- 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.
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.