# SDR ASOA200900852

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 5, 2009
- Submitted: August 7, 2009
- Operation: Air carrier
- Aircraft: [N856AS](https://openairdocs.org/aircraft/N856AS), registered now
- Make and model: Cndair CL6002B19
- Aircraft serial: 7404
- Aircraft time: 22,996 hours, 19,039 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ASOA200900852

## Discrepancy

FRAME 718.0 HAS A .025 INCH LONG CRACK FROM TOP RIVET TO EDGE OF ATTACHING POINT JUST BELOW STR 11R ON FWD SIDE OF FRAME MEMBER.  TRIMMED CRACKED FLANGE PER REO 601R-53-61-193 REV A, VIEW C.  C/W LPI OF THE RT FRAME 718.0 REPAIR CUT LINE PER REO 601R-53-61-193 "A" IAW NDTM PT 1, 51-20-08.  NO INDICATIONS NOTED AT THIS TIME.  FABRICATED -4 ANGLE AND -6 FILLER PER REO 601R-53-61-193 "A".  INSTALLED REPAIR -4 ANGLE, AND -6 FILLER PER REO 601R-53-61-193 "A".   C/W EO 600-53-0067 REV A.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
