# SDR DHL2004804524

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 9, 2004
- Submitted: August 2, 2004
- Operation: Air carrier
- Aircraft: [N804DH](https://openairdocs.org/aircraft/N804DH), registered now
- Make and model: Doug DC-8-73F
- Registry model: [Doug DC-8-73F](https://openairdocs.org/model/douglas-dc-8-73f) (OpenAirDocs)
- Aircraft serial: 46124
- Aircraft time: 80,489 hours, 29,231 cycles
- System (JASC): [5315 · Fuselage Main, Floor Beam](https://openairdocs.org/jasc/5315)
- Part: Floorbeam
- Condition: Cracked
- Location: Fuselage
- Part time: 80,489 hours, 29,231 cycles
- 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/DHL2004804524

## Discrepancy

MAIN CARGO COMPT BEAM WEB CRACK 2.500, STA 960.000 RBL 59 (MAJOR REPAIR).  PERFORMED MAJOR REPAIR IAW DC8 SRM 53-7-3 PG 17-18, DC8 SRM 51-2-0 PG 78, DC8 SRM 51-2-1 (TR 51-130) JAN 26-04 FIG 1.  REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21.  PERFORMED STOP HOLE AND FABRICATED REINFORCING ANGLE (7075-T6 51 AL 0.200) IAW DC8 SRM 51-2-1 (TR 51-130) FIG 1, SHEET 1-6, 10-12.  CLEANED, TREATED AND PRIMED AREA AND REINFORCING ANGLE IAW DC8 SRM 51-1-8B.  INSTALLED REINFORCING ANGLE IAW DC8 SRM 51-2-1 (TR 51-130), DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9.

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