N830BX, cancelled Apr 14, 2014
Service difficulty reports · 177
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 = 'N830BX' AND deregistration_id = 'N830BX-2014-04-14' 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 = 'N830BX' AND deregistration_id = 'N830BX-2014-04-14' 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 IXXA11SMN094SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR LOWER SKIN PANEL DENTED AT SEVERAL POINTS AT STA XE 246.000 - XH 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PESDR IXXA11SMN093SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 52-2-0, SRM SDR IXXA11SMN092SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR UPPER SKIN DENTED AND CRACKED AT STATION XE 246.000 - 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED RT SDR IXXA11SMN091SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER T/E UPPER SKIN CORRODED AT STA XE 29.000 - 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INNER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMEDSDR IXXA11SMN090SWeb · wornDURING ROUTINE C-CHECK INSP FOUND NR 3 ENGINE THRUST REVERSER RT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR SDR IXXA11SMN089SWeb · wornDURING ROUTINE C-CHECK INSP, FOUND NR 3 ENGINE THRUST REVERSER LT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAISDR IXXA11SMN088SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING UPPER SKIN CORRODED AT STA XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0,SDR IXXA11SMN086SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E PANEL CORRODED AT STATION XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0, SRM 51-3-0, SRM 51-1-8B, SRMSDR IXXA11SMN085SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD BATHTUB FITTING CRACKED AT STA 680.000, LONGERON 9 RT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D SDR IXXA11SMN084SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 798.000, LONGERON 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING SRM 51-1-20D, SRM 51-1-0, SRM 51-1-8B, SRM 51-1-20D,SDR IXXA11SMN087SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT OTBD FLAP UPPER EXTERNAL SKIN DENTED AT SEVERAL POINTS AT STA XF 415.000 - 440.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLESDR IXXA11SMN083SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT WING FLAP LINK SUPPORT LT SIDE CRACKED AT STA XF 409.000. REMOVED HINGE CRACKED SUPPORT FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW HINGE SUPPORT FITTING IAW S/B 27-249, REV 1, SRM 51-3-0, SRM 51-1-21, SRM SDR IXXA11SMN082SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 879.375. REMOVED CRACKED FRAME FITTING. FABRICATED NEW FITTING, SPLICERS, SHIMS AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING, DOUBLER, SPLISDR IXXA11SMN081SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND, IMPROPER REPAIR AT FWD BASKET DOOR OPENING FWD CTR LIP AT STATION FS 290, LONGERON 34.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIRSDR IXXA11SMN080SStrap · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND NLG WHEEL WELL LT TUNNEL COMPARTMENT STRAP CORRODED AT STA 8.000. REMOVED CORROSION. REMOVED DAMAGED STRAP SEGEMENT. FABRICATED STRAP SEGMENT AND SPLICE. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NSDR IXXA11SMN079SSupport Fitting · crackedDURING ROUTINE C-CHECK INSP FOUND NR 1 ALT TANK NR 6 FUEL PROBE FITTING SUPPORT CRACKED. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.SDR IXXA11SMN078SAngle · crackedDURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON INTERNAL ANGLE CRACKED AT STATION YN 321.397 AND STA XRS 495.665. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR ANGLE, STRAP DOUBSDR IXXA11SMN077Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND RT MLG WHEEL WELL DOG HOUSE FITTING CRACKED AT STA 855.000, RT BOTTOM LINE 46. