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ANC25LA030 · Cessna A185F

7 Mar 2025 · Skwentna, AK, United States

Cessna A185F · Accident: system/component malfunction/failure (non-power) while taxiing

From an unrecorded airport to Lake Hood Seaplane Base (LHD)

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Event

NTSB case
ANC25LA030
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
Event fatalities
Unknown
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Cessna A185F

Aircraft type
Cessna 185
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N1718R
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo Lake Hood Seaplane Base (LHD), Anchorage, AK
Aircraft age
About 51 years (built 1974)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Taxi
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
System/component malfunction/failure (non-power)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Aircraft › Aircraft systems
  • Personnel issues › Task performance

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The pilot reported that, while taxiing for takeoff from a remote, snow-covered lake, the right landing gear leg collapsed, resulting in substantial damage to the landing gear box assembly and door post assembly. A postaccident examination of the right landing gear leg assembly revealed that the gear leg separated from its position in the landing gear box assembly and folded under the airplane. The bolt that secured the gear leg to the landing gear box assembly remained in place; however, the nut was found in the belly of the airplane. Although the hardware installed on the airplane’s main landing gear spring differed from the hardware specified in the airplane manufacturer’s parts catalog, the composition and hardness of the installed bolt were consistent with typical specifications for an AN-type bolt. However, the bolt and nut exhibited worn threads consistent with progressive wear over time rather than a sudden overload. The mechanic who performed a landing gear change about a year and a half before the accident stated that, although he did not recall the hardware used during the gear change, when he changes landing gear, he uses the hardware provided by the owner for installing the landing gear. Based on the condition of the nut and bolt, the worn hardware was likely re-used during the installation of the landing gear assembly. Re-use of the worn bolt and nut then allowed the hardware to fail under load during taxi, resulting in collapse of the landing gear.

Probable cause

Maintenance personnel’s reuse of worn hardware during the installation of the landing gear assembly and the hardware’s failure and subsequent separation of the gear leg from the landing gear box assembly during taxi.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ANC25LA030
Event ID
20250403199961
Case number
ANC25LA030
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates, cause areas. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: ad1d0d99b28a18fba4eca81be59b3804b03760c292587a9325fda5ecc6851eef; retrieved 2026-09-16T19:47:37.728Z.