# N473AS: 1983 Airbus Industrie A300 B4-203, registration cancelled 2008-03-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 18, 2008 - Exported to: United Arab Emirates - Status when cancelled: Triennial form not returned - Airframe: [Airbus Industrie A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (registry code 3930306) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 203 - Year built: 1983 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 13, 2000 - Certificate issued: October 20, 2000 - Last registry action: October 17, 2006 - Mode S code: A5CC50 - Owner when cancelled: [Dmcmag III LLC](https://openairdocs.org/faa-owner/DMCMAG%20III%20LLC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N473AS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=473AS - Page: https://openairdocs.org/deregistered/N473AS-2008-03-18 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 Airbus Industrie A300 B4-203: https://openairdocs.org/model/airbus-industrie-a300-b4-203.md ## Service difficulty reports (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR XN0A1358](https://openairdocs.org/sdr/XN0A1358), Dec 2, 2006: HOSE. FAILED. UPON LANDING, LOST GREEN HYDRAULIC SYSTEM QUANTITY AND PRESSURE. LEVEL LOW AND PRESSURE LOW LIGHTS ON. FOUND LEFT GEAR SIDE BRACE LOCK ACTUATOR AFT HOSE FAILED. - [SDR XN0A1347](https://openairdocs.org/sdr/XN0A1347), Aug 2, 2006: ENGINE. UNKNOWN. FLIGHT LEVEL 290 MACH .75 COULD NOT MAINTAIN SPEED OR FLIGHT LEVEL, ENGINE AI WAS ON. AC SHOULD BE ABLE TO MAINTAIN MACH .78 WITH N1 OF 98.4 FLIGHT LEVEL 280 M7 - [SDR XN0A1345](https://openairdocs.org/sdr/XN0A1345), Aug 1, 2006: LINE. LOOSE. NR 2 BLEED REGULATOR FAULT 90 DEGREE CELSIUS, 0 PSI, COULD NOT PRESSURIZE. NR 1 BLEED OVER TEMP, COULD NOT PRESSURIZE, USED APU FOR PRESSURIZATION, LIMIT 15000 - [SDR XN0A1346](https://openairdocs.org/sdr/XN0A1346), Aug 1, 2006: LINE. LEAKING. ON GEAR DOWN LOST ALL GREEN HYDRAULIC FLUID AND NOSE WHEEL STEERING. REPLACED FAILED HYDRAULIC LINE AT LT MLG STRUT IAW A300 AMM CHAPTER 20-23-11, SERVICED HYDR - [SDR XN0A1339](https://openairdocs.org/sdr/XN0A1339), Jun 12, 2006: CONTROL BOX. FAULTY. DURING TAXI ALL ANTI SKID RELEASE LIGHTS ON WITH ANTI SKID SWITCH IN NORM OR ALT POSITION. REMOVED AND REPLACED ANTI SKID CONTROL BOX IAW A300 AMM CHAPTER 32-42 - [SDR XN0A1324](https://openairdocs.org/sdr/XN0A1324), Apr 30, 2006: WARNING LIGHT. ILLUMINATED. DURING CLIMBOUT NR 1 BLEED LIGHT ON, NO PRESSURIZATION ACCOMPANIED BY REGULATOR FAULT LIGHT. NR 2 BLEED HIGH TEMP LIGHT ACCOMPANIED BY BLEED FAULT LIGHT. REMOVE - [SDR XN0A1318](https://openairdocs.org/sdr/XN0A1318), Apr 18, 2006: BLEED VALVE. MALFUNCTIONED. ENGINE NR 2 BLEED AIR TEMP HI LIGHT ILLUMINATED AFTER TAKEOFF. REGUL FAULT LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED FAN AIR VALVE IAW A300 AMM CHAPTER 36-11 - [SDR XN0A1317](https://openairdocs.org/sdr/XN0A1317), Apr 14, 2006: CONTROL BOX. MALFUNCTIONED. ON TAXI OUT BRAKE CHECK RT BRAKES WERE GRABBING IN BOTH NORMAL AND ALTERNATE BRAKE SYSTEMS. REMOVED AND REPLACED BRAKE SYSTEM CONTROL BOX IAW A300 AMM CHAPTER 3 - [SDR XN0A1305](https://openairdocs.org/sdr/XN0A1305), Feb 23, 2006: SWITCH. CONTAMINATED. JAM LIGHT ILLUMINATED FOR BLUE SERVO CONTROLS. TRANSFERRED TO DMI 6202 IAW MEL 27-82-01 CAT C PLACARD INSTALLED. INSPECTED RUDDER SERVOS FOUND ALL TO BE WORKING - [SDR XN0A1281](https://openairdocs.org/sdr/XN0A1281), Dec 7, 2005: UNKNOWN. VIBRATION. ON TAKEOFF ROLL AT APPROXIMATELY 135K - SEVERE VIBRATION FELT AND SUSPECT BLOWN TIRE, NORMAL LANDING ACCOMPLISHED. ON POST-FLIGHT INSPECTION FOUND NR 8 TIRE BLO - [SDR XN0A1280](https://openairdocs.org/sdr/XN0A1280), Dec 6, 2005: EXCITER. FAULTY. NO LIGHT UP ON NR1 ENGINE ON (B) IGNITION. FOR T/S TRIED (A) IGNITION BUT NO LIGHT-UP. ABNORMAL PROCEDURES CARRIED OUT IAW QUICK REFERENCE HANDBOOK. REPAIRED (B - [SDR XN0A1279](https://openairdocs.org/sdr/XN0A1279), Dec 2, 2005: CONTROL UNIT. FAILED. NR 2 YAW DAMPER WILL NOT ENGAGE. TRANSFERRED TO DMI LOG 5951 IAW ENA MEL REFERENCE 22-21-01 CAT-A. REMOVED AND REPLACED YAW DAMPER ENGAGE UNIT, OPS CHECK OK IAW - [SDR XN0A1275](https://openairdocs.org/sdr/XN0A1275), Nov 11, 2005: BRAKE. MALFUNCTIONED. GREEN BRAKE INOP ON TAXI. YELLOW SYS PRESSURE SHOW ON BRAKE GAGE. INSPECTED BRAKES THROUGH 8, FOUND NO DEFECTS, PERFORMED OPERATIONAL CHECK OF GREEN AND YELLOW - [SDR XN0A1256](https://openairdocs.org/sdr/XN0A1256), Aug 15, 2005: ACCESS PANEL. INFLT SEPARATION. LEFT ACCESS PANEL (AC) DEPARTED AIRCRAFT ON T/O. ATC REPORTED SEEING PANEL FULL, TURNED BACK. PERFORMED L INSPECTION OF WHEEL WELL AREA, LOWER SURFACE WINES, FU - [SDR XN0A1228](https://openairdocs.org/sdr/XN0A1228), Feb 11, 2005: COUPLER. DEFECTIVE. NR 1 COMPASS FLUCTUATING + - 20 DEGREES. REPLACED NR 1 COMPASS COUPLER, OP'S GOOD IAW A300MM 34-21-34. - [SDR XNOA1217](https://openairdocs.org/sdr/XNOA1217), Dec 19, 2004: CONNECTOR. DAMAGED. CAPT'S DG FAILED IN FLIGHT. REMOVED, CONNECTOR & REINSTALLED NR 1 DG OPS, CHECKED GOOD. SWAPPED NR 1 DG & NR 3 DG PENDING FURTHER TROUBLESHOOTING, OPS CHECKED N - [SDR XNOA1181](https://openairdocs.org/sdr/XNOA1181), Mar 31, 2004: GENERATOR. INOPERATIVE. AT PUSHBACK IN SCK NR 2 GEN NO VOLT'S AND FREQ'S. SHUT DOWN ENG AND RETURNED TO THE GATE. R&R NR 2 GENERATOR CONTROL UNIT IAW A300 AMM 24-21-12 OPS CHECK GOOD. - [SDR XNOA1176](https://openairdocs.org/sdr/XNOA1176), Feb 4, 2004: DAMPER. FAILED. BTB DUE BOTH YAW DAMPERS FAILED DURING TAXI OUT. PART INSTALLED FOR YAW DAMPER AUTO STAB CONT. REPLACED