What was found
(CAN) DURING A 200 HR INSPECTION FUSLAGE FRAME PN 0512011-1, STA 108.0 WAS FOUND TO HAVE 4 CRACKS APPROXINATLY 1/2 - 1 INCH IN LENGTH ORIGINATING FROM THE INBOARD FLANGE OF THE FRAME AT EACH OF THE 4 CORNERS.
- Difficulty date
- November 4, 2004
- Submitted
- March 3, 2005
- Operation
- General aviation
- Make and model
- Cessna 172M
- Aircraft time
- 4,630 hours
- Engine
- Lyc O320E2D
- System (JASC)
- 5311 · Fuselage Main, Frame
- Part
- Frame
- Part number
- 05120111
- Condition
- Cracked
- Location
- Fuselage
- Stage of operation
- IN
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.