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Accidents · NTSB WPR22FA048 · Final report

Amateur-built Zodiac CH601XL accident near Temecula, California, November 23, 2021

On November 23, 2021 at about 6:33 pm local time, a 2007 amateur-built Zodiac CH601XL, registered N601KS, was destroyed in an accident during enroute (cruise) near Temecula, California (French Valley airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The failure of the airplane’s canopy latch system, which resulted in the canopy opening in flight and a loss of airplane control. Contributing to the accident was the lack of a secondary canopy latch as recommended by the kit manufacturer.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
November 23, 2021 · about 6:33 pm local time
Place
Temecula, California · French Valley · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built Zodiac CH601XL, built 2007
Registration
N601KS · no longer on the register · serial 6-5930
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

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

About seven minutes after departure, following what appeared to be an uneventful takeoff and initial climb, the airplane began a 180° turn toward the departure airport. A few minutes later, witnesses heard a loud bang, and the airplane pitched down aggressively, rolled inverted, and impacted the ground in a steep, nose-down attitude. During the descent, the pilot’s flight bag and other cabin contents fell out of the airplane, and the sound of buffeting wind noise and the pilot struggling were heard on the airport’s common traffic advisory frequency. Examination did not reveal any anomalies with the flight controls or engine that would have precluded normal operation, and all components from the airplane were found in the immediate vicinity of the impact site. There was no evidence of bird strike. The owner/builder of the airplane stated that he had once experienced the canopy opening on takeoff but was able to land safely. As a result of this event, he disabled the standard lock and installed a set of two small over-center latches, each mounted to the rear sides of the canopy frame with two soft aluminum rivets. Examination of the canopy system revealed damage signatures that appeared to indicate that the rivets of one latch had separated in shear, and the other latch had twisted away from the airframe. It is likely that the accident was initiated by the failure of the mounting rivets in one latch, which caused the canopy to partially open on one side, then twist the latch away from the other side, resulting in an open and possibly deformed canopy. The reason for the initial failure could not be determined; however, the owner of the airplane was shorter than the pilot and had raised the seat and moved it forward during construction. The modification would have resulted in the accident pilot having to lean inboard, or sit with his head tilted, to avoid touching the canopy. It is possible that the airplane encountered turbulence that caused the pilot to hit the canopy, resulting in the failure of one of the latches. Multiple instances of canopies opening in flight were reported for this airplane model. Because an open canopy disturbs airflow over the horizontal stabilizer, flight control difficulties can result in a loss of control nose-down pitching motion, often accompanied by a loud banging sound and cabin contents being sucked out, all which were observed in this accident. Although the Pilot Operating Handbook (POH) provides instructions for continued flight with an open canopy, evidence from both this and previous accidents suggests that both the nose-down motion and associated negative G-forces can be hard for pilots to maintain airplane control. The airplane’s POH suggested the installation of a secondary backup latch system, and 2 weeks following the accident, the manufacturer issued a safety alert recommending such. The accident airplane was not equipped with a secondary latch.

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. Sys/Comp malf/fail (non-power) during enroute (cruise) defining event
  2. Loss of control in flight during enroute (cruise)
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • Aircraft › Aircraft structures › Doors › Passenger/crew doors › Design
  • Aircraft › Aircraft structures › Doors › Passenger/crew doors › Capability exceeded
  • Aircraft › Aircraft systems › (general) › (general) › Not installed/available
  • Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › (general) › Not attained/maintained

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
  • Flight time: 1,001.3 hours in all; 10.3 in this make and model; 6.4 in the last 90 days; 2.3 in the last 30 days; 855.1 as pilot in command
  • Last flight review: September 9, 2021
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Airframe total time: 54 hours
  • Last inspection: condition inspection, September 1, 2020; 8 hours since
  • Maximum gross weight: 1,325 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: General Motors Corvair (piston); 0 hours total

The flight

  • Departed from: F70 Temecula CA at 6:20 pm
  • Flight plan: none
  • Runway 18/3, 6,000 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 240° at 3 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 70°F (21°C), dew point 21°F (-6°C)
  • Altimeter: 30.00 inHg
  • Observation at 10:35 am from KHMT, 12 miles away

Weather report (METAR): KHMT 231835Z AUTO 24003KT 10SM CLR 21/M06 A3000 RMK AO2 T02111055

Injuries

FatalSeriousMinorNone
Flight crew1

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

15 documents, released by the NTSB on June 8, 2023. 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 Airframe Examination Report PDF, 15 pages View Download
2 GPS & Ahrs - Specialist's Factual REPORT_WPR22FA048 PDF, 8 pages View Download
3 Attachment 1 to GPS & Ahrs - Specialist's Factual REPORT_WPR22FA048 - GPS Tabular Data data file Download
4 Attachment 2 to GPS & Ahrs - Specialist's Factual REPORT_WPR22FA048 - Ahrs Tabular Data data file Download
5 F70 Airport Ctaf Audio NOV-23-2021-1830Z-1900Z. Downloaded from Liveatc.net November 24, 2021 audio View Download
6 Memorandum of Record PDF, 5 pages View Download
7 Pilot Logbook Excerpts PDF, 4 pages View Download
8 Maintenance Logbook Excerpts PDF, 11 pages View Download
9 Feather Lab Report PDF, 1 page View Download
10 Zodiac 601XL Pilot Operating Handbook Excerpts PDF, 4 pages View Download
11 Mandatory Safety Alert Dec 06 2021 - Canopy PDF, 7 pages View Download
12 Previous Canopy Opening Events PDF, 1 page View Download
13 Toxicological Report PDF, 1 page View Download
14 Evidence Control Form PDF, 3 pages View Download
15 Release of Aircraft Wreckage, NTSB Form 6120.15 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.

Other NTSB records under N601KS the same tail number, which may have belonged to a different aircraft at the time

2008-02-01LAX08LA056 · accident near Murrieta, CA · substantial damage · no injuries

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 never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.