Quicksilver II N4NH

Summary

On 20 January 2026 at about 22:58 local time, a Quicksilver II registered N4NH was involved in an accident near Spring, Texas, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. No probable cause has been published yet; this accident is still under investigation.

Date

20 January 2026 at 22:58

Classification

Accident

Location

Spring, Texas, United States

Nearest airport

David Wayne Hooks Meml (DWH)

Coordinates

30.0572, -95.5515

Aircraft

Quicksilver II

Registration

N4NH

Category

Airplane

Year built

2010

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

CEN26LA097

Nobody was injured.

The NTSB has not published a probable cause for this record. The investigation is still open; a final report usually follows one to two years after the accident.

Nothing about the cause is stated here that is not in the source record.

Read the full NTSB narrative

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.

Quoted verbatim from the NTSB record.