What was found
(AUS) WING CENTRE SECTION FORWARD SPAR WEB PLATE CRACKED IN AREA OF LH UPPER WING ATTACHMENT AREA - CRACK LENGTH 25MM (0.98IN) - SEVERALSMALLER CRACKS WERE FOUND AROUND THE LOCK BOLT HOLES - CRACK LENGTHS APPROXIMATELY 7MM (0.275IN)
- Difficulty date
- March 10, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech 58
- Engine
- Cont
- System (JASC)
- 5720 · Wing Miscellaneous Structure
- Part
- Plate
- Condition
- Cracked
- Location
- Centre Wing Sys
- Component
- 00243001811
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.