# Service difficulty reports: N830UA

A list on [N830UA](https://openairdocs.org/aircraft/N830UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 112 reports

- [SDR CALA2026041315288](https://openairdocs.org/sdr/CALA2026041315288.md): Fan · failed · Apr 9, 2026 · N830UA · Airbus A319131 · Air Distribution Fan
  > LAV AND GALLEY FAN FAULT DISPLAYED ON UPPER ECAM SCREEN. ECAM COND LAV & GALLEY FAN FAULT. FLIGHT ATTENDANTS REPORTED UNUSUAL GRINDING NOISE JUST MOMENTS BEFORE ECAM. NOISE GONE. NO ODORS. PLACED ON MEL2123A. CIRCUIT BREAKERS U19 & U21 ON 122VU PULLED & CO
- [SDR CALA2025123012544](https://openairdocs.org/sdr/CALA2025123012544.md): Fuel Cap · missing · Dec 29, 2025 · N830UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING ON ARRIVAL. REPLACED MISSING FUEL CAP.
- [SDR CALA2025122212312](https://openairdocs.org/sdr/CALA2025122212312.md): Fan · failed · Dec 23, 2025 · N830UA · Airbus A319131 · Air Distribution Fan
  > POSSIBLE ELECRICAL BURNING ODOR IN FWD GALLEY & FLIGHT DECK. ODOR APEARS TO COME FROM RT RECIRC FAN. RT RECIRC FAN INOPERATIVE. PERFORMED SMOKE IN CABIN CHECK AS PER AMM TASK 05-51-10-200-801-C1. ALL EVIDENSE OF ODOR DISIPATATED. OK TO CONTINUE ON MEL. AP
- [SDR CALA2025110410861](https://openairdocs.org/sdr/CALA2025110410861.md): Battery · no test · Nov 3, 2025 · N830UA · Airbus A319131 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING TEST CIDS FAULTED 33-51-38. R & R EPSU BATT IAW AMM 33-51-00-710-812-A, OPS CHECK GOOD
- [SDR CALA2025110410858](https://openairdocs.org/sdr/CALA2025110410858.md): Battery Pack · no test · Nov 3, 2025 · N830UA · Airbus A319131 · Emergency Lighting
  > DURING EMERGENCY LIGHTIMG CABIN TEST CIDS FAULTED 33-51-38. R & R EPSU BATTERY IAW AMM 33-51-00-710-812-A, OPS CHECK GOOD
- [SDR CALA2025082508092](https://openairdocs.org/sdr/CALA2025082508092.md): Scavenge Pump · faulted · Aug 21, 2025 · N830UA · Airbus A319131 · Turbine Engine Oil System
  > ENG2/INNER EXHAUST HAS FLUID LEAKING AT THE 6 OCLOCK POSITION. SUSPECT FUEL PUDDLE, DID NOT GLOW FROM UV LIGHT AND DOES NOT HAVE A SMELL. IN CONCURRANCE WITH TOMC ENGINE DESK, SUSPECT #5 ENGINE BEARING OIL SCAVENGE TUBE MAY BE BLOCKED INTERNALLY & CAUSING THE
- [SDR CALA2025040803637](https://openairdocs.org/sdr/CALA2025040803637.md): Fuel Cap · missing · Apr 5, 2025 · N830UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELING VENDOR REPORTS FUEL CAP MISSING ON ARRIVAL FUELER FOUND FUEL CAP MISSING. PERFORMED GVI, NO DEFECTS NOTED
- [SDR CALA2025010900063](https://openairdocs.org/sdr/CALA2025010900063.md): Wheel · damaged · Jan 7, 2025 · N830UA · Airbus A319131 · Wheel/Ski/Float
  > PDA 2 RIGHT OB MLG TIRE WHEEL TIE BOLT BROKEN....REPORTED BY CREW TOMC SMITH UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK.
- [SDR CALA2024090302339](https://openairdocs.org/sdr/CALA2024090302339.md): Anchor Fitting · corroded · Aug 29, 2024 · N830UA · Airbus A319131 · Wing, Landing Gear Attach Fittings
  > AFTER REMOVAL OF RMLG ANCHOR FITTING FOUND FRETTING CORROSION ON T/E SPAR AROUND FASTENER HOLE. PERFORMED REPAIR AND REMOVED CORROSION ON THE RMLG ANCHOR FITTING T/E SPAR AROUND FASTENER HOLES IAW EC/RA 5720-03464 DATED 08/ 28/2024 CAT A.