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-8B, SRM 51-1-0, SRM 51-3-0 AND SRM SDR IXXA11SMN076SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAWSDR IXXA11SMN075SStructure · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR AT SMALL DRAIN DOUBLER FWD LOWER CENTER FUSELAGE FORWARD OF CENTER EQUIP DOOR AT STA FS 615 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED REPAIR EXISTING REPAIR. FABRICATED REPAIR DOUBSDR IXXA11SMN072SSkin · misrepairedDURING ROUTINE C-CHECK INSP FOUND IMPROPER DOUBLER REPAIR AT LT FWD FUSELAGE EMERGENCY EXIT DOOR AT STA FS 404 LONGERON 15.5 LT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR DOUBLER. INSTALLED NEW FASTENERS ANDSDR IXXA11SMN071SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTUIN FOUND IMPROPER DOUBLER REPAIR AT RT FWD FUSELAGE EMERGENCY EXIT DOOR AT STATION FS 392, LONGERON 16.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, SDR IXXA11SMN070SSkin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND IMPROPER DOUBLER REPAIR, RT FWD FUSELAGE, 2 WINDOWS FWD OF EMERGENCY EXIT DOOR AT STATION FS 300 LONGERON 16 RT. REMOVED EXISTING REPAIR. FABRICATED REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLESDR IXXA110035OControl Cable · out of rigDURING LEVEL OFF, NR 3 ENGINE COMPRESSOR STALLED WHEN THROTTLES WERE RETARDED,(N1-93 PERCENT, N2-91 PERCENT, F/F-3100, OAT-44 DEGREES AND M-.80/300KIAS). THE CREW DIVERTED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED TROUBLESHOOTING TREE NR 41, RERIGGED VSV AND SDR IXXA110022SSkin · dentedDURING PREFLIGHT FOUND LT SIDE BELLY SKIN TO BE (DENTED AND CRACKED) AT STA 55 BETWEEN 15" TO 19.2500" FROM CTR LINE. OPENSDR IXXA110008OInstrument Panel · unsecureDURING TAKEOFF ROLL AT 68 KTS THE F/O INSTRUMENT PANEL SLID OUT. THE TAKEOFF WAS ABORTED AND THE CREW RETURNED TO PARKING. MX SECURED THE F/O INSTRUMENT PANEL AND PERFORMED THE REJECTED TAKEOFF INSP. THE ACFT WAS RETURNED TO SERVICE IAW MM 31-10-2 AND MM 13SDR IXXA100046OSteering Sys · inoperativeDURING TAKEOFF, F/O HAD NO RESISTANCE IN RUDDER PEDAL AND NO NOSE WHEEL STEERING. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED THE F/O RUDDER PEDAL ASSY, OPS CHECK GOOD IAW MM 27-23-28, 27-20-03 AND 27-23-29. ACFT WAS SDR IXXA090060OConnector · dirtyDURING CRUISE, THE RT BLEED VALVE'S DO NOT SHUT OFF INDIVIDUALLY, BUT WHEN THEY ARE SHUT OFF PRESSURE DROP'S TO 10 PSI, MANIFOLD TEMP IS 10 TO 20 DEGREE CELSIUS, RT PACK SEEMS TO BE INOPERATIVE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX CLESDR IXXA090057OFuel Filter · cloggedDURING CLIMB OUT NR 1 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED FLAME OUT IN FLIGHT START CHECKLIST. THE NR 1 ENGINE STARTED ALL PARAMETER NORMAL. CREW LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 51 AND REPLACED ENGINE FUEL FILTER. OPSDR IXXA090027OMechanism · dirtyAFTER TAKEOFF AND GEAR RETRACTION FROM KDFW, A SEVERE VIBRATION WAS FELT IN THE NOSE GEAR AREA. THE CREW RECYCLED THE LANDING GEAR AND THE CONDITION PERSISTED. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. MAINTENANCE OBSERVED THE LEFT NOSE GEAR DOSDR IXXA090006ODetector · malfunctionedDURING CRUISE FROM KLAX, NR 4 ENGINE FIRE WARNING ILLUMINATED. THE CREW PERFORMED COM EMERGENCY PROCEDURES, THE CREW DISCHARGED NUMBER ONE FIRE BOTTLE, AFTER TWO MINUTES FIRE WARNING ILLUMINATED AGAIN AND DISCHARGED NR 2 FIRE BOTTLE. THE CREW SHUT NR 4 ENGINSDR IXXA090004OConnector · contaminatedDURING CRUISE FROM KTOL NR 4 ENGINE FIRE WARNING INTERMITTENTLY GOING OFF, THEN CAME ON STEADY. THE CREW SHUTDOWN NUMBER FOUR ENGINE, LIGHT IN HANDLE REMAINED ON UNTIL FL 18,000 ON DESCENT. THE CREW DISCHARGED BOTH FIRE BOTTLES. THE CREW LANDED IN KDEN WITHSDR IXXA080036OComputer · defectiveDURING CLIMB-OUT OF KTOL WITH RUDDER POWER ON, YAW DAMPER ON AND AUTO PILOT ON THE RUDDER HAD A LEFT RUDDER INPUT. THE CREW TURNED THE AUTO PILOT OFF AND THE CONDITION REMAINED, TURNED THE YAW DAMPER OFF AND NO CHANGE. THE LEFT INPUT WENT AWAY ONLY WHEN RUDDSDR IXX2008F00109Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LOWER AFT FUSELAGE BELLY FWD OF AFT BASKET DOOR HAS IMPROPER REPAIR AT STA FS1142 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTSDR IXX2008F00104Skin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER AFT PANEL CORRODED AT STA XF 195.963. