N27190
Service difficulty reports · 109
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 = 'N27190' 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 = 'N27190' 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 JJBA201906031022Panel · damagedUPON REMOVAL OF EROSION TAPE FOUND COMPOSITE DAMAGE ON PANEL 333DL. REPAIRED COMPOSITE DAMAGE AND RESTORED SURFACE PROTECTION ON PANEL 333DL.SDR JJBA2019060329021Shear Tie · damagedCRACKED/BROKEN SHEAR CLIP AT FRM 68 STRINGERS 05R - 06R. REMOVED AND REPLACED CRACKED / BROKEN SHEAR CLIP AT FRM 68 STRINGERS 05R - 06RSDR JJBA2019060328020Skin · corrodedUNDERFLOOR AREA SKIN HAS CORROSION AS MARKED BETWEEN FRAME 18-19 STRINGERS 21L-21R. REPAIRED UNDERFLOOR AREA SKIN CORROSION BETWEEN FRAME 18-19 STRINGERS 21L-21R BY BLEND OUT AND CUT OUT, FILLER AND DOUBLER FABRICATION AND INSTALLATIONSDR JJBA201906035019Shear Tie · corrodedSHEAR CLIP CORRODED FR62 STR 21-20R. REMOVED AND REPLACED SHEAR CLIP BETWEEN FR62 STR 21-20RSDR JJBA2019060355018Shear Tie · corrodedSHEAR CLIP CORRODED FR62 STR 20-19R. REMOVED AND REPLACED SHEAR CLIP BETWEEN FR62 STR 20-19RSDR JJBA20190408005Sleeve · brokenCABIN PRESSURIZATION RISING 2800' PER MINUTE WHILE CRUISING AT 17K. FOUND A BROKEN SLEEVE CONNECTING TO THE #2 ACM. R&R SLEEVE.SDR JJBA201811219011Actuator · inoperativePITCH TRIM MAIN INOP WARNING CAME ON BETWEEN 10000 AND 14000 FEET. AUTOPILOT ON. REMOVED HORIZONTAL STAB ACTUATOR. INSTALLED HORIZONTAL STAB ACTUATOR. PERFORMED OPS CHECK. OPS CHECK SAT.SDR JJBA201811075002Roller · bindingNOSE L/G DOOR DIDN`T RETRACT ON GEAR UP COMMAND,RAN QRH NOSE GEAR DOOR RETRACTED. FOUND UPLOCK ROLLER TO NOT MOVE FREELY. REMOVED, CLEANED AND REINSTALLED. OPS CHECK SATSDR ASOA201703133020Skin · corrodedREAR FUSELAGE BETWEEN FRAMES 65 - 68 AND STRINGERS 21R-21R CORRODED UNDER BOTH AFT RADIO ALTIMETER ANTENNAS. AFT RADIO ANTENNA BASES WERE REPLACED IAW SRM 51-40-02. SKIN UNDER RADIO ANTENNA BASE WAS REPAIRED IAW ETD2017-145-018880.SDR ASOA201703113017Beam · corrodedCARGO DOOR SURROUND STRUCTURE LOWER BEAM CORRODED AT FRAME 66. LOWER BEAM AND ANGLE REPLACED IAW SRM 51-40-02.SDR ASOA201703083016Angle · crackedON PAX DOOR SURROUND AT FRAME 15 BETWEEN STRINGERS 15-16L REINFORCEMENT ANGLE FOUND CRACKED. THE ANGLE WAS REPLACED IAW SRM 51-40-02.SDR ASOA201703083015Floor Support · corrodedFLOOR SUPPORT BETWEEN FRAMES 24 AND 25 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-02.SDR ASOA201703083014Plate · damagedAT THE JUNCTION OF FRAME 31 AND RT FLOORBEAM, THE FLOOR SUPPORT PLATE WAS FOUND DAMAGED. THE FLOORBEAM SUPPORT PLATE WAS REPLACED IAW SRM 51-40-02.SDR ASOA201703083013Angle · crackedLEFT OUTBOARD OMEGA BEAM ANGLES CRACKED. THE ANGLES WERE REPLACED IAW SRM 53-23-02 AND ETD2017-145-017058A.SDR ASOA201703083012Floor Support · corrodedBETWEEN FRAMES 47 AND 53 LT FLOOR SUPPORT NR 6 CORRODED. THE FLOOR SUPPORT WAS REPLACED IAW 51-40-02.SDR ASOA201703083010Floor Support · corrodedBETWEEN FRAMES 52 AND 59 LT OTBD FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASOA201703073025Floor Support · corrodedFLOOR SUPPORTCORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASOA201703073021Angle · corrodedBETWEEN FRAMES 49 AND 50 CLOSING ANGLE CORRODED. CORROSION REMOVED IAW