# Service difficulty reports: N822UA

A list on [N822UA](https://openairdocs.org/aircraft/N822UA.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 · 103 reports

- [SDR CALA2026040715162](https://openairdocs.org/sdr/CALA2026040715162.md): Frame · cracked · Apr 6, 2026 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > RIGHT FR 20 DOUBLE JOGGLE LOWER AREA HOLE 12 HAD A CRACK INDICATION IN FRAME LAYER AT 6 O`CLOCK DIRECTION, 25% S.H. REPAIRED HOLE 12 AND ASSOCIATED HOLE 11 AT FR 20 RH LOWER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, REPAIR CATEGORY B.
- [SDR CALA2026040715161](https://openairdocs.org/sdr/CALA2026040715161.md): Frame · cracked · Apr 6, 2026 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE 6 HAD A CRACK INDICATION IN FRAME LAYER A 2 O`CLOCK DIRECTION, 60% S.H. REPAIRED HOLE 6 & ASSOCIATED HOLE 5 AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B.
- [SDR CALA2026040715160](https://openairdocs.org/sdr/CALA2026040715160.md): Frame · cracked · Apr 6, 2026 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE A HAD A CRACK INDICATION IN FRAME LAYER AT 2 O`CLOCK DIRECTION, 70% S.H. REPAIRED HOLE A AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR.
- [SDR CALA2026040715159](https://openairdocs.org/sdr/CALA2026040715159.md): Frame · cracked · Apr 6, 2026 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE B HAS CRACK INDICATION IN FRAME LAYER AT 2 O`CLOCK DIRECTION, 100% S.H. REPAIRED HOLE B AT FR 20 LT UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR.
- [SDR CALA2026040715158](https://openairdocs.org/sdr/CALA2026040715158.md): Frame · cracked · Apr 6, 2026 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FR 20 DOUBLE JOGGLE UPPER AREA HOLE D HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 2 O`CLOCK DIRECTION, 60% S.H. REPAIRED HOLE D & ASSOCIATED HOLE C AT FR 20 LEFT, UPPER DOUBLE JOGGLE AREA IAW SRM 53-11-12-300-012, CATEGORY B REPAIR
- [SDR CALA2026040815192](https://openairdocs.org/sdr/CALA2026040815192.md): Window Frame · cracked · Apr 2, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FWD WINDSHIELD WINDOW FRAME CENTER POST CONTINUITY FITTING MOST INBD FASTENER HOLE HAS 2 CRACK INDICATIONS 100% SH, AT THE 10:00 O'CLOCK AND 6:00 O'CLOCK POS. FWD LOOKING AFT. PER AAR LCQ NON ROUTINE 9298444/36444. ACCOMPLISHED INTERIM RPR AT LEFT FWD WI
- [SDR CALA2026040815190](https://openairdocs.org/sdr/CALA2026040815190.md): Window Frame · cracked · Apr 2, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT FWD WINDSHIELD WINDOW FRAME CENTER POST CONTINUITY FITTING MOST INBD FASTENER HOLE HAS A CRACK INDICATION 100% SH AT THE 5:00 CLOCK POS. FWD LOOKING AFT PER AAR LCQ NON ROUTINE 9298445/3 6445 ACCOMPLISHED INTERIM RPR AT LEFT FWD WINDSHIELD FR CTR POST
- [SDR CALA2026040915236](https://openairdocs.org/sdr/CALA2026040915236.md): Gusset · damaged · Mar 28, 2026 · N822UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LEFT FR 68 GUSSET NR 6, HAS 3 HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 68 GUSSET NR 6 WITH PARD D5348002075202 IAW SRM 51-72-11-911-001 AND 51-42-11/001.
- [SDR CALA2026033114963](https://openairdocs.org/sdr/CALA2026033114963.md): Gusset · damaged · Mar 28, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR 68 GUSSET NR 2 HAS THREE HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 68 GUSSET NR 2 WITH FABRICATED PART MATE RIAL 202473-063 IAW SRM 51-42-11/001, & SRM 51-31-00/001.
