N11191
Service difficulty reports · 95
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 = 'N11191' 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 = 'N11191' 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 JJBA20220616011None · brokenSERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK FAILED. FOUND WIRE W716-0007-20 TO BE BROKEN. REPAIRED WIRE. OPS CHECK SATSDR JJBA20220502002Unknown · unknownEMERGENCY DOOR HANDLE ON EMERGENCY EXIT OVER WING RIGHT SIDE REMOVED, WILL NOT ADHERE TO WALL. REINSTALLED EMERGENCY EXIT COVER RS WINGSDR JJBA20211017053None · noneAT CF4 LH SIDE, CRACK FOUND IN FR59 AROUND FLOOR. ON LH CENTER FUSE 4, SPLICE AT FR59 AND STR 13L REMOVED FOR ACCESS. ON LH CENTER FUSE 4, SPLICE AT FR 59 REPAIRED AND ALTERNATE MATERIAL FOR FABRICATION OF FR59 SECTION AND SPLICE REPAIR. SPLICE ON FR59 AND STRSDR JJBA20211017052None · noneCF II CENTER OMEGA BEAM 2 CRACKS FOUND AT FR 25 AND FR 27. CFII, CENTER OMEGA BEAM AT FR 25-27 REPAIREDSDR JJBA20211017051None · nonePAX DOOR UPPER BALANCING BAR FUSELAGE FITTING BOLT HOLE ELONGATED. ON PAX DOOR UPPER HINGE FITTING, BOLT LUGS REWORKED. 2X BUSHINGS LOCALLY FABRICATED ON PAX DOOR UPPER HINGE FITTING, BUSHING INSTALLED ON BOTH. REWORKED LUGS.SDR JJBA20210930050None · noneFWD FUSELAGE II DENTS FOUND ON LH LOWER SKIN BTW FR 10-11 AND BTW STR 20L-21L. FWD FUSELAGE II DENT FOUND ON LH LOWER SKIN BTW FR 10-11 AND BTW STR 20L-21L REPAIRED WITH DOUBLERSDR JJBA20210928026None · noneUNRECORDED PATCH NEEDS TO BE REMOVED FOR INVESTIGATION BTW FR 19-20, STR 11-12. UNRECORDED REPAIR PATCH REMOVED BTW FR 19-20 PAINT STRIPPED BTW FR 19-20, STR 11-12 AT UNRECORDED PATCH LOCATION. PERMANENT REPAIR DOUBLER PERFORMED BTW FRAME 19-20 AND STR 10L-12LSDR JJBA20210927024None · noneCRACK FOUND RH FRAME 25 AT JOINTING OF FLOOR STRUCTURE (RH SILL #1) IN CF2. DAMAGE SECTION OF RH FRAME 25 CUT BTW STR 16R-17R SPLICED U-SHAPE FABRICATED. RH FRAME 25 BTW 15R-17R IN CF II REPAIRED.SDR JJBA20210924015None · noneAT FF, COCKPIT AT STA X3010 CENTER UPPER WEB HANDLE FOUND CRACK 2 PLACE AROUND ANCHOR NUT. PERFORMED CUTOUTS IN COCKPIT AT STA X3010 CENTER UPPER WEB AT HANDLE LOCATION. FABRICATED REPAIR DOUBLERS IN COCKPIT AT STA X3010 CENTER UPPER WEB AT HANDLE LOCATION. ATSDR JJBA20210409022Armrest · crackedCRACK FOUND IN PAX SEAT ARMREST AT 3A. REMOVED AND REPLACED PAX SEAT AT 3A. NO FURTHER DEFECTS NOTED.SDR JJBA20210206008Brake · low pressureBRAKE OVERHEAT ON EICAS AFTER TAKE-OFF RIGHT BEFORE GEAR RETRACTION (DID NOT OBSERVE ANY BRAKE TEMP INDICATIONS IN THE RED AND OVERHEAT MESSAGE EXTINGUISHED AFT GEAR RETRACTION). R&R BRAKE TEMPERATURE SENSOR. OPS CHECK SAT. NO FURTHER DEFECTS NOTED. COMPLIED WSDR JJBA201908197011Controller · inoperativeAUTO PRESS FAIL ON EICAS AND MANUAL PRESSURIZATION INOPERATIVE DURING TAKEOFF CLIMB OUT. R&R AUTO PRESSURE DIGITAL CONTROLLER. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.SDR JJBA201906043005Nut Plate · missingRUDDER II PROTRACTOR TOOLING NUT PLATE MISSING AS MARKED. INSTALLED DOUBLER AND FILLER. RESTORED ORIGINAL FINISH AS REQUIRED.SDR JJBA20190522011Frame · corrodedDURING REMOVAL OF FWD BONDING PLATE CORROSION FOUND AT FR65 STRG 14-15 AS MARKED. COMPLETED INSTALLATION OF FRAME 65 INNER REPAIR DOUBLER BETWEEN STRINGERS 14-15L.SDR JJBA20190516008Threshold · corrodedBAGGAGE DOOR THRESHOLD CORRODED FR 65-68. REMOVED AND REPLACED BAGGAGE DOOR THRESHOLD BEAM BETWEEN FR 65-68.SDR JJBA20190514007Threshold · corrodedSERVICE DOOR THRESHOLD (BEAM) CORRODED AS MARKED FRM 20-22. REMOVED DAMAGE PART AND LOCATED, DRILLED, COUNTERSUNK, ALODINED AND INSTALLED NEW THRESHOLD FOR SERVICE DOOR.SDR JJBA20190510006Floor Support · corrodedCENTER OMEGA BEAM FRM24 AND Y-0.0 CORROSION AROUND NUT PLATE AS MARKED. REMOVED AND REPLACED DOUBLER ON CENTER OMEGA BEAM FR 24 AND Y-0.0.SDR JJBA2018123128023Wire Harness · damagedAPU FIRE WARNING AND BELL IN FLIGHT FOLLOWED QRH MESSAGE EXTINGUISHED. DID NOT BLOW FIRE BOTTLE. APPROXIMATELY BETWEEN 19,000-10,000 ON DECENT THE APU WAS STARTED. IMMEDIATELY AFTER STARTUP THE CREW RECEIVED THE MASTER WARNING FOR APU FIRE AND THE AURAL BELL. SDR JJBA20181027016Tube · not reportedBLEED 1 LEAK IN FLIGHT. PACK 2 OVERHEAT IN FLIGHT. PASSENGER OXYGEN MASKS DROPPED DURING DEPRESSURIZATION AND USE. R&R Y TUBE ASSY AND RAM AIR DUCT ASSY. PERFORMED OPS CHECK OF PACK 2, OPS CHECK SAT. R&R O2 GENERATORS, PERFORMED OPS CHECK OF PASSENGER OXYGEN DSDR JJBA2018081401012Pitch Control · malfunctionedPITCH TRIM MAIN INOPERATIVE ON EICAS DURING FLIGHT. MAIN PITCH TRIM FAILED JUST AFTER T/O. BACKUP CHANNEL WAS INTERMITTENT AND THEN FAILED COMPLETELY WITH NO EICAS FAILURE MESSAGE. STAB TRIM SYSTEM TESTS FINE ON THE GROUND.SDR JJBA201808140011Control Unit · inoperativePITCH TRIM INOPERATIVE ON EICAS, DURING FLIGHT. REMOVED AND REPLACED HSCU.SDR JJBA20180519008Light · unsecureFLOOR EMERGENCY LIGHT STRIP AT ROW 6 NOT SECURE. SECURED FLOOR EMERGENCY LIGHT STRIP AT ROW 6.SDR JJBA20171207008Floor Panel · damagedDAMAGE FOUND ON FUSELAGE AFT OF RH GALLEY DOOR. PERMANENT REPAIR.SDR JJBA20170605004Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT ILLUMINATE. CHARGED THE BATTERIES. OPS CHECKED GOOD.SDR JJBA20161220018Bulb · inoperativeROW 18A OVERHEAD EMERGENCY LIGHT INOPERATIVE. R & R THE BULB.SDR ASOA20160729047Skin · crackedDURING C-CHECK, THE RT AFT SKIN WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EMB 145XR SRM 53-32-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160729046Beam · corrodedDURING C-CHECK, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160729045Fitting · crackedDURING C-CHECK, THE RT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE FITTING IAW EC5450-01207. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20141205145Acm · frozenTHE CREW REPORTED SMOKE IN THE COCKPIT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE NR 1 ACM, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140928123Acm · failedTHE CREW REPORTED A BURNING ODOR IN FLIGHT, SULFUR BURNING ODOR. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT MAINTENANCE R & R THE NR 1 ACM, OPS TESTED WITH NO DEFECTS. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140908110Acm · failedTHE CREW REPORTED HEARING A POPPING NOISE DURING CRUISE AND IMMEDIATELY SMELLING SMOKE AND NOTICED SMOKE COMING FROM THE CAPTAIN`S SIDE VENT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ACFT AND R & R THE NR 1 ACM, OPERATIONALLY TESTED WISDR ASOA20140827077Acm · seizedTHE CREW REPORTED A STRONG BURNING ODOR AFTER A LOUD THUD AND PRESSURE BUMP. MAINTENANCE INSPECTED AND FOUND NR 1 ACM SEIZED. THE NR 1 AIR CYCLE MACHINE WAS REPLACED AND OPS CHECKS WERE GOOD.SDR ASOA20140207012Display · failedDIVERTED, ODOR OF ELECTRICAL SMOKE IN COCKPIT WITH ASSOCIATED NR 4 MFD GOING BLANK. ODOR SUBSIDED AFTER MFD CIRCUIT BREAKER WAS PULLED. MX R & R THE F/O'S MFD, DU-870 OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120426033REngine · leakingCREW REPORTED SMOKE IN COCKPIT & CABIN AFTER TAKEOFF, CLEARED AFTER SEVERAL MINUTES. AIR RETURN TO DEPARTURE WITHOUT INCIDENT. MX R & R NR 1 ENGINE IAW TASK CARD 6271001 AND IPC 72-00-00. OPS AND LEAK CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICESDR C2XA11RI093Anti-Ice Valve · inoperativeFLIGHT 2636 - EWR - FLIGHT CREW REPORTED THAT INFLIGHT AIRCRAFT FAILED THE ICE PROTECTION TEST PART B - ONLY GOT 3 OPEN ; WING ANTI-ICE DID NOT OPEN. CREW ATTEMPTED THE TEST SEVERAL TIMES AND FAILED. ALSO UPON ENTERING ICING GOT A WING ANTI-ICE FAILURE ON. SDR C2XA11CL122Inverter · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 AND NR 5 EMERGENCY LIGHT INVERTERS. OPERATIONAL CHECKS WERE GOOD.SDR C2XA11CL044Fuse · leakingTHE CREW REPORTED A BRAKE INOP MESSAGE ON THE EICAS AFTER LANDING. MAINTENANCE INSPECTED AND REPLACED THE RIGHT INBOARD AND OUTBOARD HYDRAULIC FUSE. OPERATIONAL CHECKS WERE GOOD.SDR C2XA10TY086Service Door · missingFERRY FLIGHT FROM PVD TO TYS FOR REPAIR - ENGINE 1 COWLING OIL SERVICE DOOR FOUND MISSING ON POST FLIGHT WALK AROUND. TYS MX REMOVED AND REPLACED ENGINE 1 LOWER COWLING. A/C RETURNED TO SERVICE.SDR C2XA10SH186Skin · crackedSHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO HAVE CRACKS AROUND 2 FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 5L-6L. MAINTENANCE PERFORMED A BUSHING REPAIR IAW EC 5330-02137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA071Display · inoperativeIAH - FLIGHT 2196, THE CREW REPORTED THAT THE ISIS WAS BLANK AND INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE ISIS UNIT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA09TY263Flapper Valve · tornGSP - FUEL LEAK IN FLT LT WING; LOST 500 LBS OF FUEL. A/C AIR RETURNED AND CLT MX REPLACED THE LT WING FLAPPER VALVE. A/C WAS RELEASED.SDR C2XA09IA219Proximity Switch · inoperativeIAH - FLIGHT 2594, THE CREW REPORTED A SPOILER FAIL MESSAGE IN CRUISE FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT OUTBOARD SPOILER PROXIMITY SWITCH, OPERATIONALLSDR C2XA09CL097Precooler · faultyCREW REPORTED A "BLEED 2 OVERTEMP" MESSAGE CLIMBING THRU 170000. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR2 ENGINE PRECOOLER ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA08IA263Control Panel · faultyFLIGHT 2777 IAH-GSO - DURING TAXI THE EMERGENCY LIGHT PANEL LOCATED IN THE COCKPIT KEPT RE-ARMING AND TURNING ON THE EMERGENCY LIGHTS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM AND CSDR C2XA08ON070Spoiler · deployedFLT 0054 - MCI TO TUS - SPOILERS DEPLOYED ON TAKEOFF ROLL ABORTED T/O AT 10KNOTS. FLIGHT CREW FULLY DISENGAGED GUSTLOCK AND AIRCRAFT DEPARTED NO MX ACTION WAS REQUIRED. AIRCRAFT WAS RELEASED FOR SERVICE.
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