# Incident 20130121000899I: Cessna S550, Portland, OR, January 21, 2013

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: January 21, 2013, 18:52 local time
- Place: Portland, OR
- Damage: No damage
- Phase of flight: Takeoff: Climb Out
- Operating rules: General operating rules (Part 91)
- Location: 45.5235° N, 122.6762° W: Placed by OpenAirDocs: center of Portland, OR, within about 7 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=45.5235&lon=-122.6762&mi=10
- Aircraft: N84EC, a cancelled registration (https://openairdocs.org/deregistered/N84EC-2022-11-05) (OpenAirDocs)
- Registry model: Cessna S550 (registry code 2076607, https://openairdocs.org/model/cessna-s550) (OpenAirDocs)
- Registry engine: Pratt & Whitney Canada JT15D-1 series (registry code 52060, https://openairdocs.org/engine/pratt-whitney-canada-jt15d-1-series) (OpenAirDocs)
- Reported make and model: CESSNA S550
- Reported engine: P&W CANADA JT15D-1
- People aboard: 2
- Fatal injuries: 0
- Other injuries: 0
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20130121000899I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

DURING CLIMB OUT THE RIGHT (#2) ENGINGE SHUT DOWN. PILOT COMPLETED EMERGENCY CHECKLIST PROCEDURES, AND DECLARED AN EMERGENCY. AN ATTEMPT WAS MADE TO RESTART THE ENGINE WAS UNSUCSESFUL.

FOLLOWIGN AN UNEVENTFULL LANDING, IT WAS FOUND THAT THE FUEL FLOW TRANSMITER BACK COVER PLATE HAD POPPED OPEN AND TWO OF FOUR BOLTS HAD SHEARD.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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