# SDR FXGA201610141636

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 14, 2016
- Submitted: October 27, 2016
- Operation: Air carrier
- Aircraft: [N747CE](https://openairdocs.org/aircraft/N747CE), registered now
- Make and model: Doug C-118A
- Registry model: [Doug C-118A](https://openairdocs.org/model/douglas-c-118a) (OpenAirDocs)
- Aircraft serial: 44661
- Engine: Pwa R2800CB3
- Propeller: Hamstd 43E60
- 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/FXGA201610141636

## Discrepancy

CRACKED FUSELAGE FRAME AT FS 1071 STRINGER 14R.  REPAIR A 1/4" CRACK IN A FUSELAGE FRAME.  THE CRACK GOES FROM STRINGER 14R RELIEF RADIUS TO A RIVET HOLE.  INSTALL REPAIR DOUBLER ON CRACKER FRAME AT FS 1071 PER DRAWING 1636-01 AND OVERHAUL MANUAL FIGURE 12-3A.

---
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.