- [SDR CALA2024090302357](https://openairdocs.org/sdr/CALA2024090302357.md): Skin · cracked · Aug 27, 2024 · N830UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EC/RA NO.: 5311-02101 REV. - CRACK INDICATION IN HOLE NO. 2 AT 6 O''CLOCK POSITION IN THE AFT SKIN LAYER AT FRAME 35 AND 10 CM FO RWARD STGR 30 LH, ON HAECO LCQ NR 9298721, PER PART 2A OF THE LATEST REVISION OF ECRA 5331-03113 ON OR COMES FIRST. PERFORM REPEA
- [SDR CALA2024082602264](https://openairdocs.org/sdr/CALA2024082602264.md): Frame · damaged · Aug 20, 2024 · N830UA · Airbus A319131 · Fuselage Main, Frame
  > ACCOMPLISH A PERMANENT REPAIR ON FR35 STGR 30RH HOLES 2A AND 5 PER PART 3 OF THE LATEST REVISION OF ECRA 5311-03112. HOLES 2A AND 5 PER PART 3 OF THE LATEST REVISION OF ECRA 5311-03112 ON OR BEFORE 02 FEB 25. PART 1, INTERIM REPAIR PER ECRA 5331-03112 ACCOMPLI
- [SDR CALA2024081902236](https://openairdocs.org/sdr/CALA2024081902236.md): Frame · cracked · Aug 15, 2024 · N830UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR68 STGR8RH AFT UPPER CORNER FRAME VERTICAL FLANGE IS CRACKED. REPLACED FRAME UPPER PNL ON R-2 DOOR BTW FR67 - FR68 IAW A319 SR M 51-42-11.
- [SDR CALA2024081902238](https://openairdocs.org/sdr/CALA2024081902238.md): Flap · damaged · Aug 14, 2024 · N830UA · Airbus A319131 · Trailing Edge Flaps
  > RH WING OB FLAP JUST IB OF #4 FLAP TRACK HAS DAMAGE TO COMPOSITE. GEN BY V892442 ON HAECO LCQ NR 9298895 / 26895
- [SDR CALA2024072602108](https://openairdocs.org/sdr/CALA2024072602108.md): Bushing · cracked · Jul 20, 2024 · N830UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH AFT UPPER DOOR BOX UPPER DOOR SILL AFT ATTACH POINT TO FR68 AT STR 8 BOTTOM/MOST INBD FASTENER HOLE HAS A CRACK INDICATION IN THE DOOR SILL LAYER AT THE 2:0''CLOCK POSITION 100%+SHPER HAECO LCQ N/R 9298618/26618 GEN BY V062335 ACCOMPLISHED INTERIM REPAIR TO
- [SDR CALA2024072402094](https://openairdocs.org/sdr/CALA2024072402094.md): Frame · cracked · Jul 20, 2024 · N830UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR 68 AT STR 8 CRACK ADJACENT TO UPPER MOST FASTENER IN WEB PER 53-41-12-300-012. PERFORMED NDT WITH NO DEFECTS NOTED. THIS TABLE 1, FROM TIME OF REPAIR OF 54,700 FC AND SUBSEQUENT REPAIR IS A CAT B. INSPECTION REQUIRED IAW SRI 53-41-12-205-014, INSPECTION
- [SDR CALA2024071002001](https://openairdocs.org/sdr/CALA2024071002001.md): Stringer Splice · corroded · Jul 9, 2024 · N830UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CORROSION OF STR 43L AT FR 47/51 TO 52 ON SPLICE PER HAECO LCQ N/R 9298944/26944.
