CEN21LA457

NTSB accident investigation · Beech 95-B55 (T42A) · Lancaster, OH · September 24, 2021

Accident · Serious injuriesClass 4 · LimitedFinal report
Date
September 24, 2021, 13:07 local (17:07 UTC)
Place
Lancaster, OH
Injuries
1 serious, 1 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N85RRBeech 95-B55 (T42A)
Defining event
Approach: Fuel starvation
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Central Region
Parties
FAA FSDO
FAA report
20210924016369A
Case key
103975

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 loss of engine power due to fuel starvation.

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.

Fluids: fuelAircraft › Fluids/misc hardware · Fluid managementBeech 95-B55 (T42A): 15 casesAll aircraft: 1,695 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 and passenger departed on a flight to add fuel to the airplane’s fuel tanks. The airplane was originally manufactured with 2 main fuel tanks and 2 auxiliary fuel tanks. A modification installed 2 additional wingtip tanks that fed into the main tanks via transfer pumps. When in cruise flight, the pilot selected the main fuel tanks and turned on the wingtip tank transfer pumps. However, one light indicating that the pump was operating did not illuminate. The pilot reselected the auxiliary tanks and decided to return to his home airport. The pilot entered the airport traffic pattern and he selected the main fuel tanks but noted that “not much fuel [was] showing in the left main tank.” Due to traffic already in the pattern, the pilot had to perform additional maneuvering to remain clear and then reestablish a final approach. On short final, the pilot determined that the landing was assured and selected full flaps. Shortly after, the left engine stopped producing power. The pilot knew the airplane would not make the runway with the landing gear and flaps down. He performed an off-field landing resulting in substantial damage to the fuselage, elevators, and wings. The pilot informed a Federal Aviation Administration inspector that the reason for the loss of engine power was due to fuel mismanagement.

Aircraft

Registration
N85RR
Reported as
Beech 95-B55 (T42A)
Category
Airplane
Serial number
TC-1365
Built
1970
Engines
Continental IO-550E, 300 horsepower, reciprocatingContinental IO-550E, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Tw Air LLC
Airworthiness certificate
Standard, Normal
Airport
LHQ · Fairfield County, runway 28, 5,004 × 75 ft, asphalt

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
67
Injuries
None
Certificates
Airline transport, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
260° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 45 °F
Altimeter
30.11 inHg
Observed at
KLHQ
METAR
KLHQ 241653Z AUTO 26010KT 10SM CLR 21/07 A3011 RMK AO2 SLP191 T02110067

Docket · 4

The files NTSB released with the investigation on February 17, 2022, on NTSB’s docket system: statements, records, photos and specialists’ reports. 8.3 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.