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NTSB Report

April 28, 2025 · Beech C90 · N501MS

Lancaster, TX

Overview

Report Status
Probable Cause
Event Type
Accident
Date
April 28, 2025
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury), 1 uninjured
Location
Lancaster, TX
Aircraft
Beech C90 (1974)
Tail Number
N501MS
Operator
Gm Intercom
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
CEN25LA176

The twin-engine airplane departed for the international cross-country flight with 380 gallons of Jet A fuel onboard. No fuel stops were performed during the flight. During the approach to the destination airport, the pilot reported that the right engine instruments began to display a decrease in power, until a total loss of power occurred. Shortly after, the left engine sustained a total loss of power. The pilot performed a forced landing to a flat corn field, located about 19.5 miles southeast of the destination airport. The two controllable pitch propellers were not feathered, and the main landing gear was not extended prior to landing in the field. The airplane came to rest upright in the field. The three occupants were able to egress from the airplane without further incident. The airplane sustained substantial damage to the fuselage and the left wing, and no evidence of a reported fire was noted with the right engine. During the recovery operation, the airframe fuel system was found intact and there were no visible signs of fuel leakage on the airframe. The airframe can contain up to 384 gallons of usable fuel. For the left side of the airplane, about 1 pint of fuel was recovered from the main fuel tank and about 9 gallons of fuel were recovered from the nacelle fuel tank. For the right side of the airplane, about 2 pints of fuel were recovered from the main fuel tank and no fuel was recovered from the nacelle fuel tank. The pilot did not provide any accident flight fuel planning calculation documents. The airplane was not equipped with a low fuel warning light system, nor was it required to be.

NTSB Probable Cause

The pilot’s improper fuel planning, which resulted in fuel exhaustion and a total loss of power to both engines.

Full Narrative

The twin-engine airplane departed for the international cross-country flight with 380 gallons of Jet A fuel onboard. No fuel stops were performed during the flight. During the approach to the destination airport, the pilot reported that the right engine instruments began to display a decrease in power, until a total loss of power occurred. Shortly after, the left engine sustained a total loss of power. The pilot performed a forced landing to a flat corn field, located about 19.5 miles southeast of the destination airport. The two controllable pitch propellers were not feathered, and the main landing gear was not extended prior to landing in the field. The airplane came to rest upright in the field. The three occupants were able to egress from the airplane without further incident. The airplane sustained substantial damage to the fuselage and the left wing, and no evidence of a reported fire was noted with the right engine. During the recovery operation, the airframe fuel system was found intact and there were no visible signs of fuel leakage on the airframe. The airframe can contain up to 384 gallons of usable fuel. For the left side of the airplane, about 1 pint of fuel was recovered from the main fuel tank and about 9 gallons of fuel were recovered from the nacelle fuel tank. For the right side of the airplane, about 2 pints of fuel were recovered from the main fuel tank and no fuel was recovered from the nacelle fuel tank. The pilot did not provide any accident flight fuel planning calculation documents. The airplane was not equipped with a low fuel warning light system, nor was it required to be.

Flight

Event TypeAccident
Event Time15:37 CDT
Nearest Airport0nm
Flight Plan FiledIFR
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBeech C90
Tail NumberN501MS
Aircraft CategoryAir
DamageSubstantial
OperatorGm Intercom
Operating RulePart 91
Engines2
Engine TypeTurboprop
Engine DetailsPratt & Whitney Canada · PT6A-20 · Turboprop · 550 | Pratt & Whitney Canada · PT6A-20 · Turboprop · 550
Seats8

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury), 1 uninjured
Fatal0
Serious1
Minor1
Uninjured1
Total3
Crew 1Age 21 · Third Class · Serious
Crew 2Age 20 · First Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind170° @ 9 kt
Visibility10 sm
CeilingOvercast 3100 ft
Temperature / Dew Point70 F
Altimeter29.96 inHg
Observation Time15:35
Weather SourceWFAC

Appendix: Source Data