- [SDR CALA2024070801966](https://openairdocs.org/sdr/CALA2024070801966.md): Skin · dented · Jul 2, 2024 · N830UA · Airbus A319131 · Service Doors
  > R1 DOOR JUST 3 IN AFT OF FRAME 20 BETWEEN STR 19RH AND STR 20RH HAS PREVIOUS DAMAGE THAT REQUIRES PERMANENT REPAIR PER EC/RA 5311-03116 PER HAECO LCQ N/R 9298900/26900 GEN BY V080280 PERFORMED DOUBLER AND FILLER REPAIR ON THE R1 DOOR 3 IN AFT OF FR20 BTWN STR
- [SDR CALA2024070301961](https://openairdocs.org/sdr/CALA2024070301961.md): Structure · damaged · Jun 29, 2024 · N830UA · Airbus A319131 · Rudder Structure
  > RUDDER L/H AND R/H HOIST POINTS ROTATE IN SKIN TOP 2EA. REMOVED AND REPLACED L/H AND R/H UPPER #3 HOIST POINTS IAW A319 SRM 55-41-13-300-029 CATEGORY A REPAIR.
- [SDR CALA2024070801971](https://openairdocs.org/sdr/CALA2024070801971.md): Support Angle · cracked · Jun 28, 2024 · N830UA · Airbus A319131 · Wing Miscellaneous Structure
  > R/H WING RIB 15 O/B WEB SUPPORT ANGLE CRACKED PER HAECO LCQ N/R 9298670/26670 GEN BY V926223 REMOVED AND REPLACED SUPPORT ANGLE ON R/H WING RIB 15 O/B WEB IAW SRM A319 51-72-11-911-001 BY MECH V934190 INSP BY V892442
- [SDR CALA2024062801919](https://openairdocs.org/sdr/CALA2024062801919.md): Door Frame · cracked · Jun 25, 2024 · N830UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W ESCAPE HATCH FWD VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED R/H O/W ESCAPE HATCH FWD VERTICAL FRAME IAW SRM 51- 72-11 AND 51-42-11.
- [SDR CALA2024062801918](https://openairdocs.org/sdr/CALA2024062801918.md): Door Frame · cracked · Jun 25, 2024 · N830UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED R/H O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A319 SRM 51 -72-11 AND 51-42-11.
- [SDR CALA2024062801917](https://openairdocs.org/sdr/CALA2024062801917.md): Door Frame · cracked · Jun 25, 2024 · N830UA · Airbus A319131 · Fuselage Main, Structure
  > L/H O/W ESCAPE HATCH AFT VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED LH O/W ESCAPE HATCH AFT VERTICAL FRAME IAW SRM 51-72-11 AND 51-11-12.
- [SDR CALA2024062801913](https://openairdocs.org/sdr/CALA2024062801913.md): Door Frame · cracked · Jun 25, 2024 · N830UA · Airbus A319131 · Fuselage Main, Structure
  > L/H O/W ESCAPE HATCH FWD VERTICAL FRAME APPEARS TO BE CRACKED. REPLACED L/H O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A319 SRM 51 -72-11 AND 51-42-11.
- [SDR CALA2024062601904](https://openairdocs.org/sdr/CALA2024062601904.md): Skin · none · Jun 21, 2024 · N830UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER AT FUSELAGE EXTERNAL SKIN FR 34 STR 43 REQUIRES INFORMATION/ECRA ABOUT EXISTING DOUBLER PER HAECO LCQ N/R 9298217/26217 GEN BY V080280 53-00-11-300-043 CRITERIA. NO DEFECTS NOTED ON DOUBLER. REPLACE SRI 53-21-11-205-073 TABLE 2, ZONE A, INSPEC
- [SDR CALA2024061901871](https://openairdocs.org/sdr/CALA2024061901871.md): Angle · cracked · Jun 18, 2024 · N830UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R/H AFT FR 41-42 TI ANGLE APPEARS TO BE CRACKED PER HAECO LCQ N/R 9298433/26433. REMOVED AND REPLACED TI-ANGLE AT R/H AFT FR 41-42 PER UAL EA5331 -01718 REV D CAT 4 REPAIR.
