Plane Crash List

Quicksilver MXL II SPORT N105SE

18 August 2018 · Westminster, Maryland, United States · Fatal

Summary

On 18 August 2018 at about 14:40 local time, a Quicksilver MXL II SPORT registered N105SE was involved in an accident near Westminster, Maryland, United States. 2 people were on board and 2 died. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 14:40
Classification
Accident
Location
Westminster, Maryland, United States
Nearest airport
Baugher's Orchard Airport (07MD)
Coordinates
39.6147, -77.0478
Aircraft
Quicksilver MXL II SPORT
Registration
N105SE
Category
Airplane
Year built
2006
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Westminster → Westminster
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ERA18FA221

People

2 people died.

On board Died Serious Minor Uninjured
2 2 0 0 0

Probable cause

The in-flight fracture of a stainless steel bolt that was used to secure the upper and lower wing cables to the outer attach point at the leading edge spar of the right wing due to stress corrosion cracking, which caused the right wing to fail and precluded controlled flight. Contributing to the bolt failure was the installation of a bolt that did not conform with the company's specification.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The private pilot and a passenger departed on a local flight and returned for landing about 15 minutes later. While the airplane was on final approach at an altitude between 100 and 200 ft, several witnesses heard a loud sound, and one of the witnesses saw the right wing fold and the airplane enter a steep descent. The airplane subsequently impacted terrain in a field near the airport. A witnesses reported observing the airframe parachute system deploy. The inspection of the components of the airframe ballistic parachute system indicated that the system had likely deployed just before or at the time of impact. Deployment of the parachute system at that low altitude would have been insufficient to adequately arrest the airplane's descent prior to impact. A stainless steel bolt secured the upper and lower wing cables to the outer leading edge spar of the right wing. Examination of the bolt showed that it fractured during flight due to stress corrosion cracking that extended across about 95% of the cross-section area of the bolt shank. The bolt failure allowed the leading edge spar to rotate upward relative to the trailing edge spar and fracture at the inboard cable attach point, precluding controlled flight. The stainless-steel material used for the wing cable attachment bolt was susceptible to stress corrosion cracking when exposed to a chloride-containing environment (such as the ocean). The airplane was previously equipped with floats, and was likely operated as an amphibious airplane at some point before the pilot purchased it. In addition, the installed bolt was a different material than the AN5-30A bolt specified in the Quicksilver Assembly, Maintenance, and Parts Manual for securing the outer upper and lower wing cables to the leading edge spar of the right wing. The material of the bolt recommended in the manual would be generally resistant to stress corrosion cracking as a result of a chloride-containing environment. The maintenance records did not indicate when the stainless steel bolt was installed. Evidence of stress corrosion cracking might not be apparent during visual inspections of the bolted joint. Also, the location of the stress corrosion cracking on the bolt would likely not have been detected during a condition inspection with the bolted joint in place. Further, the assembly, maintenance, and parts manual did not provide for a specific inspection of the bolt that secured the upper and lower wing cables to the outboard leading edge spar. However, the manual indicated that the security of all bolts should be checked every 50 hours. Although the pilot was taking a medication that could impair his ability to perform tasks requiring judgment or motor and cognitive skills, his use of the medication did not contribute to the accident.

Quoted verbatim from the NTSB record.

Other Quicksilver MXL accidents

Date Aircraft Location Operator Outcome Died
14 Jul 2018 Quicksilver MXL II
N594TC
Arecibo, United States - Serious injuries -
19 Nov 2017 Quicksilver MXL SPORT
N7712
Point Mugu, California, United States - Minor injuries -
7 Mar 2017 Quicksilver MXL II
UNREG
Hesperia, California, United States - Fatal 1
25 Jun 2015 Quicksilver MXL II SPORT
UNREG
Ute, Iowa, United States - Serious injuries -
15 Aug 2015 Quicksilver MXL II SPORT
UNREG
Pittsboro, North Carolina, United States - Serious injuries -
3 Apr 2015 Quicksilver MXL II
N476VB
Petaluma, California, United States - Fatal 1

All 20 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
23 Aug 2018 Cessna 172
N419SP
Churchville, Maryland, United States C K Leasing Servics Llc No injuries -
26 May 2018 Cessna 172
N789EP
Westminster, Maryland, United States Dream Aviation Inc No injuries -
13 Apr 2018 Textron G58
N67WM
Easton, Maryland, United States - No injuries -
1 Mar 2018 Cessna 172
N615JA
Ocean City, Maryland, United States Middle River Aviation LLC Fatal 2
7 May 2018 Boeing 737-8H4
N8655D
Baltimore, Maryland, United States Southwest Airlines Co No injuries -
7 Mar 2018 Cirrus SR20
N101AD
Churchville, Maryland, United States - Minor injuries -

All 170,864 records in United States