NTSB CAROL · Event
Event ANC10LA026
Registry · N3492C
FAA Aircraft Registry record.
Make / Model
CESSNA 170B
Year of manufacture
1954 · 56 years old at event
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19561123
ADS-B equipped
Yes — Mode-S A3E15E
Registrant of record
PISCOYA THOMAS G
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The structural failure of the right main landing gear leg, resulting in the collapse of the landing gear.
Factual narrative
On March 17, 2010, about 1530 Alaska daylight time, a ski-equipped Cessna 170B airplane, N3492C, sustained substantial damage when the main landing gear collapsed during taxi for takeoff, at Lake Hood Seaplane Base, Anchorage, Alaska. The airplane was being operated by the pilot as a visual flight rules (VFR) personal local flight under Title 14, CFR Part 91, when the accident occurred. The airline transport pilot and sole passenger were not injured. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on March 18, the pilot said he was taxiing for takeoff on Lake Hood when the right main landing gear leg broke near where the leg exits the fuselage. He said when the leg broke the right wing impacted the ground, bending the wing from the aileron outward toward the tip. He said there were no mechanical problems with the airplane prior to the accident. During a meeting with the NTSB IIC on March 25, the pilot presented the broken gear leg to the IIC and an FAA air safety inspector. The break appeared to be a single linear break perpendicular to the leading edge of the gear leg. The break was about 6 inches from the gear leg mounting bolt hole, at the widest portion of the gear leg. No other damage was observed. The gear leg was retained by the FAA inspector for metallurgical examination. The airline transport pilot was on a personal flight in a ski-equipped airplane. The pilot said that he was taxiing for takeoff when the right main landing gear leg broke near where the leg exits the fuselage. When the leg broke the right wing impacted the ground, bending the wing from the aileron outward toward the tip. An examination of the break showed a single linear break perpendicular to the leading edge of the gear leg. The break was about 6 inches from the gear leg mounting bolt hole, at the widest portion of the gear leg. The gear leg was retained for metallurgical examination by the Federal Aviation Administration. 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).
- C Aircraft-Aircraft systems-Landing gear system-Main landing gear-Failure - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ANC10LA026.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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