N562SW, cancelled Jul 8, 2016
Service difficulty reports · 101
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 = 'N562SW' AND deregistration_id = 'N562SW-2016-07-08' 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 = 'N562SW' AND deregistration_id = 'N562SW-2016-07-08' 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 SWIA200718093Computer · malfunctionedAUTOPILOT PITCHES AIRCRAFT UP AND DOWN. REPLACED NR 1 AUTOPILOT COMPUTER IAW MM 22-00-00, P/N - 622-8315-102 S/N OFF - 1303.SDR SWIA200718089Computer · malfunctionedWITH AUTOPILOT ENGAGED, AIRCRAFT PITCHED NOSE UP THEN NOSE DOWN. REPLACED NR 2 AUTOPILOT COMPUTER.SDR SWIA200617246Cap · looseCLIMBING OUT OF DEN STARTED LOSING OIL PRESSURE ON LEFT ENGINE AND RECEIVED OIL PRESSURE WARNINGS. IMMEDIATELY SHUT DOWN NR 1 ENGINE AND RETURNED TO FIELD. SERVICED ENGINE WITH OIL TO PROPER LIMITS AND REINSTALLED OIL CAP PROPERLY.SDR SWIA200617195Rib · crackedRIGHT INBOARD LEADING EDGE RIB IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT INBOARD LEADING EDGE RIB IAW EMB 120 SRM 51-40-02.SDR SWIA200617194Door Frame · crackedCRACK ON PAX DOOR AFT CENTER FRAME. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000, PN OFF: 120-21059-001.SDR SWIA200617193Door Frame · crackedCRACK ON PAX DOOR FORWARD CENTER FRAME, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR FORWARD CENTER FRAME SECURED IAW EMB 120 SRM 51-40-02, PN OFF: 120-21058-003.SDR SWIA200617192Rail · corrodedPAX DOOR AFT STEP RAIL CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FWD STEP RAIL INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000.SDR SWIA200617191Rail · corrodedPAX DOOR FORWARD STEP RAIL CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FORWARD STEP RAIL INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND IAW RII CARD 52-800-1000.SDR SWIA200617190Frame · corrodedPAX DOOR BOTTOM END STEP FRAME CORRODED, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII CARD 52-800-1000.SDR SWIA200617189Frame · crackedPAX DOOR BOTTOM STEP FORWARD SIDE FRAME CRACKED, DISCOVERED DURING C-CHECK INSPECTION. NEW FRAME INSTALLED IAW SRM 120 51-10-02 PG 3 SEC 3A AND RII CARD 52-800-1000.SDR SWIA200617188Bellcrank · corrodedPAX DOOR 3RD STEP AFT BELLCRANK CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR 3RD STEP AFT BELLCRANK, PN OFF: 120-20935-001.SDR SWIA200616961Battery Pack · dischargedBACK HALF OF EMERGENCY LIGHTS TURN OFF AFTER 2 SECONDS OF PERFORMING TEST. REPLACED MIDDLE AND AFT ELBP'S. OPERATIONAL CHECKS GOOD. NR 2 SN OFF 1336.SDR SWIA200616938A/C Pack · leakingRT PACK FAIL AND ASSOCIATED DUCT LEAK CAUSED SMOKE IN CABIN AND COCKPIT. OPERATED PACKS FROM ENGINE BLEED WITH NO SMOKE OR OTHER