- [SDR CALA2024061801855](https://openairdocs.org/sdr/CALA2024061801855.md): Skin · contaminated · Jun 17, 2024 · N830UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR UPPER SURFACE HAS LIQUID INGRESS AT 57 IN FROM I/B END 18 IN FROM T/E 4 IN DIAMETER PER HAECO LCQ N/R 9298526/26526 GEN BY V061632
- [SDR CALA2024061801854](https://openairdocs.org/sdr/CALA2024061801854.md): Skin · contaminated · Jun 17, 2024 · N830UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR UPPER SURFACE HAS LIQUID INGRESS AT 115 IN FROM I/B END 7 1/2 IN FROM T/E 1 1/2 IN DIAMETER PER HAECO LCQ N/R 9298527/26527 GEN BY V061632 REPAIRED L/H ELEVATOR UPPER SURFACE IAW A319 SRM 55-21-11-300- 004 AND FOUND NO LIQUID REPAIRED IAW A319 AMM
- [SDR CALA2024061801847](https://openairdocs.org/sdr/CALA2024061801847.md): Skin · contaminated · Jun 17, 2024 · N830UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR UPPER SURFACE HAS LIQUID INGRESS AT 32 IN FROM I/B END 17 1/2 IN FROM T/E 2 IN DIAMETER PER HAECO LCQ N/R 9298524/ 26524 GEN BY V061632 REPAIRED LH ELEVATOR UPPER SKIN LIQUID INGRESS IAW A319 SRM 55-2 1-11-300-005.
- [SDR CALA2024061801845](https://openairdocs.org/sdr/CALA2024061801845.md): Skin · contaminated · Jun 17, 2024 · N830UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR UPPER SURFACE HAS LIQUID INGRESS AT 47 IN FROM I/B END 20 IN FROM T/E 2 1/2 IN DIAMETER. REPAIRED L/H UPPER SKIN LIQUID INGRESS IAW A319 SRM 55-21-11-300 -005
- [SDR CALA2024061701829](https://openairdocs.org/sdr/CALA2024061701829.md): Frame · cracked · Jun 15, 2024 · N830UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 68 AT STR 8, CRACK ADJACENT TO UPPER MOST FASTENER IN WEB. PERFORMED FRAME FITTING REPAIR @ FR68 L/H STR8 IAW A319 SRM 53-4 1-12-300 REPAIR CAT B INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 54700FC SUBSEQUENT INSPECTION AT INTERVALS OF 2400
- [SDR CALA2024061701828](https://openairdocs.org/sdr/CALA2024061701828.md): Shear Web · corroded · Jun 15, 2024 · N830UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE CORROSION AT L/H SHEAR WEB BETWEEN FR69 AND FR 70. REMOVED AND REPLACED LH SHEER WEB BTW FR69 AND FR70 IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2024061901869](https://openairdocs.org/sdr/CALA2024061901869.md): Shear Web · corroded · Jun 14, 2024 · N830UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE CORROSION AT R/H SHEAR WEB BETWEEN FR 69 A ND 70 AFT OF R-2 DOOR. REMOVED AND REPLACED RH SHEAR WEB BETWEEN FR69-70 AFT OF R-2 DOO R IAW A319 SRM 51-42-11/001.
- [SDR CALA2024061201783](https://openairdocs.org/sdr/CALA2024061201783.md): Door Sill · corroded · Jun 11, 2024 · N830UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE CORROSION AT R-2 SILL AT FR 68 PER HAECO LCQ N/R 9298632/26632 GEN BY V899045
- [SDR CALA2024041101039](https://openairdocs.org/sdr/CALA2024041101039.md): Fuel Cap · missing · Apr 10, 2024 · N830UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELER REPORTS FUEL CAP MISSING ON ARRIVAL. REQUESTING CDL 28A. PARTS NIS IN ATL. DEFERED PER CDL 28A. PLACARD APPLIED. INSTALLED NEW CAP REF AMM 28-25-41-400-005-A.
- [SDR CALA2024030800666](https://openairdocs.org/sdr/CALA2024030800666.md): Fuel Cap · missing · Mar 4, 2024 · N830UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING NOTIFIED TOMC PLACED ON CDL REF. PAGE 7245006. REQUESTING DEFERREL COMLIED WITH MEL REQUIRMENTS. A/C OKAY TO CONTINUE. FUEL CAP INSTALLED PRIOR TO ARRIVAL, VERIFIED CAP ASSY, NO DEFECTS NOTED.
- [SDR CALA2023111003318](https://openairdocs.org/sdr/CALA2023111003318.md): Outflow Valve · defective · Nov 6, 2023 · N830UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > REJECTED TAKEOFF AT 65KNOTS FOR AVIONICS VENT FAULT ON ECAM REMOVED AND REPLACED SKIN AIR OUTLET VALVE IAW AMM 21-26-53. PERFORMED AVEC TEST ON CFDS MCDU. OPS CK GOOD, NO FAULTS NOTED AT THIS TIME.
