N31131
Service difficulty reports · 116
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 = 'N31131' 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 = 'N31131' 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 RAIA201901230002Door Sill · corrodedRT FLOOR SILL BETWEEN FR 50 & 51 HAVE CORROSION ON UPPER SURFACE. REMOVED CORRODED FLOOR SILL BETWEEN FRAMES 48-53 AND INSTALLED NEW FLOOR SILL. HI LOKS NEED TO BE INSTALLED. INSTALLED NEW FLOOR SILL AT FRAME 48-53 INSTALLED HI LOK FASTENERS.SDR RAIA201901230001Door Sill · corrodedLT FLOOR SILL HAS CORROSION BETWEEN FR 54 & 55. REMVED & REPLACED LT FLOOR SILL AT FR 52-56.SDR RAIA2019020820016Seat Track · corrodedCENTER OMEGA BEAM SHORT SEAT TRACKS HAVE CORROSION FROM FRAME 23 THRU 32- REMOVED CENTER OMEGA BEAM SHORT SEAT TRACKS FROM FR 23 THRU FR 32. BLENDED PAX SEAT TRACKS BY FR 24/25, FR 28/29 & FR 30/31/32, THEY ARE WITHIN LIMITS. REPLACED CENTER OMEGA BEASDR RAIA2019020420015Floor Support · corrodedLH FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FRAME 37 THRU 40- REMOVED FL SILL. INSTALLED LH SILL.SDR RAIA2019020420014Support Bracket · crackedFRAME 46LH LOWER SUPPORT BRACKET IS CRAQCKED AT STR 15 BELOW LEFT FLOOR SILL- REMOVED ALL FASTNERS. INSTALLED LH LOWER SUPPORT BRACKET AT FR 46 STR 15L, FUEL TANK SEALANT STILL NEEDS TO BE APPLIED. INSTALLED SEALANT TO REPAIR.SDR RAIA2019020420013Support Bracket · crackedFRAME 46 LOWER SUPPORT BRACKET IS CRACKED @ STR 15 BELOW RIGHT FLOOR SILL- REMOVED ALL FASTNERS. REMOVED & PICKED UP HOLES ON NEW BRACKET. INSTALLED RH LOWER SUPPORT BRACKET AT FR 46, FUEL TANK SEALANT NEEDS TO BE APPLIED. INSTALLED SEALANT 1440 B2 TOSDR RAIA2019020420012Floor Support · corrodedCENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION ATOUND NUTPLATE HOLES FROM FR 59 THRU 61- CORROSION IN THIS AREA WENT THROUGH UPPER DIGITAL OMEGA BEAM, UNDER DIGITAL NEEDS TO BE INSPECTED AFTER REMOVALE OF DIGITAL. REMOVED DIGITAL SUPPORT, NO DASDR RAIA2019020420011Floor Support · corrodedFLOOR SUPPORT BETWEEN LH & CENTER OMEGA BEAM HAVE CORROSION BETWEEN FRAME 24 & 25- R&R CROSS BEAM L/H BETWEEN FRAME 24 & 25.SDR RAIA2019020120010Floor Support · corrodedLH OMEGA BEAM UPPER SURFACE HAS CORROSION BETWEEN FR 40 & 41- REMOVED FASTENERS & BLENDED AREA OF CORROSION. ORIGINAL THICKNESS=.040 BEFORE BLEND. THICKNESS AFTER BLEND = .010. .030 MATERIAL LOSS= OUT OF LIMITS. REMOVED LH OMEGA BEAM UPPER GUSSET BETWSDR RAIA2019020120009Floor Support · corrodedRH FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM FRAME 41 THRU 43- REMOVED FLOOR SILL. INSTALLED FLOOR SILL.SDR RAIA2019020120008Floor Support · corrodedRH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 59- UPPER DIGITAL SUPPORT FOUND TO BE OUT OF LIMITS. STARTED REMOVING UPPER DIGITAL. REMOVED UPPER DIGITAL SUPPORT. LOCATED, DRILLED NEW DIGITAL SUPPORT AND INSTALLED.SDR RAIA2019020120007Floor Support · corrodedLH FLOOR SILL HAS CORROSION AROUND FASTNER HOLE AT FRAME 61- LH FLOOR WAS FOUND TO BE OUT OF LIMITS. REMOVED DEFECTIVE LH FLOOR SILL. INSTALLED NEW L/H FLOOR SILL F/S 61.SDR RAIA2019020120006Floor Support · corrodedRH FLOOR SILL HAS CORROSION FROM FRAME 33 THRU 35 RH- R&R RH FLOOR SILL AT FR 33 TO 35.SDR RAIA2019020120005Floor Support · corrodedLH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 26- REMOVED FLOOR SILL, LOCATED HOLES IN NEW FLOOR SILL AND INSTALLED EXCEPT FWD & AFT SILL SPLICE. SEE NRWO 22270-616 FOR FWD SPLICE. INSTALLED AFT FLOOR SILL SPLICE.SDR RAIA2019020120004Floor Support · corrodedLH FLOOR SILL HAS CORROSION FROM FRAME 19 THRU 23- R&R LH FLOOR SILL FROM FRAMES 19-23.SDR RAIA201901220003Door Sill · corrodedLT