# N821SC: 1982 Airbus Industrie A300 B4-203, registration cancelled 2018-02-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 9, 2018 - Status when cancelled: Registration expired, pending cancellation - 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: 211 - Year built: 1982 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 9, 1999 - Certificate issued: September 23, 2008 - Last registry action: April 16, 2012 - Mode S code: AB3625 - Owner when cancelled: [Sky Lease I Inc](https://openairdocs.org/faa-owner/SKY%20LEASE%20I%20INC) - Location: [Greensboro, NC](https://openairdocs.org/faa-place/NC/Greensboro) - Owner type: Corporation - Owner's area on the map: 36.0718° N, 79.9648° W: Placed by OpenAirDocs at the center of ZIP code 27409, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N821SC - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=821SC - Page: https://openairdocs.org/deregistered/N821SC-2018-02-09 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 Airbus Industrie A300 B4-203: https://openairdocs.org/model/airbus-industrie-a300-b4-203.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WRNA201200006](https://openairdocs.org/sdr/WRNA201200006), May 11, 2012: GYRO. UNSERVICEABLE. BOTH NR 1 & NR 2 YAW DAMPERS WOULD NOT ENGAGE. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MX FOUND NR 1 & NR 2 YAW RATE GYRO'S AT FAULT. REMOVED AND REPLACE - [SDR WRNA201110210010](https://openairdocs.org/sdr/WRNA201110210010), Oct 21, 2011: GPS. MALFUNCTIONED. NR 1 GPS MESSAGE "HEADING REQUIRED" RENDERING, GPS AND NR 1 AUTOPILOT INOPERATIVE. VECTORED SO ACFT STAYED ON HEADING MODE. AUTOPILOT NR 2 SELECTED BUT DID NOT - [SDR WRNA2009004](https://openairdocs.org/sdr/WRNA2009004), Dec 30, 2009: PITOT LINE. CLOGGED. ON TAKEOFF ROLL, DEPARTING FROM SJU, CREW NOTICED THAT THERE WAS NO AIRSPEED INDICATION FROM F/O INDICATOR. CAPTAIN INDICATOR SHOWING BETWEEN 75-80 KTS AND FLUC - [SDR WRNA20080009](https://openairdocs.org/sdr/WRNA20080009), Mar 28, 2008: PIN. DISCONNECTED. DURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECONNECTED, OPS CHECKED GOOD. AIRCRAFT RELEAS - [SDR WRNA200700042](https://openairdocs.org/sdr/WRNA200700042), Jun 16, 2007: GIRT BAR. CORRODED. DURING REPLACEMENT OF SLIDE, FOUND L1 DOOR SLIDE GIRT BAR ASSEMBLY CORRODED BEYOND LIMITS. REPLACED GIRT BAR ASSEMBLY IAW MM 25-61-15 PG 401. - [SDR WRNA200700026](https://openairdocs.org/sdr/WRNA200700026), May 24, 2007: TIRE. SEPARATED. NR 6 TIRE RUBBER SEPARATION ON TAKEOFF FROM SJU, FLIGHT CONTINUED TO MIA AND MADE A SAFE LANDING. ON INSPECTION OF AIRCRAFT, FOUND LEFT INBOARD FOREFLAP, AFT FL - [SDR WRNA200700061](https://openairdocs.org/sdr/WRNA200700061), Jan 18, 2007: WARNING MESSAGE. FALSE ACTIVATION. DURING