ASN Wikibase Occurrence # 362734
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| Date: | Tuesday 27 October 1992 |
| Time: | 10:00 LT |
| Type: |  Beechcraft A35 |
| Owner/operator: | Private |
| Registration: | N8501A |
| MSN: | D1923 |
| Year of manufacture: | 1948 |
| Total airframe hrs: | 2280 hours |
| Engine model: | CONTINENTAL 225-8 |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Vancouver, WA -
 United States of America
|
| Phase: | Unknown |
| Nature: | Private |
| Departure airport: | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
IT WAS REPORTED SEVERAL MONTHS AFTER THE OCCURRENCE, THAT WRINKLES IN THE SKIN WERE FOUND NEAR THE EMPENNAGE DURING A PREFLIGHT CHECK. FURTHER INSPECTION REVEALED THAT THE AFT BULKHEAD AND STRINGERS WERE DAMAGED. THE PILOT REPORTED THAT THE AIRPLANE HAD BEEN REPAINTED, THEN UNDERWENT AN ANNUAL INSPECTION. THE AIRPLANE HAD BEEN FLOWN APPROXIMATELY TWO HOURS AFTER THE ANNUAL INSPECTION. SEVERAL DAYS AFTER THE LAST FLIGHT, THE PILOT NOTED THE WRINKLES IN THE FUSELAGE. A MECHANIC INSPECTED THE AIRPLANE AND REPORTED THAT THE BALANCE OF BOTH RUDDERVATORS WAS FOUND TO BE WITHIN LIMITS AS SPECIFIED IN THE BEECH MAINTENANCE MANUAL. THE PILOT DOES NOT RECALL ANY TIME IN WHICH THE AIRPLANE WAS OPERATED BEYOND THE AIRCRAFT OPERATING SPECIFICATIONS.
Probable Cause: DESIGN STRESS LIMITS OF THE AIRCRAFT WERE EXCEEDED.
Accident investigation:
 |
|
Sources:
NTSB SEA93LA019
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 18-Mar-2024 09:43 | ASN Update Bot | Added |
Corrections or additions? ... Edit this accident description
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