N821SC, cancelled Feb 9, 2018
Service difficulty reports · 26
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WRNA201200006Gyro · unserviceableBOTH 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 WRNA201110210010Gps · malfunctionedNR 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 WSDR WRNA2009004Pitot Line · cloggedON 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 WITHSDR WRNA20080009Pin · disconnectedDURING 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 WRNA200700042Girt Bar · corrodedDURING 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 WRNA200700026Tire · separatedNR 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 WRNA200700061Warning Message · false activationDURING 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 WRNA200600037Cadc · dirtyAT 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 WRNA200600025Slide · will not armR1 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 RELEASESDR WRNA200600027Clamp · brokenAFTER 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 WRNA200600021Rib · damagedDURING 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 INSTALLEDSDR WRNA200600023Doubler · debondedDURING 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 TECHNICALSDR WRNA200600024Skin · corrodedDURING 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 WRNA200600022Skin · corrodedDURING 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 ASDR WRNA200600020Bulkhead · corrodedDURING 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 ARSDR WRNA200600019Skin · corrodedDURING 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 RESDR WRNA200500025Wire Harness · sparksFLIGHT 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 WRNA200500022Compressor · stalledNR 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 WASDR WRNA200500023Valve · unserviceableUNABLE 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 WRNA200500020Solenoid Valve · leakingWHILE 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. ISDR WRNA200500017Dampener · leakingAIRCRAFT 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 WRNA200400008Warning Light · illuminatedAFTER 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 WRNA200300009Landing Light · failedRT LANDING LIGHT INOP, POPS CONTROL CIRCUIT BREAKER R&R LANDING LIGHT ASSY IAW 33-42-11. OPS CK SATISFACTORYSDR WRNA200300002DoorAfter 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. AircraftSDR WRNA200200002Fuel Control · out of adjustDURING 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 2001F00262Sensor · failedAFTER 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
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