power.  Without warning      the right engine lost power.  I immediately switched to      other main tank - also full - and moved mixture to rich      and props to full and fuel pumps on.  At about the end      of this process (about 30 sec. after right engine      failure) the left engine quit.  It turned left tank      selector to other main tank, checked mix rich - fuel      pumps on - and turned crossfeed valve on - no      response...I tried throttle positions - carb heat -      mags ck/on, pumps ck/on, x-feed ck/on - occasionally      one or the other engine would run for 3 - 4 seconds but      neither one continued to run.  The spurts of power did      not seem to be related to any of my actions.  When I      finally saw the airport and attempted to land, I did      not have enough altitude to reach the runway - final      approach was about 45 degrees left base/final.  When I      realized runway was out of reach, I leveled the wings      and landed.  The aircraft struck the ground wings      level, under control on a grassy area, at near stalling      speed, and slid into brush and small trees....

When interviewed the pilot said he moved the right fuel selector valve to the right inboard main tank and did not change its position again.  When the left engine failed a few seconds later, he was not certain although he believed he did position the left fuel selector valve to the left inboard main tank.

The fuel selector valves were controlled by 2, three position locking levers (Fwd - Outboard Mains, Middle - OFF, Aft - Inboard Mains) located between the seats and connected to the selector valves by cables.  A crossfeed valve handle was located between the two fuel selector handles.  When moved forward, crossfeed was selected on, and when moved aft, the crossfeed was turned off.

The airplane was examined by Mr. Jay Wilkins, an FAA Airworthiness Inspector from the Columbus Flight Standards District Office.  In a written statement, he reported both inboard wing tanks were full of fuel.  The right outboard tank was empty and the left outboard tank was damaged in the accident and had no fuel.  The right tip tank was empty and the left tip tank was damaged in the accident.  The right fuel shutoff valve [fuel selector valve] was damaged by impact and its pre-impact position was not determined.  The left fuel shutoff valve [fuel selector valve] operated normally in all positions.  No obstructions were found in the fuel lines leading to the carburetors, and no mechanical anomalies were found with the carburetors.  The fuel levels inside the float chambers of the carburetors were below the pickup level.

In a telephone interview, Mr. Wilkins reported that the cockpit control handles for the fuel valves were found in the forward position (outboard mains) and the cockpit control handle for the crossfeed was found forward (crossfeed on).  Although the left outboard fuel tank was ruptured, there was no smell of gasoline at the scene.  When the cockpit control handle for the left fuel valve was selected to a tank with fuel, fuel flowed via gravity, and when turned off no fuel flowed.  Due to impact damage the right fuel valve was disconnected from its actuation cables.  When the valve was positioned by hand to a tank with residual fuel in the line, fuel flowed via gravity.  When position to off, no fuel flowed.  Additionally, neither propeller had been feathered.

In the NTSB Form 6120.1/2, the pilot reported, he had a total time of 576 hours, with 30 hours in multi-engine airplanes and 24 hours in the Piper PA-23-250.

## Aircraft

- Registration: [N99BR](https://openairdocs.org/deregistered/N99BR-1995-07-03), registration cancelled 1995-07-03, S/N 27370 (OpenAirDocs)
- Reported make and model: PIPER PA-23-250
- Registry model: [Piper PA-23-250](https://openairdocs.org/model/piper-pa-23-250) (registry code 7102308) (OpenAirDocs)
- Category: Airplane
- Serial number: 27-370
- Airframe hours: 4147
- Engines: LYCOMING O-540-A1D5 250 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Michael E. Smucker,
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, January 15, 1994, 15 hours before
- Departed: LNS, LANCASTER, PA
- Destination: CGX, CHICAGO, IL
- Flight plan: IFR
- Airport: 42I, Parr, runway 28, 2,600 × 26 ft

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 43; private; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 3, valid medical--no waivers/lim.; seat: left; flight hours: 576 total, 24 in this make and model, 500 as pilot in command, 14 in the last 90 days, 14 in the last 30 days, 2 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 290° at 6 knots
- Visibility: 3 statute miles
- Lowest ceiling: none
- Temperature: 36 °F, dew point 30 °F
- Altimeter: 29.00 inHg
- Observed at: ZZV, 9 nm away

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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