FLOOR SILL HAS CORROSION FROM FRAME 33 THRU 35 LT. REMOVED & REPLACED LT FLOOR SILL FROM FR 28-35.SDR RAIA201901220002Door Sill · corrodedRT FLOOR SILL HAS CORROSION BETWEEN FRAME 37 & 38. R&R RT FLOOR SILL BETWEEN FR 37 & 38.SDR RAIA201901220001Angle · crackedLT OMEGA BEAM I/B LOWER SPLICE ANGLE IS CRACKED BETWEEN FR 16 & 17. REMOVED & REPLACED SPLICE ANGLE.SDR RAIA2019020410004Shear Tie · crackedMAIN CABIN FRAME 16 SHEER CLIP IS CRACKED AT STR 15 RH- REMOVED SHEER CLIP. INSTALLED SHEER CLIP AT FR 16 STR 15R.SDR RAIA2019020410003Shear Tie · crackedMAIN CABIN FRAME 15 SHEER CLIP IS CRACKED AT STR 15 RH- REMOVED SHEER CLIP AT FR15 STR15R. DRILLED UP NEW CLIP, INSTALLED WET RIVETS THRU SKIN AND FUSELAGE, NEEDS 2 STRINGER RIVETS INSTALLED. INSTALLED 2 RIVETS THROUGH THE STRINGER FROM THE SHEER CLIPSDR RAIA2019020410002Skin · gougedFUSELAGE SKIN LH SIDE HAS GOUGE INSIDE PYLON ACCESS PANEL 414DB- REMOVED EXISTING DOUBLER FROM FUSELAGE SKIN, REMOVED POUGE AND DAMAGE FROM SKIN, BEGAN FABRICATING DOUBLER. CONTINUED FABRICATING DOUBLER, MAPPING AND LOCATING HOLES, ALODINE AND PRIMED DOSDR RAIA201902010001Skin · gougedFUSELAGE SKIN HAS DEEP GOUGES INSIDE OF PYLON ACCESS PANEL 424DB- REMOVED THE #2 ENG BLEED VALVE IN THE R/H PYLON & THE BLEED DUCTS. FABRICATED DOUBLER & FILLER & REMOVED DAMAGE FROM FUSELAGE IN R/H PYLON ACCESS PANEL 424DB. INSTALLED REPAIR DOUBLER &SDR RAIA201902010004Door · crackedFWD ACCESSORY DOOR 123BL IS CRACKED UNDER HINGE BRACKET- CUT OUT DAMAGE, FITTED, FABRICATED PARTS. CUT OUT 3 CRACKS, REPAIRED AREA.SDR RAIA201901200003Shear Tie · crackedAFT CARGO FRAME 72 SHEER CLIP IS CRACKED AT STR 15L. REMOVED AFT CARGO FR 72 SHEAR CLIP AT STR 15L. INSTALLED SHEAR CLIP AT FRAME 72 STR 15L.SDR RAIA201901200002Fitting · crackedAFT CARGO FRAME 65 SHEAR CLIP IS CRACKED AT STGR 16L. REMOVED & REPLACED CRACKED SHEAR CLIP FS 65 STR 16L.SDR RAIA201703310001Duct · unsecureNR 2 BLEED LEAK DURING CLIMB OUT. R & R THE BLEED AIR DUCT AND BOTH CLAMPS FWD OF THE VALVE IN NR 2 PYLON IAW AMM 36-11-05. OPS CHECKED GOOD.SDR ASOA20150722037Light · inoperativeDURING ROUTINE MAINTENANCE, THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT OVERWING EMERGENCY LIGHT ASSY. OPS CHECKS WERE GOOD.SDR ASOA20150514026Charger · inoperativeDURING MX INSPECTION THE RT & LT OVERWING AND AFT AISLE EMERGENCY LIGHTS WERE INOPERATIVE. MX R & R THE NR 4 BATTERY CHARGER AND INVERTER WITH OPS CHECKS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150319020Sign · no testTHE CREW REPORTED MIDDLE EMERGENCY LIGHT WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AFT AISLE EXIT LOCATION SIGN. OPS CHECKS WERE GOOD.SDR ASOA20140525046O-Ring · leakingCREW REPORTED FUEL VENTING FROM RT WING DURINHG FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE O-RING ON FITTING FOR VENT RELIEF VALVE ON RT WING. OPS CHECKS WERE GOOD. NO LEAKS FOUND.SDR ASOA20130819214Frame · corrodedDURING C-CHECK, FR 65 HAS CORROSION BETWEEN STR 16 - 17L. REPAIRED FR 65 IAW EC5310-01505. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130819213Skin · corrodedDURING C-CHECK, BAGGAGE DOOR UPPER CUTOUT HAS CORROSION BETWEEN 65-66. REPAIRED BAGGAGE DOOR UPPER CUTOUT IAW EC5310-01718. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130819212Skin · corrodedDURING C-CHECK, INTERNAL SKIN CORRODED AT FR 16-17, STR 21L-21R. REPAIRED SKIN IAW EC5320-01829. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130819211VFloor Support · corrodedDURING C-CHECK. RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EC5320-01443. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130819210VFloor Support · corrodedDURING C-CHECKK, RT OMEGA BEAM HAS CORROSION BETWEEN FR 59-61. REPAIRED RT OMEGA BEAM IAW EC5310-01473. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130611330Floor Support · corrodedDURING C-CHECK INSPECTION, CORROSION WAS FOUND AT THE LT FLOOR SUPPORT AT FR 18 THRU FR 23. CORRROSION WAS BLENDED TO OUT OF LIMITS. R & R IAW SRM 51-40-02 AND SRM 51-21-01.SDR ASOA20130611329Sill · corrodedDURING C-CHECK, CORROSION WAS FOUND AT THE AFT SERVICE DOOR SILL AROUND THE SCREW HOLES. MX BLENDED OUT THE CORROSION AND REPAIRED THE AREA AND INSTALL FABRICATED PART IAW SRM 53-21-10 AND CPM 51-21-06.SDR ASOA20120515075Control Module · inoperativeDURING PREFLIGHT INSPECTION THE CREW REPORTED SMOKE IN THE CABIN ABOVE SEAT 1A. CONTRACT MX INSPECTED THE ACFT AND R & R THE CABIN LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120313002Charger · inoperativeDURING SCHEDULED MX INSPECTION, COCKPIT AND FORWARD LT OTBD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120104002HConnector · corrodedDURING CRUISE, CREW RECEIVED DAU MISCOMPARE WITH BAGGAGE FIRE DETECTION WARNING MESSAGES. CREW ELECTED TO DISCHARGE CARGO COMPARTMENT FIRE BOTTLES IAW QRH AND DIVERTED, ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE DAU COMPUTER AND FOUND THE CARGO COMPARTMENTSDR ASOA2011112510004Control Unit · faultyFLT NR 4163 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON SHORT FINAL. MX INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPS CHECKED GOOD.SDR C2XA11IA186Connector · dirtyIAH - FLIGHT 2511, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESASAGE EICAS MESSAGE ON FINAL APPROACH DURING GEAR EXTENSION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE CLEANED THE CONNECTORS ON THE WEIGHT ON WHEELS PROXIMITY SENSORS, OPERSDR C2XA11IA184Warning System · false activationIND - FLIGHT 2298, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON APPROACH TO IND. THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH WHERE IT AGAIN LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL CHECKS OF THE AIR GROUND SYSTEM, WITH NO DESDR C2XA11TY126Support Bracket · corrodedLT LOWER SUPPORT BRACKET FOR AILERON DISCONNECT CORRODED AT SKIN. REMOVED AND REPLACED BRACKET IAW EMB 145XR SRM 51-40-02.SDR C2XA11TY122Sill · corrodedCARGO CUTOUT THRESHOLD HAS AREAS OF CORROSION. REMOVED AND REPLACED DOOR SILL IAW EMB 145XR SRM 51-40-02.SDR C2XA11SH051Proximity Switch · inoperativeOKC FLIGHT 6017 AC N31131 LG AIR/GND FAIL/MX FERRY TO SHV FOR REPAIRS/LP 2735979. MFY TO SHV FOR REPAIR. MAINTENANCE ADJUSTED RT MLG PROX TARGET. REMOVED AND REPLACED NLG PROX SWITCH IAW EMB-145 AMM 32-60-00 AND 32-61-01. OPERATIONAL CHECK GOOD. AIRCRAFT SDR C2XA10IA030Antenna · inoperativeTUL - FLIGHT 2415, THE CREW REPORTED THAT ON APPROACH INTO MCI THE ILS SYSTEM WAS INOPERATIVE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE ILS ON MEL 34-32-00/1 AND THE AIRCRAFT WAS APPROVESDR C2XA10IA029Antenna · inoperativeTUL - FLIGHT 2415, THE CREW REPORTED THAT ON APPROACH INTO MCI THE ILS SYSTEM WAS INOPERATIVE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE ILS ON MEL 34-32-00/1 AND THE AIRCRAFT WAS APPROVESDR C2XA09IA297Warning System · malfunctionedIAH - FLIGHT 2238, THE CREW REPORTED RECEIVING TWO BRIEF EMERGENCY LIGHTS NOT ARMED MESSAGES DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, FUNCTIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THESDR C2XA09IA202Switch · misalignedIAH - FLIGHT 2581, THE CREW REPORTED A BAGGAGE DOOR OPEN INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT VERIFIED THE DOOR AS CLOSED AND PLACED THE INDICATION ON MEL. ON 08/12/09 MAI
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