DEFECTS. OPERATIONAL CHECKS GOOD.SDR SWIA200616891Brake · contaminatedSMOKE FROM LEFT MAIN TIRE/BRAKE ASSEMBLY AFTER PARKING. CLEANED RESIDUAL OIL OFF OF GEAR ASSEMBLY. OPERATIONAL CHECKS GOOD.SDR SWIA200616811Relay · malfunctionedCHEMICAL ODOR IN THE FLIGHT DECK MOSTLY FROM RIGHT SIDE. REPLACED OVERHEATED APU FEEDER PROTECTION RELAY IAW MM 24-37-00. OPERATIONAL CHECKS GOOD, P/N - 44B258051-002.SDR SWIA200616593Control Unit · malfunctionedRUDDER FEELS STIFF. REPLACED RUDDER PCU. OPERATIONAL CHECK GOOD.SDR SWIA200616332Actuator · malfunctionedRUDDER IS EXTREMELY STIFF AND DIFFICULT TO MOVE, BOTH INFLIGHT AND ON THE GROUND. REPLACED THE BLUE HYD RUDDER PCU ACTUATOR IAW MM 27-22-02.SDR SWIA200515443Wire · looseTURNED ON WINDSHIELD CLIMBING THROUGH FL180. BEGAN TO SMELL ELECTRICAL BURNING. SHORTLY THEREAFTER, SAW SMOKE COMING FROM UNDER FORWARD GLARESHIELD. TIGHTENED LOOSE GROUND WIRE ON TERMINAL BLOCK. OPERATIONAL CHECK GOOD.SDR SWIA200514877Servo · malfunctionedRUDDER PEDALS BINDING ON FIRST FLIGHT TEST. REPLACED RUDDER SERVO IAW EMB MM 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200514660Light · inoperativeEMERGENCY LIGHTS WILL NOT ILLUMINATE. CHANGED EMERGENCY LIGHTS, OPERATIONAL CHECK OK.SDR SWIA200514403Wire · brokenFLOOR EMERGENCY LIGHTING INOPERATIVE AT GALLEY. REPAIRED WIRES AS REQUIRED.SDR SWIA200514362Bushing · seizedMCD IS VERY HARD TO OPEN/CLOSE. REMOVED AND REPLACED FORWARD INTERMEDIATE TORQUE TUBE BUSHING PER EMB 120 MM 52-11-00. OPERATIONAL CHECK GOOD.SDR SWIA200414270Battery Pack · dischargedTHE FIRST EMERGENCY EXIT LIGHT ABOVE CENTER AISLE IN PASSENGER CABIN WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR SWIA200414621Support Angle · crackedCRACKED SUPPORT ANGLE, FORWARD OF PAX DOOR AFT HINGE ARM, UNDER FLOOR (MARKED). ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE ON FORWARD OF PAX DOOR AFT HINGE ARM UNDER FLOOR.SDR SWIA200413725Computer · malfunctionedFO'S AUTOPILOT KICKED OFF AT LEVEL OFF , 25,000 FT. REMOVED AND REPLACED AUTOPILOT COMPUTER IAW MM 22-10-02, OPERATIONAL CHECKED GOOD.SDR SWIA200413083Sign · brokenFORWARD BULKHEAD EXIT SIGN IS BROKEN. REMOVED AND REPLACED BROKEN EXIT SIGN, OPS CHECK OK. P/N: 10-1301-15.SDR SWIA200312308Relay · overheatedJUST PRIOR TO ENGINE START, FLIGHT DECK BEGAN TO SMELL OF SOMETHING ELECTRICAL OVERHEATING. ISOLATED TO APU PANEL RT SIDE CONSOLE. FOUND APU FEEDER PROTECTION RELAY SHOWING SIGNS OF EXCESSIVE HEAT. REMOVED AND REPLACED FEEDER PROTECTION RELAY IAW W/M 20-10-SDR SWIA200311926Light · inoperativeSECOND FROM FRONT RED EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED RED EMERGENCY EXIT LIGHT. OPS CHECK GOOD.SDR SWIA200311678Indicator · malfunctionedABORTED TAKEOFF AT 50-60 KNOTS DUE TO TRIPLE CHIME, RED MASTER WARNING LIGHT AND HIGH SPEED AURAL ANNUNCIATION. REPLACED BOTH LT AND RT AIRSPEED INDICATORS. GROUND TESTED OPS CHECK GOOD. LEFT S/N OFF AJ102.SDR SWIA200211690Wire · burnedFOUND BURNED WIRE IN LEFT RELAY BOX ON CAPTAIN'S SIDE. WIRE IS FOR LEFT WINDSHIELD HEAT. