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Accidents · NTSB WPR09LA453 · Final report

Quad City CHALLENGER II accident near Redlands, California, September 16, 2009

On September 16, 2009 at about 11:42 pm local time, a Quad City CHALLENGER II, registered N732LS, was substantially damaged in an accident during approach (VFR pattern base) near Redlands, California (Redlands Municipal Airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

Structural failure of the right wing during the landing approach due to the separation of the wing's fabric covering.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
September 16, 2009 · about 11:42 pm local time · cases in 2009
Place
Redlands, California · Redlands Municipal Airport · cases near this airport · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Quad City CHALLENGER II · all CHALLENGER IIs on the register
Registration
N732LS · no longer on the register · serial CH2 0991-0732
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

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.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Aircraft structural failure during approach (VFR pattern base) defining event
  2. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

Pilot

  • Certificate: commercial pilot
  • Ratings: single-engine land; rotorcraft: glider
  • Flight time: 1,228 hours in all; 4 in this make and model; 3 in the last 90 days; 2 in the last 30 days
  • Last flight review: July 21, 2009
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: frt
  • Injury: fatal

Co-pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 144 hours in all; 8 in this make and model; 8 in the last 90 days; 2 in the last 30 days
  • Last flight review: July 26, 2009
  • Medical certificate: Class 3
  • Seat: rear
  • Injury: fatal

The aircraft

  • Last inspection: condition inspection, July 18, 2009; 18 hours since
  • Maximum gross weight: 1,010 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 503 (piston); 0 hours total

The flight

  • Departed from: F70 French Valley CA at 11:02 pm
  • Destination: REI Redlands CA
  • Flight plan: none
  • Runway 26, 4,505 ft by 75 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 270° at 9 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 11,000 ft
  • Temperature: 93°F (34°C), dew point 48°F (9°C)
  • Altimeter: 29.80 inHg
  • Observation at 11:51 pm from SBD, 6 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

48 documents, released by the NTSB on July 15, 2010. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

#DocumentWhat it is
1 Witness Statements PDF, 2 pages View Download
2 GPS Data from Accident Flight data file Download
3 Image 1: Recorded GPS Positions During Landing Approach PDF, 1 page View Download
4 GPS Data from September 3, 2009 Flight data file Download
5 Diagram: Right Wing PDF, 1 page View Download
6 Photo A-right Wing Aft Spar PDF, 1 page View Download
7 Photo B-right Wing Aft Strut PDF, 1 page View Download
8 Photo C1-RIGHT Wing Forward Spar PDF, 1 page View Download
9 Photo C2-RIGHT Wing Forward Spar PDF, 1 page View Download
10 Photo D-right Wing Forward Strut PDF, 1 page View Download
11 Photo E-right Wing Brace Cable PDF, 1 page View Download
12 Photo F-right Wing Aft Spar Attach Point PDF, 1 page View Download
13 Photo G1-RIGHT Wing Aft Strut Attach Bracket PDF, 1 page View Download
14 Photo G2-RIGHT Wing Aft Strut Attach Point at Fuselage PDF, 1 page View Download
15 Photo H1-RIGHT Wing Forward Spar Attach Point PDF, 1 page View Download
16 Photo H2-RIGHT Wing Forward Spar Attach Point PDF, 1 page View Download
17 Photo H3-RIGHT Wing Forward Spar Attach Point PDF, 1 page View Download
18 Photo H4-RIGHT Wing Forward Spar Attach Point at Fuselage PDF, 1 page View Download
19 Photo I1-RIGHT Wing Forward Strut Attach Point at Fuselage PDF, 1 page View Download
20 Photo I2-RIGHT Wing Inboard Cable Brace Attach Point PDF, 1 page View Download
21 Photo J-outboard Right Wing Forward Strut Attach Point PDF, 1 page View Download
22 Photo K-outboard Right Wing Aft Strut Attach Point and Cable Brace PDF, 1 page View Download
23 Photo L-right Wing Rib Former PDF, 1 page View Download
24 Photo M1-UNDERSIDE Right Aft Spar and Aileron with Propeller Blade PDF, 1 page View Download
25 Photo M2-UNDERSIDE Right Aft Spar and Aileron with Propeller Witness Marks PDF, 1 page View Download
26 Photo 1-ENGINE and Fuel Lines PDF, 1 page View Download
27 Photo 2-CURVED Right Wing Aft Spar PDF, 1 page View Download
28 Photo 3-VERTICAL Stabilizer Forward Spar Attach Point PDF, 1 page View Download
29 Photo 4-VERTICAL Stabilizer Aft Spar Attach Point PDF, 1 page View Download
30 Photo 5-TAILWHEEL PDF, 1 page View Download
31 Photo 6-SPARK Plugs PDF, 1 page View Download
32 Photo 7-MAIN Landing Gear Corrosion PDF, 1 page View Download
33 Photo 8-RIGHT Wing at Accident Site PDF, 1 page View Download
34 Photo 9-FUSEALGE and Left Wing at Accident Site PDF, 1 page View Download
35 Photo 10- Wing Rib Covering Reinforcement PDF, 1 page View Download
36 Engine Exam Report (NTSB) PDF, 3 pages View Download
37 Toxicological Report: Fowler PDF, 1 page View Download
38 Toxicological Report: Kelly PDF, 2 pages View Download
39 Statement of Party Representatives to NTSB Investigation PDF, 2 pages View Download
40 Release of Aircraft Wreckage, NTSB Form 6120.15 PDF, 1 page View Download
41 Airplane Reference Speeds PDF, 1 page View Download
42 Airworthiness Application Including Prior History PDF, 2 pages View Download
43 Challenger II Construction Manual Excerpts PDF, 1 page View Download
44 Logbook Excerpts: Fowler PDF, 6 pages View Download
45 Logbook Excerpts: Kelly PDF, 6 pages View Download
46 Airframe Logbook Excerpts PDF, 7 pages View Download
47 Engine Logbooks PDF, 4 pages View Download
48 Airplane Weight and Balance PDF, 1 page View Download

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Connections how this case links to the rest of the register

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The whole map of how records connect · these connections as data: /graph/accident/WPR09LA453.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.