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Atlas / NTSB / ANC95LA122

NTSB CAROL · Event

Event ANC95LA122

1995-07-31 KODIAK, Alaska, United States Airport · ADQ None 1 aircraft Status: Completed

Registry · N17481

FAA Aircraft Registry record.

Make / Model

GRUMMAN G-44

Year of manufacture

1944 · 51 years old at event

Engine

LYCOMING GO-435 (210 hp)

Seats / Engines

5 seats · 2 engines

Last airworthiness date

19740621

ADS-B equipped

Yes — Mode-S A12B93

Registrant of record

BALL FRED E

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

OVERLOAD FAILURE OF THE MAIN LANDING GEAR WHEEL.

Factual narrative

On July 31, 1995, at 1840 Alaska daylight time, an amphibious Grumman G-44, N17481, crashed during takeoff at Kodiak airport, Kodiak, Alaska. The airplane was being operated as a visual flight rules (VFR) cross- country on-demand passenger flight to Danger Bay, Alaska, under Title 14 CFR Part 135 when the accident occurred. The airplane, operated by Peninsula Airways Inc., received substantial damage. The certificated commercial pilot and the sole passenger were not injured. Visual meteorological conditions prevailed. Company VFR flight following procedures were in effect. The operator reported that the pilot was departing on runway 07. During the takeoff run, the pilot noticed a loud noise and the airplane lurched to the right. To maintain directional control of the airplane, the pilot aborted the takeoff and attempted to apply the left brake without any response. The pilot was unable to prevent the airplane from ground looping to the right. The left wing float and tail wheel were damaged. The left wingtip contacted the runway and was bent upward. Inspection of the airplane revealed that the left wheel rim was broken near the bolt holes. The wheel rim was submitted to the National Transportation Safety Board's Materials Laboratory for examination. The examination did not reveal any evidence of fatigue. All fracture surfaces exhibited evidence of overload. THE CERTIFICATED COMMERCIAL PILOT AND A PASSENGER WERE DEPARTING A HARD SURFACED RUNWAY IN AN AMPHIBIOUS AIRPLANE FOR AN ON-DEMAND CHARTER FLIGHT. DURING THE TAKEOFF ROLL, THE AIRPLANE LURCHED TO THE RIGHT. THE PILOT APPLIED THE LEFT BRAKE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE WITHOUT ANY RESPONSE. HE ABORTED THE TAKEOFF, BUT WAS UNABLE TO PREVENT THE AIRPLANE FROM GROUND LOOPING TO THE RIGHT. INSPECTION OF THE AIRPLANE REVEALED THAT THE LEFT WHEEL RIM WAS BROKEN NEAR THE HUB BOLT HOLES. A METALLURGICAL EXAMINATION OF THE WHEEL DID NOT REVEAL ANY EVIDENCE OF FATIGUE. ALL FRACTURE SURFACES EXHIBITED EVIDENCE OF OVERLOAD. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_ANC95LA122.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. 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 ↗