TAKEOFF, RECEIVED A CONFIGURATION DEVIATION WARNING, TAKEOFF ABORTED. UNABLE TO DUPLICATE CONFIGURATION DEVIATION WARNING. PREPARED A/C FOR TEST FLIGHT, - [SDR WRNA200600037](https://openairdocs.org/sdr/WRNA200600037), Oct 16, 2006: CADC. DIRTY. AT START OF TAKEOFF, F/O AIR SPEED INDICATION RAPIDLY WENT TO 90 KNOTS, CAPT MOVED NORMALLY. TAKEOFF WAS ABORTED, RETURNED TO GATE. CLEANED AND RE-RACKED NR 2 C - [SDR WRNA200600025](https://openairdocs.org/sdr/WRNA200600025), Jun 27, 2006: SLIDE. WILL NOT ARM. R1 EVACUATION SLIDE ARMING LEVER DOES NOT ENGAGE EVACUATION SLIDE. LEVER IS STUCK IN DISENGAGED POSITION. PLACED ON MEL 52-61-01-2 CAT-C. LUBRICATED R1 EVACUATI - [SDR WRNA200600027](https://openairdocs.org/sdr/WRNA200600027), Jun 22, 2006: CLAMP. BROKEN. AFTER TAKEOFF NR 2 ENGINE FIRE LIGHT AND BELL CAME ON, REDUCED POWER, LIGHT WENT OUT. RETURNED TO FIELD AND MADE A SAFE LANDING. REPLACED BROKEN CLAMP ON 14TH S - [SDR WRNA200600021](https://openairdocs.org/sdr/WRNA200600021), Jan 28, 2006: RIB. DAMAGED. DURING INSPECTION, DAMAGE WAS FOUND ON RT WING NR 3 SLAT INBOARD END AT RIB 3 LEADING EDGE. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-8-01-06, (AIRBUS TECHNIC - [SDR WRNA200600023](https://openairdocs.org/sdr/WRNA200600023), Jan 24, 2006: DOUBLER. DEBONDED. DURING INSPECTION, TWO DIS-BONDED DOUBLERS WERE FOUND ON LEFT WING OUTBOARD FLAP SKIN UPPER SURFACE ON RIB 4 AND 15 TRAILING EDGE AREA. AFTER DOUBLERS WERE REMO - [SDR WRNA200600024](https://openairdocs.org/sdr/WRNA200600024), Jan 18, 2006: SKIN. CORRODED. DURING INSPECTION, FOUND 3 AREAS OF CORROSION ON FUSELAGE SKIN BETWEEN S26R AND S27R FRAME 58 - 60. REPAIRED PER AVBORNE REPAIR REF 25599-3-01-18-06, (AIRBUS RE - [SDR WRNA200600022](https://openairdocs.org/sdr/WRNA200600022), Jan 18, 2006: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT RIGHT HAND WING SKIN UPPER SURFACE PANEL NR 2 AT THREE FASTENER LOCATION JUST INBOARD OF RIB NR 5, APPROXIMATELY 17 IN - [SDR WRNA200600020](https://openairdocs.org/sdr/WRNA200600020), Jan 18, 2006: BULKHEAD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE FORWARD SIDE OF THE FORWARD PRESSURE BULKHEAD AT -Z180 AND +Y1000. REPAIR WAS ACCOMPLISHED PER AVBORNE REPAIR REF: - [SDR WRNA200600019](https://openairdocs.org/sdr/WRNA200600019), Jan 18, 2006: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN ABOVE THE RT FORWARD PASSENGER DOOR, TWO AREAS, AT S9L BETWEEN FR 14C AND FR 14B AND 1 AREA AT S11L BETW - [SDR WRNA200500025](https://openairdocs.org/sdr/WRNA200500025), Oct 31, 2005: WIRE HARNESS. SPARKS. FLIGHT ENGINEER SEAT HAD SPARKS COMING OUT OF ELECT CONNECTOR ON RIGHT SIDE OF SEAT, THEN C/B POPPED. FOUND WIRES FUSED TOGETHER AT SEAT CANNON PLUG. SEAT DEACT - [SDR