QUAD CITY CHALLENGER II near Redlands, CA — 2009-09-16
- Date
- 2009-09-16
- Location
- Redlands, CA, USA
- Airport
- REI
- Aircraft
- QUAD CITY CHALLENGER II
- Registration
- N732LS
- Category
- Airplane
- Highest injury
- Fatal
- Fatalities
- 2
- Phase of flight
- Approach
Probable cause
Structural failure of the right wing during the landing approach due to the separation of the wing's fabric covering.
NTSB narrative
The pilot of the experimental light-sport airplane had just completed a 40-minute-flight, and was turning from the downwind to base leg when at 450 feet above ground level, the airplane rapidly descended and collided with terrain below. The damage to the forward section of the fuselage, the position of the main wreckage, and the minimal damage to surrounding trees indicated a near vertical impact attitude. The location of the right wing, along with the aft downward bending damage observed to its main spars and tensile failure of the forward spar attach point, indicated that the wing separated from the airplane in a down and aft motion during flight. The airplane's flight profile was not conducive to a negative overload failure of the right wing. The outboard right wing ribs failed in tensile overload, and the wing fabric material was observed attached only at the aft spar, and in-trail of the wing. These signatures indicated that the material had become separated from the wing structure in flight. The separation most likely created a high drag, ‘parachute’ effect with resultant failure of the wing. The airplane was built about 18 years prior to the accident, and appeared to have been flown as an unregistered airplane prior to purchase by the two pilots. New wing covering had been installed by the pilots the year prior to the accident, and cursory tensile testing of fabric samples revealed that the material had a breaking strength comparable to similar light aircraft fabric. The pilot-rated passenger was an insulin-dependent diabetic, however, it was not possible to determine whether his condition had any relation to the circumstances of the accident.
Analysis
- Primary failure mode
- Controlled flight into terrain
- First missed decision gate
- Pilot could have recognized unusual left traffic pattern and adjusted approach accordingly.
NTSB coding
Evidence available
- ADS-B / radar
- Photos
- 48 docket documents
Docket documents48
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statementsinterview
- Airframe Logbook Excerptsother
- Airplane Reference Speedsother
- Airplane Weight And Balanceother
- Airworthiness Application Including Prior Historyother
- Challenger II Construction Manual Excerptsother
- Diagram: Right Wingother
- Engine Logbooksother
- GPS Data From Accident Flightother
- GPS Data From September 3, 2009 Flightother
- Logbook Excerpts: Fowlerother
- Logbook Excerpts: Kellyother
- Image 1: Recorded GPS Positions During Landing Approachphotos
- Photo 1-Engine and Fuel Linesphotos
- Photo 10- Wing Rib Covering Reinforcementphotos
- Photo 2-Curved Right Wing Aft Sparphotos
- Photo 3-Vertical Stabilizer Forward Spar Attach Pointphotos
- Photo 4-Vertical Stabilizer Aft Spar Attach Pointphotos
- Photo 5-Tailwheelphotos
- Photo 6-Spark Plugsphotos
- Photo 7-Main Landing Gear Corrosionphotos
- Photo 8-Right Wing at Accident Sitephotos
- Photo 9-Fusealge and Left Wing at Accident Sitephotos
- Photo A-Right Wing Aft Sparphotos
- Photo B-Right Wing Aft Strutphotos
- Photo C1-Right Wing Forward Sparphotos
- Photo C2-Right Wing Forward Sparphotos
- Photo D-Right Wing Forward Strutphotos
- Photo E-Right Wing Brace Cablephotos
- Photo F-Right Wing Aft Spar Attach Pointphotos
- Photo G1-Right Wing Aft Strut Attach Bracketphotos
- Photo G2-Right Wing Aft Strut Attach Point at Fuselagephotos
- Photo H1-Right Wing Forward Spar Attach Pointphotos
- Photo H2-Right Wing Forward Spar Attach Pointphotos
- Photo H3-Right Wing Forward Spar Attach Pointphotos
- Photo H4-Right Wing Forward Spar Attach Point at Fuselagephotos
- Photo I1-Right Wing Forward Strut Attach Point at Fuselagephotos
- Photo I2-Right Wing Inboard Cable Brace Attach Pointphotos
- Photo J-Outboard Right Wing Forward Strut Attach Pointphotos
- Photo K-Outboard Right Wing Aft Strut Attach Point And Cable Bracephotos
- Photo L-Right Wing Rib Formerphotos
- Photo M1-Underside Right Aft Spar And Aileron With Propeller Bladephotos
- Photo M2-Underside Right Aft Spar And Aileron With Propeller Witness Marksphotos
- Engine Exam Report (NTSB)report
- Toxicological Report: Fowlerreport
- Toxicological Report: Kellyreport