CEN26LA097

NTSB accident investigation · Quicksilver II · Spring, TX · January 20, 2026

Accident · No injuriesClass 3 · LimitedPreliminary report
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.

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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.