N837UA
Service difficulty reports · 139
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 = 'N837UA' 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 = 'N837UA' 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 CALA2026101620404Pump · leakingHYD G ENG 1 PUMP LO PR, HYD G SYS LO PR, GREEN SYS DEPLETED SDR INFO ADDED FOUND AN ACTIVE LEAK WITH HYD PRESSURE OFF ON LINE AT THE TOP OF NR 1 ENGINE OTBD SIDE. JUST BEHIND THE PYLON INTERFACE BRACKET. REPLACED DAMAGED PYLON HYDRAULIC LINE ON #1 ENGINE REF SDR CALA2026041415358Filter · dirtyCABIN RE-CIRCULATION FILTERS NEEDS TO BE REPLACE WITHIN 2 DAYS REF LOG# 8508734 CABIN RE-CIRCULATION FILTERS TO BE REPLACEWITHIN 2 DAYMM 05-51-10-200-801-C1 NO ODOR OBSERVED OR ABLE TS REF AO BE IDENTIFIED BY MX. RECIRC FILTERS REQUIRE REPLACEMENT WITHIN 2 DAYSDR CALA2026030214202Pressure Switch · damagedAFTER RAT FAN BLADE INSPECTION RED LIGHT ACTUATOR PRESSURE LGHT IS ILLUMINATED ON RAT CONTROL MODULE AFTER STOWING RAT ALSO RAT FAULT DISPLAYED ON UPPER ECAM WITH AMBER TRIANGLE DISPLAYED ON HYDRAULICS PAGE. REPLACED RAT ACTUATOR PRESURE SWITCH, LEAK CK OK OPSSDR CALA2026021813891Light · inoperativeEMERGENCY LIGHTS AT SEAT 25C INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-51-19. OPS CHECKED GOOD.SDR CALA2025082608123Fuel Cap · missingRAMP REPORT OF FUEL COUPLING CAP MISSING. RIGHT WING. INSTALLED FUEL CAP IAW AMM 28-25-41-400-005-A, SUB TASK 28-25-41-420-056-C, FROM STEP B2N TO B2Q,SDR CALA2025062505856Slide · faultedPLEASE CHECK THE SLIDE PRESSURE GAUGE AT DOOR 2L AND REPLACE SLIDE IF THE NEEDLE IS IN AREA B CARRIED BY ELB ORIGINAL CYCLES LIMIT OF: 001 EXTENDED BY 001 NEW TIME REMAINING 001. REMOVED AND REPLACED DOOR 2 LEFT EVACUATION SLIDE REF 25-62-44. OPS CHECK SATISDR CALA2025062505855Gauge · no discrepancyFA REPORTS DOOR 2L PRESSURE GAUGE IN RED. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS. INSPECTED GAUGE PER AMM 25-62-00. SLIDE PRESSURE IS WITHIN AMM LIMITS.SDR CALA2025060205157Light · disconnectedSEAT 23ABC EMERGENCY PATHWAY LIGHT FOUND INOP. REPLACED LENS COVER AND RECONNECTED EMERGENCY LIGHT AT SEAT 23ABC PER AIRBUS 319/320 AMM 33-51-19. OPS CHECK GOODSDR CALA2025051404662Bottle · no discrepancyFA REPORTS DOOR 2L SLIDE PRESSURE GUAGE IN RED. INDICATOR NEEDLE IS ONE NEEDLE WIDTH OVER THE GREEN BAND TO THE HIGH SIDE INTO THE RED ALLOWED TEMPERTURE CONDITIONS TO STABILIZE. PRESSURE INDICATION IS IN AREA A BAND. PER AMM TASK 25-62-00-210-001-A. OKAY FOR SDR CALA2025050604498Slide · noneL2 DOOR PRESSURE GAUGE SHOWS OVER PRESSURE SLIDE PRESSURE INDICATION FALLS WITHIN SERVICEABLE LIMITS. REF AMM 25-62-00-210- 001-A.SDR CALA2025032703256Eec · faultedENG 2 COMPRESSOR STALL A T CRZ ALT FL370 ENG 2 STALL ECAM ENG 2 EPR MODE FAULT CREW REPORTED MULTIPLE LOUD BANGS FOLLOWED BY STALL AND EPR MODE ECAM, ENGINE WAS REDUCED TO IDLE & RAN REMAINDER OF FLIGHT AT IDLE. CREW REPORTED ONE MORE LOUD BANG AFTER LANDING PSDR CALA2025020502215Vsv · failedENG2 FAIL ON T/O ROLL. NO INDICATION NOTICED PRIOR TO FAILURE ENG 2 STALL