- [SDR CALA2026033114962](https://openairdocs.org/sdr/CALA2026033114962.md): Gusset · damaged · Mar 28, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR 66 GUSSET NR 6 HAS (3EA) HOLES WITH A OUT OF ROUND CONDITION HOLES NR 2, NR 3 FROM TOP ARE STEPPED. REMOVED AND REPLACED LH FR66 GUSSET #6 WITH PART D5348002075802 IAW SRM 51-72-11-911-001 AND SRM 53-41-12-300-018.
- [SDR CALA2026040915234](https://openairdocs.org/sdr/CALA2026040915234.md): Gusset · damaged · Mar 27, 2026 · N822UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LEFT FR 66 GUSSET NR 7, HOLE NR 1, GUSSET NR 8, HOLE NR 2, HAS AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR 66 GUSSET NR 7 & 8 WITH PART 2EA D534 800207 5802 IAW SRM 51-72-11-911-001 SRM 51-42-11/001.
- [SDR CALA2026033014908](https://openairdocs.org/sdr/CALA2026033014908.md): Gusset · damaged · Mar 27, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR 69 GUSSET NR 4 HAS (5EA) HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPLACED LT FR68 GUSSET NR 4 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/ 001, & SRM 53-41-12-300-018.
- [SDR CALA2026033014907](https://openairdocs.org/sdr/CALA2026033014907.md): Plate · damaged · Mar 27, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR 68 GUSSET NR 7 HAS (4EA) HOLES WITH AN OUT OF ROUND CONDITION. REMOVED AND REPACED LT FR 68 GUSSET NR 7 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44- 11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/0 01, AND 53-41-12-300-018.
- [SDR CALA2026033014906](https://openairdocs.org/sdr/CALA2026033014906.md): Plate · damaged · Mar 27, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR66 GUSSET NR 4 HOLE 3 FROM TOP HAS AN OUT OF ROUND CONDITION WITH CHAMFER. REMOVED AND REPLACED LT FR66 GUSSET NR 4 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/001, AND SRM 53-41
- [SDR CALA2026033014905](https://openairdocs.org/sdr/CALA2026033014905.md): Plate · damaged · Mar 27, 2026 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR66 GUSSET NR 5 HAS (3EA) HOLES WITH A OUT OF ROUND CONDTI ON WITH CHAMFER. REMOVED AND REPLACED LT FR66 GUSSET NR 5 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, SRM 51-44 -11/001, SRM 51-75-12-911-006, SRM 53-41-79-02-A, SRM 51-76-11/001, AND SRM 53-41-
- [SDR CALA2026090119160](https://openairdocs.org/sdr/CALA2026090119160.md): Skin · dented · Mar 13, 2026 · N822UA · Airbus A319131 · Passenger/Crew Doors
  > DENT FOUND ON WALKAROUND AT DOOR 1 LEFT. DENT IS LOCATED APPROXIMATELY 5 INCHES AFT OF FR23 AND BETWEEN STR L24 AND L25. DENT MEASURES 1 INCH BY.489 INCH AND.133 INCH DEPTH. EVALUATED DENT PER SRM 53-11-11-283-012. DENT IS TYPE 1 IN ZONE 1 AREA 2. DENT DRE
- [SDR CALA2025110310840](https://openairdocs.org/sdr/CALA2025110310840.md): Light · inoperative · Oct 30, 2025 · N822UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY AFT LIGHT MESSAGE POPULATED WHEN PERFORMING EMERGENCY LIGHT TEST VIA PTP. NO SYS OK. REMOVED AND REPLACED EPSU BATTERY AFT LIGHT PER PTP IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. PERFORMED OPS CHECK OF THE EMERGENCY POWER SUPPLY UNITS,
- [SDR CALA2025102410498](https://openairdocs.org/sdr/CALA2025102410498.md): Actuator · faulted · Oct 20, 2025 · N822UA · Airbus A319131 · Fuel Controlling System
  > ENG 1 COMPRESSOR VANEECAM CREW REPORTED THAT ABORTED T-OFF AT 70 KNOTS. (LOW SPEED). DUE TO #1 ENG SN. V10406 (TSI= 1990 HRS / 1082 CYC) DUE TO ENG1 COMP VANE ECAM. FADEC 1A SHOW ENG1 COMP VANE CH. A VSV ACT / HC/ EEC1 CELL 38 (FAULT CODE SVATK). AHM SHOW DURI
- [SDR CALA2025081407726](https://openairdocs.org/sdr/CALA2025081407726.md): Bottle · no discrepancy · Aug 13, 2025 · N822UA · Airbus A319131 · Emergency Equipment
  > DOOR 2R SLIDE PRESS GAUGE IN THE RED. FOUND WITHIN LIMITS REF AMM 25-62-00-210-001-A GAUGE MODEL A.
