CEN23LA066

NTSB accident investigation · Beech A36 · Harrison, AR · December 19, 2022

Accident · No injuriesClass 3 · LimitedFinal report
Date
December 19, 2022, 15:05 local (21:05 UTC)
Place
Harrison, AR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N8137PBeech A36
Defining event
Approach: Unknown or undetermined
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Central Region
Parties
FAA Little Rock FSDO
FAA report
20221219019149A
Case key
106479

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A loss of engine power for reasons that could not be determined.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Engine (reciprocating)Aircraft › Aircraft power plant · Unknown/Not determinedBeech A36: 13 casesAll aircraft: 497 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot reported the airplane was topped off with fuel before the flight. He reported that the flight was normal, and he switched fuel tanks when he reached the initial approach fix for the instrument approach. The pilot then canceled his instrument clearance and continued a visual approach to the airport that was normal until he was on short final when the engine stopped producing power. The pilot stated he made one attempt to restore the engine power, which included switching fuel tanks. Unable to restore engine power, the pilot performed a forced landing to a field about one mile short of the runway. During the forced landing the airplane’s fuselage was substantially damaged and a postimpact fire ensued, consuming a majority of the fuselage. A postaccident examination of the engine revealed the engine had been exposed to the postimpact fire. Valvetrain continuity was established throughout the engine. The magnetos and spark plugs were functionally tested and performed normally. The cylinders were examined with a borescope and showed signs of normal wear. The engine fuel components were examined and appeared clear of debris. The remainder of the airplane’s fuel system could not be tested due to the postimpact fire. All of the metal propeller blades had chordwise scratches observed on the cambered side as well as nicks and gouges on the leading edges indicative of the propeller producing some amount of power at impact. The engine examination did not reveal any malfunction or failure that would have precluded normal operation of the engine; therefore, the cause of the reported loss of engine power could not be determined.

Factual narrative

On December 19, 2022, about 1505 central standard time, a Beech A36 airplane, N8137P, was substantially damaged when it was involved in an accident near Harrison, Arkansas. The pilot and passenger were not injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. The pilot reported the airplane was topped off with fuel before departure. He reported that the flight was normal, and he switched fuel tanks when he reached the initial approach fix for the RNAV 18 approach at the Boone County Airport (HRO), Harrison, Arkansas. He stated that he canceled his instrument clearance as he had visual contact with the airport and the approach to the airport was normal until he was on short final, when the engine stopped producing power. The pilot stated he made one attempt to restore the engine power, which included switching fuel tanks. Unable to restore engine power, the pilot performed a forced landing to a field about one mile short of the runway. During the forced landing the airplane’s fuselage was substantially damaged and a postimpact fire ensued, consuming a majority of the fuselage. The airplane was transported to a secure facility for further examination. The engine was examined, and it exhibited signs of exposure to the postimpact fire. All 12 spark plugs were removed, bench tested, and all operated normally. The rocker box covers and engine-driven fuel pump were removed. The propeller was rotated by hand and thumb compression, valvetrain continuity, and crankshaft continuity to the accessories were all established. The cylinders were inspected using a borescope and were unremarkable. Both magnetos were removed and operated using a powered drill. The ignition harness suffered thermal damage and could not be tested. The fuel flow divider was inspected and found unremarkable. All the fuel nozzles were clear of debris. The fuel-air mixture unit was examined. All arms remained connected to the unit and the throttle arm moved freely. The fuel screen was removed and clean of debris. All the metal propeller blades had chordwise scratches observed on the cambered side as well as nicks and gouges on the leading edges. Due to the postimpact fire, the airplane’s fuel system could not be thoroughly examined.

Aircraft

Registration
N8137P
Reported as
Beech A36
Category
Airplane
Serial number
E-2653
Built
1991
Airframe hours
5,018
Engine
Cont Motor IO-550-B, 300 horsepower, reciprocating
Damage
Substantial damage
Fire
On-Ground
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 12, 2022 · 12 hours before
Departed
KCMI · Kansas City, MO
Destination
KHRO · Harrison, AR
Flight plan
IFR
Airport
HRO

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
44
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
110° at 8 knots
Lowest ceiling
5,000 ft overcast
Temperature
37 °F, dew point 18 °F
Altimeter
30.21 inHg
Observed at
KHRO, 1 nm away
METAR
METAR KHRO 192053Z AUTO 11008KT OVC050 03/M08 A3021 RMK AO2 SLP238 T00331078 56018=

Docket · 6

The files NTSB released with the investigation on March 28, 2024, on NTSB’s docket system: statements, records, photos and specialists’ reports. 7.6 MB in all.

FAA reports on this event · 1

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