# Service difficulty reports: N821SC, cancelled Feb 9, 2018

A list on [N821SC, cancelled Feb 9, 2018](https://openairdocs.org/deregistered/N821SC-2018-02-09.md).

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

- [SDR WRNA201200006](https://openairdocs.org/sdr/WRNA201200006.md): Gyro · unserviceable · May 11, 2012 · N821SC · Airbus A300B4203 · Speed-Attitude Correction System
  > 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 REPLACED NR 1 & NR 2 YAW RATE GYROS IAW 22-21-45. OP'S CHECK SATISFACTORY. A/C RETURNED TO SERVICE.
- [SDR WRNA201110210010](https://openairdocs.org/sdr/WRNA201110210010.md): Gps · malfunctioned · Oct 21, 2011 · N821SC · Airbus A300B4203 · Global Positioning System
  > 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 ENGAGE. NOT SUCCESSFUL AFTER SEVERAL ATTEMPTS. RETURN TO AIRPORT. LANDED NORMAL. MX CHECKED W
- [SDR WRNA2009004](https://openairdocs.org/sdr/WRNA2009004.md): Pitot Line · clogged · Dec 30, 2009 · N821SC · Airbus A300B4203 · Pitot/Static System
  > 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 FLUCTUATING. ABORTED T/O PROCEDURES FOLLOWED. RETURNED TO GATE. MAINT FOUND PITOT LINES CLOGGED WITH
- [SDR WRNA20080009](https://openairdocs.org/sdr/WRNA20080009.md): Pin · disconnected · Mar 28, 2008 · N821SC · Airbus A300B4203 · Light System Wiring
  > DURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECONNECTED, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200700042](https://openairdocs.org/sdr/WRNA200700042.md): Girt Bar · corroded · Jun 16, 2007 · N821SC · Airbus A300B4203 · Emergency Equipment
  > 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.md): Tire · separated · May 24, 2007 · N821SC · Airbus A300B4203 · Tire
  > 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 FLAP AND CENTER HINGE FAIRINGS DAMAGED. REPLACED TIRE AND WHEEL ASSY, FLAP ASSY AND FLAP TAB ASSY.
- [SDR WRNA200700061](https://openairdocs.org/sdr/WRNA200700061.md): Warning Message · false activation · Jan 18, 2007 · N821SC · Airbus A300B4203 · Central Warning
  > DURING TAKEOFF, RECEIVED A CONFIGURATION DEVIATION WARNING, TAKEOFF ABORTED. UNABLE TO DUPLICATE CONFIGURATION DEVIATION WARNING. PREPARED A/C FOR TEST FLIGHT, TEST FLIGHT COMPLETED SATISFACTORY 11-26-07. AIRCRAFT RELEASED FOR SERVICE.
- [SDR WRNA200600037](https://openairdocs.org/sdr/WRNA200600037.md): Cadc · dirty · Oct 16, 2006 · N821SC · Airbus A300B4203 · Airspeed/Mach Indicator
  > 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 CADC. OPS CHECKED OK IAW AMM 34-12-34, AIRCRAFT RETURNED TO SERVICE.
- [SDR WRNA200600025](https://openairdocs.org/sdr/WRNA200600025.md): Slide · will not arm · Jun 27, 2006 · N821SC · Airbus A300B4203 · Escape Slide
  > 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 EVACUATION SLICE ARMING LEVER MECHANISM. OPS CHECKED OK IAW A300 AMM 52-22-22. CLEARED MEL AND RELEASE
- [SDR WRNA200600027](https://openairdocs.org/sdr/WRNA200600027.md): Clamp · broken · Jun 22, 2006 · N821SC · Airbus A300B4203 · Pneumatic Distribution System
  > 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 STAGE BLEED MANIFOLD IAW 36-00-00 PAGE 425, LEAK CHECKED OK IAW AMM 71-00-00 PAGE 501. OPS CHECK,
- [SDR WRNA200600021](https://openairdocs.org/sdr/WRNA200600021.md): Rib · damaged · Jan 28, 2006 · N821SC · Airbus A300B4203 · Leading Edge Devices
  > 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 TECHNICAL DISPOSITION #FOK/036/2006) CUT OUT DAMAGED AREA, MODIFIED NOSE RIB 3, MANUFACTURED AND INSTALLED
- [SDR WRNA200600023](https://openairdocs.org/sdr/WRNA200600023.md): Doubler · debonded · Jan 24, 2006 · N821SC · Airbus A300B4203 · Trailing Edge Flaps
  > 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 REMOVED, CORROSION WAS FOUND. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-9-01-24-06 (AIRBUS TECHNICAL
- [SDR WRNA200600024](https://openairdocs.org/sdr/WRNA200600024.md): Skin · corroded · Jan 18, 2006 · N821SC · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > 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 REPAIR DESIGN APPROVAL SHEET RAS/DAHM/40204/2006) REMOVE FASTENERS, SMOOTH BLEND CORROSION, HFEC AND
- [SDR WRNA200600022](https://openairdocs.org/sdr/WRNA200600022.md): Skin · corroded · Jan 18, 2006 · N821SC · Airbus A300B4203 · Wing, Plate/Skin
