- 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.
On this page
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.
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.