N482UA
Service difficulty reports · 137
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 = 'N482UA' 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 = 'N482UA' 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 CALA2021082701436Seat Track · corroded(A3NB-53-3-6040) CORROSION AT MAIN CABIN SEAT TRACK FR20-FR22 Y- 1292. DOT NO. 17-10() REMOVED SEAT TRACK LOCATED AT FR20-FR22 DAMAGE BLENDED IAW SRM 5 1-73-00 BLENDED AREA MEASURED L=2.0" X W=1.5" X D=0.060" ORIG TH ICKNESS 0.087" REMOVED MATERIAL 0.060" REMASDR CALA2021082701435Floor Support · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y1292 FR68 CORRODED.(DOT 38-27)() REPLACED FLOOR SUPPORT P/N: D5347218820400 BTCH: 0002716528 IAW A320 SRM 51-42-11 AND SRM 51-72-11-911-001. ATTACHED FORMS 46-00 24 AND 44-0008. EMP# V934700 WORK ACCOMPLISHED AT ST ENGISDR CALA2021082501433Floorbeam · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y1292 FR68 CORRODED.(DOT 38-27)() REPLACED FLOOR SUPPORT P/N: D5347218820400 BTCH: 0002716528 IAW A320 SRM 51-42-11 AND SRM 51-72-11-911-001. ATTACHED FORMS 46-00 24 AND 44-0008. EMP# V934700 WORK ACCOMPLISHED AT ST ENGISDR CALA2021082501426Floorbeam · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y765 HAS CORROSION AT FR 66.(DOT 38-39)() AFTER CHECKING THE DAMAGE IS OUT OF LIMITS CORROSION IN HARD POI NT EXCLUDED AREA IAW SRM 53-00-14-283-002 FIG 00, REMOVED DAMAGE AREA IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPOSDR CALA2021082301404Floorbeam · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y1292 FR68 CORRODED. (D OT 38-33)() REPLACED FLOOR SUPPORT P/N:D5347218920400 BETWEEN FR68-69 AND -Y 1292 IAW SRM 51-72-11. ATTACHED FORM 44-008. EMP#V934611 WORK AC COMPLISHED AT ST ENGINEERING MOBILE AT BFM ON NR#0013SDR CALA2021082301403Floor Support · corroded(A3NB-53-3-6185)-Y1292 FLOOR BEAM FR66-68 HAS MULTIPLE CORROSION SPOTS. (REMOVE DAMAGE, CHECK LIMITS) REPLACED FLOOR SUPPORTS P/N:D5347220924500 AND P/N:D534721722050 0 BETWEEN FR64-FR68 AND -Y1292 IAW SRM 51-72-11.SDR CALA2021082301402Floor Support · corroded(A3NB-53-3-6040) CORROSION AT MAIN CABIN FLOOR SUPPORT FR16 Y765 . DOT NO 17-15() REMOVED AND REPLACED FLOOR SUPPORT P#5311281300251 AT MAIN CABIN Y765 FR12-24 IAW SRM 51-42-11.SDR CALA2021082301399Floorbeam · corroded(A3NB-53-3-6040) CORROSION AT MAIN CABIN FLOOR SUPPORT FR 16 BET WEEN Y254 & Y765. NO REWORK ALLOWED IAW SRM 53-11-14-283-007 FIG 005 NOTE 3 REMOVE D DAMAGE AREA IAW SRM 51-42-11 RECEIVED NEW PART P/N 53112826002 00 BIN0002961235 INSALLED NEW PART IAW SRM 51-4SDR CALA2021082001390Floor Support · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y765 HAS CORROSION AT FR 66.