N899UA

Service difficulty reports · 45

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 = 'N899UA' 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.

SDR CALA2026091819538Fire Bottle · dischargedTROUBLESHOOT LOUD NOISE FROM APU FIRE BOTTLE AREA. UPON INSPECTION, APU FIRE BOTTLE FOUND DISCHARGED.APU FIRE BOTTLE. REMOVED AND REPLACED IAW AMM 26-22-41-000-001-A AND MM 26-22-41-400-001-A.OPC GOOD IAW AMM 26-22-00-710-001-A.Sep 16, 2026 · N899UA · Airbus A319132 · Fire Bottle, FixedSDR CALA2026092819929Skin · ground damageDENT BELOW FORWARD CARGO DOOR DUE TO BELT LOADER CONTACT. DENT EVALUATED PER SRM 53-21-11-283-020. DENT MEASURES 2.5" LONG AND 1" WIDE 1" FWD OF FR 27 BTWN STRINGERS 42-43R WITH A MAX DEPTH OF 0.015". DENT IS TYPE 1 & LOCATED IN ZONE 1, FIGURE 7 & AREA 1, FSep 13, 2026 · N899UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2025111411208Controller · faultedCABIN PRES WARNING AT FL390. PILOTS STATED THEY SAW A FLUCTUATION OF 2500 FT BUT FELT NO PRESSURE IN EARS.CPC 2 TOOK OVER RIGHT AFTER CPC 1 FAIL. PERFORMED CPC1 OPS CHECK SEVERAL TIMES WITH NO FAILURES. IAW AMM TASK 21-31-34-400-001-A,Nov 10, 2025 · N899UA · Airbus A319132 · Cabin Pressure ControllerSDR CALA2025110911025Girt Bar · frayedREMOVED L1 DOOR SLIDE ASSY PER AMM TASK 25-62-44-000-012-A FOR FURTHER TROUBLESHOOTING. CLEARANCE FOR INSTAL L1 SLIDE NEW 1L SLIDE P/N D30664-705 S/N A5775 GIRT BAR LACING IS FRAYING IN MULTIPLE AREAS. INSTALLED L1 DOOR SLIDE ASSY IAW AMM TASK 25-62-44-400-00Nov 7, 2025 · N899UA · Airbus A319132 · Emergency EquipmentSDR CALA2025110911021Elec Connector · damagedEPSU INT LOAD FWD L MSG DURING CABIN EMERGENCY LIGHT TEST PERFORMED WIRE CHECKS PER ASM 33-51-01 SCH 01, PAGE 169. FOUND RESISTANCE AT PIN T OF 10WL EPSU CONNECTOR TO GROUND TO BE 27K OHMS. SUSPECT BAD LIGHT INSIDE ESCAPE SLIDE FWD DOOR LH. REMOVED ESCAPE SLINov 7, 2025 · N899UA · Airbus A319132 · Light System WiringSDR CALA2025092409199Battery Pack · no testEPSU UNIT EMERGENCY LIGHT L AND R TEST FAILED. REMOVED AND REPLACED LEFT AND RIGHT EPSU BATTERY UNITS. REF AMM 33-51-38. EMERGENCY POWER SUPPLY UNIT BITE CHECK NORMAL. REF AMM 33-51-00-710-001-A; CIDS BITE TEST NORMAL. REF AMM 23-73-00-740-005-A.Sep 23, 2025 · N899UA · Airbus A319132 · Emergency LightingSDR CALA2025031402813Switch · malfunctionedEMERGENCY EXIT LIGHTS ON WITH SWITCH OFF ON ARMED CYCLED SWITCH.Mar 14, 2025 · N899UA · Airbus A319132 · Emergency LightingSDR CALA2024120201367Unknown · odorFUMES IN THE COCKPIT ON DESCENT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. CREW REPORTED ODOR IN THE FLIGHT DECK THA T SMELLED LIKE PAINT OR LACQUER ON DESCENT INTO CHS. NO ODOR PRE SENT ON ARRIVAL TO ACFT. SUSPECT ODOR WAS FROM AN EXTERNAL SOURC E. COMPNov 29, 2024 · N899UA · Airbus A319132 · Air Distribution SystemSDR CALA2024042301205Bypass Valve · failedRAPID DEPRESSURIZATION OR EMERGENCY DESCENT. SLOW DEPRESSURIZATION AT FL360 EMERGENCY DESCENT. SCREEN FOUND DUCT BLOWN OFF OF VALVE BYPASS ON NR 2 PACK. AND THE SEAL THAT GOES ALONG WITH IT, THE BYPASS VALVE WAS R & R IAW AMM 21-61-53/401 CONFIG 00. PERFOApr 20, 2024 · N899UA · Airbus A319132 · Cabin Cooling SystemSDR CALA2024012900235Fitting · crackedFLIGHT DECK FR4 WINDSHIELD CENTER POST LOWER STRUCTURE L/H CONTI NUITY FITTING PRODUCED CRACK INDICATIONS DURING HFEC INSPECTION PER HAECO LCQ N/R 9290288/42288 GEN BY V061690 LH & RH CONTINUITY FITTING HAS