WITH ORIGINAL UNIT. TRANSFERRED TO DMI 4053, ORIGINAL DM - [SDR XNOA01153](https://openairdocs.org/sdr/XNOA01153), Sep 6, 2003: CONTROL CABLE. LACK OF LUBE. FLIGHT CONTROLS LOCKED TO LEFT ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KTS. INSPECTED AIL CABLES AND TENSION REG. LUBED TENSION REG. OPS CHECK NORMAL IAW A300 MM - [SDR XNOA01146](https://openairdocs.org/sdr/XNOA01146), Aug 20, 2003: RADIO. INOPERATIVE. NR 1 VHF RADIO WILL NOT TRANSMIT OR RECEIVE. NR 2 VHF WILL ONLY TRANSMIT ON 121.9. DISCONNECTED AND RECONNECTED THE CAPTAINS FREQUENCY SELECT PANEL AND AUDIO SE - [SDR XNOA01137](https://openairdocs.org/sdr/XNOA01137), Jul 1, 2003: B-NUT. LOOSE. LOST GREEN HYD FLUID AND PRESSURE. MOTOR DUMPED FUEL TO MAX LANDING AND RETURNED TO SJU. ACTION TAKEN: TIGHTENED LOOSE AND LEAKING B-NUT ON LEFT MLG DRAG BRACE - [SDR XNOA01135](https://openairdocs.org/sdr/XNOA01135), Jun 24, 2003: TIRE. FAILED. AFTER T/O TOWER SAID LT MLG TRAILING SMOKE-NO ABNORMAL INDS ON BRAKE TEMP GUAGES. THEN TWR ADVISED THEY FOUND TIRE DEBRIS ON RWY-HAD NOT RETRACTED GEAR AS PRECA - [SDR XNOA01110](https://openairdocs.org/sdr/XNOA01110), Mar 26, 2003: ENGINE. MALFUNCTIONED. ENGINE 1 N1 114 EGT 410 DEGREE C N2 47 PERCENT FF 2300. ACTED LIKE A HUNG START AT 50 SEC. WE REJECTED TAKE OFF. PERFORMED ENG RUN. ALL PARAMETERS NORMAL IAW A3 - [SDR XNOA01102](https://openairdocs.org/sdr/XNOA01102), Jan 31, 2003: ENGINE. MALFUNCTIONED. ON TAKEOFF, POWER APPLICATION NR 2 ENG N2 INDICATED LOW. TAKEOFF REJECTED (NO HIGH ENERGY STOP). AS PER MAINTENANCE CONTROL INLET & EXHAUST INSPECTED. NO DEFECT - [SDR XNOA01099](https://openairdocs.org/sdr/XNOA01099), Jan 7, 2003: LANDING GEAR. MALFUNCTIONED. DURING FINAL APPROACH TO DAY MLG WOULD NOT EXTEND. MANUAL EXTENSION PROCEDURE WAS USED. REMOVED & REPLACED ELECTRO VALVE IAW A300 MM 32-31-12. PERFORMED INSPECT - [SDR XNOA01086](https://openairdocs.org/sdr/XNOA01086), Nov 8, 2002: PROXIMITY SENSOR. MALFUNCTIONED. UNABLE TO RETRACT LANDING GEAR WITH EITHER SYSTEM. REMOVED & REPLACED RT MLG BOAGIE TRIM PROXIMITY SENSORS 8GA IAW A300 MM 32-00-00. REMOVED & REPLACED LANDING - [SDR XNOA01081](https://openairdocs.org/sdr/XNOA01081), Oct 15, 2002: LINE. CLOGGED. NO AIRSPEED ON FO'S AIRSPEED INDICATOR ON TAKEOFF. ABORTED AT 90 KTS. ACTION TAKEN: FLUSHED NR 2 AIR DATA COMP. LINE. OPS CHECK GOOD IAW A300 MM 34-11-10. - [SDR XNOA01067](https://openairdocs.org/sdr/XNOA01067), Sep 4, 2002: HYDRAULIC SYSTEM. DIRTY. NR 1 EDP INOP (GREEN SYSTEM). CLEANED AND RESECURED CONNECTION AT BYPASS. SOL SYS CHECKED GOOD PER A300 MM 29-11-32. - [SDR XNOA01037](https://openairdocs.org/sdr/XNOA01037), Feb 9, 2002: DAMPER. LOW. THREE TRIES TO GET GEAR RETRACTED OUT OF DENVER. INSPECTED LANDING GEAR. FOUND PITCH DAMPERS