# N5408G: 1991 Cessna 550, registration cancelled 2022-02-05

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 5, 2022
- Status when cancelled: Registration expired, pending cancellation
- 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: 550-0666
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Multiple
- Airworthiness date: August 30, 1991
- Certificate issued: November 15, 1991
- Last registry action: May 14, 2018
- Mode S code: A6DB63
- 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/N5408G
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5408G
- Page: https://openairdocs.org/deregistered/N5408G-2022-02-05

From the FAA registry file of November 5, 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 (5)

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

- [SDR 4DSR20141102](https://openairdocs.org/sdr/4DSR20141102), Nov 24, 2014: DUCT. CRACKED. DURING SCHEDULED INSPECTION FOUND THE INLET ANTI-ICE HOT AIR DISTRIBUTION DUCT CRACKED FORWARD WHERE THE BLEED AIR TAP IS WELDED INTO THE DUCT. THIS AREA IS DIF
- [SDR 2005FA0001354](https://openairdocs.org/sdr/2005FA0001354), Jul 26, 2005: DRIVE ASSY. STIFF. THE PILOT REPORTED THAT THE CONTROLS WERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE CB WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LAND
- [SDR 2005FA0001129](https://openairdocs.org/sdr/2005FA0001129), Jul 26, 2005: DRIVE ASSY. INOPERATIVE. THE PILOT REPORTED THAT THE CONTROLS WHERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE C/B WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LA
- [SDR B3OR20010007](https://openairdocs.org/sdr/B3OR20010007), Jul 20, 2001: HARNESS. DETERIORATED. DUR HI-PWR ENG RUN, NOTICED LT ENG ITT AT 690 DEG. ITT CLIMBED, REDUCED PWR IN ORDER NOT TO EXCEED 700 DEG RED LINE OF ITT. A 5 PT PERFORMANCE RUN PERF AT P&W R
- [SDR B3OR200000008](https://openairdocs.org/sdr/B3OR200000008), Dec 4, 2000: SKIN. DAMAGED. INSPECTED THIS AC FOR LING LEADING EDGE SKIN CONTACT DAMAGE FROM HEATED LEADING EDGE RETAINING SCREWS DUE TO CONTACT DAMAGE BEING FOUND IN SISTER SHIP. DAMAGE W

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