- [SDR CALA2025080707447](https://openairdocs.org/sdr/CALA2025080707447.md): Brake · faulted · Aug 4, 2025 · N822UA · Airbus A319131 · Landing Gear Brake System
  > LARGE SWERVE AT 90KTS, REJECTED. SUSPECT BRAKE GRABBED. REMOVED AND REPLACED LT OTBD BRAKE IAW AMM TASK 32-42-27-400-001-A. OPS CHECKED GOOD.
- [SDR CALA2025040303468](https://openairdocs.org/sdr/CALA2025040303468.md): Light · malfunctioned · Mar 29, 2025 · N822UA · Airbus A319131 · Passenger Compartment Lighting
  > EMERGENCY EXIT LIGHT ROW 22D ILLUMINATES INTERMITENTLY OVERHEAD LIGHT SEAT 22D ILLUMINATING RED. DEACTIVATED LIGHT SUFFICIENT LIGHTING IN CABIN. COMPLIED WITH MEL 3320A LIGHT IS A CABIN OVERHEAD LIGHT, NOT AN EMERGENCY LIGHT. PLACE ON MEL 3320A. PULLED AND COL
- [SDR CALA2025040203425](https://openairdocs.org/sdr/CALA2025040203425.md): Bottle · low pressure · Mar 26, 2025 · N822UA · Airbus A319131 · Escape Slide
  > DOOR 2R PRESSURE RED INSPECTED SLIDE PRESSURE REF AMM 25-62-00; PRESSURE IS WITHIN LIMITS AT THIS TIME.
- [SDR CALA2024103000970](https://openairdocs.org/sdr/CALA2024103000970.md): Lever · binding · Oct 26, 2024 · N822UA · Airbus A319131 · Passenger/Crew Doors
  > DOOR 2R HARD TO DISARM. LEVER SEEMS TO HANG UP ON SOMETHING. POP PINGSOUND. NOT PRESSURIZATN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CHECK THE OPERATION OF THE EMERGENCY ESCAPE SLIDE ARM AND DISARM FUNCTION AFTER YOU ACCOMPLISH THE RENDER SAFE CHEC
- [SDR CALA2024052901623](https://openairdocs.org/sdr/CALA2024052901623.md): Computer · malfunctioned · May 27, 2024 · N822UA · Airbus A319131 · Air Data Computer
  > ON TAKEOFF ROLL CA AIRDATA LOST UPDATED MANHOURS REQUIRED. CONTINUED WITH TSM 31-63-82-810-801-A. STILL HAVE ADC 1 BUS FULT IN I/P TEST. REMOVED AND REPLACED ADIRU 1 REF AMM 34-12-34-000-001-A/34-12-34-400-001-A. INSTALLATION TESTS PASSED. STILL MISSING AIR DA
- [SDR CALA2024032500853](https://openairdocs.org/sdr/CALA2024032500853.md): Lock · misinstalled · Mar 24, 2024 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > ON MARCH 24, 2024 WHILE PERFORMING A CABIN CHECK, 2 SERVICE, AND LIFE VEST WRITE UPS ON A/C 4022 FOUND MULTIPLE SEAT ASSEMBLY ATTACH BOLT SAFETY LOCKS NOT PROPERLY INSTALLED OR DAMAGED. WHILE TRYING TO INSTALL CLIPS THE CORRECT WAY DISCOVERED 7 ROWS OF SEATS,
- [SDR CALA2023032200829](https://openairdocs.org/sdr/CALA2023032200829.md): Skin · corroded · Mar 21, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > AFT BULK HEAD FR 65 R/H 32 SKIN AND STRINGER CORROSION PER HAECO LCQ NR 9290590/22590 GENERATED BY V798788 PART 3 OF THE LATEST REVISION OF ECRA 5341-01379 ON OR BEFORE 20 LATEST REVISION OF ECRA 5341-01379 ON OR BEFORE 20 SEP 2023. TOLERANCE UNDER 14CFR 26.43
- [SDR CALA2023032200834](https://openairdocs.org/sdr/CALA2023032200834.md): Stringer · cracked · Mar 21, 2023 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > STR31R PRODUCED CRACK INDICARIONS APPROX. 7 INCHES FWD FR66 BELO W THE OUTFLOW VALVE DURING HFEC INSPECTION.GENERATED AT HAECO LC Q PER NR 9290886 (22886) BY V061690 REMOVED AND REPLACED STR31 RT IAW A319 SRM 51-72-11 ACPM BY V052 030
- [SDR CALA2023032200822](https://openairdocs.org/sdr/CALA2023032200822.md): Frame · cracked · Mar 20, 2023 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68 LH AT STR 22 WEB FLANGE HAS CRACK INDICATION IN RADIUS ABO VE LOWER IB DOOR STOP BOLT APPROX.750 INCHES LONG STARTING AT I B RADIUS PER HAECO LCQ NR 9290477/22477 GENERATED BY V892444 48667 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION AT OR BEFORE
- [SDR CALA2023032000808](https://openairdocs.org/sdr/CALA2023032000808.md): Unknown · corroded · Mar 19, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO FR 59 STR 38 SIGNS OF CORROSION (A3NB 53-4-6179). GENE RATED BY V798788 PER NR 9290613 (22613) AT HAECO LCQ. REMOVED AND REPLACED STRINGER 38RT FR59 IAW A319 SRM 51-72-11. P ERFORMED BY V052030 AND INSP BY V892285.
- [SDR CALA2023032000794](https://openairdocs.org/sdr/CALA2023032000794.md): Unknown · corroded · Mar 17, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO BETWEEN FR 54 AND FR 55 LST 43 CORROSION PER HAECO LCQ NR 9290598/22598 GENERATED BY V798788 REPAIRED STR 43 LEFT IN AFT CARGO PIT BETWEEN FRAME 54-55 IAW A3 19 SRM 53-41-13-300-10 ACMP BY MECH V052030 INSP BY V935513
- [SDR CALA2023030900649](https://openairdocs.org/sdr/CALA2023030900649.md): Fitting · corroded · Mar 7, 2023 · N822UA · Airbus A319131 · Fuselage Main, Frame
  > AFT CABIN AT R2 FRAME 68 HAS CORROSION AROUND NUT PLATE HOLE(A3N B-53-3-6357) GENERATED AT HAECO LCQ PER NR 9290811 (22811) BY V0 52030 LE REWORK =0.020?. REWORK IS BEYOND ALLOWABLE LIMIT. REPAIRED DI WITH AN INSPECTION THRESHOLD FROM AIRCRAFT FIRST FLT 24000F
- [SDR CALA2023030600627](https://openairdocs.org/sdr/CALA2023030600627.md): Door Sill · corroded · Mar 3, 2023 · N822UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT R2 DOOR SILL CORRODED MULTIPLE PLACES PER HAECO LCQ N/R 9290 546/22546 GENERATED BY V937268 REMOVED AND REPLACED R-2 DOOR SILL AT FR 66-68 IAW A319 SRM 51-7 2-11-911-001 ACMP BY MECH V061650 INSP V061757
- [SDR CALA2023030600626](https://openairdocs.org/sdr/CALA2023030600626.md): Door Sill · corroded · Mar 3, 2023 · N822UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT L2 DOOR SILL FASTENER HOLE CORRODED AT FRM 66 PER HAECO LCQ N/R 9290545/22545 GENERATED BY V937268 REMOVED AND REPLACED L-2 DOOR SILL AT FRM 66-68 IAW A319 SRM 51- 72-11-911-001 ACMP BY MECH V061630 INSP V061757
- [SDR CALA2023030600625](https://openairdocs.org/sdr/CALA2023030600625.md): Floor Panel · corroded · Mar 3, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO ENTRY DOOR FLOOR PANEL HAS CORROSION PER HAECO LCQ N/R 9290604/22604 GENERATED BY V798788 REMOVED AND REPLACED AFT CARGO ENTRY DOOR COVER SHEET/DOOR FLOOR PANEL IAW A319 SRM 51-72-11 DND SRM 51-42-11 ACMP BY MECH V9290 87 INSP V061757.
