# N221CJ: 1996 Beech 1900D, registration cancelled 2010-06-01 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 1, 2010 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162) - Engine: [Pratt & Whitney Canada PT6A-6 series](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-6-series) (registry code 52150) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Serial number: UE-221 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: June 21, 1996 - Certificate issued: May 11, 2010 - Last registry action: May 11, 2010 - Mode S code: A1E4F3 - Owner when cancelled: [General Aviation Services LLC](https://openairdocs.org/faa-owner/GENERAL%20AVIATION%20SERVICES%20LLC) - Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) - Owner type: Corporation - Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N221CJ - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=221CJ - Page: https://openairdocs.org/deregistered/N221CJ-2010-06-01 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 Beech 1900D: https://openairdocs.org/model/beech-1900d.md ## Service difficulty reports (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2010FA0000185](https://openairdocs.org/sdr/2010FA0000185), Feb 2, 2010: TAB. MISMANUFACTURED. RECEIVED NEW AILERON TRIM TAB FROM VENDOR. TAB WAS A NEW PART FROM MFG. INCOMING INSP NOTED THE RIVETS THAT SHOULD HAVE BEEN INSTALLED TO SECURE THE ACTUATOR HO - [SDR 2010F00024](https://openairdocs.org/sdr/2010F00024), Feb 2, 2010: TAB. MISMANUFACTURED. RECEIVED NEW AILERON TRIM TAB FROM VENDOR. TAB WAS A NEW PART FROM THE MFG. INCOMING INSP NOTED THE RIVETS THAT SHOULD HAVE BEEN INSTALLED TO SECURE THE ACTUATO - [SDR NSVA20070198](https://openairdocs.org/sdr/NSVA20070198), Jul 31, 2007: GAS GENERATOR. LEAKING. SMALL AMOUNT OF SMOKE IN THE COCKPIT, ODOR. LANDED SAFELY. FOUND GAS GENERATOR LEAKING OIL INTO COMPRESSOR SECTION (UNDETERMINED INTERNAL LEAK) LT ENGINE, REQUI - [SDR NSVA20070148](https://openairdocs.org/sdr/NSVA20070148), Jun 1, 2007: SPRING. BROKEN. BOTH THROTTLE LEVERS ARE LOOSE. REMOVED LT AND RT POWER LEVERS IAW BEECH 1900D MM 76-10-00, FOUND RT AND LT POWER LEVER ARM ASSY WORN AND GUILD PINS WORN IN POW - [SDR NSVA20070145](https://openairdocs.org/sdr/NSVA20070145), May 30, 2007: WARNING LIGHT. UNKNOWN. NO PUSH TO EXTINGUISH LIGHT DURING AMP TEST ON RIGHT SIDE. REMOVED AND REPLACED RIGHT ENG. FIRE BOTTLE AND SQUIB ASSY. REMOVED AND REPLACED RIGHT FIRE "T" HANDL - [SDR NSVA20070139](https://openairdocs.org/sdr/NSVA20070139), May 24, 2007: SWITCH. OUT OF ADJUST. MAIN CABIN DOOR LIGHT ILLUMINATED ON PUSHBACK. ADJUSTED AIRSTAIR DOOR LATCH PRESSURE LOCK SWITCH IAW BMM 52-70-02. OPERATIONAL CHECK SAT. - [SDR NSVA20070099](https://openairdocs.org/sdr/NSVA20070099), Apr 15, 2007: LATCH. UNSECURE. BOTH EMERGENCY EXIT OUTSIDE HANDLES OPEN. INSPECTED DOORS, BOTH DOORS STILL LATCHED WITH HANDLES PUSHED IN TOO FAR. RESECURED LATCHES ON BOTH DOORS. REF BMM 52- - [SDR NSVA200600141](https://openairdocs.org/sdr/NSVA200600141), Sep 11, 2006: LIMIT SWITCH. MALFUNCTIONED. FLAPS WILL NOT RETRACT BEYOND 17 DEGREES. FOUND INBD UPLIMIT SWITCH IN RT INBD WING STICKING FROM CORROSION. CLEANED, INSPECTED AND LUBED. OPS CK NORMAL. - [SDR NSVA200600135](https://openairdocs.org/sdr/NSVA200600135), Sep 9, 2006: VANE. CONTAMINATED. ON ROTATION AT115KIAS, STALL HORN SOUNDED, AND WOULDN`T TURN OFF UNTIL LNDG GEAR RETRACTED PULLED STALL WARNING CB TO EXTINGUISH WARNING HORN. FOUND BUG/DEBRIS - [SDR NSVA200600130](https://openairdocs.org/sdr/NSVA200600130), Aug 30, 2006: