ASN Wikibase Occurrence # 358750
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Saturday 1 July 1995 |
Time: | 07:50 LT |
Type: | Cessna 401A |
Owner/operator: | Private |
Registration: | N444RJ |
MSN: | 401A0017 |
Year of manufacture: | 1968 |
Total airframe hrs: | 3700 hours |
Engine model: | CONTINENTAL TSIO-520E |
Fatalities: | Fatalities: 0 / Occupants: 5 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Van Nuys, CA -
United States of America
|
Phase: | Taxi |
Nature: | Private |
Departure airport: | (KVNY) |
Destination airport: | (MMSB) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:THE AIRCRAFT WAS MAKING A RIGHT-HAND TURN IN THE RUN-UP AREA AT A SLOW SPEED WHEN THE LEFT MAIN LANDING GEAR COLLAPSED. THE SIDE BRACE FOR THE MAIN LANDING GEAR IS ATTACHED TO A CASTING, WHICH IN TURN IS BOLTED TO THE INBOARD WING RIB IN THE LANDING GEAR WHEEL WELL. EXAMINATION REVEALED THAT THE WING RIB WEB CRACKED AROUND THE CASTING, WHICH ALLOWED THE SIDE BRACE TO MOVE AND THE LANDING GEAR TO COLLAPSE. PORTIONS OF THE CRACK APPEARED DISCOLORED AND OLD. REVIEW OF THE AIRCRAFT MAINTENANCE RECORDS REVEALED NO HISTORY OF LANDING GEAR DAMAGE OR HARD LANDING RELATED MAINTENANCE ACTIVITY. THE AIRCRAFT WAS LAST INSPECTED DURING AN ANNUAL INSPECTION 7 MONTHS AND 60 FLIGHT HOURS PRIOR TO THE ACCIDENT. CESSNA AIRCRAFT COMPANY REPORTED THAT IN RESPONSE TO CRACKS FOUND ON THE INBOARD WING RIB WEB AROUND THE SIDE BRACE FITTING, SERVICE LETTER ME76-2 WAS ISSUED ON JANUARY 5, 1976. THE LETTER DETAILS THE INSTALLATION OF A STEEL REINFORCEMENT/DOUBLER PLATE ON THE WING RIB WEB BEHIND THE LANDING GEAR SIDE BRACE FITTING. INSPECTION OF THE AIRCRAFT REVEALED THAT SERVICE LETTER ME76-2 WAS NOT ACCOMPLISHED.
Probable Cause: the failure of the wing rib web due to undetected cracking in an area of known crack development around the landing gear side brace fitting. The operator's failure to accomplish a Service Letter addressing the problem is a factor in the accident.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | LAX95LA232 |
Status: | Investigation completed |
Duration: | 7 months |
Download report: | Final report |
|
Sources:
NTSB LAX95LA232
Location
Revision history:
Date/time | Contributor | Updates |
14-Mar-2024 17:48 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation