FTW98LA071 · Unknown QUICKSILVER GT-500 QUICKSILVE
Unknown QUICKSILVER GT-500 QUICKSILVE · Accident: airframe, component or system failure en route
From Kitty Hawk Flying Field (TS67) to an unrecorded destination
Event
- NTSB case
- FTW98LA071
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- 0
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Unknown QUICKSILVER GT-500 QUICKSILVE
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- UNREG
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Kitty Hawk Flying Field (TS67)To not recorded
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 103: Ultralight
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Airframe, component or system failure
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Other person › Maintenance, installation, improper
- Wing, wing attachment bolt › Not engaged
- Wing, wing attachment fitting › Failure, total
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
During cruise flight, the left leading edge wing strut fitting failed, & the amateur-built aircraft, which was being operated as an ultralight vehicle under an exemption to Title 14 CFR Part 103, entered a left spin. The ultralight instructor pilot deployed the aircraft's emergency parachute, which inflated partially & slowed the aircraft's rate of descent. A witness observed the aircraft impact the ground in a nose down attitude at an estimated speed of 25 to 30 mph. Examination revealed the wing strut fitting failed due to improper installation of the 3 bolts, used to secure the fitting to the leading edge wing spar. The bolts had been inserted through the forward holes of the fitting, through holes in the tubular spar, but not through the rear holes of the fitting. This defect was not visible during preflight inspections; however, it could have been found during a condition inspection, since a zipper installed in the fabric lower wing surface provided access to examine the rear of the fitting with the aid of a flashlight & mirror. No record was found to indicate that a condition inspection had been performed on the kit-built aircraft, in accordance with provisions for using the '2-Place Training Exemption.' The aircraft was first flown in February 1995 & had been owned by the pilot since June 1995. The main line, which fastened the Ballistic Recovery System (BRS) parachute to the airplane, was found wrapped around the propeller drive shaft of the rear-mounted (pusher) engine.
Probable cause
the kitplane builder's improper installation of the bolts attaching the left leading edge wing strut fitting to the leading edge spar, which resulted in the eventual failure of the fitting and the ensuing loss of control. Related factors were: the owner/pilot's failure to ensure that a condition inspection of the aircraft was performed, and failure of the aircraft's emergency (Ballistic Recovery System) parachute to fully deploy.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record FTW98LA071
- Event ID
- 20001208X09309
- Case number
- FTW98LA071
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 078428eac5f86d93721d818f11ca82621c31f17908046cfa5f3f84f012bd3ae3; retrieved 2026-09-21T11:41:23.370Z.