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Atlas / NTSB / ANC99LA071

NTSB CAROL · Event

Event ANC99LA071

1999-06-08 PALMER, Alaska, United States Airport · 4AK6 None 1 aircraft Status: Completed

Registry · N7560K

FAA Aircraft Registry record.

Make / Model

CESSNA 180J

Year of manufacture

1976 · 23 years old at event

Engine

CONT MOTOR O-470 SERIES (230 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19760317

ADS-B equipped

Yes — Mode-S AA32B5

Registrant of record

ALBERT BRYAN WAYNE

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The failure of the pilot to maintain directional control during the water landing.

Factual narrative

On June 8, 1999, about 1700 Alaska daylight time, a float equipped Cessna 180J airplane, N7560K, sustained substantial damage during landing on Wolf Lake, Palmer, Alaska. The airline transport pilot and the one, pilot-rated passenger aboard were not injured. The airplane was being operated as a Visual Flight Rules (VFR) personal flight under 14 CFR Part 91. The flight departed from Alexander Creek, Alaska, about 1630. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. The pilot told the NTSB investigator-in-charge (IIC), during an interview on June 9, that he was landing the airplane with a left crosswind. He stated that the airplane landed on the left float first. The pilot stated that when the right float touched down, the airplane swerved left. He indicated that the airplane pitched nose down, striking the right wing and propeller. The pilot did not remember hitting anything with the floats, although the right float had a one foot long crease along the keel near the forward compartment aft bulkhead. The right wing and aileron sustained substantial damage. Postaccident inspection revealed that the float struts were straight, and the lengths of the float flying wires varied by 3/4 inches. No other mechanical anomalies were noted with the airplane or floats. The floats were installed 14 hours prior to the accident. This was the second landing of the day. The pilot was landing the floatplane with a left crosswind. After touchdown on the water, the floatplane swerved left, then nosed down, damaging the right wing, right aileron, and propeller. Postaccident inspection revealed the float struts were straight, and the length of the float flying wires varied by 3/4 inch. The pilot did not remember hitting anything with the floats, but the bottom of the right float had a one foot long crease near the forward compartment. No other mechanical anomalies were noted. The floats were installed 14 hours prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1999_ANC99LA071.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). 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 ↗