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PART AS NEESDR IXX2008F00116Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND RT OTBD FLAP EXHAUST GATE LOWER SKIN HAS IMPROPER REPAIR. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FSDR IXX2008F00114Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND LT AFT CORNER OF A PIT DOOR OPENING HAS IMPROPER REPAIR AT STA FS340, LONGERON 31 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAISDR IXX2008F00112Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND RT OTBD FLAP LOWER SKIN HAS IMPROPER REPAIR AT STA XF 238.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEWSDR IXX2008F00115Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND AFT LOWER FUSELAGE AFT OF OUTFLOW VALVE HAS IMPROPER REPAIR AT STA FS1688, LONGERON 35.75 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NOSDR IXX2008F00111Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND FWD LWR FUSELAGE AFT OF AFT ADF ANTENNA HAS IMPROPER REPAIR AT STA FS 172 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK AND NSDR IXX2008F00101Skin · misrepairedDURING ROUTINE C-CHECK, FOUND DOUBLER FWD OF A-PIT DOOR ON LWR CENTERLINE, HAS IMPROPER REPAIR AT FS220, LONGERON 36. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CRACK, NO CORROSION FOSDR IXX2008F00117Fitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.00-1060.000 LONGERON 31 RIGHT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRSDR IXX2008F00113Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN HAS IMPROPER REPAIR AND AT STA XF420.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PSDR IXX2008F00110Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.000-1060.000 LONGERON 31 LT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED, ASDR IXX2008F00105Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING UPPER SKIN CRACKED AT STRINGER 8 STA XW 408.00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFOMRED NDT INSP. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLESDR IXX2008F00103Skin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E UPPER SKIN DENTED AT STA SFS 120.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER, ANGLES, FILLER, AND FAIRING. PERFORMED HEAT TREATMENT TO REPAIR ANGSDR IXX2008F00102Skin · misrepairedDURING ROUTINE C-CHECK, FOUND LWR FWD FUSELAGE BELLY AFT OF FWD BASKET DOOR HAS IMPROPER REPAIR AT STA FS403, LONGERON 35.5 LT. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, REPAIRSDR IXX2008F00100Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND LT FWD FUSELAGE AFT AND BELOW EMERGENCY EXIT DOOR HAS IMPROPER REPAIR AT FS 447 LOGN 25.5 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNAL SDR IXX2008F00099Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND AFT LOWER FUSELAGE AFT AND BELOW L-2 AND R-2 DOORS HAS IMPROPER REPAIR AT STA FS 1695, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. REPASDR IXX2008F00107Seat Track · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND P-1-5 SEAT TRACK DAMAGED. REMOVED DAMAGED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED, AND PRIMED AREA AND SPLICES. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-7-1, FIG 4, SHEET 1 ITEM C, SRM 51-2-0,
Back to N830BX, cancelled Apr 14, 2014