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED WIRE AS NEEDED PE-88022-116.SDR SWIA200211689Frame · crackedFUSELAGE FRAME CRACKED BEHIND CAPTAIN'S DV WINDOW. FOUND DURING C-CHECK INSPECTION. REPLACED AFFECTED BRACKET IAW EMB120 SRM 51-10-02.SDR SWIA200211209Acm · malfunctionedVENTILATION SYSTEM BLOWING SMOKE INTO CABIN. REMOVED & REPLACED LEFT AND RIGHT ACM, OPS CHECK GOOD.SDR SWIA200210828Warning System · malfunctionedABORTED TAKEOFF IN SFO DUE TO RED FLASHING WARNING LIGHT AND TRIM FAIL ON MAP. RETURNED TO GATE. INSPECTED AND TESTED ELECTRIC TRIM SYSTEM. OPS CHECK GOOD.SDR SWIA200210778Door Seal · looseON CLIMBOUT LOST CABIN PRESSURIZATION FOR ABOUT 1 MINUTE, THEN THE SYSTEM BEGAN WORKING NORMALLY AGAIN IN MANUAL AND AUTO MODE. RETURNED TO LAX. SECURED CARGO DOOR SEAL. PRESSURIZED AIRCRAFT TO 7 PSID. OPS CHECK GOOD. NO DISCREPANCIES NOTED.SDR SWIA200210558Indicator · defectiveHIGH SPEED VOICE WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. REPLACED NR 2 AIRSPEED INDICATOR. PERFORMED OPS CHECK. OPS CHECK GOOD.SDR SWIA200110008Proximity Switch · faultyUPON APPLICATION OF TAKEOFF POWER RECEIVED TRIM AURAL WARNING. REPLACED ELEVATOR RIGHT TRIM PROXIMITY SENSOR WITH SERVICEABLE UNIT IAW MM 27-32-05. ADJUSTED PROXIMITY SWITCH IAW MM 27-32-00. OPS CHECK GOOD AT THIS TIME.SDR SWIA972568Flux Detector · malfunctionedYELLOW HEADING FLAG BOTH SIDES, RED HEADING FLAG FIRST OFFICER''S SIDE. BOTH DG''S OFF OF MAG COMPASS 35 DEGREES. RED FLAGS BOTH RMIS. GYRO SLAVING ON CAPTAINS SIDE PEGGED NEG (-), GYRO SLAVING ON F/O SIDE PEGGED POS (+). DIVERTED TO FAT. FOUND AIRCRAFT HSDR SWIA972559Flux Detector · defectiveUPON TAKEOFF OUT OF IYK, GOT THE HDG FLAG. SHORTLY THEREAFTER, GOT THE PIT AND ROL FLAGS. ATTEMPTED QRH RESET, NO RESULTS. THE FIRST OFFICERS ATTITUDE INDICATOR SHOWED PITCH DOWN 10 PERCENT THE WHOLE FLIGHT. THE CAPTAINS ADI AND HEADING INDICATOR SHOWED FLSDR SWIA972533Generator · vibrationVIBRATION FELT FROM LEFT ENGINE DURING OPERATION. REMOVED AND REPLACED LEFT ENGINE HYD PUMP. (NO FIX). PUMP OPS CHECKS GOOD IAW 29-13-00. REMOVED AND REPLACED LEFT AUX GEN. VIBRATION FIXED, NO DEFECTS. OPS CHECKS GOOD. PUMP - P/N ON PV3-022-2A, S/N ON SDR SWIA972507Hydraulic Line · leakingDURING FLIGHT, LOSS OF FLUID QUANTITY WAS NOTED ON GREEN HYDRAULIC SYSTEM. ON DEPARTURE, QUANTITY WAS APPROXIMATELY 7/8 ON GAUGE. APPROX 30-35 MINUTES