What was found
(AUS) FUSELAGE RIB LOCATED AT STN 81 IN AREA OF REAR SEAT FORWARD ATTACHMENT NUTS CRACKED LONGITUDINALLY IN SEVERAL PLACES - CRACK LENGTHS 50.8MM TO 76.2MM (2IN TO 3IN)
- Difficulty date
- May 8, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Cessna 172M
- Propeller
- Mcauly 1C160DTM
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Rib
- 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.