BEEN REPLACED IAW ECRA V914231 INSPECTED BY LC 04 ANDJan 25, 2024 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2024012900236Window Frame · crackedFR4 WINDSHIELD CTR POST LOWER NODE LH IB HOLE HAS CRACK INDICA TION AT LOWER FACE EXTENDING FWD .020 PER HAECO LCQ N/R 9290577/ 42577 GEN BY V892444 SH INITIAL INSPECTION PER PART 2 OF THE LATEST REVISION OF ECRA REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 61Jan 24, 2024 · N899UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024012400208Intercostal · crackedL1 DOOR STOP #7 UPPER INBD BOLT HOLE PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 3,4 AND 5:00 POSITIONS AND THE LOWER INBD BOLT HOLE PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 2:00 POSITION FR16 PER NR9290266/42266 . PERFORMED REPAIR IAW R-DJan 19, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2024012400207Door Frame · crackedL1 DOOR STOP #1 AT FR16 LOWER INBD BOLT HOLE PRODUCED CRACK INDICATIONS AT THE 3:00 AND 8:00 POSITION PER NR9290267/42267 GEN BY V061690 NITIAL INSP ON THE LH FR16 DOORSTOP FITTING #1 HOLES 3 AND 4 PER FT REACHES 37,546 TOTAL ACFT FC. PERFORM REPEAT INSP AT INJan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024012200174Intercostal · crackedR1 FR16 DOOR STOP #7 UPPER INBD BOLT PRODUCED CRACK INDICATIONS IN THE INTERCOSTAL AT THE 6:00 POSITION AND IN THE FRAME AT 11:0 0 POSITION LOWER INBD HOLE PRODUCED CRACK INDICATIONS IN THE INT ERCOSTAL AT 6:00 POSITION IN THE FRAME PER NR9290268/42268.Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2024012200173Door Frame · crackedR1 FR16 DOOR STOP #1 LOWER INBD BOLT PRODUCED CRACK INDICATIONS IN THE FRAME AT THE 12:00 POSITION AND AT 6:00 POSITION, PER NR9 290271/42271 PERFORMED REPAIR IAW A319 R-DWG R53113118 REV F CAT A REPAIR NO FURTHER RE-INSPECT REQUIRED.Jan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024012200169Stop Fitting · crackedR1 FR20 DOOR STOP #1 UPPER INBD BOLT PRODUCED CRACK INDICATIONS IN THE FRAME AT THE 6:00 POSITION LOWER INBD HOLE PRODUCED CRACK INDICATIONS IN THE FRAME AT 9:00 POSITION PER NR9290270/42270 PERFORMED REPAIR IAW A319 R-DWG R53113118 REV F CAT A REPAIR NO FURTHJan 19, 2024 · N899UA · Airbus A319132 · Fuselage Main, StructureSDR CALA2024011200084Stringer · corrodedAFT CARGO DOOR FLOOR STRUCTURE, FR52 THROUGH FR54 LH STR.42 CORROSION PER NR9290527/42527. PERFORMED STRINGER SPLICE REPAIR IAW A319 R1-R534-70620_F CAT A REPAIR. NO REINSPECT REQUIRED.Jan 11, 2024 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2024010800051Threshold · corrodedAFT CARGO FLOOR STRUCTURE FR56 THROUGH FR58 DOOR SEAL SUPPORT STRUCTURE MULTIPLE FLAGGED SPOTS OF CORROSION PER NR9290533/42533 GEN BY V920443 RMVD AND RPLD AFT CARGO THRESHOLD AT FR56-58 AND REAPPLIED PROTE CTIVE COATINGS IAW SRM 51-72-11-911/001, 51-42-11/00Jan 3, 2024 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2024010200008Stringer · corrodedAFT CARGO FLOOR STRUCTURE FR64 THROUGH FR 65 RH STR 31 EXFOLIATION/CORROSION. . REMOVED AND REPLACED STR 31RH FR 64 TO 66.9" AFT CARGO FLOOR STR PERFORMED BY V932428 AND INSP BY V892285. UCTURE IAW A319 SRM 51-42-11/001. FOUND STR 31RH FR 64 THROUGHT FR65 OUT Dec 29, 2023 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2023122903755Fitting · corrodedFWD CARGO DOOR AFT ECCENTRIC BOLT FITTING FWD LUG FWD FACE HAS CORROSION AT BUSHING BORE PER HAECO LCQ NON ROUTINE 9290415/42415 GENERATED