20000715013559A

Accident · No damage

FAA accident report · Cessna 182 · Snohomish, WA · July 15, 2000

Date
July 15, 2000 · 10:30 local
Place
Snohomish, WA
Airport
Harvey Field Airport
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N6473A
NTSB investigation
NTSBSEA00LA134
Reported as
Cessna 182

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) While taxing onto grass at Harvey field in Snohomish Washington, the right landign gear support failed. Inspection at the owners facility revealed p/n 0741009-4 right landing gear spring failed at the mating area of the p/n 0541121-2 landing gear outside support, located inside the aircraft fuselage. This failure caused the landing gear to penetrate the cabin aft to the right crew door. Substantial damage also occurred to the right side of the horizontal stabilizer, right elevator, and outboard section of the right wing. Inspection of aircraft records found an annual inspection had been completed 60.27 hours prior to the failure on June 15, 2000. No activation of the aircraft ELT was noted. Part total time 14306 hours. No propeller strike damage noted.

As the FAA filed it

(-23) WHILE TAXING ONTO GRASS AT HARVEY FIELD IN SNOHOMISH WASHINGTON, THE RIGHT LANDIGN GEAR SUPPORT FAILED. INSPECTION AT THE OWNERS FACILITY REVEALED P/N 0741009-4 RIGHT LANDING GEAR SPRING FAILED AT THE MATING AREA OF THE P/N 0541121-2 LANDING GEAR OUTSIDE SUPPORT, LOCATED INSIDE THE AIRCRAFT FUSELAGE. THIS FAILURE CAUSED THE LANDING GEAR TO PENETRATE THE CABIN AFT TO THE RIGHT CREW DOOR. SUBSTANTIAL DAMAGE ALSO OCCURRED TO THE RIGHT SIDE OF THE HORIZONTAL STABILIZER, RIGHT ELEVATOR, AND OUTBOARD SECTION OF THE RIGHT WING. INSPECTION OF AIRCRAFT RECORDS FOUND AN ANNUAL INSPECTION HAD BEEN COMPLETED 60.27 HOURS PRIOR TO THE FAILURE ON JUNE 15, 2000. NO ACTIVATION OF THE AIRCRAFT ELT WAS NOTED. PART TOTAL TIME 14306 HOURS. NO PROPELLER STRIKE DAMAGE NOTED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.