(DOT 38-39)() AFTER CHECKING THE DAMAGE IS OUT OF LIMITS CORROSION IN HARD POI NT EXCLUDED AREA IAW SRM 53-00-14-283-002 FIG 00, REMOVED DAMAGE AREA IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPOSDR CALA2021082001389Seat Track · damagedA3NB-53-3-6185 MAIN CABIN SEAT TRACK Y7652 HAS CORROSIVE MATERIA L UNDER PAINT AND GOUGES BETWEEN FR52 AND FR54.(DOT 38-42)() REMOVED CORROSION AND GOUGE END FOUND WITHIN ALLOWABLE DAMAGE IA W SRM 51-74-00 AND 53-41-15-283 FIGURE 001CHECK LIMITS CORROSION L=3.SDR CALA2021082001388Seat Track · damagedA3NB-553-3-6185 MAIN CABIN SEAT TRACKY765 HAS GOUGES BETWEEN FR5 2 AND FR53.(DOT 38-44)() REMOVED GOUGE AND FOUND WITHIN ALLOWABLE DAMAGE IAW SRM 53-41-15 -283-002 FIGURE 001 CHECK LIMITS 51-73-00 L=2.525" W=0.745" D=0. 005" TRT92925 TRT14717 RESTORED SURFACE SDR CALA2021082001387Seat Track · damagedA3NB-53-3-6185 MAIN CABIN SEAT TRACK Y765 HAS GOUGES BETWEEN FR5 1 AND FR52. REMOVED GOUGE AND FOUND WITHIN ALLOWABLE DAMAGE IAW SRM 53-41-15 -283-002 FIGURE 001 CHECK LIMITS L=2.020" W=0.800" D=0.006" TRT2 925 TRT14717. SRM 451-73-00 RESTORED SURFACE PROTECSDR CALA2021082001384Fitting · corrodedA3NB-53-3-6185 MAIN CABIN LH AFT DOOR SILL AT Y1732 FR68 FLOOR SUPPORT ANGLE AND FILLER CORRODED.(DOT38-28)() REMOVED REPAIR ANGLE IAW SR, 51-42-11. FABRICATED NEW REPAIR ANG LE AND FILLER TRAVELER #2111567542 FILLER MATERIAL ID:7075T6 371 " B/N3288578 LOCATORSDR CALA2021082001383Floor Support · damagedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y765 FR68 UPPER SURFACE DAMAGED. (DOT 38-31)() REPLACED FLOOR BEAMP/N: D5347219220000 BATCH: 0002716632 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001.SDR CALA2021081801373Floor Support · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y1292 FR68 CORRODED. (D OT 38-33)() REPLACED FLOOR SUPPORT P/N:D5347218920400 BETWEEN FR68-69 AND -Y 1292 IAW SRM 51-72-11. ATTACHED FORM 44-008. EMP#V934611 WORK AC COMPLISHED AT ST ENGINEERING MOBILE AT BFM ON NR#0013SDR CALA2021081801372Floor Support · corroded(A3NB-53-3-6185)-Y1292 FLOOR BEAM FR66-68 HAS MULTIPLE CORROSION SPOTS. (REMOVE DAMAGE, CHECK LIMITS) REPLACED FLOOR SUPPORTS P/N:D5347220924500 AND P/N:D534721722050 0 BETWEEN FR64-FR68 AND -Y1292 IAW SRM 51-72-11. ATTACHED FORM 4 4-0008 EMP# V934611 WORK ACCSDR CALA2021081801370Floor Support · corroded(A3NB-53-3-6040) CORROSION AT MAIN CABIN FLOOR SUPPORT FR16 Y765 . DOT NO 17-15() REMOVED AND REPLACED FLOOR SUPPORT P#5311281300251 AT MAIN CABIN Y765 FR12-24 IAW SRM 51-42-11. FORM 44-0008 ATTACHED EMP#V93434 0 WORK