# N573ML: 1998 Canadair CL-600-2B19, registration cancelled 2003-04-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 22, 2003
- Exported to: India
- Status when cancelled: Valid registration
- Airframe: [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19) (registry code 1900309)
- Engine: [GE CF34 series](https://openairdocs.org/engine/ge-cf34-series) (registry code 30015)
- Data sheets: [TCDS A21EA-1](https://openairdocs.org/tcds/A21EA-1) (OpenAirDocs)
- Serial number: 7227
- Year built: 1998
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 2, 1998
- Certificate issued: September 12, 2002
- Last registry action: September 12, 2002
- Mode S code: A75AAC
- Owner when cancelled: [State Street Bank And Trust Co Of Ct Na Trustee](https://openairdocs.org/faa-owner/STATE%20STREET%20BANK%20AND%20TRUST%20CO%20OF%20CT%20NA%20TRUSTEE)
- Location: [Hartford, CT](https://openairdocs.org/faa-place/CT/Hartford)
- Owner type: Corporation
- Owner's area on the map: 41.7651° N, 72.6708° W: Placed by OpenAirDocs at the center of ZIP code 06103, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N573ML
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=573ML
- Page: https://openairdocs.org/deregistered/N573ML-2003-04-22

From the FAA registry file of October 28, 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 Canadair CL-600-2B19: https://openairdocs.org/model/canadair-cl-600-2b19.md

## Service difficulty reports (10)

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

- [SDR AEO2002F00000](https://openairdocs.org/sdr/AEO2002F00000), Jan 16, 2002: SHAFT. BROKEN. ENGINE ARRIVED FOR REPAIR OF SEIZED ROTOR CONDITION. UPON DISASSEMBLY FOUND TURBINE ROTORSHAFT SEPARATED AT BASE OF TURBINE ROTOR. THIS IS THE SECOND INSTANCE O
- [SDR JBXA000314](https://openairdocs.org/sdr/JBXA000314), Aug 10, 2001: WARNING SYSTEM. ACTIVATED. ON TRANSFER OF BLEEDS FROM APU TO ENGINE CAUTION MESSAGE, L-PACK HI PRESSURE FOLLOWED. QUICK REFERENCE MANUAL CAUTION STILL PERSISTED AIRCRAFT COMPLETELY DEPRES
- [SDR JBXA000241](https://openairdocs.org/sdr/JBXA000241), Feb 10, 2001: PITOT LINE. CONTAMINATED. INDICATED AIR SPEED ON FIRST OFFICERS SIDE SHOWS 65 KNOTS ABOVE CAPTAINS. STALL FAIL MESSAGE ON TAKEOFF. INSPECTED AIRCRAFT FOR MAINTENANCE FERRY FLIGHT FROM BU
- [SDR JBXA000214](https://openairdocs.org/sdr/JBXA000214), Nov 9, 2000: SMOKE DETECTOR. MALFUNCTIONED. SMOKE CARGO WARNING IN FLIGHT FROM RDU TO DCA. CAPTAIN DECLARED AN EMERGENCY. ACTIVATED FIRE BOTTLE, LANDED AT DCA WITH NO PROBLEM. CARGO COMPARTMENT AND AFT BA
- [SDR JBXA000213](https://openairdocs.org/sdr/JBXA000213), Nov 7, 2000: SMOKE DETECTOR. MALFUNCTIONED. SMOKE CARGO MSG GRD INTERMEDIATE ACTION: MEL NR 2 SMOKE DETECTOR. PERFORMED OPERATIONAL CHECK OF SMOKE DETECTOR IAW CRJ AMM 26-15-00. OPERATIONAL CHECK GOOD AT 
- [SDR JBXA9900133](https://openairdocs.org/sdr/JBXA9900133), Dec 25, 1999: DOOR. OPEN. AIR NOISE COMING FROM FUSELAGE NOSE SECTION, F/O SIDE ON TAKEOFF. CLOSED GROUND POWER CONNECTION DOOR AS REQUIRED, NO DAMAGE FOUND.
- [SDR JBXA9800059](https://openairdocs.org/sdr/JBXA9800059), Dec 1, 1998: ACTUATOR. MALFUNCTIONED. STALL FAIL MESSAGE ON EICAS ON TAKEOFF AFTER GEAR RETRACTION. REMOVED AND REPLACED STICK PUSHER ACTUATOR. OPERATIONAL TEST OF STALL PROTECTION SYSTEM GOOD. WORK
- [SDR JBXA9800058](https://openairdocs.org/sdr/JBXA9800058), Nov 21, 1998: COMPUTER. TRIPPED. STALL FAIL MESSAGE ON EICAS. RESET STALL PROTECTION COMPUTER MEMORY IAW CL-65 MM 27-35-01. OPERATIONAL TEST OF STALL PROTECTION COMPUTER CHECK GOOD, IAW CL-65 M
- [SDR JBXA980048](https://openairdocs.org/sdr/JBXA980048), Aug 30, 1998: PITOT. CONTAMINATED. NO AIRSPEED ON TAKEOFF, TAKEOFF ABORTED AT 80 KNOTS. FOUND BUG STUCK ON PITOT HEAT NR 1 SYSTEM. CLEANED PITOT HEAD CAPTAIN'S SIDE. OPERATION CHECK AIRSPEED INDI
- [SDR JBXA980040](https://openairdocs.org/sdr/JBXA980040), Jun 2, 1998: FCP. INOPERATIVE. AUTOPILOT FAILED TO ENGAGE IN FLIGHT, HAD FCC INDICATIONS, APC FLASHES, NO FLIGHT DIRECTOR INDICATIONS ON CAPT SIDE AND 1/2 BANK CAME ON. LIGHT ON NAV LT SIDE, 

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