BY N078625Dec 27, 2023 · N899UA · Airbus A319132 · Cargo/Baggage DoorsSDR CALA2023122903753Floor Support · corrodedFWD CARGO THRESHOLD STILL PLATE FR24.5-28 HAS CORROSION THROUGHO UT (A3NB-53-3-6105) PER HAECO LCQ NON ROUTINE 9290462/42462 GENE RATED BY N078625Dec 27, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2023122203716Door Sill · corrodedR2 DOOR CUTOUT SILL CENTER SHAPE HAS MULTI AREAS OF CORROSION. REMOVED AND REPLACED R2 DOOR CUTOUT SILL CENTER SHAPE IAW A319 S RM 51-72-11.Dec 21, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2023122203715Door Sill · damagedL2 DOOR CUTOUT SILL, IB OF AFT GRIT BAR FITTING IB AFT HOLE SILL BENT PER NR9290445/42445. REPAIRED L2 DOOR CUTOUT SILL IB OF AFT GRIT BAR FITTING IB AFT H OLE SILL IAW SRM 53-41-14-300-001 FIG 1.Dec 21, 2023 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2023121503649Intercostal · crackedLH OW EMERG HATCH LOAD TRANSMITTING PROFILE IS CRACKED PER 92901 85/42185. RMVD AND RPLD LOAD TRANSMITTING PROFILE ON LH WING EMERGENCY EXIT HATCH RE-APPLIED SURFACE PROTECTION IAW SRM 51-72-11-911-001, 51-42-11 & 51-75-12/001Dec 8, 2023 · N899UA · Airbus A319132 · Emergency ExitsSDR CALA2023012700230Power Supply · inoperativeEMER EXIT LIGHTS ON INAFT GALLEY OVER BOTHDOORS AND LAV. REPLACED 13WL EPSU AND BATTERY PER AMM 31-51-38-000-001-A. PARTS USED: 31-3350-9-9001, ACP VERIFICATION EMER LIGHTS NOW WORK AND NEW BOX SYS TEST OK. IDT INSPECTED PER GMM 09-10-05.Jan 27, 2023 · N899UA · Airbus A319132 · Emergency LightingSDR CALA2022071101710None · odorAIRCRAFT FLIGHT DECK ANDCABIN AIR STRONG ODOR LOOKING INTO TSM 05-50-00-810-831-A AND AMM 36-10-00-615-801-A. ALSO COULD CHANGE CABIN CARTARAGE RETURN FILTERS, M&E 31-2121-3-0008. SMELL VARIES IN CABIN WITH APU/PACKS RUNNING AND/OR PCAIR OIL LEAK APPEARS TO BEJul 11, 2022 · N899UA · Airbus A319132 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2021053100767Clamp · missingPDA 3 REF LOGPAGE #6349863 RH LANDING LIGHT CLAMP MISSING. THIS ITEM IS CONSIDERED A CLASS 3 PDA. RPREPLACED RING AND SCREW INSTALLED PER AMM 33 -42-11-01A ALSO NOTIFED AIRPORT OPS AND PREFORMED RAMP INSPECTION.May 31, 2021 · N899UA · Airbus A319132 · Exterior LightingSDR CALA2019031100398Fastener · missingFASTENER MISSING ON LEADING EDGE CORNER OF PNL 196BB UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CALL TOMC 847-700-9980 MM 53-35-00-200-002A. CANNOT BE MISSING FROM CORNER FOR CARRY. V ACCESS DOOR 196BB IS ATTACHED TO BELLY FAIRING PANEL 196AB REF A ARGAS TOMMar 11, 2019 · N899UA · Airbus A319132 · Fuselage Main, Plate/SkinSDR CALA2019020800231Limit Switch · stuckFA REPORT WATER LEAKINGFROM BOTH FWD/AFT GALLEYWATER QNTY 100 AT T/OLEAK TO 0 CHECKED POTABLE WATER SYSTEM PER TSM 38-12-00-810-815A. DRAINED AND FILLED TANK AND VERIFIED QUANTITY INDICATION CORRECT. PRESSURIZED TANK AND LEAK CHECKED ALL GALLEY AND LAV WATER Feb 8, 2019 · N899UA · Airbus A319132 · Potable Water SystemSDR CALA2018021600628Frame · corrodedAFT CARGO DOOR LOWER CUT OUT FRAME SUPPORT AT FRAME 59, STRINGERS 37 - 38R HAS CORROSION. REPAIRED IAW ECRA 5341-011161.Feb 14, 2018 · N899UA · Airbus A319132 · Fuselage Main, FrameSDR CALA2018020900516Threshold · corrodedAFT CARGO BAY, FRAMES 55 - 59, RT DOOR THRESHOLD HAS SURFACE CORROSION. REMOVED AND REPLACED THE THRESHOLD IAW SRM 5 1-42-11.Feb 8, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2018012600308Hinge Fitting · corrodedLEFT MLG DOOR FWD FITTING ON KEEL BEAM FWD LUG, FWD FACE HAS CORROSION. CORROSION EXCEEDS MANUFACTURE DRAWING TOLERANCES IAW IAW SRM 53 -36-11 DRAWING, 4-3 SHEET. INSTALLED A NEW HINGE FITTING IAW SRM 51-72-11, PG 2, PARA D-1.Jan 25, 2018 · N899UA · Airbus A319132 · Landing Gear DoorsSDR CALA2018011900213Web · corrodedFORWARD CARGO BAY, BETWEEN FRAMES 25 - 27 DOOR SILL WEB HAS THREE SPOTS OF CORROSION ON UPPER SURFACE, BELOW TIE DOWN FITTINGS. REMOVED AND REPLACED THE WEB IAW SRM 51-42-11, PARA 2.E, PARA 2.F.Jan 16, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2018011400191Stringer Splice · corrodedAFT CARGO BAY, FRAMES 63 - 64 STRINGER SPLICE 42L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51- 42-11, PARA F.Jan 14, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2018011300181Longeron Splice · corrodedAFT CARGO BAY STRINGER SPLICE 40L, FRAMES 63 - 64 HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2018011300180Longeron Splice · corrodedAFT CARGO BAY STRINGER SPLICE 43L, FRAMES 63 - 64 HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2018011300179Stringer Splice · corrodedAFT CARGO BAY FRAMES 63 - 64 STRINGER SPLICE 41L HAS SURFACE CORROSION. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-11, PARA F.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Longeron/StringerSDR CALA2018011200137Shear Web · corrodedRIGHT SIDE SHEAR WEB BETWEEN FRAMES 69 & 70, HAD SEVERAL AREAS OF CORROSION ON TOP & BOTTOM SIDES. REMOVED AND REPLACED THE SHEAR WEB AND FRAME SUPPORT IAW SRM 51 -42-11, PG 2, STEP 2 A-H.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2018011200136Fitting · corrodedR2 DOOR SILL HAS CORROSION AT FRAME 68 INBD & OTBD. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS, INSTALLED A NEW FITTING IAW SRM 51-72-11-911-001, & 51-42-11-001.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2018011200135Fitting · corrodedR2 DOOR SILL AFT CORNER FITTING AT FRAME 68 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED THE CORNER FITTING IAW SRM 51-72-11-911-001 & 51-42-11-001.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2018011200133Fitting · corrodedR2 DOOR SILL HAS CORROSION ON FWD CORNER FITTING AT FRAME 66. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. INSTALLED A NEW CORNER FITTING IAW SRM 51-72-11-911-001, & 51-4 2-11-001.Jan 11, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2018011200124Door Sill · corrodedL2 DOOR SILL HAS CORROSION INBD SIDE OF FRAME 66. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11, PARA 2.Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous StructureSDR CALA2018011200123Fitting · corrodedL2 DOOR SILL HAS CORROSION ON FWD CORNER FITTING AT FRAME 66. REMOVED AND REPLACED THE FITTING IAW SRM 51-72-11, PARA 2.Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2018011200122Fitting · corrodedL2 DOOR SILL AFT CORNER FITTING HAS CORROSION AT FRAME 68. REMOVED AND REPLACED THE DOOR SILL AFT FITTING IAW SRM 51-72-11.Jan 8, 2018 · N899UA · Airbus A319132 · Fuselage Main, Attach FittingsSDR CALA2018010500032Shear Web · corrodedLEFT SIDE SHEAR WEB 3 INCHES AND 7 INCHES FORWARD OF FRAME 70 SEVERAL AREAS OF CORROSION ON TOP AND BOTTOM SIDES OF SHEAR WEB. REMOVED AND REPLACEDTHE SHEAR WEB AND SUPPORT IAW SRM 51-42-11 REV.Jan 4, 2018 · N899UA · Airbus A319132 · Fuselage Miscellaneous Structure
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