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Atlas / NTSB / ANC93LA090

NTSB CAROL · Event

Event ANC93LA090

1993-06-12 KIVALINA, Alaska, United States Airport · KVL None 1 aircraft Status: Completed

Registry · N222JA

FAA Aircraft Registry record.

Make / Model

ROBINSON HELICOPTER R22 BETA

Year of manufacture

2000

TCDS

H10WE · ROBINSON HELICOPTER CO

Engine

LYCOMING I0360 SER (180 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

20000320

ADS-B equipped

Yes — Mode-S A1E938

Registrant of record

JEFF ABRAMS LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE FAILURE OF THE PIVOT LINK FOR THE DOWNLOCK MECHANISM AND THE IMPROPER RIGGING OF THE LANDING GEAR LOCKING MECHANISM BY COMPANY MAINTENANCE PERSONNEL.

Factual narrative

On June 12, 1993, at 1410 Alaska daylight time, a retractable gear, wheel equipped Cessna 402 airplane, N222JA, registered to and operated by Alaska Island Air of Anchorage, Alaska, experienced a right main gear collapse during the landing roll at Kivalina, Alaska. The air taxi flight, operating under 14 CFR Part 135, departed Kotzebue and the destination was Kivalina. A company flight plan was in effect and visual meteorological conditions prevailed. The Airline Transport Certificated Pilot- in-Command, the sole occupant, was not injured and the airplane received substantial damage. According to the Pilot-in-Command, the landing was normal and during the rollout when the airplane slowed to 40 knots, the right wing settled to the runway. Examination of the airplane showed that the pivot link, which is the link between the push pull tubes and the over center link assembly, had failed. According to the Certificate Repair Station employed to repair the airplane, the landing gear system was out of rig. The Company stated they submitted an NTSB Form 6120.1/2 to the FAA FSDO Office in Fairbanks. The FSDO Office has no record of having received this form. DURING THE LANDING ROLL THE PILOT STATED THE RIGHT WING SETTLED TO THE RUNWAY. EXAMINATION OF THE AIRPLANE SHOWED THAT THE PIVOT LINK BETWEEN THE PUSH PULL TUBES AND THE OVER CENTER LINK ASSEMBLY FAILED. ACCORDING TO THE REPAIR STATION EMPLOYED TO REPAIR THE AIRPLANE, THEY CHECKED THE LANDING GEAR SYSTEM RIGGING AND FOUND IT TO BE OUT OF TOLERANCE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1993_ANC93LA090.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 (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 ↗