- Date
- January 20, 2026, 16:58 local (22:58 UTC)
- Place
- Spring, TX · KDWH Runway 17L Taxiway H
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Takeoff
- Aircraft
- N4NHQuicksilver II
- Defining event
- Takeoff: Loss of engine power (partial)
- Weather
- Visual (VMC) · Day
- Status
- Investigation ongoing
- Investigation class
- Class 3
- NTSB office
- Central Region
- Parties
- FAA
- FAA report
- 20260120002699A
- Case key
- 202331
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Preliminary report
What NTSB knew early in the investigation. It may change in the final report.
On January 20,2026, 1658 central standard time, a Quicksilver II, N4NH, sustained substantial damage when it was involved in an accident at David Wayne Hooks Memorial Airport, DWH, in Spring, Texas. The pilot, sole occupant, sustained no injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot departed runway 17L with intentions of staying in the traffic pattern and making a water landing at the adjacent water runway at the airport. After retracting the landing gear, the engine ran very rough and lost power from the normal 6,500 rpm to about 1,800 rpm. The airplane was about 100 ft above ground level (agl) as the pilot lowered the nose and prepared for landing on the remaining runway. The airplane landed hard on the left side of the runway with the wings level and the landing gear still retracted. The airplane continued into the grass on the left side of runway 17L and came to rest near taxiway H. Just before touchdown, the engine power began to recover, and the engine returned to full power as the airplane was sliding on its floats. The pilot closed the throttle to idle, turned off the engine, and exited the airplane. During the hard landing the aluminum tubes from the rear engine area to the main landing gear were bent. The engine was displaced aft and the propeller contacted the elevator control tube and severed it. The elevator control horn was fractured and the elevator trim cable was damaged by contact with the propeller. The pilot also reported that several aluminum structural tubes were bent. He stated that there was no other damage to the airplane. The pilot, with the help of ground personnel, lowered the landing gear, and returned the airplane to the hangar for further inspection.
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.
Aircraft
- Registration
- N4NH
- Reported as
- Quicksilver II
- Category
- Airplane, amateur-built
- Serial number
- 0622
- Built
- 2010
- Airframe hours
- 415.5
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Special, Experimental light sport (Special)
- Last inspection
- Condition · June 17, 2025 · 18.5 hours before
- Destination
- Same as departure
- Airport
- DWH · David Wayne Hooks Meml, runway 17L/35R, 3,500 × 35 ft, concrete
- Equipment
- None
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.
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 150° at 7 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- 3,000 ft overcast
- Temperature
- 64 °F, dew point 61 °F
- Altimeter
- 30.10 inHg
- Observed at
- KDWH ATIS
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.