# SDR DHL9980211C

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 21, 1999
- Submitted: March 26, 2000
- Operation: Air carrier
- Aircraft: [N802DH](https://openairdocs.org/aircraft/N802DH), 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: 46076
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- Location: Bs 1600
- Stage of operation: IN
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DHL9980211C

## Discrepancy

C-CHECK, UPPER CARGO COMPT AT STA 1600 CIRCUMFERENTIAL FRAME AT CUSP LINE WAS CRACKED RT SIDE.  CUT OUT CRACKED SECTION OF FRAME AT FS 1580 RT M CARGO CABIN IAW DC-8 SRM 53-2-0 FIG 2.  FABRICATED NEW SECTION OF FRAME:  6 X 2.5 AND 2 SPLICES 10 X 2.5 IAW MHA ENGINEERING NR 3126.  HEAT TREATED FRAME & SPLICES 7075-0 TO 7075-T6 IAW DC-8 SRM 51-1-1, PG 1 TO 21, CLEANED REPAIR AREA PER SRM 51-1-8 PAR 6A.  DRILLED NEW SECTION OF FRAME & SPLICES PER SRM 51-3-2, PG 1, 51-1-4, PG 1. TREATED, PRIMED AREA & PARTS IAW DC-8 SRM 51-1-8, PG 13 & 16.  OK TO INSTALL FRAME REPAIR IAW DC-8 SRM 51-1-20D, PAR 7.

---
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.