- [SDR CALA2023030100578](https://openairdocs.org/sdr/CALA2023030100578.md): Tray · none · Feb 28, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CABIN WET AREA RH FR68-FR69 O/B TRAY FASTENER HOLES ELONGATE D PER HAECO LCQ N/R 9290816/22816 GENERATED BY V061629. FABRICATED TRAY AT AFT CABIN WET AREA R/H FR68-69 O/B IAW A319 D RAWING 18D53480019 & REMOVED & REPLACED OLD TRAY IAW A319 SRM 51 -72-11-91
- [SDR CALA2023030100573](https://openairdocs.org/sdr/CALA2023030100573.md): Support · cracked · Feb 27, 2023 · N822UA · Airbus A319131 · Fuselage Structure (General)
  > LH E&E COMPARTMENT FR 11 WEB SUPPORT CRACKED PER HAECO LCQ N/R 9 290215/22215 GENERATED BY V798788 REMOVED/REPLACED WEB @ FR11 L/H IAW A-319 SRM TASK 51-42-11/001. SRM TASK 51-44-11/001 AND SRM 51-21-11/001 PER MECH V929087 INS P V061757.
- [SDR CALA2023021600449](https://openairdocs.org/sdr/CALA2023021600449.md): Panel · corroded · Feb 15, 2023 · N822UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT WET AREA LH SHEAR PLATE BETWEEN FRM 69 AND 70 FASTENER HOLE CORRODED (A3NB-53-3-6357) PER HAECO LCQ NON ROUTINE 9290558/2255 8 GENERATED BY V937268 REMOVED AND REPLACED CORRODED SHEAR PLATE AT L/H AFT WET AREA BE TWEEN FR 69+70 IAW A319 SRM 51-42-11/001+51
- [SDR CALA2023021400434](https://openairdocs.org/sdr/CALA2023021400434.md): Unknown · cracked · Feb 13, 2023 · N822UA · Airbus A319131 · Doors
  > RH INTERNAL EMERGENCY DOOR FWD AND AFT WEB SUPPORTS SIGNS OF CRACK (SUPPORT TASK). GENERATED BY V798788 AT HAECO LCQ PER NR 9290 486 (22486). REMOVED AND REPLACED RH EMERGENCY DOOR FWD AND AFT WEB SUPPORTS IAW A319 SRM 51-42-11/001 PARG. E. PERFORMED BY V92908
- [SDR CALA2023020600337](https://openairdocs.org/sdr/CALA2023020600337.md): Not Reported · not reported · Feb 5, 2023 · N822UA · Airbus A319131 · Rudder, Plate/Skin
  > R/H RUDDER SIDE PANEL PRODUCED AN INDICATION OF WATER INGRESS AP PROX. 178-186INS. FROM BOTTOM AND 2-6INS. FROM T/E. {A3NB-55-3-6 024} PER HAECO NON ROUTINE 9290079/22079 GENERATED BY V061690 AT HAECO LCQ REPAIRED RUDDER PN D5547100200000B TS-2319 178 TO 186 I
- [SDR CALA2022080801996](https://openairdocs.org/sdr/CALA2022080801996.md): Fuel Cap · missing · Aug 7, 2022 · N822UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/08/22. PDA 3 FOUND FUEL CAP MISSING. INSTALLED CAP COUPLING REFUEL UNDERWING NOW OK.
- [SDR CALA2021070101016](https://openairdocs.org/sdr/CALA2021070101016.md): Window Frame · damaged · Jul 1, 2021 · N822UA · Airbus A319131 · Fuselage Main, Structure
  > REFERENCE ECRA 5310-07862 LH FR4 LATERAL WINDOW FRAME UPPER STIF FENER-INTERIM REPAIR. PER PART 1 STEP "8" "BEFORE FURTHER FLIGHT PERFORM A PERMANENT REPAIR PER PART 3 OF ECRA 5310-07862." ACCOMPLISH A PERMANENT REPAIR AT LH LATERAL WINDSHIELD FR 4 STIF FENE
- [SDR CALA2019060400877](https://openairdocs.org/sdr/CALA2019060400877.md): Cap · missing · Jun 2, 2019 · N822UA · Airbus A319131 · Fuel Storage
  > PDA 2 REFUELING CAP FOUND MISSING BY FUELER.
- [SDR CALA2019032200452](https://openairdocs.org/sdr/CALA2019032200452.md): Wire Harness · damaged · Mar 21, 2019 · N822UA · Airbus A319131 · Light System Wiring
  > (SUPPORT TASK) EEPL WIRING HARNESS FOUND DAMAGED AT SEAT ROW 22A BC. N/R 9617226. REMOVED AND REPLACED EEPL WIRING HARNESS FOR SEAT ROWS 21ABC AND 22 ABC IAW AMM 33-51-22-400-802C1. OPS CHK GOOD IAW AMM 33-51-00-710-008-A.
- [SDR CALA2018072401690](https://openairdocs.org/sdr/CALA2018072401690.md): Check Valve · unserviceable · Jul 24, 2018 · N822UA · Airbus A319131 · Air Distribution System
  > AIR RETURN. AFTER LIFT OFF RECEIVED RECEIVED AVEC EXTRACT FAN FAULT WITH BLOWER FAN ON MEL. UNABLE TO PRESSURIZE AC. FOUND AIR INLET CHECK VALVE STUCK OPEN. VALVE DID CLOSED AFTER CLAMP WAS REMOVED. NEW VALVE AND CLAMP PLACED IN FLT DECK. REPLACED AIR CHECK VA
- [SDR CALA2018040901138](https://openairdocs.org/sdr/CALA2018040901138.md): Power Supply · no test · Apr 9, 2018 · N822UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHT TEST FAILED. FAULTED LEFT FWD EPSU, REPLACED POWER SUPPLY UNIT AND BATTERY PACK, TESTED, NO FAULTS IAW AMM 33-51-38.
- [SDR CALA2017100903569](https://openairdocs.org/sdr/CALA2017100903569.md): Lens · missing · Oct 9, 2017 · N822UA · Airbus A319131 · Emergency Lighting
  > FWD LT ENTRY DOOR, EMERGENCY LIGHT, ON THE LOWER FWD WALL, OTBD OF FA SEAT, IS MISSING THE LENS. REPLACED THE LENS. OPS CHECKED GOOD.
- [SDR CALA2017032400677](https://openairdocs.org/sdr/CALA2017032400677.md): Safety Valve · damaged · Mar 24, 2017 · N822UA · Airbus A319131 · Hydraulic System, Main
  > G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. FOUND SAFETY VALVE 49GA IN RIGHT WHEEL WELL DAMAGED AND CAUSING FLUID LOSS. REPLACED LANDING GEAR SAFETY VALVE IAW AMM 32-31-17. SERVICED GREEN HYD IAW AMM12-12-29. TESTED NORMAL IAW AMM32-33
- [SDR CALA2017032100671](https://openairdocs.org/sdr/CALA2017032100671.md): Power Supply · inoperative · Mar 21, 2017 · N822UA · Airbus A319131 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTS OPERATIONAL CHECK THE TEST FAILED, MESSAGE ESPU BATTERY FWD L 33-51-38. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 10WL IAW 33-51- 38. OPS CHECK GOOD.
- [SDR CALA2016070195501](https://openairdocs.org/sdr/CALA2016070195501.md): Connector · loose · Jun 28, 2016 · N822UA · Airbus A319131 · Engine Fuel System Wiring
  > NR 2 ENGINE INCREASING SURGE DURING CLIMB, CLOSE TO NORMAL AT IDLE. FOUND J1 EEC CONNECTOR LOOSE. SECURED, PERFORMED POWER ASSURANCE RUNS TWICE. ALL ENGINE PARA NORMAL
- [SDR CALA2016050495328](https://openairdocs.org/sdr/CALA2016050495328.md): Diaphragm · damaged · May 1, 2016 · N822UA · Airbus A319131 · Passenger/Crew Doors
  > DUE TO 2L DOOR SLIDE DEPLOYMENT, EMER CYLINDER DIAPHRAGM SHOULD BE REPLACED. REPLACED 2L DOOR EMER CYLINDER DIAPHRAGM IAW AMM 52-13-14. CHECKED OPERATIONS, ALL GOOD.

Next page: https://openairdocs.org/aircraft/N822UA/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 = 'N822UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N822UA/reports

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