# NTSB NYC94LA043: Beech A-36-TC, N3736F, Hillsboro, NH, December 26, 1993

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: December 26, 1993, 16:15 local (21:15 UTC)
- Place: Hillsboro, NH
- Location: 43.1156° N, 71.8968° W: Placed by OpenAirDocs: center of Hillsborough, NH, within about 6 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=43.1156&lon=-71.8968&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 2 uninjured
- Status: Completed, report September 26, 1994
- Report: Approved by Office Director
- NTSB case key (mKey): 38723
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC94LA043
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/38723/pdf
- Page: https://openairdocs.org/ntsb/NYC94LA043

## Probable cause

LOSS OF ENGINE POWER FOR UNDETERMINED REASONS.

## Sequence of events

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

- Loss of engine power, cruise
  - reason for occurrence undetermined (cause)
- Forced landing, descent - emergency
- In flight collision with terrain/water, landing
  - terrain condition - none suitable (contributing factor)

## Analysis

THE PILOT DEPARTED ON A CROSS COUNTRY FLIGHT AND CLIMBED TO AN ALTITUDE OF 10,500 FEET.  THE OUTSIDE AIR TEMPERATURE AT THIS ALTITUDE WAS MINUS 34 DEGREES CENTIGRADE.  AFTER CRUISING FOR ABOUT 30 MINUTES THE ENGINE BEGAN TO RUN ROUGH AND THE FUEL FLOW INCREASED FROM 18 TO 25 GALLONS PER HOUR.  THE PILOT INITIATED A DESCENT AND TRIED CHANGES IN MIXTURE AND BOOST PUMP SETTINGS, AND CHANGED FUEL TANK SELECTION.  BETWEEN 3000 AND 4000 FEET, AND AN AIRSPEED OF 120 KNOTS, THE ENGINE STOPPED COMPLETELY.  THE PILOT  OBSERVED AN AIRPORT RUNWAY ABOUT 1/2 MILE AHEAD OF HIM.  THE PILOT DID NOT THINK HE COULD MAKE THE RUNWAY AND LANDED GEAR-UP IN A SWAMP.  INVESTIGATION REVEALED THAT THERE WAS FUEL IN BOTH WING TANKS.  AN ENGINE RUN WAS ACCOMPLISHED AND NO DISCREPANCIES WERE NOTED.

## Factual narrative

On December 26, 1993, about 1615 eastern standard time, a Beech A-36-TC, N3736F, owned and piloted by Wright B. Lewis, was substantially damaged during a forced landing to the Hawthorne- Feather Airpark, Hillsboro, New Hampshire.  The pilot and passenger were not injured.  Visual meteorological conditions prevailed.  A flight plan had not been filed for the flight operating under 14 CFR 91.

In the NTSB Form 6120.1/2, the pilot stated he departed the Morrisville Airport about 1530, and climbed to 10,500 feet.  After cruising for 30 minutes his engine began to run rough and his fuel flow increased from 18 gallons per hour (GPH) to 25 GPH without any changes in the mixture control.  He initiated a descent to a nearby airport.  During the descent he tried changes in the mixture and boost pump settings, and changed his fuel tank selection.

The pilot further stated:

"...The engine quit completely between 3000' [feet] and 4000'.  My airspeed was 120K [knots].  I spotted the runway about 1/2 mile ahead while heading southeast...I realized I would not make the runway at about 1000' and leveled the wings at about 90K - glided between a tree line and landed gear up in a swamp..."

A Federal Aviation Administration (FAA) Inspector's report stated that a post accident investigation revealed fuel in both wing tanks, and that the landing gear was retracted.  He further stated, "...All flight controls functioned normally...the fuel gauges read approximately half full on the left and full on the right..."

An examination of the engine was performed by an Airframe and Powerplant (A&P) Mechanic on January 21, 1994, at the Hawthorne- Feather Airpark (8B1).  During the examination no contamination was found in fuel system.  A test propeller was installed and the engine was run.  In his report the A&P stated, "...Run up and operational check all limits within factory specifications ... Complete inspection after run and found no discrepancies or problems..."

ADDITIONAL INFORMATION

The National Weather Service reported the temperature at 10,000 feet in the Portland, Maine area to be a minus 34 degrees celsius (minus 30 degrees fahrenheit) at the time of the accident.

The Pilot's Operating Handbook does not address fuel additives for cold weather operations.

Teledyne Continental Motors published a service bulletin on November 1987.  The subject of this bulletin was recommended fuel and oil grades.  In the bulletin it states:

"Under certain ambient conditions of temperature/      humidity, water can be supported in the fuel in      sufficient quantities to create restrictive ice      formation along various segments of fuel system.  To      alleviate the possibility of this occurring, it is      permissible to add isopropyl Alcohol to the fuel      supply...Also, ethylene glycol monomethyl ether      compounds conforming to military specification MIL-1-      27686E, if approved for use in the aircraft fuel system      by the aircraft manufacturer..."

In a letter from the owner of a Beech 36TC, he stated that the previous owner of his airplane experienced 3 unexplained cold weather engine failures.  He further stated that by adding Prist to the fuel "...We haven't seen the problem since."

In another FAA Inspector's report, he stated:

"...All indications are that Mr. Lewis' engine was a      victim of the severe cold weather...It is uncommon to      this office, but, as indicated by operators having      aircraft with Continental IO-520 engines installed,      this is not uncommon.  The answer to this problem is to      add LO-FLO-PRIST..."

## Aircraft

- Registration: N3736F (not matched to a registry record)
- Reported make and model: BEECH A-36-TC
- Category: Airplane
- Serial number: EA-148
- Airframe hours: 1756
- Engines: CONTINENTAL TSIO-520-UB 300 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Wright B. Lewis
- Airworthiness certificate: Standard, Normal
- Departed: MVL, MORRISVILLE, VT
- Destination: PVD, PROVIDENCE, RI
- Airport: 8B1, Hawthokrne-Feather, runway 2, 3,260 × 75 ft, asphalt

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 60; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, valid medical--no waivers/lim.; seat: left; flight hours: 6,000 total, 1,100 in this make and model, 5,500 as pilot in command, 19 in the last 90 days, 6 in the last 30 days, 1 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 250° at 15 knots, gusting 25
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 10 °F, dew point -0 °F
- Altimeter: 29.00 inHg
- Observed at: EEN, 19 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 (OpenAirDocs).

- [Accident 19931226052589A](https://openairdocs.org/incident/19931226052589A), Dec 26, 1993: Beech A36TC, Hillsboro, NH, Substantial damage. Rough engine at FL100. Diverted to 8B1. Engine quit. Landed gear up in swamp. Ice in fuel. 30 degrees below zero.

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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