ERA26LA247

NTSB accident investigation · Piper PA-22-150 · Morganton, NC · June 24, 2026

Accident · Serious injuriesClass 4 · LimitedFinal report
Date
June 24, 2026, 11:42 local (15:42 UTC)
Place
Morganton, NC
Injuries
1 serious, 1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N4552APiper PA-22-150
Defining event
Takeoff: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report October 1, 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
20260624010609A
Case key
203238

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 pilot and flight instructor’s failure to maintain directional control while maneuvering on the runway, which resulted in a runway excursion. Contributing to the accident was the pilot’s failure to complete a positive exchange of flight control following the loss of directional control.

Findings · 3

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.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedPiper PA-22-150: 38 casesAll aircraft: 3,958 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · Flight crewPiper PA-22-150: 52 casesAll aircraft: 9,295 casesProbable cause
Action: lack of actionPersonnel issues › Action/decision · PilotPiper PA-22-150: 4 casesAll aircraft: 792 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 private pilot recently purchased the tailwheel-equipped airplane and was receiving make/model specific recurrency training from the flight instructor. Following a successful landing, the flight instructor briefed the pilot that the next takeoff would be an exercise in rudder management and maintaining runway alignment by reducing engine power during the takeoff roll after the tail rose off the ground. The exercise would end when about 1,000 feet of runway remained, after which the pilot would take off. The pilot stated that he understood the exercise would be a type of high-speed taxi, and that the flight instructor would operate the throttle. During the subsequent maneuver, the flight instructor described that when the tail rose up and he reduced engine power, the pilot initially applied right rudder to correct for the airplane’s minimal drift to the left, but then did not relax that right rudder input. The flight instructor then called for the pilot to apply left rudder, and the flight instructor began to apply left rudder himself, but he felt resistance to the control input. The flight instructor then repeatedly verbalized for the pilot to transfer control of the airplane to him, but that did not occur until after the airplane departed the right side of the runway. The airplane subsequently traversed an excavated area and an earthen berm before striking a drainage ditch and coming to rest. The flight instructor was seriously injured and the airplane’s fuselage was substantially damaged. Following the accident, the pilot described that this takeoff technique was different from the one that he had originally been trained to perform. Specifically, the flight instructor told him to place the control yoke full forward at the start of the takeoff roll so that the tail would rise up immediately, rather than holding the control yoke aft and raising the tail only after speed was attained. Of the previous takeoffs he had made using this technique, including the accident maneuver, the pilot stated that he felt that he never had the control authority that he should. The pilot reported that there were no preimpact mechanical malfunctions or failures of the airplane that would have precluded normal operation.

Aircraft

Registration
N4552A
Reported as
Piper PA-22-150 (NO SERIES)
Category
Airplane
Serial number
22-3862
Built
1956
Airframe hours
3,381
Engine
Lycoming O-320-D2B, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 20, 2026
Departed
7A8 · Spruce Pine, NC
Destination
Same as departure
Airport
MRN · Foothills Rgnl, runway 21, 5,500 × 75 ft, asphalt
Equipment
ADS-B, Handheld GPS

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
Flight instructor
Age
54
Injuries
Serious
Certificates
Private, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
March 20, 2026
Seat
Right
Restraint
4-point
Flight hours
5,323 total · 156 in this make and model · 5,109 as pilot in command · 130 in the last 90 days · 29 in the last 30 days · 1 in the last 24 hours
Role
Pilot
Age
73
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
June 22, 2026
Seat
Left
Restraint
4-point
Flight hours
1,172 total · 2 in this make and model · 1,172 as pilot in command · 2 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
73 °F, dew point 57 °F
Altimeter
30.17 inHg
Observed at
KMRN
METAR
METAR KMRN 241435Z AUTO 00000KT 10SM CLR 23/14 A3017

Docket · 6

The files NTSB released with the investigation on October 1, 2026, on NTSB’s docket system: statements, records, photos and specialists’ reports. 24.3 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.

Other investigations on N4552A · 1

Matched to the same aircraft by N-number and date.