What was found
(AUS) FUSELAGE STIFFENER LH CRACKED IN AREA OF TORQUE TUBE SUPPORT REAR ANCHOR NUT HOLE - FOUND DURING INSPECTION IAW SOCATA 10-77-53
- Difficulty date
- March 27, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Socata TB10TOBAGO
- Engine
- Lyc O360A1A
- Propeller
- Hartzl HCC2YK2
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- TB1021029165
- Condition
- Cracked
- Location
- Main Frame Sys
- 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.