- [SDR CALA2023110803304](https://openairdocs.org/sdr/CALA2023110803304.md): Outflow Valve · warning message · Nov 3, 2023 · N830UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > CREW REPORTED AN ABORTED TAKEOFF AT 90 KNOTS. DUE TO AVIONICS VENT SYS FAULT (BLOWER AND EXTRACT) MAX BRAKE TEMP. AT 590 ON #3 WHEEL CFDS REPORT FAULTING (22HQ) SKIN AIR OUTLET VALVE. REQ MEL SKIN AIR OUTLET SECURED AS REQUIRED. PERFORMED DDP, VALVE 24HQ CO
- [SDR CALA2023110303271](https://openairdocs.org/sdr/CALA2023110303271.md): Outflow Valve · warning message · Oct 30, 2023 · N830UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > ABORTED TAKE OFF AT 100 KNTS DUE TO AEVC SKIN VALVE FAULT. REF AMM 05-51-16-200-001-A...TOMC SMITH VISUALLY INSPECTED IAW 05-51-16-200-001-A OPS CHECK GOOD. VENT SKIN VALVE FAULT LAST LEG REPORT AND AEVC OP TEST FAULTED ''SKIN AIR OUTLET V 22HQ''. REF AMM21-2
- [SDR CALA2023100903009](https://openairdocs.org/sdr/CALA2023100903009.md): Manifold · faulty · Oct 7, 2023 · N830UA · Airbus A319131 · Brake
  > BRAKES AUTO BRK FAULT ECAM ON FINAL APPROACH. ECAM CLEARED ON NE XT APPROACH. BITE OF BSCU2 SHOWS SERVOVALVE 4 FAULT (18GG). REPLACED RH NORMAL BRAKE SERVOVALVE MANIFOLD ASSEMBLY REF AMM 32-42-16. NO HELP. BSCU2 TEST ALSO SHOWS TRANSDUCER 4 FAULT ALONG WITH SE
- [SDR 2023FA0000346](https://openairdocs.org/sdr/2023FA0000346.md): Disk · damaged · Jun 30, 2023 · N830UA · Airbus A319131 · Turbine Section
  > SCRAP OF A PVL BEFORE THE END OF LIMITED LIFE. NICKS, DENT IN AREA A4 MORE THAN SERVICEABLE/REPARAIBLE LIMIT IN ACCORDING WITH SUBTASK 72-50-31-220-020 B(1)(B) AND TASK 72-50-31-300-004 REPAIR004 (VRS4157) SUBTASK 72-50-31-350-054 B(1) AREA A1 NO BLENDS PERMIT
- [SDR CALA2023040300963](https://openairdocs.org/sdr/CALA2023040300963.md): Frame · cracked · Mar 31, 2023 · N830UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68, STR 22 RH, FLANGE HAS CRACK AT LOWER RADIUS, BEGINNING AT IB RADIUS EXTENDING OUT APPROX. 1.30 INCHES. "CONTACT ENGINEERI NG FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT." AD RELATED SUPPO RT TASK (AD 2022-15-05) GEN AT HAECO LCQ BY V892444 PER NR 92940 4
- [SDR CALA2023040300962](https://openairdocs.org/sdr/CALA2023040300962.md): Flange · cracked · Mar 31, 2023 · N830UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > FR 68, STR 22 LH, FLANGE HAS CRACK AT LOWER RADIUS APPROX. 1.7 I NCHES LONG AND PENETRATES THROUGH TO IB FACE OF INNER CAP APPROX. 1.0 INCH LONG VERTICALLY. "CONTACT ENGINEERING FOR REPAIR INST RUCTIONS BEFORE NEXT FLIGHT." AD RELATED SUPPORT TASK(AD 2022-15
- [SDR CALA2023032900905](https://openairdocs.org/sdr/CALA2023032900905.md): Unknown · corroded · Mar 27, 2023 · N830UA · Airbus A319131 · Aileron Control System
  > RH WING T/E O/B SIDE PANEL BRACKET AT UNDERNEATH NO.5 AILERON HI NGE HAS CORROSION. PER HAECO LCQ NR 9294322/20322 RMVD AND RPLD BRACKET IAW SRM 51-72-11-911-001 BY MECH V061732 I NSP BY V061588