ACCOMPLISHED AT ST ENGINEERING MOBILE AT BSDR CALA2021081801360Floor Support · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y1292 CORROSION AT FR66. (DOT 38-38)() REPLACED FLOOR BEAM P/N D5347204001000 BATCH 0003777934 IAW A320 SRM 51-42-11 AND SRM 51-72-11-911-001.SDR CALA2021081801359Floor Support · corrodedA3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT Y254 HAS CORROSION FROM FR68 TO FR70 (DOT 38-32)() REPLACED MAIN CABIN FLOOR SUPPORT Y254 FROM FR68-FR70. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14-283-002 FIG.1 MEASURED AT L=3. 0" X W=1.5" X D=0.031" T14905.SDR CALA2020021200408Display · fumesON DESCENT CAPT DISPLAY WENT BLANK ACCOMPANIEDBY ELECTRICAL FUME S.TURNED DISPLAY OFF REPLACED CAPT DISPLAY PER AMM 31-63-22-000-001-A. OPS CHECKS GOOD. UPDATED PART REMOVAL RECORD ROTABLE PARTS CHANGE WAS INDICATED - TT # 1057943 SN OFF 6351 DISPLAY, CRT EC SDR CALA2019121902238Stiffener · corrodedINTERNAL FUSELAGE, JUST FWD OF THS ACCESS HOLE 312AR, FR71 STIFF ENER HAS CORROSION (A3NB-53-4-6229) PER HAECO LCQ NR#9290209 GEN ERATED BY N078570 REMOVED AND REPLACED STIFFNER IAW A320 SRM 51-42-11-801-PAR 6 & P6-8SDR CALA2019121702223Fitting · crackedR/H MLG DOOR FWD HINGE FITTING FWD LUG FWD FACE PRODUCED CRACK I NDICATIONS DURING HFEC INSPECTION AD 2015-02-14 PER HAECO LCQ NR #9290234 GENERATED BY: V061690. REMOVED CRACKED FITTING, DRILLED AND INSTALLED NEW FWD RMLG HING E FITTING IAW AIRBUS REPAIR INSTRSDR CALA2019032500467Slide · unserviceableL2 DOOR SLIDE NEEDS TO BE REPLACED. REMOVED L2 SLIDE IAW 25-62-44-000-010-A. REPLACED L2 DIAPHRGRAM IN THE PERCUSSION MECHANISIM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER OF THE PASSENGER DOOR IAW 52-10-00-610-001-A. PERFORMED STEPS UP TO AND INCLUDISDR CALA2017042101082Power Supply · inoperativeAFT CABIN EMERGENCY LIGHTS INOP. REPLACED EPSU REF AMM 33-51-38-000-001-A AND IPC 33-51-38-01B. OPS CHECK GOOD.SDR CALA2017021300365Unknown · malfunctionedEMERGENCY EXIT LIGHTS KEEP FLICKERING AT GATE IN ARM POSITION WITH EXTERNAL POWER CONNECTED WHEN I ARRIVED ON AIRCRAFT, EMERGENCY LIGHTS WERE NO LONGER FLICKERING. CYCLED EMERGENCY LIGHT SWITCH IN COCKPIT, OPS CHECKED GOODSDR CALA2016022495132Fire Bottle · dischargedAFT CARGO DET FAULT DISPLAYED ON UPPER ECAM SCREEN, SHOWING AFT CARGO SMOKE DISCHARGE AGENT 2 DISPLAYED. INSPECTION FOUND SECURE. REPLACED FWD CARGO FWD BOTTLE IAW AMM 26-23-00-200-005-A SEE PTT 5002010.SDR CALA2015012393017Epsu · faultedEMERGENCY LIGHT FAILED TEST, FAULTS CTR LT EPSU. REPLACED CTR LT EPSU & BATTERY IAW AMM 33-51-38, TESTED OK.SDR CALA2014071191445Structure · crackedRIGHT WW SIDE BOX FLANGE CRACKED AFT SIDE OF FASTENER JUST FWD OF FRAME 43. REPAIRED RT WW SIDE BOX FLANGE CRACK IAW ECRA 5330-04874. NO SRI INSPECTION IS REQUIRED IAW ECRA.SDR CALA2014071191444Beam · crackedLEFT MLG WW SIDE BOX BEAM FLANGE CRACKED AFT SIDE OF FASTENER, JUST FWD OF FRAME 43. REPAIRED THE CRACK ON LT WW SIDE BOX BEAM FLANGE JUST FWD OF FRAME 43 IAW ECRA 5330-04874. NO SRI INSPECTION REQUIRED IAW ECRA.SDR CALA2014071191419Stringer · corrodedSTRINGER 42L CORRODED IN AFT PIT AFT OF FRAME 56. REMOVED CORRODED SECTION OF STRINGER & REPLACED WITH A NEW STRINGER. FABRICATED NEW STRINGER SPLICE & INSTALLED. REPAIR REQUIRES SRI INSPECTION. FIRST INSPECTION DUE AT 60000FC & 75000FH AFTER REPAIR EMBODIMSDR CALA2014071191418Stringer · corrodedSTRINGERS 41L & 42L CORRODED IN AFT CARGO COMPARTMENT BETWEEN FRAME 63 & 64. REMOVED CORRODED SECTIONS OF STRINGERS & REPLACED WITH NEW STRINGERS. FABRICATED NEW STRINGER SPLICES & INSTALLED. REPAIR REQUIRES RE-INSPECTION. FIRST INSPECTION DUE AT 60000FC ASDR CALA2014071191417Stringer · corrodedAFT CARGO JUST AFT OF FRAME 56 STRINGER 40 CORROSION STRINGER. REMOVED DAMAGED SECTION OF STRINGER 40L & FRAME 56. FABRICATED & INSTALLED STRINGER SPLICE REPAIR. REPAIR HAS SRI AT 60000 FC & 7500 WITH SUBSEQUENT INSP & METHOD TBD.SDR CALA2014071191416Door Sill · corrodedCABIN R2 DOOR SILL FRAME 66 HAS EVIDENCE OF CORROSION. R & R R2 DOOR SILL AT FRAME 66 - 68 IAW SRM51-42-11. NO SRI INSPECTION NOTED.SDR CALA2014071191415Skin · saturatedRIGHT UPPER SKIN SHOWS SIGNS OF WATER INGRESS AT 101 INCHES FROM INBD END 5 INCHES FROM TE 7 INCHES IN DIAM. REPAIRED IAW SRM 55-21-11 RPR 5 E PARA 2 A - B CONFIG 1 FIG 205. THIS REPAIR REQUIRES INSPECTION IAW SRI 55-21-11-2-002-00 TABLE 203. FIRST INSPECTISDR CALA2014071191414Skin Panel · saturatedRIGHT ELEVATOR UPPER SKIN PANEL HAS A WATER INGRESS INDICATION AT 39 INCHES FROM INBD END 6 INCHES FROM TE 6 INCHES IN DIAM. DRILLED WITNESS HOLES, CUT OUT 28.26 SQ INCHES OF SKIN. REMOVED WATER & APPLIED A NEW CORE PLUG. THIS REPAIR REFERS TO IIR 55-21-11-SDR CALA2014042190875Fan · failedSMOKING ELEC BURNING SMELL REPORTED BY FLIGHT ATTENDANT AT ROW 6 - 7 & 1L. CABIN FAN FAULT INDICATION ON COND AIR PAGE ON LOWER ECAM SYS PAGE. BREAKER FOR RT FAN SUPPLY POPPED. OPERATIONS CHECKED RT FAN LOUD GRINDING HEARD & BREAKER POPPED AGAIN. VERIFIED RTSDR CALA2013123094000Light · inoperativeFROM ROW 22 AFT NO EMERGENCY LIGHTS. EMERGENCY LIGHT TEST SHOWED NO FAULTS.SDR CALA2013123094023Contactor · faultyCOMPLETE LOSS OF ELECT PWR & AFTER PUSH DURING ENG 1 START. WITH BAT ON NO CAPTS RADIO NO GREEN