N1718RCESSNA A185F2025-03-07 NTSB Accident Report

Substantial
None

CESSNA A185FS/N: 18502439

Summary

On March 07, 2025, a Cessna A185F (N1718R) was involved in an incident near Highline Lake, AK. All 1 person aboard were uninjured. The aircraft sustained substantial damage.

On March 7, 2025, about 1430 Alaska standard time, a Cessna 185 airplane, N1718R, sustained substantial damage when it was involved in an accident near Skwentna, Alaska. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The airplane was taxiing for takeoff from a remote snow-covered lake. The pilot reported that as he was turning the airplane for takeoff the right gear leg collapsed. The failed gear leg resulted in substantial damage to the landing gearbox and door post assembly.

This incident is documented in NTSB report ANC25LA030. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N1718R.

Accident Details

Date
Friday, March 7, 2025
NTSB Number
ANC25LA030
Location
Skwentna, AK
Event ID
20250403199961
Coordinates
61.765010, -151.577640
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

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.

Aircraft Information

Registration
Make
CESSNA
Serial Number
18502439
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
A185FC185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A185F

Registered Owner (Current)

Name
STRIPE JOSEPH
Address
4403 62ND AVE SE
City
OLYMPIA
State / Zip Code
WA 98513-4914
Country
United States

Analysis

On March 7, 2025, about 1400 Alaska standard time, a ski-equipped Cessna 185 airplane, N1718R, sustained substantial damage when it was involved in an accident near Skwentna, Alaska. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane was taxiing for takeoff from a remote snow-covered lake when the right landing gear leg collapsed, resulting in substantial damage to the landing gear box assembly and door post assembly.

According to maintenance records, the airplane had flown about 83 hours between May 2023 and the time of the accident. The owner reported that in October 2023, floats and float rigging were removed from the airplane and the main landing gear and wheels were installed. A review of the maintenance records did not reveal this alteration. Further review of the maintenance records indicated the wheels were removed in December 2023 and skis were installed on the airplane’s main landing gear legs.

The mechanic who performed the landing gear change in October 2023 stated that, although he did not recall the hardware used during the landing gear change, when he changes landing gear he uses the hardware provided by the owner for installing the gear. When asked why there was no entry made in the maintenance logbook for the landing gear assembly change, he said the owner never provided the logbooks for him to sign.

The hardware found installed on the airplane’s main landing gear spring was an AN7-20 bolt with a cross-drilled hole through the threaded portion of the bolt and an MS20365-720A nylon locking nut. According to the Cessna 180 and 185 Parts Catalog the hardware at the inboard end of the main landing gear spring should have consisted of an AN7-20A bolt that does not have a cross-drilled hole and an MS20365-70C nut, which is a locking nut with an all-metal design, and a spring adjustment shim.

The hardware was submitted to the NTSB’s Materials Laboratory for examination. The examination indicated that the bolt exhibited patchy and faint remnants of cadmium plating on the flats of the head. The shank of the bolt did not exhibit any remaining cadmium plating. The composition and hardness of the bolt were consistent with typical specifications for an AN-type bolt. The nut had worn and patchy cadmium plating.

Both the bolt and nut exhibited worn threads. The worn threads near the end of the bolt contained bits of the nut’s nylon locking insert. The nylon locking insert was worn down to the depth of the worn threads inside the nut; the wear was consistent with the thread wear occurring over time and not from a sudden instance of overload.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC25LA030