# N2663Y: 1989 Cessna 550, registration cancelled 2020-08-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 2, 2020
- 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: 550-0602
- Year built: 1989
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 21, 1989
- Certificate issued: April 3, 2017
- Last registry action: April 3, 2017
- Mode S code: A2981F
- Owner when cancelled: [Jet Air Inc](https://openairdocs.org/faa-owner/JET%20AIR%20INC)
- Location: [Iowa City, IA](https://openairdocs.org/faa-place/IA/Iowa%20City)
- Owner type: Corporation
- Owner's area on the map: 41.6484° N, 91.5968° W: Placed by OpenAirDocs at the center of ZIP code 52246, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N2663Y
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2663Y
- Page: https://openairdocs.org/deregistered/N2663Y-2020-08-02

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 (6)

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

- [SDR 2007H0002](https://openairdocs.org/sdr/2007H0002), Mar 5, 2007: ACTUATOR. MISOVERHAULED. ACTUATOR RODS PROVIDED WITH UNIT WERE TOO SHORT TO MOVE ELEVATOR TABS THE REQUIRED AMOUNT.
- [SDR L3WSA](https://openairdocs.org/sdr/L3WSA), Nov 18, 2005: CONTROL CABLE. FRAYED. WE HAVE FOUND THE ELEVATOR AUTOPILOT SERVO LT CABLE WITH BROKEN STRANDS ON 3 SUCCESSIVE AIRCRAFT THAT WERE UNDERGOING A PHASE 5 INSPECTION. ON CABLE HAD 50 PERC
- [SDR 2005R0037](https://openairdocs.org/sdr/2005R0037), Dec 16, 2004: BRAKE DISC. CRACKED. BRAKE ASSEMBLY P/N: 2-1528-6, S/N'S: 0110 AND 1390. BOTH OF THESE BRAKES ARE IN COMPLIANCE WITH MFG SB 2-1528-32-2, REV 5, DATED 3 APR, 2003. BOTH BRAKES WERE U
- [SDR R3R2001201](https://openairdocs.org/sdr/R3R2001201), Dec 1, 2000: SCREW. INCORRECT. THE OUTBOARD ATTACH SCREW IN THE HEATED LEADING EDGE IS TOO LONG AND CAN DAMAGE THE WING SKIN BELOW IT. THE IPC CALLS OUT A MS24694-C48 SCREW IT IS TOO LONG. (X
- [SDR 97ZZZX2000](https://openairdocs.org/sdr/97ZZZX2000), Apr 22, 1997: MOTOR ASSY. INTERMITTENT. REMOVED AND REPLACED ANTI-SKID HYDRAULIC POWER PACK ASSY. AFTER 29.8 HRS OF USAGE, THE MOTOR BECAME INTERMITTENT. SUSPECT A LOOSE CONNECTION WITHIN THE MOTOR AS
- [SDR 97ZZZX1999](https://openairdocs.org/sdr/97ZZZX1999), Apr 22, 1997: MOTOR ASSY. MALFUNCTION. AFTER REPLACING THE ANTI-SKID BRAKE MOTOR ASSY WITH THE GREEN AND BLACK WIRES CONNECTED PROPERLY, THE MOTOR ASSY RUNS IN A COUNTER CLOCKWISE DIRECTION, OPPOSITE

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