- [SDR CALA2023032700878](https://openairdocs.org/sdr/CALA2023032700878.md): Door Sill · corroded · Mar 25, 2023 · N830UA · Airbus A319131 · Fuselage Structure (General)
  > RH AFT DOOR SILL CORRODED MULTIPLE SPOTS. GEN BY V937268 ON HAEC O LCQ NR#9294323(20323) REPAIRED AFT RH DOOR SILL IAW A319 SRM 53-41-14-300-001 ACMP BY MECH V892938 INSP BY V892442
- [SDR CALA2023032400848](https://openairdocs.org/sdr/CALA2023032400848.md): Plate · corroded · Mar 22, 2023 · N830UA · Airbus A319131 · Fuselage Structure (General)
  > RH SHEAR PLATE B/W FRM 69 AND 70 CORRODED GEN BY V937268 ON HAEC O LCQ NR 9294337(20337) REMOVED AND REPLACED CORRODED SHEAR PLATE BETWEEN FR 69-70 R/H I AW A319 SRM 51-72-11 ACMP BY MECH V914121 INSP BY V916884
- [SDR CALA2023032000796](https://openairdocs.org/sdr/CALA2023032000796.md): Rib · chafed · Mar 17, 2023 · N830UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO DOOR FAIRING SUPPORT CHAFED THRU AT FWD LOWER EDGE. GE N BY N078599 ON HAECO LCQ NR 9294394/20394 REMOVED AND REPLACED AFT CARGO DOOR RIB IAW A319 SRM 51-72-11 AN D 51-42-11/001 ACMP BY MECH V077956 INSP BY V926223
- [SDR CALA2023031700771](https://openairdocs.org/sdr/CALA2023031700771.md): Unknown · corroded · Mar 15, 2023 · N830UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT LH DOOR SILL CORRODED AT FRM 68 GEN BY V937268 ON HAECO LCQ NR#9294327(20327) REPAIRED L2 DOOR SILL IAW A319 SRM 53-41-14-300-001 ACMP BY MEC H V077956 INSP BY V892442
- [SDR CALA2021070501029](https://openairdocs.org/sdr/CALA2021070501029.md): Transmitter · faulted · Jul 4, 2021 · N830UA · Airbus A319131 · Engine Oil Quantity
  > ENG 2 OIL QUANTITY INDICATION INOP ON ENG ECAM SYSTE M PAGE. OIL PRESSURE AND TEMP NORMAL. - ENG 2 IN FLT OIL QUANTITY WENT TO 0. RETURNED TO NORMAL ON TAXI BACK T O GATE. ALL OTHR INDCNS NORMAL. REMOVED AND REPLACED OIL QUANTITY TRANSMITTER, LEAKED CHECKED GO
- [SDR CALA2020032100682](https://openairdocs.org/sdr/CALA2020032100682.md): Strut · low · Mar 20, 2020 · N830UA · Airbus A319131 · Nose/Tail Landing Gear Strut/Axle
  > A/C RETURNED TO FIELD UNABLE TO RETRACT GEAR, CREW DID NOT MAKE A LOG WRITE UP FOUND LAST LEG REPORT NOTED LGCIU 1 AND 2 FAULT NLG SHOCK ABSORB ER. NOSE STRUT LOW NO EVIDENCE OF FLUID LEAKAGE, SERVICED STRUT REF AMM 12-12-32-610-001-A01 ADD EMP:U074071, LOTS O
- [SDR CALA2020012600263](https://openairdocs.org/sdr/CALA2020012600263.md): Controller · odor · Jan 24, 2020 · N830UA · Airbus A319131 · Pitot/Static Anti-Ice System
  > STBY R STAT DISPLAYED ON UPPER ECAM SCREEN. - ANTI ICE ACCOMPANIED WITH STRONG ELECTRICAL BURNING ODOR WHICH SUBSIDED A FTER5-10 MIN REMOVED PHC 3 TO INVESTIGATE SMOKE SMELL, CONTROLLER HAS BURNT SMELL. REPLACED IAW AMM 30-31-34 OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N830UA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N830UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N830UA/reports

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