ERA26LA191

NTSB accident investigation · Beech F33A · Sanford, NC · April 24, 2026

Accident · No injuriesClass 4 · LimitedFinal report
Date
April 24, 2026, 12:15 local (16:15 UTC)
Place
Sanford, NC
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N85WMBeech F33A
Defining event
Enroute: Electrical system malf/failure
Weather
Visual (VMC) · Day
Status
Completed · report July 15, 2026
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20260424010719A
Case key
202902

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 electrical power as a result of broken stator leads within the alternator, which resulted in the pilot’s inability to extend the airplane’s landing gear.

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 reported that after practicing instrument approaches with the flight instructor, they were returning to the airport. While in the traffic pattern, the pilot lowered the flaps with no problems noted, but as he attempted to lower the landing gear, the airplane lost electrical power. The pilot performed a low pass of the airport and reported that individuals on the ground confirmed that the landing gear were down, but they were unsure if they were in the locked position. The pilot then attempted to lower the landing gear with the hand crank, and he managed to make about 20 total turns (of about 50 normally needed to fully extend the landing gear) before he was unable to turn the crank any further. During the subsequent landing, the nose landing gear collapsed and the airplane sustained substantial damage to the lower fuselage. Postaccident examination flight data recovered from avionics onboard the airplane revealed that shortly after departing on the accident flight, current parameter indicated a discharge from the battery for the remainder of the flight and electrical bus voltage began to slowly decrease. A postaccident examination and functional test of the alternator revealed that the case halves of the alternator had vibrated apart and that the alternator had was not functioning. It was disassembled and the stator leads were found to be broken at the rectifier attachment point.

Aircraft

Registration
N85WM
Reported as
Beech F33A
Category
Airplane
Serial number
CE-943
Built
1981
Airframe hours
5,776.4
Engine
Continental Aerospace Technologies IO-520-BB, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 16, 2025 · 11.6 hours before
Airport
TTA · Raleigh Exec Jetport At Sanford-Lee County, runway 21, 6,501 × 100 ft, asphalt
Equipment
ADS-B, Auto-pilot, Electronic primary flight display

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
66
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Without waivers/limitations
Last flight review
April 4, 2025
Seat
Left
Restraint
None
Flight hours
289.28 total · 115.3 in this make and model · 179.88 as pilot in command · 10.8 in the last 90 days · 2.6 in the last 30 days
Role
Flight instructor
Age
66
Injuries
None
Certificates
Airline transport, Flight instructor, Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
BasicMed
Last flight review
November 30, 2025
Seat
Right
Restraint
3-point
Flight hours
4,078.3 total · 32.6 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 7 knots
Visibility
10 statute miles
Lowest ceiling
1,500 ft overcast
Temperature
59 °F, dew point 55 °F
Altimeter
30.00 inHg
Observed at
TTA
METAR
METAR KTTA 261615Z AUTO 05007KT 10SM OVC015 15/13 A3000 RMK AO2 T01500127

Docket · 10

The files NTSB released with the investigation on July 15, 2026, on NTSB’s docket system: statements, records, photos and specialists’ reports. 11.1 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.