Skip to content

Atlas / NTSB / WPR22LA159

NTSB CAROL · Event

Event WPR22LA159

2022-04-19 Long Beach, California, United States Airport · LGB None 1 aircraft Status: Completed

Registry · N822SA

FAA Aircraft Registry record.

Make / Model

DIAMOND AIRCRAFT DA 42

Year of manufacture

2006 · 16 years old at event

Engine

AUSTRO E4 SERIES (168 hp)

Seats / Engines

4 seats · 2 engines

Last airworthiness date

20110608

ADS-B equipped

Yes — Mode-S AB39DA

Registrant of record

PUGHS AIR WEST LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The failure of the right main landing gear brace rib for reasons that could not be determined based on available information.

Factual narrative

On April 19, 2022, about 1538 Pacific daylight time, a Diamond Aircraft Inc. DA-42 airplane, N822SA, was substantially damaged when it was involved in an accident at Long Beach Airport (Daugherty Field), Long Beach, California. The flight instructor and the pilot receiving instruction were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. The pilot receiving instruction reported that he was conducting a multiengine training flight and had performed multiple maneuvers before the accident. During the rollout after a short-field landing, about 750 ft from the touchdown point, the right main landing gear collapsed, and the right wing contacted the ground, which substantially damaged the right aileron. According to the flight instructor, the approach was normal, and the touchdown occurred with no sideloading. The flight instructor also stated that he checked the gear three times; the pilot receiving instruction checked it twice; and the gear appeared to be in the down and locked position, as indicated by the three green landing gear lights. A representative from the Federal Aviation Administration (FAA), along with maintenance personnel from the operator, examined the airplane at the accident site and observed the composite right landing gear brace rib had separated from the wing structure. Further examination of the airframe revealed the right main landing gear brace rib had separated from its attachment points at the spar and upper wing skin. The bonding paste material was still adhered to both the brace rib and the spar/wing skin attachment points, consistent with correct adhesion of the components. There was no evidence of faulty adhesion from the original installation. The examination also revealed an 8- to 10-inch crack between the upper and lower wing skin bonds to the airplane’s center section spar. A coin tap test and a visual examination revealed no cracks on the left main landing gear brace. A review of maintenance documents revealed that the latest service bulletins and airworthiness directives had been performed on the airplane. Also, the airplane had recently completed a 100-hour/annual inspection about 3 weeks before the accident, with no report of damaged or faulty components related to the landing gear. The airplane had been flown for about 35 hours since the annual inspection by multiple pilots. The pilot receiving instruction performed a short-field landing to a runway. During the rollout, about 750 ft from the touchdown point, the right main landing gear collapsed, and the right wing contacted the runway, which resulted in substantial damage to the right aileron. A postaccident inspection revealed the right main landing gear brace rib had separated from the wing structure. Examination of the failed components revealed the separation did not occur due to faulty adhesion from the original installation. In addition, an 8- to 10-inch crack was discovered between the upper and lower wing skin bonds to the airplane’s center section spar. That crack would have resulted from some type of force or stress to the airplane, such as a hard landing. However, no hard landings in the airplane had been reported. The airplane had undergone a 100-hour/annual inspection about 3 weeks before the accident, with no reports of damage or faults related to the landing gear. The airplane had been flown for about 35 hours since the inspection by multiple pilots. It is likely that the separation of the right main landing gear support assembly and the crack were initiated by a hard landing that was not reported since the inspection. The condition of the right main landing gear brace rib likely began to deteriorate and the right main landing gear subsequently collapsed during the accident flight. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • Not determined-Not determined-(general)-(general)-Unknown/Not determined
  • Aircraft-Aircraft systems-Landing gear system-Main gear strut/axle/truck-Unknown/Not determined

Verbatim from NTSB's published report. Source file NTSB_2022_WPR22LA159.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