ANTENNA. CORRODED. NR 1 AND NR 2 COMM'S ARE INTERMITTENTLY WORKING. REMOVED AND REPLACED LOWER COMM ANT DUE TO CORROSION PN ON/OFF 90-384036, SN ON 8808, SN OFF 09989. ALSO, REMOV - [SDR 04012006C](https://openairdocs.org/sdr/04012006C), Mar 29, 2006: DRAG BRACE. OUT OF ADJUST. GEAR WARNING HORN GOING OFF AND GEAR INTRANSIT LIGHT ON DURING TAXI, THEN STOPPED. FOUND LT & RT MLG DRAG BRACE CLEARANCE EXCESSIVE, ADJUSTED OPS CHECK GOOD. - [SDR 04012006B](https://openairdocs.org/sdr/04012006B), Mar 26, 2006: WIRE. BROKEN. WHEN BATTERY IS TURNED ON LANDING GEAR WARNING HORN COMES ON. FOUND BROKEN WIRE IN RIGHT DOWNLOCK SWITCH HARNESS. REPAIRED BROKEN WIRE. - [SDR 09212005B](https://openairdocs.org/sdr/09212005B), Sep 19, 2005: HANDLE. OUT OF RIG. LEFT EMERGENCY EXIT EXTERIOR HANDLE NOT FLUSHED. RIGGED DOOR HANDLE. - [SDR 09092005A](https://openairdocs.org/sdr/09092005A), Sep 7, 2005: DRAIN LINE. LEAKING. FUEL LEAKING FROM LT WHEEL WELL. REMOVED AND REPLACED DRAIN TUBE ASSY. FUEL LINE, OPS CHECK GOOD. - [SDR 09082005E](https://openairdocs.org/sdr/09082005E), Sep 5, 2005: GOVERNOR. FAILED. LT ENGINE FAILED AUTO FEATHER. REMOVED AND REPLACED LT OVERSPEED GOVERNOR. OPS CHECKED GOOD. - [SDR 09022005C](https://openairdocs.org/sdr/09022005C), Sep 1, 2005: ENGINE. OVERTEMP. NR 1 ENG OIL OVERTEMP AT 130 DEGREES, AND PSI AT OR BELOW 60. SHUT DOWN ENG IN-FLIGHT AT 7000'. ENGINE CHANGE IN PROGRESS. - [SDR 08082005I](https://openairdocs.org/sdr/08082005I), Aug 9, 2005: ELEVATOR. LOOSE. RT ELEVATOR, OUTBOARD HINGE HAS LOOSE RIVET ON BOTTOM SIDE OF ELEVATOR. - [SDR 08082005H](https://openairdocs.org/sdr/08082005H), Aug 9, 2005: ELEVATOR. LOOSE. LT ELEVATOR, OUTBOARD HINGE HAS LOOSE RIVET ON BOTTOM SIDE OF ELEVATOR. - [SDR 07152005A](https://openairdocs.org/sdr/07152005A), Jul 15, 2005: WARNING LIGHT. ILLUMINATED. CARGO DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. - [SDR 328031](https://openairdocs.org/sdr/328031), Nov 23, 2003: WHEEL. LOCKED. AIR RETURN DUE TO MANUAL RUDDER TRIM WHEEL LOCKING UP IN CENTER POSITION, PILOTS RUDDER PEDALS RESPONDED NORMAL. - [SDR NSVA0210](https://openairdocs.org/sdr/NSVA0210), Apr 25, 2002: WHEEL. SEPARATED. AIR DISPATCH RECEIVED A REPORT THAT AIRCRAFT HAD LOST THE NR 4 MAIN WHEEL ASSEMBLY DURING TAKEOFF. CREW CONTINUED TO IAD WHERE THE TOWER CONFIRMED THAT A WHEEL - [SDR NSVA0121](https://openairdocs.org/sdr/NSVA0121), Oct 14, 2001: GYRO. FAILED. ON A REPOSITION FLIGHT FROM HEF TO HYA, THE CREW ENCOUNTERED ERRONEOUS HEADING INFORMATION WITH A SUBSEQUENT HEADING COMPARATOR ANNUNCIATOR. BECAUSE OF IMC COND - [SDR NSVA0117](https://openairdocs.org/sdr/NSVA0117), Sep 20, 2001: ENGINE. MALFUNCTIONED. LGA - DURING TAXI BACK TO GATE AFTER LANDING. PILOT WAS NOTIFIED VIA RAMP CONTROL THAT ANOTHER AIRCRAFT APPARENTLY SAW SPARKS AND FLAMES COMING FROM THE NR 2 EN ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20070731015299I](https://openairdocs.org/incident/20070731015299I), Jul 31, 2007: Beech 1900D (N221CJ), Portland, ME, No damage. (-23) This inspector observed colgan flight 4934, N221CJ land in Portland, Maine, accompanied by crash fire rescue. Upon further investigation it was revealed… ## Other aircraft with N221CJ - [Cancelled 2024-02-26](https://openairdocs.org/deregistered/N221CJ-2024-02-26): Sikorsky S-76C, S/N 760659. Exported to Israel. Owner: [Nickravesh Niknam](https://openairdocs.org/faa-owner/NICKRAVESH%20NIKNAM), [San Jose, CA](https://openairdocs.org/faa-place/CA/San%20Jose) --- 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.