  > 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 INCHES AFT OF REAR SPAR. REPAIRED PER AVBORNE REPAIR REFERENCE 25599-6-10-18-06. REMOVED FASTENERS A
- [SDR WRNA200600020](https://openairdocs.org/sdr/WRNA200600020.md): Bulkhead · corroded · Jan 18, 2006 · N821SC · Airbus A300B4203 · Fuselage Main, Bulkhead
  > 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: 25599-10-01-25-06, (AIRBUS TECHNICAL DISPOSITION 942.042586/004/2006) SMOOTH REWORK OF CORRODED AR
- [SDR WRNA200600019](https://openairdocs.org/sdr/WRNA200600019.md): Skin · corroded · Jan 18, 2006 · N821SC · Airbus A300B4203 · Fuselage Main, Plate/Skin
  > 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 BETWEEN FR13 AND FR13A. ACCOMPLISHED REPAIR PER AVBORNE REPAIR REFERENCE 25599-7-02-02-2006, (AIRBUS RE
- [SDR WRNA200500025](https://openairdocs.org/sdr/WRNA200500025.md): Wire Harness · sparks · Oct 31, 2005 · N821SC · Airbus A300B4203 · Equipment/Furnishings Wiring
  > 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 DEACTIVATED AND PLACED ON MEL 25-11-01.
- [SDR WRNA200500022](https://openairdocs.org/sdr/WRNA200500022.md): Compressor · stalled · Sep 14, 2005 · N821SC · Airbus A300B4203 · Turbine Engine Compressor Section
  > 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 104 PERCENT. ALL OTHER PRIMARY ENGINE PARAMETERS WERE FLUCTUATING. WHEN THE NR 1 THRUST LEVER WA
- [SDR WRNA200500023](https://openairdocs.org/sdr/WRNA200500023.md): Valve · unserviceable · Sep 2, 2005 · N821SC · Airbus A300B4203 · Landing Gear Retraction/Extension System
  > UNABLE TO LOWER GEAR, LANDING GEAR EXT C/B POPPED, PERFORMED ALTERNATE GEAR EXTENSION. LANDING NORMAL. REMOVED AND REPLACED LANDING GEAR ELECTRO VALVE IAW 32-31-12. OP'S CHECK AND LEAK CHECK SATISFACTORY IAW 32-30-00. AIRCRAFT RETURNED TO SERVICE.
- [SDR WRNA200500020](https://openairdocs.org/sdr/WRNA200500020.md): Solenoid Valve · leaking · Aug 24, 2005 · N821SC · Airbus A300B4203 · Hydraulic System, Main
  > WHILE IN FLT, CLIMB, LOSS OF GREEN HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED TO AIRFIELD, LANDING NORMAL. FOUND GREEN SYSTEM EDP SOLENOID VALVE LEAKING. REMOVED AND REPLACED EDP SOLENOID, OP'S CHECK SATISFACTORY IAW 29-11-32. AIRCRAFT LANDED OVERWEIGHT. I
- [SDR WRNA200500017](https://openairdocs.org/sdr/WRNA200500017.md): Dampener · leaking · Jun 25, 2005 · N821SC · Airbus A300B4203 · Main Landing Gear Strut/Axle/Truck
  > AIRCRAFT TOOK OFF, MLG WOULD NOT RETRACT. RETURNED TO BASE. LANDING NORMAL. FOUND LT PITCH DAMPNER LEAKING FLUID. REMOVED AND REPLACED PITCH DAMPNER IAW 32-11-05. FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE.
- [SDR WRNA200400008](https://openairdocs.org/sdr/WRNA200400008.md): Warning Light · illuminated · Aug 3, 2004 · N821SC · Airbus A300B4203 · Landing Gear Position and Warning
  > 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. FUEL JETTISON PROCEDURE WAS ACCOMPLISHED TO MAX. LANDING WEIGHT. AIRCRAFT LANDED NORMAL.
- [SDR WRNA200300009](https://openairdocs.org/sdr/WRNA200300009.md): Landing Light · failed · Mar 17, 2003 · N821SC · Airbus A300B4203 · Exterior Lighting
  > 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.md): Door · Jan 31, 2003 · N821SC · Airbus A300B4203 · Cargo/Baggage Doors
  > 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 MM 52-34-00. Door indication op's checked normal. Door was verified to be closed and locked. Aircraft
- [SDR WRNA200200002](https://openairdocs.org/sdr/WRNA200200002.md): Fuel Control · out of adjust · Jul 25, 2002 · N821SC · Airbus A300B4203 · Fuel Control/Turbine Engines
  > 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 CONTROL PRESSURIZATION DUE TO NR 1 BLEED VALVE CURRENTLY ON MEL (LOCKED OUT) NR 2 HP BLEED FAULT
- [SDR 2001F00262](https://openairdocs.org/sdr/2001F00262.md): Sensor · failed · Aug 14, 2001 · N821SC · Airbus A300B4203 · Stall Warning System
  > 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. AIRCRAFT LANDED NORMAL. CHECKED AND FOUND CODE 71 AND NR 1 PITCH TRIM AND NR 1 AOA SENSOR FAILE

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N821SC' AND deregistration_id = 'N821SC-2018-02-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N821SC-2018-02-09/reports

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