# N588X: 1953 General Dynamics CV-340/580, registration cancelled 2012-02-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 10, 2012
- Exported to: Mexico
- Status when cancelled: Triennial form not returned
- Airframe: [General Dynamics CV-340/580](https://openairdocs.org/model/general-dynamics-cv-340-580) (registry code 3790243)
- Engine: [Allison 501-D13](https://openairdocs.org/engine/allison-501-d13) (registry code 03055)
- Data sheets: [TCDS E-282](https://openairdocs.org/tcds/E-282) (OpenAirDocs)
- Serial number: 52
- Year built: 1953
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: July 13, 2006
- Certificate issued: February 17, 2006
- Last registry action: February 17, 2009
- Mode S code: A795AD
- Owner when cancelled: [N580 Inc](https://openairdocs.org/faa-owner/N580%20INC)
- Location: [Spanaway, WA](https://openairdocs.org/faa-place/WA/Spanaway)
- Owner type: Corporation
- Owner's area on the map: 47.0609° N, 122.3889° W: Placed by OpenAirDocs at the center of ZIP code 98387, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N588X
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=588X
- Page: https://openairdocs.org/deregistered/N588X-2012-02-10

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the General Dynamics CV-340/580: https://openairdocs.org/model/general-dynamics-cv-340-580.md

## Service difficulty reports (6)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR I5HA0858015](https://openairdocs.org/sdr/I5HA0858015), Dec 26, 2008: SKIN. DAMAGED. DURING CLIMB OUT, EN-ROUTE, THE CREW FELT A "THUMP" POSSIBLY FROM THE LT WING. THE CREW COULD NOT SEE ANY DAMAGE AND DID NOT EXPERIENCE ANY CONTROL PROBLEMS. TH
- [SDR I5HA0858001](https://openairdocs.org/sdr/I5HA0858001), Mar 6, 2008: BOLT. BROKEN. DURING CLIMBOUT, THE CREW LOST THROTTLE CONTROL ON THE NR 2 ENGINE. THEY PREFORMED THE EMERGENCY PROCEDURES AND SHUTDOWN THE ENGINE. UPON ARRIVAL MAINT INSPECTE
- [SDR I5HA0758009](https://openairdocs.org/sdr/I5HA0758009), May 1, 2007: PUMP. OUT OF LIMITS. WHILE EN-ROUTE FROM BORINQUEN (BQN) TO PORT-O-SPAIN (POS) APPROXIMATELY ONE HOUR INTO THE FLIGHT, THE CREW OBSERVED THE RIGHT HAND REDUCTION GEARBOX OIL PRESSUR
- [SDR I5HA0658010](https://openairdocs.org/sdr/I5HA0658010), Oct 12, 2006: BYPASS VALVE. STUCK. WHILE CLIMBING THROUGH 10,000 FT, A STRONG HYDRAULIC FLUID ODOR WAS NOTED IN THE COCKPIT AND THE CREW OBSERVED THAT THE HYD RESERVOIR QUANTITY DROPPING . CAPTAI
- [SDR I5HA0658008](https://openairdocs.org/sdr/I5HA0658008), Sep 28, 2006: CLAMP. DISCONNECTED. AFTER TAKEOFF, THE AIRCRAFT FAILED TO PRESSURIZE. THE CAPTAIN RETURNED TO DEPARTURE WITHOUT INCIDENT. SUBSEQUENT INSPECTION FOUND THAT THE EDC DISCHARGE DUCT HA
- [SDR I5HA058006](https://openairdocs.org/sdr/I5HA058006), Aug 1, 2005: METER. VIBRATION. AUG 1, 2006 DURING THE TAKEOFF ROLL, THE CREW OBSERVED WHAT THEY BELIEVED TO BE A LOSS OF POWER FROM THE LT HAND ENGINE AND FELT A VIBRATION. THE TAKEOFF WAS AB

---
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.