WITH CFDS VSV MECH/BLD VLV/LPC2 REFERENCE TSM 71-00-00-810-809-A, ALSO SUGGEST MCD INSPECTION PER AMM 79-22-45-000-010-A TO DETERMINE ENGINE SERVICEABILITY. TOMC-MEREDITH FLAGGING SDRSDR CALA2025020502214Slide · no testDOOR 2 LEFT SLIDE DID NOT DEPLOY PROPERLY. REMOVED L2 SLIDE IAW AMM 25-62-44/401. INFO ONLY... PER FIRE DEPT, L2 SLIDE DID INFLATE AND 3 PASSENGERS WENT DOWN UNTIL IT DEFLATED AND FLIGHT ATTENDANT KEPT PEOPLE FROM USING IT.SDR CALA2025012802086Sdac · unknownHYD G RSVR OVHT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN . UPDATED MASDR CALA2024101102628Frame · crackedRH FR16 DOUBLE JOGGLE HOLES FOUND CRACKED, REQUIRING PARTIAL FRAME REPLACEMENT AT C CK IN BFM AS NOTED ON N/R''S 110289 &; 110293. 1, PART 1.2 REQUIRES DIP AS FOLLOWS; ACCOMPLISH INITIAL INSPS A ST REV OF ECRA5311-03281 ON/BEFORE ACFT REACHES 37002 TTL FC (FHSDR CALA2024101102627Frame · cracked(SUPPORT TASK) DURING ROTO TEST OF RH FRAME 16 HOLE 6 FOUND CRAC KED IN FRAME LAYER AT THE 3:00 POSITION. REPAIR BEFORE NEXT FLIG HT.() TRANSFERRED REPAIR INFORMATION AND DIP REQUIREMENTS TO LP''S 9509350, 9509474 & 9509861. THIS ITEM CAN BE CLEARED.SDR CALA2024083000521Seal · missingPDA 2 RH OB FLAP IB CUSHION SEAL AND PLATE MISSING FROM AIRCRAFT UPON ARRIVAL. 55SQ IN. UPDATED SDR INFORMATION.SDR CALA2022060101415Hydraulic Line · leakingHYD Y ENG2 PUMP LOPRESSURE PILOT SAID PARKING BRAKE INOP DUE TO LOW PRESS ,FOUND LARGE HYD LEAK UNDER ENG 2 ALSO GREEN SYST HYD AND YELLOW HYD LOW . 29-13-00-810-804-A UPON INSPECTION FOUND HYDRAULIC LINE TO THE HCU AT 12 O CLOCK R/R PER AMM 29-13-51-400-010-SDR CALA2022032800811Accumulator · leakingCREW REPORTS HYD Y RSVR LO LVL MESSAGE. CREW FOLLOWED QRH 130.44 PTU SWITCHED OFF AND ENG 2 HYD PUMP SWITCHED OFF. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V928786 PLEASE CSDR CALA2022022800520Reservoir · noneABOUT/40 MINT AFTER T/OGOT G RSVR OVHT ECAM.WHEN OVHT OUT G ENG PUMP+ PTU ON GOT AIRFRM.FLIGHT CREW TURNED THE GREEN HYD ENG PUMP AND THE PTU BACK ON. AND GREEN HYD SYSTEM OVERHEAT DID NOT COME BACK ON. SEEMED SUSPICIOUS. WITH LEFT ENGINE RUNNING, PTU OPERATEDSDR CALA2022021600399Drain Mast · cloggedREF L/P 7964207- AFT GALLEY DRAIN CLOGGED AND LEAKING. SPILL CLEANUP REQUIRED. CABIN FLOOR FRAME 62 THUR 66 (CTR AISLE ROW 32 TO AFT GALLEY). NO WATER IN AFT CARGO COMPT DETECTED. PLACED ON DIP. WITHIN 7 DAYS, ACCOMPLISH ECRA 2011-01000, GALLEY SPILL, SECTION SDR CALA2022020100282Control Unit · unserviceableBRAKE SYS 1 FAULT, SYS RESET THEN FAULT CAME BACK LOCKED FOR FIX ITEM UNLOCKED FOR CLEARING ACTION. REMOVED AND REPLACED #1 BSCU PER AMM 32-42-34-400AND TESTED OK, LAND VERIFY PASSED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1248627 SN OFF 5694 UNIT, BRAKE SSDR CALA2022012000197Keelbeam · elongatedWHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19. REPAIRED RH KEEL BEAM FASTENER HOLE AND FITTING IAW EC/RA 5330-0 6891. EMP: V935774 WC: 0018386 STA: ST ENG BFM SFR# 1SDR CALA2022012000195Fastener · cracked(SDR) DOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW, HO