ERA26LA122

NTSB accident investigation · Hughes 269A · Gettysburg, PA · February 21, 2026

Accident · Minor injuriesClass 4 · LimitedFinal report
Date
February 21, 2026, 11:59 local (16:59 UTC)
Place
Gettysburg, PA
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N1020SHughes 269A
Defining event
Takeoff: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report June 25, 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
20260221003679A
Case key
202481

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 flight instructor’s failure to identify the excess power required to lift off from soft and muddy ground, which resulted in a loss of control and subsequent collision with a hangar during takeoff.

Findings · 2

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.

Attention/monitoring: monitoring environmentPersonnel issues › Psychological · Instructor/check pilotHughes 269A: 1 caseAll aircraft: 809 casesProbable cause
Performance/control parametersAircraft › Aircraft oper/perf/capability · Not attained/maintainedHughes 269A: 2 casesAll aircraft: 1,269 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 student pilot and the flight instructor performed a preflight inspection of the helicopter and then moved it from the hangar onto an area of soft, muddy ground outside. They pushed the helicopter as far away from the hangar as they could due to the soft ground, about 25 to 30 ft. The student pilot described that where the helicopter was positioned, it was “leaning back” with the aft portion of both skids several inches deep in the mud. During the subsequent takeoff attempt, the student pilot noted that the helicopter required the application of additional engine power than he had observed during previous takeoffs before it became “light on the skids.” During a postaccident interview, he postulated that the helicopter might have been “stuck in the mud.” The flight instructor then felt that the helicopter’s tail might strike the ground, so he nudged the cyclic control forward. Immediately after, the helicopter began moving forward toward the hangar in a significantly nose low attitude. Despite their subsequent control inputs, neither pilot was able to arrest the helicopter’s forward motion and it struck the hangar less than 2 seconds later and came to rest on its right side. The helicopter’s fuselage, tailboom, and main rotor blades were substantially damaged during the accident sequence. The flight instructor reported that there were no preimpact mechanical malfunctions or failures of the helicopter that would have precluded normal operation, and FAA inspectors who examined the helicopter after the accident were unable to find evidence of a preimpact mechanical malfunction or failure of the flight controls that would have precluded normal operation. Based on this information, it is likely that the helicopter suddenly dislodged itself from the soft, muddy ground during the takeoff when the flight instructor applied nose down cyclic input, which resulted in an unexpected, rapid forward movement and collision with the hangar. Had the flight instructor recognized the abnormal amount of engine power being applied by the student and discontinued the takeoff attempt, it is likely that the accident could have been avoided.

Aircraft

Registration
N1020S
Reported as
Hughes 269A (UNDESIGNATED SERIES)
Category
Helicopter
Serial number
26-0467
Built
1966
Airframe hours
5,618.9
Engine
Lycoming HIO-360-B1A, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Tactical Turtle LLC
Registered owner
Tactical Turtle LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 17, 2025
Destination
W05 · Gettysburg, PA
Airport
None · None
Equipment
ADS-B

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
49
Injuries
Minor
Certificates
Flight instructor, Commercial
Instrument ratings
Helicopter
Medical
Class 2, With waivers/limitations
Last flight review
February 5, 2026
Seat
Left
Restraint
3-point
Flight hours
7,544 total · 628 in this make and model · 7,420 as pilot in command · 79 in the last 90 days · 28 in the last 30 days
Role
Student pilot
Age
52
Injuries
Minor
Certificate
Student
Medical
Class 2, With waivers/limitations
Seat
Right
Restraint
3-point
Flight hours
62 total · 34 in this make and model · 15 in the last 90 days · 11 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
39 °F, dew point 32 °F
Altimeter
29.95 inHg
Observed at
KRSP, 14 nm away
METAR
METAR KRSP 211654Z AUTO 32007KT 260V020 10SM CLR 04/00 A2995 RMK AO2

Docket · 6

The files NTSB released with the investigation on June 25, 2026, on NTSB’s docket system: statements, records, photos and specialists’ reports. 8.2 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.