WRNA200500022](https://openairdocs.org/sdr/WRNA200500022), Sep 14, 2005: COMPRESSOR. STALLED. NR 1 ENGINE COMPRESSOR STALLED 4 TIMES CLIMBING THROUGH 15,500 FT. AFTER COMPRESSOR STALL, WITH SAME THROTTLE ANGLE, NR 1 ENG N1 WAS 98.4 PERCENT WHILE NR 2 WAS - [SDR WRNA200500023](https://openairdocs.org/sdr/WRNA200500023), Sep 2, 2005: VALVE. UNSERVICEABLE. UNABLE TO LOWER GEAR, LANDING GEAR EXT C/B POPPED, PERFORMED ALTERNATE GEAR EXTENSION. LANDING NORMAL. REMOVED AND REPLACED LANDING GEAR ELECTRO VALVE IAW 32-31 - [SDR WRNA200500020](https://openairdocs.org/sdr/WRNA200500020), Aug 24, 2005: SOLENOID VALVE. LEAKING. WHILE IN FLT, CLIMB, LOSS OF GREEN HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. FOUND GREEN SYSTEM EDP SOLENOID VALVE LEAKING. REMOVED - [SDR WRNA200500017](https://openairdocs.org/sdr/WRNA200500017), Jun 25, 2005: DAMPENER. LEAKING. AIRCRAFT TOOK OFF, MLG WOULD NOT RETRACT. RETURNED TO BASE. LANDING NORMAL. FOUND LT PITCH DAMPNER LEAKING FLUID. REMOVED AND REPLACED PITCH DAMPNER IAW 32-11-0 - [SDR WRNA200400008](https://openairdocs.org/sdr/WRNA200400008), Aug 3, 2004: WARNING LIGHT. ILLUMINATED. AFTER TAKE OFF, GEAR HANDLE UP, LT GEAR DOOR AMBER AND LT GEAR UNLOCK RED LIGHT STAYED ON, ON BOTH FWD AND F/E'S PANEL. AIRPLANE START TO VIBRATE ABOVE 230 KTS. - [SDR WRNA200300009](https://openairdocs.org/sdr/WRNA200300009), Mar 17, 2003: LANDING LIGHT. FAILED. RT LANDING LIGHT INOP, POPS CONTROL CIRCUIT BREAKER R&R LANDING LIGHT ASSY IAW 33-42-11. OPS CK SATISFACTORY - [SDR WRNA200300002](https://openairdocs.org/sdr/WRNA200300002), Jan 31, 2003: DOOR. After Departure bulk cargo door illuminated in flight. A/C returned to field, landing normal, no fuel was dumped.Corrective Action: Cycled aft bulk door I/A/W M - [SDR WRNA200200002](https://openairdocs.org/sdr/WRNA200200002), Jul 25, 2002: FUEL CONTROL. OUT OF ADJUST. DURING CLIMB NR 2 ENGINE BLEED VALVE REG FAULT LIGHT CAME ON. TEMP INCREASE TO 230 DEGREES AND TEMP HI LIGHT CAME ON FOLLOWED BY A/C PACK FAULT LIGHT. UNABLE TO - [SDR 2001F00262](https://openairdocs.org/sdr/2001F00262), Aug 14, 2001: SENSOR. FAILED. AFTER DEPARTING BQN, SLATS WOULD NOT RETRACT, STALL WARNING AND STICK SHAKER ACTIVATED AT 175 KNOTS. DUMPED APPROXIMATELY 38,000 LBS OF FUEL AND RETURNED TO BQN ## Other aircraft with N821SC - [Registered now](https://openairdocs.org/aircraft/N821SC): Gulfstream Aerospace G-V, S/N 5030, built 2003 - [Cancelled 1993-10-06](https://openairdocs.org/deregistered/N821SC-1993-10-06): Piper PA-32-260, S/N 32558. Owner: [Lindy George Howard](https://openairdocs.org/faa-owner/LINDY%20GEORGE%20HOWARD), [Lino Lakes, MN](https://openairdocs.org/faa-place/MN/Lino%20Lakes) --- 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.