# SDR ZZDA2008078

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 9, 2008
- Submitted: March 12, 2008
- Operation: Air carrier
- Aircraft: [N920AT](https://openairdocs.org/aircraft/N920AT), registered now
- Make and model: Boeing 717-200
- Registry model: [Boeing 717-200](https://openairdocs.org/model/boeing-717-200) (OpenAirDocs)
- Aircraft serial: 55083
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ZZDA2008078

## Discrepancy

CRACK NOTICED AFT FUSELAGE INT LEFT CANTED FRAME AREA STA 1178.225 BELOW L16L AFT OF HYD S/O VALVE.  INSTALLED ANGLE REPAIR AT LEFT CANTED FRAME STA 1178.225 BELOW L161L, AFT OF HYD S/O VALVE IAW B717 SRM 51-70-11 FIG 201 REPAIR 1.  MATERIAL USED 7075-0 .080 SIZE 11" X 21.2".  HEAT TREATED FROM 0 TO T6 IAW AVBORNE HEAVY MAINTENANCE, GENERAL PROCESS SPEC 98PMS.24PS-01.

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