SEA07LA155

NTSB accident investigation · Quad City Ultralight Challenger II · Lodi, CA · June 12, 2007

Accident · No injuriesLimited investigationFinal report
Date
June 12, 2007, 10:50 local (17:50 UTC)
Place
Lodi, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N204DCQuad City Ultralight Challenger II
Weather
Visual (VMC) · Day
Status
Completed · report November 29, 2007
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20070612009449A
Case key
65974

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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Probable cause

The improper assembly of the rony bracket which attached the right wing forward lift strut to the fuselage, the subsequent failure of that bracket, and separation of the right wing from the aircraft.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionManeuvering
Wing,bracing strut - failure,totalCause
Maintenance,installation - improperOther maintenance personnelCause
Miscellaneous,bolt/nut/fastener/clamp/spring - failure,totalCause
In flight collision with terrain/waterDescent - uncontrolled
Terrain condition - ground

Analysis

The pilot said that he was maneuvering at 2,000 feet above the ground when the right wing separated from the aircraft. He said that the aircraft was equipped with a Ballistic Recovery System (BRS) emergency parachute, which he immediately deployed. The pilot said that the fuselage and left wing came to rest in a grape vineyard, and he was able to walk away uninjured. Postaccident examination of the wreckage, by a fellow Challenger II pilot, revealed that the "rony bracket" that attached the forward lift strut to the fuselage failed. The bracket was not attached per the Challenger II building manual. The manufacturer's instructions state that the bolt should only be snug. It also warns to not over tighten these bolts holding the brackets to the hollow tubes and that there should be no more than two threads showing past the nut. The bolt on this rony bracket had at least five to six threads showing. Additionally, the end of the hollow tube was deformed into an oval shape, and not round. The remaining rony brackets did have only two threads showing and they could be rotated by hand, per the manufacturer's instructions.

Factual narrative

On June 12, 2007, at approximately 1050 Pacific daylight time, a Quad City Ultralight Aircraft, Challenger II experimental light sport aircraft (ELSA), N204DC, was substantially damaged when its right wing separated in flight near Lodi, California. The sport pilot, the sole occupant in the aircraft, was not injured. The pilot/owner was operating the aircraft under Title 14 CFR Part 91. Visual meteorological conditions prevailed for the personal, local flight, which had originated approximately 5 minutes before the accident. A flight plan had not been filed.

The pilot said that he was maneuvering at 2,000 feet above the ground when the right wing separated from the aircraft. He said that the aircraft was equipped with a Ballistic Recovery System (BRS) emergency parachute, which he immediately deployed. The pilot said that the fuselage and left wing came to rest in a grape vineyard, and he was able to walk away uninjured.

Postaccident examination of the wreckage, by a fellow Challenger II pilot, revealed that the "rony bracket" that attaches the forward lift strut to the fuselage had failed. The bracket was not attached per the Challenger II building manual. The manufacturer's instructions state that the bolt should only be snug. It also warns to not over tighten these bolts holding the brackets to the hollow tubes and that there should be no more than two threads showing past the nut. The bolt on this rony bracket, on the accident aircraft, had at least five to six threads showing. Additionally, the end of the hollow tube was deformed into an oval shape and not round. The remaining rony brackets did have only two threads showing and they could be rotated by hand, per the manufacturer's instructions.

Aircraft

Registration
N204DC
Reported as
Quad City Ultralight Challenger II
Category
Airplane
Serial number
CH2-0799-1894
Airframe hours
1,291
Engine
Rotax 503 DCDI, 52 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Terry L. Miller
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Condition · May 1, 2007
Departed
1O3 · Lodi, CA
Destination
1O3

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.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
50
Injuries
Minor
Certificate
Sport Pilot
Airplane ratings
Single-engine land
Medical
Sport pilot
Last flight review
March 1, 2007
Seat
Front
Flight hours
829 total · 500 in this make and model · 829 as pilot in command · 143 in the last 90 days · 46 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
290° at 7 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 50 °F
Altimeter
29.95 inHg
Observed at
SCK, 18 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.