INTO FLIGHT, RESERVOIR LOW LEVEL LIGHT ILLUMINATED; QTY WAS IN YELLOW ARC. CONSTANT DECREASE IN QUANTITY WSDR SWIA972270Warning System · malfunctionedTAKEOFF TRIM AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. TRIM IN GREEN BAND. POWERED DOWN AIRCRAFT. POWERED UP AIRCRAFT. PERFORMED OPERATIONAL CHECK OF AURAL TRIM WARNING SEVERAL TIMES. TRIM AURAL WARNING OPERATES NORMAL. OPS CHECKS GOOD. COULD NOT DUPLSDR SWIA972227Warning System · activatedAURAL WARNING TRIM ALERTER WENT OFF ON TAKE OFF, TRIM SET AT 27. ABORTED TAKEOFF. POWERED DOWN AIRCRAFT THEN BACK UP, ALL CHECKS GOOD AT THIS TIME.SDR SWIA971988Warning Light · illuminatedANTI-SKID OUTBOARD INOP LIGHT ILLUMINATED DURING APPROACH, LIGHT EXTINGUISHED DURING GO-AROUND. RETURNED TO LAX. CHECKED OUTBOARD WHEEL SPEED TRANSDUCER FOR SECURITY. JACKED AIRCRAFT AND CYCLED GEAR 10 TIMES. UNABLE TO DUPLICATE PROBLEM. OPS CHECK GOOD.SDR SWIA971931Fuel Door · openSERVICE DOOR WARNING LIGHT CAME ON EARLY IN TAKEOFF ROLL. ABORTED TAKEOFF. FOUND CAMLOCK ON OUTBOARD FUEL DOOR CAME LOOSE. RESECURED DOOR CLOSED. OPS CHECKS GOOD.SDR SWIA971682Switch · failedLEFT ENGINE INLET DEICING BOOT FAILED IN FLIGHT. NUMEROUS ATTEMPTS TO RESET ALSO FAILED. DIVERTED TO SBA. REPLACED LEFT INLET PRESSURE SWITCH WITH SERVICEABLE UNIT, OPS CHECK GOOD. (S/N 2230) ON, (S/N 0141) OFF.SDR SWIA971644Ejector Valve · failedRIGHT ENGINE AIR INLET DE-ICE FAILED. RETURNED TO THE FIELD. REPLACED RIGHT ENGINE INLET EJECTOR VALVE IAW 300000. OPS CHECKS GOOD ON GROUND. PN ON 3D237606, SN: N677SN OFF: N3479.SDR SWIA971642Boot · failedRIGHT INBOARD STAB BOOT FAILED ABOVE 10,000, RESET ON DESCENT BELOW 10,000. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST OF EMPENNAGE LEADING EDGE DE-ICERS USING ENGINE PNEUMATIC POWER PER MM 301000. SYSTEM OPERATED PER FUNCTIONAL TEST REQUIREMENTS, UNABLE TOSDR SWIA971498Wire · brokenLEFT DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. APU BLEED ON, ENGINE BLEEDS OFF. STARTED QUICK REFERENCE HANDBOOK PROCEDURE, LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND BROKEN SOLDER JOINT ON LEFT PACK DUCT LEAK SENSOR NEAR BLEED AIR CONTROL VALVE. RESOLDESDR SWIA971304Boot · damagedRIGHT ENGINE INLET DEICE FAILED AGAIN IN FLIGHT. COULD NOT ESCAPE ICING CONDITIONS ALONG ROUTE AND DIVERTED BACK TO SFO. INSTALLED SERVICEABLE EJECTOR VALVE AND INSTALLED SERVICEABLE PRESSURE SWITCH AND PATCHED SMALL HOLE IN THROAT BOOT SYSTEM. OPS CHECKS GSDR SWIA971208Solenoid Valve · failedLANDING GEAR CYCLED UP AND DOWN UPON EXTENSION, GEAR LIGHTS ON PANEL. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. CYCLED LANDING GEAR NUMEROUS TIMES, OPS CHECKS GOOD.
Back to N562SW, cancelled Jul 8, 2016