IND ON GEAR. REPLACED 6-PD-2 CONTACTOR IAW MM 24-38-55-000-001-A. OPERATIONS CHECKED GOOD ALL POWER FUNCTIONS OPERATE NORMAL. OPERATES GOOD ON APU & GND SERVICESDR CALA2013120993541Unknown · unknownEMERGENCY EXIT LIGHTS ILLUMINATED ON GND WITH SWITCH IN ARM. IAW AMM 23-73-00, WITH THIS AIRCRAFT AFFECTIVITY, NS SWITCH IN AUTO, LANDING GEAR DOWN & LOCKED, THE EXIT SIGNS WILL BE ILLUMINATED.SDR CALA2013120993542Warning System · false activationSDCU CLASS 2 ON LOWER ECAM. ACCOMPLISHED TSM 26-17-00 -810-802-A RESET BREAKERS C06 & T18. NO GND FAULTS NOTED & ALL SMOKE DETECTOR TESTED OK IAW MT 26-002 REV A. NOTE PFR INDICATED FLIGHT PHASE 02 POWER TRANSFER.SDR CALA2013112593215Director · faultySLIDE AT DOOR 2R INDICATES ARMED FROM FLIGHT DECK. FLIGHT ATTENDANT REPORTS SLIDE DISARMED. REPLACED CIDS DIRECTOR 1. CABIN INTERCOM, CIDS DIRECTOR BITE TESTED GOOD, SMOKE DETECTOR FUNCTION TESTED GOOD, OPERATIONS 2R DOOR THRU ARM, DISARMED POSITIONS, INDICSDR CALA2013111492928Fastener · missingFASTENER MISSING PANEL 575KB, UNDER LE LT WING NEAR TIP. REPLACED FASTENER.SDR CALA2013102992459Screw · missingTWO SCREWS MISSING ON PANEL 192KB RT UNDERSIDE OF FUSELAGE. REINSTALLED TWO EACH SCREWS ON PANEL 192KB, OK TO CONTINUE.SDR CALA2013100991876Oxygen Mask · brokenCAPT O2 MASK BROKEN RED INFLATE BUTTON BROKEN. R & R CAPT O2 MASK, OPERATIONS CHECKED GOOD.SDR CALA2013090991100Skin · dentedDENT NR 2 ENGINE OTBD SIDE AT 3 O'CLOCK POSITION MEASURING 1.1 INCH X 2 INCH BY .020 INCH DEEP. INSPECTED DENT FOUND TO BE 1.1 INCH BY 2 INCH BY .020 INCH DEEP WITHIN SRM LIMITS V2500 54-30-FM PG 118 CONFIG 2.SDR UALA2013062604448Extinguisher · dislodgedHALON EXTINGUISHER CAME OUT BRACKET CANNOT RESTOW. SECURED EXTINGUISHER.SDR UALA2013061804225Connector · looseEMERGENCY LIGHTS AT ROW 7, 8, 10 AND ROWS 27 AND 28 FOUND INOP, DURING SERVICE CHECK. DURING TROUBLESHOOTING, FOUND CONNECTORS, CONNECTOR PLUGS UNDER THE SEATS AND SIDE WALLS LOOSE. SAME FIXED AMM. OPS CK GOOD.SDR UALA2013032501833Seal · leakingFWD LAVATORY HAS HOSE LEAK. SHUTOFF WATER AND NO LEAKS NOTED. SINK DRAIN LEAKING AT SEAL BTWN SINK AND THE STOPPER.SDR UALA2013031201454Battery · failedLEFT MID EMERGENCY LIGHT BATTERY FAILED EMERGENCY LIGHT TEST. REPLACED BATTERY IAW MM, TESTED GOOD.SDR UALA2013010700103Wire Harness · damagedFOUND BAD EGT HARNESS 4012KS5 ON NR 1 ENGINE RIGHT SIDE AFT HARNESS BY 'J' BOX. STARTED INSTALLING NEW HARNESS PER MM 77-21-43. INSTALLED J-BOX AND CONNECTED EGT CORE HARNESS. NEED TO CONTINUE WITH CLAMPS & PROBE CONNECTIONS. REPLACED HARNESS & INSTALLED 2
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