# N5314J: 1991 Cessna 550, registration cancelled 2019-11-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 12, 2019
- Status when cancelled: Valid registration
- Airframe: [Cessna 550](https://openairdocs.org/model/cessna-550) (registry code 2076604)
- Engine: [Pratt & Whitney Canada JT15D-4 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-4-series) (registry code 52112)
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (OpenAirDocs)
- Serial number: 550-0663
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 5, 1991
- Certificate issued: January 15, 1992
- Last registry action: February 15, 2019
- Mode S code: A6B711
- Owners when cancelled: [U S Department Of Homeland Security](https://openairdocs.org/faa-owner/U%20S%20DEPARTMENT%20OF%20HOMELAND%20SECURITY), [U S Customs & Border Protection](https://openairdocs.org/faa-owner/U%20S%20CUSTOMS%20%26%20BORDER%20PROTECTION)
- Location: [Washington, DC](https://openairdocs.org/faa-place/DC/Washington)
- Owner type: Government
- Owner's area on the map: 38.8951° N, 77.0364° W: Placed by OpenAirDocs: center of Washington, DC, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N5314J
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5314J
- Page: https://openairdocs.org/deregistered/N5314J-2019-11-12

From the FAA registry file of November 7, 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 Cessna 550: https://openairdocs.org/model/cessna-550.md

## Service difficulty reports (7)

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

- [SDR 2007FA0000303](https://openairdocs.org/sdr/2007FA0000303), Apr 3, 2007: ACTUATOR. BINDING. AFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM 
- [SDR 2007FA0000302](https://openairdocs.org/sdr/2007FA0000302), Apr 3, 2007: ACTUATOR. BINDING. AFTER A PHASE 1-4 INSPECTION THE ELEVATOR TRIM WAS FOUND TO BE BINDING. INSPECTION OF THIS SYSTEM FOUND THAT THE WILKIE BUTTON IN THE BACK OF THE ACTUATOR TRIM 
- [SDR 2001FA0000512](https://openairdocs.org/sdr/2001FA0000512), Nov 8, 2001: CONTROLLER. MISREPAIRED. UPON INSTALLATION OF A REPAIRED CABIN PRESSURE RATE CONTROLLER IT WAS FOUND THAT THE AC WOULD NOT TEST OR PRESSURIZE ON THE GROUND. AFTER CHECKING THE ATTACHING
- [SDR B3OR00000007](https://openairdocs.org/sdr/B3OR00000007), Nov 30, 2000: SKIN. DAMAGED. WHILE REPLACING A WING DEICE BOOT, DISCOVERED THAT ONE OF THE HEATED LEADING EDGE RETAINING SCREWS HAD MADE CONTACT WITH THE WING SKIN AT WS60. THE DAMAGE IS BE
- [SDR B3OR200000007](https://openairdocs.org/sdr/B3OR200000007), Nov 30, 2000: SKIN. DAMAGED. WHILE REPLACING A WING DEICE BOOT, DISCOVERED ONE OF THE HEATED LEADING EDGE RETAINING SCREWS HAD MADE CONTACT WITH THE WING SKIN AT WS 60. THE DAMAGE IS FAR BE
- [SDR 96ZZZX5150](https://openairdocs.org/sdr/96ZZZX5150), Sep 20, 1996: COUPLING. OVERTORQUE. WHILE PERFORMING MAINTENANCE TO ACM, COUPLING (V-BAND CLAMP) WAS FOUND SEVERELY OVERTORQUED ALMOST TO THE POINT OF FAILURE. CLAMP WAS REPLACED USING CORRECT TOR
- [SDR 95ZZZX6044](https://openairdocs.org/sdr/95ZZZX6044), Sep 19, 1995: REGULATOR. GASKET FAILED. AT ALMOST EVERY PHASE INSPECTION, FIND THE 23 PSI PNEU REGULATOR LEAKING BLEED AIR DUE TO BLOWN GASKET. REGULATOR IS LOCATED NEXT TO THE AFT PRESSURE BULKHEAD A

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