# N443LX: 1999 Raytheon 400A, registration cancelled 2024-03-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 14, 2024 - Status when cancelled: Valid registration - Airframe: [Raytheon 400A](https://openairdocs.org/model/raytheon-400a) (registry code 7150010) - Engine: [Pratt & Whitney Canada JT15D 5 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5-series) (registry code 52113) - Data sheets: [TCDS A16SW](https://openairdocs.org/tcds/A16SW) (OpenAirDocs) - Serial number: RK-237 - Year built: 1999 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 29, 1999 - Certificate issued: December 30, 2009 - Last registry action: July 18, 2023 - Mode S code: A556D2 - Owner when cancelled: [Flight Options LLC](https://openairdocs.org/faa-owner/FLIGHT%20OPTIONS%20LLC) - Location: [Richmond Heights, OH](https://openairdocs.org/faa-place/OH/Richmond%20Heights) - Owner type: LLC - Owner's area on the map: 41.5532° N, 81.4743° W: Placed by OpenAirDocs at the center of ZIP code 44143, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N443LX - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=443LX - Page: https://openairdocs.org/deregistered/N443LX-2024-03-14 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 Raytheon 400A: https://openairdocs.org/model/raytheon-400a.md ## Service difficulty reports (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DJFA20120827001](https://openairdocs.org/sdr/DJFA20120827001), Aug 27, 2012: MOUNT. CRACKED. DURING INSPECTION OF NR 1 ENGINE FORWARD MOUNT AFT BRACKET AS CALLED OUT BY AD 2002-01-23, THE MOUNT WAS FOUND CRACKED. MX R & R BRACKET WITH KIT 128-4035, REV - [SDR DJFA20120508002](https://openairdocs.org/sdr/DJFA20120508002), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSPECTION, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT - [SDR DJFA20120508003](https://openairdocs.org/sdr/DJFA20120508003), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX TECH FOUND 8 RIBS CRACKED IN THE HORIZ STAB. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES - [SDR DJFA20120508004](https://openairdocs.org/sdr/DJFA20120508004), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGE - [SDR DJFA20120508005](https://openairdocs.org/sdr/DJFA20120508005), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX TECH FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT - [SDR DJFA20120508006](https://openairdocs.org/sdr/DJFA20120508006), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGE - [SDR DJFA20120508007](https://openairdocs.org/sdr/DJFA20120508007), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX TX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLA - [SDR DJFA20120508008](https://openairdocs.org/sdr/DJFA20120508008), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLAN - [SDR DJFA20120508001](https://openairdocs.org/sdr/DJFA20120508001), May 8, 2012: RIB. CRACKED. DURING SCHDULED INSPECTION, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMEN - [SDR DJFA2011012](https://openairdocs.org/sdr/DJFA2011012), Mar 30, 2011: VALVE. INOPERATIVE. DURING TAXI, AFTER LANDING, CREW NOTED LOSS OF BRAKING ACTION FROM THE PILOTS AND COPILOTS RT BRAKE PEDAL. BRAKING ACTION WAS RETURNED AFTER REPEATED PUMPING OF - [SDR DJFA2011009](https://openairdocs.org/sdr/DJFA2011009), Feb 8, 2011: POWER SUPPLY. FAILED. DURING FLIGHT, CREW REPORTED SMOKE AND FUMES IN THE COCKPIT. ACFT DIVERTED AND, AFTER LANDING, CREW REPORTED SMOKE DISSIPATED WHEN CTR PEDESTAL LIGHTS WERE EXTI - [SDR DJFA2010036](https://openairdocs.org/sdr/DJFA2010036), Nov 27, 2010: POWER SUPPLY. FAILED. ACFT DIVERTED, DUE TO SMOKE SMELL IN COCKPIT. EMERGENCY WAS DECLARED. MX EVALUATED AND CONFIRMED "BURNED ELECTRICAL" ODOR FROM ALTITUDE AWARENESS PANEL. ALSO FO - [SDR DJFA2009031](https://openairdocs.org/sdr/DJFA2009031), Jul 29, 2009: BRAKE ASSY. WEAK. ON LANDING CREW REPORTED INITIAL ATTEMPTS TO BRAKE WERE UNSUCCESSFUL. CREW HAD TO PUMP THE BRAKES IN ORDER TO OBTAIN BRAKING ACTION. MAINTENANCE FOUND THE BRAKE - [SDR DJFA2009015](https://openairdocs.org/sdr/DJFA2009015), Apr 19, 2009: BRAKE SYS. MALFUNCTIONED. ON LANDING, THE FLIGHT CREW REPORTED ABNORMAL PRESSURE REQUIRED TO STOP THE ACFT. SUCH ABNORMAL BRAKING ACTION CAUSED THE RT BRAKE TO GRAB. ACFT FINALLY CAME TO - [SDR DJFA2008012](https://openairdocs.org/sdr/DJFA2008012), Jan 29, 2008: RIB. CRACKED. DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WA --- 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.