# SDR 08FDEA04581

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 27, 2008
- Submitted: October 29, 2008
- Operation: Air carrier
- Aircraft: [N920FD](https://openairdocs.org/aircraft/N920FD), registered now
- Make and model: Boeing 757-23A
- Registry model: [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a) (OpenAirDocs)
- Aircraft serial: 24289
- Aircraft time: 68,579 hours, 21,958 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Part number: 70750063C
- Condition: Damaged
- Location: Bs 800
- 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/08FDEA04581

## Discrepancy

AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT BS 800, FOUND SEVERAL   HOLES ON FRAME.  REMOVED DAMAGE AT BS 800 FROM S4R TO 4L IAW SRM 53-00-07.  FABRICATED NEW ZEE FRAME PER MAE TRAVELER T8/763342.  FABRICATED NEW SPLICES PER MAE TRAVELER T8/761971.  DRILLED REPAIR PARTS IAW SRM 53-00-07 .  TREATED AND PRIMED REPAIR PARTS IAW SRM 53-00-07.  INSTALLED REPAIR PARTS AT BS 800 IAW SRM 53-00-07.  DO A HFEC INSPECTION EVERY 12,000 FLT CYCLES AS GIVEN IN NDT 6,51-00-01 REPEAT THIS INSPECTION AT EVERY 12,000 FLT CYCLES INTERVALS AS ALTERNATIVE DO A DETAILED VISUAL INSPECTION EVERY 9,000 FLT CYCLES AFTER INITIAL INSPECTION.  THIS IS A CAT "B" REPAIR .

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