# SDR ASOA201000884

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 8, 2010
- Submitted: June 14, 2010
- Operation: Air carrier
- Aircraft: [N748EV](https://openairdocs.org/aircraft/N748EV), registered now
- Make and model: Cndair CL6002C10
- Aircraft serial: 10158
- Aircraft time: 15,717 hours, 10,821 cycles
- Engine: Ge CF348C1
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Angle
- 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/ASOA201000884

## Discrepancy

SUPPORT ANGLE LT SIDE FOR COCKPIT PANEL 221ALF CRACKED.   BEGAN REMOVING FASTENERS ON LT SIDE FLOOR SUPPORT ANGLE FOR COCKPIT PANEL 221ALF. IAW SRM 51-42-06-001-001-A01.   R & R LT SIDE COCKPIT FLOOR SUPPORT ANGLE WITH SERVICEABLE PART ALL WORK DONE IAW SRM 51-42-06-001-001-A01.  A023 PROTECTIVE COATING NEEDS TO BE APPLIED.  COMPLIED WITH APPLICANCE OF PROTECTIVE COATING OF AREAS WORKED ON LT SUPPORT ANGLE OF PANEL 221ALF IAW SRM 51-25-06-001-001-(AO1).

---
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.