LE B HAS A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED LH FR16 HOLE B DOUBLE JOGGLE IAW EC/RA 5311-02735. SEE DTA DIP #7806847 FOR INSPECTION REQUIREMENTS. ESDR CALA2022012000194Keelbeam · elongatedWHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT) REPAIRED LH KEEL BEAM FASTENER HOLES AND FITTINGS IAW EC/RA 5330 -06891 EMP: V935774 WC: 0018385 STA: ST ENT BFM SFR# 1027501SDR CALA2022011800184Keelbeam · elongatedWHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE RH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. -06891 (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PESDR CALA2022011800179Keelbeam · elongatedWHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D OF THE LH FUSELAGE KEEL BEAM MLG ATTACHMENT STRUCTURE, PRODUCTION REPORTED ALL HOLES OUT OF LIMITS AND ELONGATED. 02712. (SEE FIGURE 1 - 17 OF EC/RA 5311-02712 FOR LOCATIONS). ACCOMPLISH A PERMANENT REPAIR PESDR CALA2022011800176Frame · crackedDOUBLE JOGGLE FASTENER HOLES LH FR16 TOP HOLES AFT ROW. HOLE B H AS A CRACK INDICATION. MUST BE REPAIRED BEFORE NEXT FLIGHT PER E A 5311-02442. WITH EC/RA 5311-02735. WORK ACCOMPLISHED BY VTMAE EMPLOYEE AIRCRAFT FLIGHT CYCLES, AND AT INTERVALS NOT TO EXCEED 4,SDR CALA2022011800175Rib · elongatedWHILE ACCOMPLISHING FCD 5330-05575 LH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE (NO DOT)SDR CALA2022011800174Rib · elongatedWHILE ACCOMPLISHING FCD 5330-05575 RH HOLES, FOUND ALL HOLES OUT OF SIDE LIMITS AND ELONGATED WITH VISUAL DAMAGE EXCEPT HOLES #R 13 AND #R19.SDR CALA2022011700164Stop Fitting · crackedRH FR16 DOORSTOP #7 HAS CRACK INDICATIONS. ACCOMPLISHED BY VTMAE EMPLOYEE V935774. ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 INTERVALS NOT TO EXCEED 15,500 FLIGHT CYCLES THEREAFTER. INSPECTION REQUIREMENTS PER PART 2A OF LATEST REVISSDR CALA2022011700163Fastener · crackedDOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442. REPAIRED L/H FR20 DOUBLE JOGGLE FASTENER HOLES IAW EC/RA 5311-02 726. SEE DTA DIP LP# 7802054 FOR INSPECTION REQUIREMESDR CALA2022011400144Pressure Panel · crackedCRACK INDICATIONS NOTED AT LEFT FR36 PRESSURE PANEL HOLES #3 THRU #9. PER ECRA 5330-06903. WORK ACCOMPLISHED BY V935774 TOTAL AIRCRAFT FLIGHT CYCLES, OR 128,977 TOTAL PERFORM AN INSPECTION PER PART 2 OF THE LATEST REF LP 7800794. UPON THE ACCUMULATION OF 60,65SDR CALA2022011400142Frame · crackedLH FRAME 20 DOUBLE JOGGLE HOLE "A" CRACKED 5311-02726. WORK ACCOMPLISHED BY VTMAE EMP V935774. ON OR CYCLES, AND AT INTERVALS NOT TO EXCEED 5,900 FLIGHT CYCLES, REVISION OF ECRA 5311-02726. BEFORE THE ACCUMULATION OF 35,451 TOTAL AIRCRAFT FLIGHT THEREAFTER, PSDR CALA2022011400134Intercostal · crackedROTO PROBE OF RH FR20 #7 DOOR STOP FITTING FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 15,500 FLIGHT CYCLES THEREAFTER. ISDR CALA2022011400133Frame · crackedDOUBLE JOGGLE FASTENER HOLES LHFR20 TOP HOLES AFT ROW, HOLE A HA S A CRACK INDICATION, MUST BE REPAIRED BEFORE NEXT FLIGHT PER EA 5311-02442.SDR CALA2022011400136Frame · crackedLH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION 001/002. WORK ACCOMPLISHED BY VTMAE EMP V935774 ACCOMPLISH EC/RA 5311-02712 ON OR BEFORE THE AIRCRAFT REACHES 40,251 TOTAL EXCEED 13,700 FLIGHT CYCLES THEREAFTER. INSPSDR CALA2022011400135Frame · crackedLH FR35 ROTO PROBE AT STGR 30 FASTENER HOLES FOUND THE BOTTOM AF T HOLE CRACKED ACCOMPLISHED BY VTMAE EMP V935774 ON OR BEFORE JUNE 20, OF ECRA5310-07963 2022, PERFORM AN INSPECTION PER PART 2 OF THE LATEST REVISION PERFORMED INTERIM REPAIR TO LH FR35 STGR 30 SDR CALA2022011400124Actuator · failed inspR1 DOOR DAMPER FAILED OPS CHECKSDR CALA2022011300123Frame · crackedTWO ADDTIONAL FASTENER HOLES WERE FOUND CRACKED AT FR36 PRESSURE PANEL O/B OF ALLOWABLE CUT-OUT AREA REPAIRED ADDITIONAL FASTENER HOLES FOUND CRACK AT FR36 PRESSURE PANEL IAW EC/RA 5330-01903. EMP: V935774 WC: 0018304 STA: ST ENG BFM SFR# 1027449SDR CALA2022011300122Intercostal · crackedRH FR16 #1 DOOR STOP FITTING ROTO PROBE FOUND THAT THE BOTTOM IB HOLE HAS A CRACK INDICATION REPAIRED RH FR16 #1 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017897 STA: ST ENG BFM SFR# 0017897SDR CALA2022011300121Frame · crackedRH FR16 #7 DOOR STOP ROTO PROBE FOUND THAT THE TOP IB AND BOTTOM IB HOLES HAVE CRACK INDICATIONS REPAIRED RH FR16 #7 DOOR STOP FITTING AREA IAW EC/RA 5311-02712. EMP: V935774 WC: 0017896 STA: ST ENG BFM SFR# 1027447SDR CALA2021122002414Beam · corrodedFWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION. REMOVED FLOOR BEAM Y254 BETWEEN FR16 AND FR20 CORROSION AROUND T D5311281820401 IAW SRM 51-42-11. EMP: V933870 WC: 0018103 STA: S HE SELF-LOCKING CLIP NUT IS NOT PERMITTED IAW SRM 53-11-14-283-0 T ENG BSDR CALA2021122002412Frame · gougedCABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292 REMOVED CORROSION CABIN FLOOR STRUCTURE FR68 Y1292 BEAM IAW SRM BFM SFR# 1027223 51-74-00 BLENDED AREA MEASURES L=1.5" W=1.250" D=0.019" ORIGINAL THICKNESS 0/155" REMAINING THICKNESS 0.136" FOUND OUT OF LSDR CALA2021121702388None · corrodedCABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765 REMOVED CORROSION ON CABIN STRUCTURE FLOOR BEAM Y765 AT FRAME 65 51-72-11-911 AND 51-42-11. EMP: V933866 WC: 0018116 STA: ST ENG IAW SRM 51-74-00. FRAME FOUND OUT OF LIMITS IAW SRM 53-00-14-28 BFM SFR#SDR CALA2021121702384Beam · corrodedFWD CABIN, FLOOR BEAM Y254 BETWEEN FR16/20 HAS CORROSION.SDR CALA2021121702383Beam · gougedCABIN FLOOR STRUCTURE FRAME HAS GOUGE AT FRAME 68 Y1292SDR CALA2021121402364Beam · corrodedCABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 65 Y765SDR CALA2021121202349Floor Support · elongatedAFT CABIN, LH DOOR SILL FLANGE FR67-FR68 NUT PLATE HOLE IS ELONG ATEDSDR CALA2021121202343Beam · corrodedCABIN FLOOR STRUCTURE FRAME HAS CORROSION AT FRAME 68 Y765 REMOVED CORROSION ON CABIN FLOOR STRUCTURE FRAME Y765 FR68 IAW S -11-911 AND 51-42-11. EMP: V933866 WC: 0018126 STA: ST ENG BFM S RM 51-74-00. FRAME FOUND OUT OF LIMITS. ORIGINAL THICKNESS 0.160 FR# 10
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