N16987
Service difficulty reports · 81
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 = 'N16987' AND registry_match = 'registration' 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 = 'N16987' AND registry_match = 'registration' 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 ASOA20191115112Fuse · failedMX REPORTED MULTIPLE EXTERNAL EMERGENCY LIGHTS INOP. MX FOUND EMERGENCY LIGHT TRAY #1 FUSE BLOWN TO LH WING FUSELAGE FRONT AND CEILING PANEL LIGHT AISLE AND AT BATTERY TRAY #2 FOR RH WING. REPLACED FUSES WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVSDR ASOA2019062065078Unknown · odorCREW REPORTED BURNING SMELL WHEN COFFEE MAKER #2 IN OPERATION. ITEM PLACED ON MEL. MX PERFORMED OPERATIONAL CHECK GOOD WITH NO BURNING SMELL NOTED.SDR ASOA201905237050Frame · chafedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND CHAFFING FROM A SCREW AT FRAME 70 BETWEEN STRINGER 12R AND 13R. MAINTENANCE REPAIRED THE CHAFE AREA FROM STR.12R TO 13R IAW ETD 2019-145-066859. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201905237049Trunnion · crackedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND THE LT MLG AFT TRUNION CRACKED. MAINTENANCE REMOVED AND REPLACED THE LT TRUNION ON THE LT MLG AFT SIDE IAW ECTC ETD 2019-145-068830. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE C-CHECK.SDR ASOA201905147046Rib · crackedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND RIB 21 INSIDE ACCESS PANEL 551CB CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND FAB. A FILLER AND DOUBLER FOR RIB 21 IAW SRM 57-20-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201905147045Rib · crackedTYS A/C IS IN C-CHECK WHEN INSPECTION FOUND A CRACK AT RIB 21 INSIDE ACCESS PANEL 651CB. MAINTENANCE REMOVED THE DAMAGED AREA OF RIB 21 AND REPLACED WITH FILLER AND DOUBLER IAW SRM 57-20-07. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201901023001Coffeemaker · faultyTHE CREW REPORTED ELECTRICAL SMELL COMING FROM GALLEY, WENT AWAY WHEN COFFEE MAKERS WERE SHUT OFF. MAINTENANCE REPLACED COFFEE BREWER IN LT POSITION. OPS CHECK GOODSDR ASOA201705113145Stringer · crackedLEFT REAR FUSELAGE STRINGER 2L CRACKED AT FRAME 75. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.SDR ASOA201705093143Channel · corrodedSERVICE DOOR CHANNEL CORRODED. CHANNEL REPLACED AS PER SRM 51-40-02.SDR ASOA201705093142Structure · corrodedPAX DOOR SILL AFT "U" SHAPE CORRODED. AFT "U" SHAPE REPLACED AS PER SRM 51-40-02.SDR ASOA201705093141Structure · corrodedPAX DOOR SILL FORWARD U SHAPE CORRODED. FORWARD U SHAPE REPLACED AS PER SRM 51-40-02.SDR ASOA201705073140Seat Track · corrodedCABIN SEAT TRACK LT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.SDR ASOA201705073139Seat Track · corrodedCABIN SEAT TRACK RT NR 3 INBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.SDR ASOA201705073138Seat Track · corrodedCABIN SEAT TRACK RT NR 4 OUTBOARD CORRODED. THE SEAT TRACK WAS REPLACED IAW SRM 53-01-06-400-801.SDR ASOA201705073137Bearing · corrodedRT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-CO2-A00.SDR ASOA201705073136Bearing · corrodedLT MLG AFT LOWER HALF BEARING CAP CORRODED. THE BEARING CAP WAS REPLACED IAW 57-26-00-220-C02-A00.SDR ASOA201705053135Doubler · corrodedCORROSION ON DOUBLER AROUND POTABLE WATER NIPPLES. DOUBLER REPLACED IAW SRM 51-40-02.SDR ASOA201705053134Stringer · corrodedSTRINGER 15R BETWEEN FRAMES 40 AND 41 CORRODED BEYOND LIMITS. REPLACED IAW SRM 53-10-02.SDR ASOA201705043133Door Sill · corrodedSERVICE DOOR AFT SILL CORRODED. SERVICE DOOR AFT SILL REPAIRED AS PER SRM 53-21-10 ITEM 5 FIG 204 SHEET 3. HFEC PERFORMED WITH NO FAULT FOUND.SDR ASOA201705023128Floorbeam · corrodedCENTER FUSELAGE MIDDLE FLOORBEAM CORRODED AROUND ANCHOR NUT HOLES. FLOORBEAM REPLACED IAW SRM 51-40-02.SDR ASOA201705023127Channel · crackedRIGHT WEB CRACKED ON FORWARD PRESSURE BULKHEAD IN NOSE WHEELWELL. CHANNEL REPLACED IAW SRM 51-40-02.SDR ASOA201704203096Crossbeam · crackedNLG UPLOCK AFT CROSSBEAM CRACKED. THE UPLOCK CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.SDR ASOA201704203095Crossbeam · crackedNLG UPLOCK FORWARD CROSSBEAM CRACKED. THE CROSSBEAM WAS REPLACED IAW SRM 53-11-08, FIG 25, ITEM 50.SDR ASOA201612223088Battery Pack · inoperativeDURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING AFT EMERENGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.SDR ASOA20150305007Rib · crackedACFT IS IN C-CHECK WHEN INSPECTION FOUND A CRACK ON THE LT WING AT RIB NR 5 IN AREA FWD OF PREVIOUS SB MOD. CRACK RUNS FROM LOWER FLANGE OTBD THRU THE HYLOCK HOLE AND CONTINUOUS VERTICALLY 6". R & R THE NR 5 RIB IAW EC5710-01239. ALL WORK ACCOMPLISHED AND SDR ASOA20150305006Skin · gougedACFT IS IN A C-CHECK STATUS WHEN INSPECTION FOUND TOOLING MARKS ON THE LT WING ZONE 532 UPPER SKIN, THAT SHOWED A GROOVE CUT INTO THE SKIN. MAINTENANCE INSTALLED A REPAIR TO THE UPPER SKIN IAW EC5710-01240. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE ENSDR ASOA20140124022Engine · smokeSTRONG SMELL AND A SMOKE HAZE WAS PRESENT IN CABIN WHEN PACK 1 WAS SELECTED. MAINTENANCE R & R THE NR 1 ENGINE IAW MM.SDR ASOA20130812062Valve · leakingTHE CREW REPORTED A SUSPECTED FUEL LEAK IN OTBD LT WING DURING FLIGHT. MX INSPECTED AND REPLACED A LT WING FUEL FLAP VALVE. OPS CHECKS WERE GOOD .SDR ASOA20130525052Control Unit · faultyCREW REPORTED OTBD BRAKE INOPERATIVE. MX R & R THE BRAKE CONTROL UNIT WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130423152Door Frame · corrodedDURING A-CHECK, PAX DOOR CUTOUT WAS FOUND CORRODED AT FRAME 18 BETWEEN STRINGERS 15-16L. MX REMOVED THE CORRODED SECTION AND PERFORMED A SPLICE REPAIR IAW EC5310-01690. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR V0XR201303100178Floorbeam · damagedFLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04, 51-21-05, AND 51-21-06.SDR V0XR201303100177Floorbeam · damagedFLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02, CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.SDR V0XR201303100176Floorbeam · damagedFLOORBEAM AT BS 5125 IS DAMAGED. R & R FLOORBEAM IAW SRM 51-40-02,CPM 51-04-00, 51-21-04,51-21-05, AND 51-21-06.SDR V0XR20130310J0175Fairing · looseLOOSE FASTENERS AT FRAME BETWEEN 59/60 BETWEEN STR 21L AND 21R. INSTALLED DOUBLERS IAW EC5320-01761 AND INSTALLED RT AND LT FAIRINGS IAW SRM 51-40-02.SDR V0XR201303100174Door Frame · corrodedSURFACE UNDER LOWER AFT MAIN DOOR GUIDE AT FRAME 18 BS 5417 CORRODED. BLENDED CORRODED AREA , FOUND WITHIN LIMITS AT FRAME 18 STA. 5417 IAW EC5310-01684 (TEMPORARY REPAIR OF 600 FC'S PERMANENT REPAIR EC5310-01690)SDR V0XR201303100173Floorbeam · corrodedPAX FLOORBEAM CORRODED AT FS 693.80 R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.SDR V0XR201303100172Floorbeam · corrodedPAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.SDR V0XR201303100171Floorbeam · corrodedPAX FLOORBEAM CORRODED AT FS 693.80. R & R PAX FLOORBEAM IAW SRM 51-40-02 AND CPM 51-20-04.SDR V0XR201303100170Skin · scratchedMULTIPLE SCRATCHES (3) FRAME 59 STR.17R AND FRAME 78 STR. 18R. PERFORMED REPAIR ON SCRATCH AT FRAME 59 STR 17R IAW EC 5330-02788.TWO OTHER SCRATCHES AT FRAME 22-23 STR. 20L AND ON FRAME 78 STR. 18R ARE STRUCTURALLY EXCEPTABLE IAW ETD2012-145-017252-A (REF. W/SDR ASOA20121017093RBolt · unsecureCREW REPORTED MAIN CABIN DOOR LEVER PRODUCES LOUD METAL POP SOUND WHEN OPENING AND FEELS UNUSUALLY HARD TO OPEN. MX INSPECTED AND FOUND HARDWARE LOOSE, RESECURED THE INTERNAL HANDLE BOX BOLTS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICESDR C2XA11CL228Connector · looseORD FLT 5983 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED PROXIMITY SWITCH INSPECTION OF BOTH THE MAIN AND NOSE GEAR. FOUND THE NOSE GEAR WOW PROXIMISDR C2XA11CL212Wire Harness · chafedTHE CREW REPORTED AN ENGINE NR 2 FIRE DETECT FAIL MESSAGE ONLY DURING DESCENT, LOW PITCH ATTITUDE AND THRUST LEVER AT IDLE. MAINTENANCE INSPECTED AND REPLACED NR 2 ENGINE FIRE DETECT HARNESS. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11IA169Unknown · odorIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG FUEL SMELL IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND GROUND RAN THE ENGINES ALL WITH NO DEFECTS OR SMELL NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11RI048Unknown · smokeFLIGHT 2540 - EWR - FLIGHT CREW REPORTED SMOKE IN CABIN AND PERFORMED AIR RETURN UNEVENTFULLY. EWR MX PERFORMED ENGINE RUNUP (1 & 2) AT HIGH POWER WITH BLEED SYSTEM ON FOR 5 MIN. NO SMOKE NOTICED. ACFT APPROVED TO RETURN TO SERVICE.SDR C2XA11SHO54Skin · crackedSHV - DURING C-CHECK CRACK AROUND RIVET FRAME 75 STRINGER 2L-3L (VERIFIED WITH EDDY CURRENT). MAINTENANCE PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 75 STRINGER 2L-3L IAW EC5330-02353. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11RI008Unknown · smokeFLIGHT 2513 - MHT - FLIGHT CREW REPORTED LAV FIRE WARNING ON CLIMB - SMOKE IN THE LAV - CREW PERFORMED AIR RETURN AND LANDED SAFELY - NO EMERGENCY DECLARED. CONTRACTED MX INSPECTED LAV - NO DEFECTS FOUND - AND PERFORMED ENGINE FULL POWER RUN, APU AND PACKS CHSDR C2XA10IA347Skin · crackedDURING MAINTENANCE INSPECTION THE LEFT WING SKIN WAS FOUND TO BE CRACKED AT THE INBOARD SPOILER CENTER HINGE POINT CUTOUT. MAINTENANCE STOP DRILLED THE CRACK, AND PLACED THE AIRCRAFT ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE PESDR C2XA09CL157Carbon Seal · malfunctionedCLE FLT 2542 THE CREW REPORTED SMOKE IN THE CABIN AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE. TEAR DOWN REPORT FROM ROLLS ROYCE INDICATED THE NR 0 CARBON SEAL RUNNER WASDR C2XA09IA144Drain · damagedIAH - FLIGHT 2627 DURING CLIMB THE CREW REPORTED, LOST IAS INDICATIONS ON BOTH SIDES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED DAMAGED PITOT DRAINS ON NR 1 & 2 SIDES, LEAK CHECK WITH NO DEFECTS NOTED. TSDR C2XA09IA143Ahrs · malfunctionedIAH - FLIGHT 2627 - DURING CLIMB THE CREW REPORTED THAT BOTH THE PILOT AND COPILOT ATT AND HDG FAILED. THE AIRCRAFT RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS AHRS COMPUTER, OPERATIONALLY TESTED
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