NITROGEN CHARGE LOW ALL 4. SERVICED PITCH DAMPERS IAW A300 MM 12-12 - [SDR XNOA01034](https://openairdocs.org/sdr/XNOA01034), Feb 8, 2002: SWITCH. LOOSE. ON TAKEOFF GEAR WOULD NOT RETRACT. PERFORMED CHECK LIST. WOULD NOT RETRACT. OVERWEIGHT LANDING NOT FACTOR. CLEANED AND RESECURED NOSE GEAR CENTERING SWITCH. C/P - [SDR XN0A01030](https://openairdocs.org/sdr/XN0A01030), Nov 22, 2001: PITOT TUBE. OBSTRUCTED. ABORTED TAKEOFF DUE TO CPT AIRSPEED IND FAILURE. REMOVED DEBRIS FROM PILOT TUBE, FUNCTIONALLY. OPS CHECK GOOD IAW A300 MM 34-11-40. - [SDR XN0A01029](https://openairdocs.org/sdr/XN0A01029), Nov 6, 2001: MODULE. MALFUNCTIONED. AFTER TAKEOFF AT GEAR RETRACT, GEAR HANDLE WOULD NOT GO PAST NEUTRAL. PERFORMED QRH L/G LEVER INTERLOCKED CHECK LIST. TRIED SYS 2 AND SAME AS SYS 1, GEAR HANDLE - [SDR XN0A01028](https://openairdocs.org/sdr/XN0A01028), Oct 25, 2001: MODULE. FAILED. LANDING GEAR FAILED TO SELECT UP SYS 1 OR 2. LANDING PERFORMED AT 300 FT PER MINUTE. FOUND FAILED PROXIMITY MODULE UNIT. REMOVED AND REPLACED PROXIMITY DETECTOR - [SDR XNA01015](https://openairdocs.org/sdr/XNA01015), Jul 28, 2001: JACKSCREW. LACK OF LUBE. DURING TAXI, NO SLATS INDICATION ON THE FCPI. SERVICED SLAT JACKSCREW AT LEFT WING ROOT. OPS CHECK GOOD IAW A300 MM 27-80. - [SDR XNA01013](https://openairdocs.org/sdr/XNA01013), Jul 17, 2001: WARNING LIGHT. ILLUMINATED. CLIMBING THRU 13,000 FEET HEARD LOUD BANGING NOISE FROM CARGO SECTION FOLLOWED BY FLAPPING NOISE COMING FROM AIR CONDITIONING DUCTS. DOORS LIGHT CAME ON, ON MAS - [SDR XNA01011A](https://openairdocs.org/sdr/XNA01011A), Jun 8, 2001: INDICATOR. FAULTY. DURING CONTROL CHECK, LT&RT AIL INDICATORS SHOWED LESS THAN FULL THROW. MEASURED LT & RT LS & AS AILERONS FOR PROPER DEFLECTION UP AND DOWN. CHECKED NORMAL IAW - [SDR XNA01008](https://openairdocs.org/sdr/XNA01008), May 5, 2001: INDICATOR. INOPERATIVE. TAKEOFF ABORTED. NO AIRSPEED INDICATION ON CAPTAIN A/S INDICATOR. REMOVED AND REPLACED MACH/AIRSPEED INDICATOR. PERFORMED PITOT OPS AND LEAK CHECK. OPS AND LEAK - [SDR XNA01007](https://openairdocs.org/sdr/XNA01007), Apr 11, 2001: PITOT LINE. OBSTRUCTED. ABORTED T/O AT 120 KTS. CAPTS AIRSPEED HAD NO INDICATION AT 70 KTS AND INDICATED APPROX 90 TO 100 KTS W/FO''S STBY AIRSPEED AT 120 KTS. AFTER ABORT W/FO''S INDI ## Other aircraft with N473AS - [Registered now](https://openairdocs.org/aircraft/N473AS): Simpson Arthur MONNETT SONERAI IILT, S/N 080706-0831, built 2025 - [Cancelled 2012-04-26](https://openairdocs.org/deregistered/N473AS-2012-04-26): Boeing 747-400, S/N 24777. Owner: [Aersale Inc](https://openairdocs.org/faa-owner/AERSALE%20INC), [Coral Gables, FL](https://openairdocs.org/faa-place/FL/Coral%20Gables) --- 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.