SRM 51-10-03.SDR ASOA201703073009Floorbeam · corrodedFLOORBEAM CORRODED AROUND ANCHOR NUT AT FRAME 59. REPAIRED THE FLOORBEAM. DOUBLER INSTALLED IAW SRM 53-24-10 PARA 3. HFEC INSPECTION PERFORMED ON REPAIRED AREA WITH NO FAULTS FOUND.SDR ASOA201703073008Floor Support · corrodedBETWEEN FRAME 59 AND 61 RT OUTBOARD FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASOA201703041290Floor Support · corrodedLT OMEGA BEAM FOUND CORRODED BETWEEN FRAME 23-23. LT OMEGA BEAM REPAIRED AS PER SRM 53-21-10 ITEM 7 FIG 206. SHEET 2, HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT FOUND.SDR ASOA201703041291Door Sill · corrodedCF3 BETWEEN FRAME 35 AND 41. RT SILL 3 CORRODED. SILL REPLACED AS PER SRM 51-40-02.SDR ASOA201702181291Door Sill · corrodedCF3 BETWEEN FRAME 35 AND 41. RT SILL 3 CORRODED. SILL REPLACED AS PER SRM 51-40-02.SDR ASOA201702181290Floor Support · corrodedLT OMEGA BEAM FOUND CORRODED BETWEEN FRAME 23-23. LT OMEGA BEAM REPAIRED AS PER SRM 53-21-10 ITEM 7 FIG 206. SHEET 2, HFEC PERFORMED ON REPAIRED AREA WITH NO FAULT FOUND.SDR ASOA201703041288Rib · corrodedCARGO DOOR SURROUND STRUCTURE FWD FLOOR SIDE PLATE AT FRAME 65 CORRODED. RIB REPLACED AS PER SRM 51-40-02.SDR ASOA201703041287Door Sill · corrodedRT SILL 5 BETWEEN FR 48 AND FR 52 CORRODED. RT SILL 5 REPLACED AS PER SRM 51-40-02.SDR ASOA201703031292Door Sill · corrodedRT SILL 4 BETWEEN FR 41 AND FR 48 CORRODED. RT SILL 4 REPLACED AS PER SRM 51-40-02.SDR ASOA20160707031Battery Pack · dischargedEMERGENCY LIGHTS REPORTED INOPERATIVE. MX CHARGED EMERGENCY LIGHT BATTERIES AND OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20160206009Inverter · inoperativeDURING ROUTINE MAINTENANCE, THE FORWARD CENTER OVERHEAD EMERGENCY SIGN WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER AND OPS CHECKS WERE GOOD.SDR ASOA20151116088HSkin · dentedA DENT WAS DISCOVERED BEHIND THE CARGO DOOR BETWEEN FRAMES 73-74 STRINGERS 12L-13L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-31-01 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140820089RSWire Harness · shortedSUP: ORIGINAL REPORT SDR PILOT REPORTED AN APU GENERATOR FAIL MESSAGE WITH STRONG ELECTRICAL ODOR. MAINTENANCE R & R APU ELECTRICAL HARNESS ASSY, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140820089Starter Gen · failedPILOT REPORTED AN APU GENERATOR FAIL MESSAGE WITH STRONG ELECTRICAL ODOR. FOUND APU STARTER/GENERATOR INOPERATIVE.SDR ASOA20140123008Engine · smokeTHE CREW REPORTED THE ACFT FILLED WITH SMOKE AT APPROXIMATELY 12000 FT, ALONG WITH LAVATORY SMOKE ALARM. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.SDR ASOA20131230089Unknown · smokeTHE CREW REPORTED SMOKE IN CABIN, AIR RETURN. REPORTED SMOKE CLEARED ON APPROACH. MAINTENANCE INSPECTED AND PERFORMED OPS CHECKS OF BLEED AIR SYSTEM IAW 36-00-00. NO SMOKE IN CABIN OR COCKPIT NOTED.SDR ASOA20130911107RWire · chafedCREW REPORTED AN NR 2 ENGINE FIRE DETECT FAIL MESSAGE IN FLIGHT ON EICAS. MX REPAIRED CHAFED WIRE TO FIRE LOOP CONNECTOR. OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120824135Flapper Valve · leakingFUEL LEAK AFTER TAKEOFF. R & R LT WING OTBD FLAPPER VALVE. ACFT RELEASED AND RETURNED TO SERVICE.SDR ASOA20120528040Skin · corrodedDURING C-CHECK. CARGO DOOR LOWER CUT OUT CORRRODED. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120216015Sign · inoperativeDURING SCHEDULED MX INSPECTION, 12A EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX RESET AND PERFORMED. OPS CHECKED SUCCESSFULLY IAW AMM 33-50-00. ACFT WAS APPROVED FOR RETURN SERVICE.SDR ASOA20120215014Carbon Seal · leakingCREW REPORTED ON DESCENT ENGINE NR 1 SHOWED LOW OIL PRESSURE AND 3 QUARTS OF OIL INFLIGHT. SHUT ENGINE DOWN DUE TO CONDITION. SHOWED 2 QUARTS OF OIL ON GROUND. MX FOUND 1 ENGINE ATS AGB CARBON SEAL LEAKING AND CASE DAMAGED. R & R NR 1 ENGINE AGB IAW MM 72-SDR C2XA11CL217Engine · vibrationEWR FLT 4683 THE CREW REPORTED A ENGINE NR 1 HP VIBRATION AMBER INDICATION IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT NR 1 ENGINE VIB INDICATION PER RRFIM 77-41-00-810-802. VIBES WERE WITHIN SDR C2XA11IA091Light · inoperativeIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE AISLE PATH LIGHT STRIP AT THE GALLEY TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICSDR C2XA11TY045Control Module · inoperativeNR 1 ENGINE FIRE DETECTOR FAIL AND E1 & E2 SHORT DISPATCH BEFORE TAKEOFF. ABORTED TAKEOFF. PERFORMED OPERATIONAL TEST OF NR 1 AND NR 2 ENGINES AND RESET E1 AND E2 FADECS. OPS CHECKED GOOD. NR 2- E1 FIRE DETECTOR FAIL ON TAKEOFF. ABORT TAKEOFF. INSPECTED SDR C2XA11CL078Anti-Ice Valve · faultyCREW REPORTED AN ENGINE 2 ANTI-ICE FAIL MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL PROCEDURES. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE ANTI-ICE VALVE AND NR SDR C2XA11IA027Unknown · smokeOKC - FLIGHT 4934, THE CREW RETURNED TO OKC FOR LAV SMOKE IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT, AND IAH MAINTENANCE PERFORMED ENGINE RUNS, AND BLEED SYSTEMS OPERATIONAL CHECKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA10SH312Floor Support · corrodedSHV - DURING C-CHECK RT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 23 IAW EMB-145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10IA087Door · crackedIAH - FLIGHT 2553, DURING PREFLIGHT INSPECTION THE CREW REPORTED TAHT THE RIGHT MAIN LANDING GEAR AUX DOOR WAS CRACKED. MAINTENANCE REMOVED THE AUX DOOR, AND PLACED THE AIRCRAFT IN CDL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 2/28/2010, THE IAHSDR C2XA09IA322Pressure Switch · inoperativeIAH - FLIGHT 2633, THE CREW REPORTED A RUDDER 1-2 INOP MESSAGE ON EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 & NR 2 RUDDER PRESSURE SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTSDR C2XA09IA321Pressure Switch · inoperativeIAH - FLIGHT 2633, THE CREW REPORTED A RUDDER 1-2 INOP MESSAGE ON EICAS DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 & NR 2 RUDDER PRESSURE SWITCHES, OPERATIONALLY TESTED WITH NO DEFECTSDR C2XA09IA274Sensor · inoperativeIAH - FLIGHT 2172 - THE CREW REPORTED, RECEIVED A PACK ONE VALVE CLOSED MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PACK DUCT TEMPERATURE SENSOR, OPERATIONALLY TESTED WITH NSDR C2XA09IA266Filter · dirtyIAH - FLIGHT 2160, DURING CLIMB THE CREW REPORTED A BLEED ONE OVERTEMP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE FAN AIR VALVE FILTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAF
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