# Service difficulty reports: N813UA

A list on [N813UA](https://openairdocs.org/aircraft/N813UA.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 · 113 reports

- [SDR CALA2026062217229](https://openairdocs.org/sdr/CALA2026062217229.md): Fuel Cap · missing · Jun 19, 2026 · N813UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING SDR INFO UPDATED SDR FILED. FUELER REPORTS MISSING FUEL CAP REMOVED AND REPLACED REFUEL CAP IAW AMM 28-25-41.
- [SDR CALA2025020402202](https://openairdocs.org/sdr/CALA2025020402202.md): Fuel Cap · missing · Jan 31, 2025 · N813UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING. SEARCH AREA NO FUEL CAP FOUND,REF LOG PG 3725830 FUEL CAP MISSING SEARCHED RAMP AREA, FUEL CART, AND WORK STAND, TALKED TO FUELER AND HE SAID AIRCRAFT ARRIVED WITHOUT CAP,
- [SDR CALA2024041001024](https://openairdocs.org/sdr/CALA2024041001024.md): Hydraulic System · low quantity · Apr 6, 2024 · N813UA · Airbus A319131 · Hydraulic System, Main
  > HYDRAULIC QUANTITY LOW LEFT OR GREEN SYSTEM. PRESSURIZED, AND CHECKED FOR ANY OBVIOUS LEAKS. SERVICED GREEN SYSTEM PER AMM 12-12-29.
- [SDR CALA2024011900137](https://openairdocs.org/sdr/CALA2024011900137.md): Fuel Cap · missing · Jan 16, 2024 · N813UA · Airbus A319131 · Fuel Storage
  > PDA 2, FUELER REPORTS RH UNDERWING FUEL CAP MISSING. FUEL CAP MISSING REQUEST CDL 28A COMPLIED WITH CDL 28A DISPATCH DESK: 13 NAME: MC DATE: 16-JAN-24- OK TO DEFER FUEL CAP MISSING FUEL CAP AND LANYARD MISSING. NO DAMAGE AND NO FUEL LEAKING
- [SDR CALA2023042401242](https://openairdocs.org/sdr/CALA2023042401242.md): Frame · cracked · Apr 24, 2023 · N813UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 16 UPPER DOUBLE JOGGLE AREA HOLE 6 HAS CRACK INICATION IN FRAME LAYER AT 2 O''CLOCK DIRECTION PER HAECO LCQ N/R 9298535/ 40535 GEN BY V892444 JOGGLE REPAIRED HOLES #E AND #F PER PART 2 OF THE LATEST 38884 TOTAL AIRCRAFT CYCLES. ACCOMPLISH REPEAT INSPECTI
- [SDR CALA2023042401241](https://openairdocs.org/sdr/CALA2023042401241.md): Frame · cracked · Apr 24, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > LH FR 16 CROSSBEAM HOLE H2,H3 AND H4 HAVE CRACK INICATIONS IN FR AME LAYER PER HAECO LCQ N/R 9298767/40767 GEN BY V892444 CROSSBEAM JUNCTION HOLES #H2, H3, H4 PER PART 2 OF THE LATEST 67384 TOTAL AIRCRAFT CYCLES. REVISION OF ECRA 5310-08147 ON OR BEFORE THE AI
- [SDR CALA2023042401225](https://openairdocs.org/sdr/CALA2023042401225.md): Fitting · cracked · Apr 21, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68 STR 22 LH HAS CRACK AT FLANGE LOWER RADIUS BEGINS AT IB RADIUS & EXTENDS OB APPROX 1.20" PER LCQ N/R 9298469/ 40469, AT LH FR68 STR22LH PER PART 2A OF LATEST REVISION OF ACFT FLT CYCLES. PERFORM REPEAT INSPS NOT TO EXCEED ECRA 5341-01388 ON OR BEFORE AC
- [SDR CALA2023042401217](https://openairdocs.org/sdr/CALA2023042401217.md): Frame · cracked · Apr 21, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68 STR 22 RH HAS CRACK AT FLANGE LOWER RADIUS BEGINS AT IB RADIUS AND EXTENDS OB APPROX.70" PER HAECO LCQ N/R 9298470/4047 0 FR68 STR22RH PER PART 2A OF THE LATEST REVISION OF ECRA CYCLES. PERFORM REPEAT INSPECTIONS NOT TO EXCEED NTERVALS OF 5341-01387 ON
- [SDR CALA2023042401216](https://openairdocs.org/sdr/CALA2023042401216.md): Frame · corroded · Apr 21, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > L-1 DOOR CUTOUT FR 20 JUST ABOVE GIRT BAR FITTING HAS CORROSION PER HAECO LCQ N/R 9298511/40511 FACE REPAIR AT Z-520 FLOOR LEVEL PER PART 2 OF THE LATEST 63784 TOTAL AIRCRAFT CYCLES. REVISION OF ECRA 5311-02974 ON OR BEFORE THE AIRCRAFT REACHES ACCOMPLISHED IN
- [SDR CALA2023042401215](https://openairdocs.org/sdr/CALA2023042401215.md): Frame · corroded · Apr 21, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > R-1 DOOR CUTOUT FR 20 JUST ABOVE GIRT BAR FITTING HAS CORROSION WEB FACE AT Z-520 FLOOR LEVEL PER PART 3 OF THE LATEST REVISION AIRCRAFT FLIGHT CYCLES OF ECRA 5311-02975 ON OR BEFORE THE AIRCRAFT REACHES 50984 TOTAL INTERIM REPAIR ACCOMPLISHED IAW ECRA 5311-0
- [SDR CALA2023042101204](https://openairdocs.org/sdr/CALA2023042101204.md): Flange · cracked · Apr 20, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68 STR 22 LH HAS CRACK AT FLANGE LOWER RADIUS BEGINS AT IB RADIUS AND EXTENDS OB APPROX 1.20" PER HAECO LCQ N/R 9298469/ 40469 GEN BY V892444 PART AT LH FR68 STR22LH PER PART 2A OF THE LATEST REVISION OF AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTIONS NO
- [SDR CALA2023042101203](https://openairdocs.org/sdr/CALA2023042101203.md): Fitting · corroded · Apr 20, 2023 · N813UA · Airbus A319131 · Fuselage Main, Frame
  > L-1 DOOR CUTOUT FR 20 JUST ABOVE GIRT BAR FITTING HAS CORROSION PER HAECO LCQ N/R 9298511/40511 GEN BY V926223 FACE REPAIR AT Z-520 FLOOR LEVEL PER PART 2 OF THE LATEST 63784 TOTAL AIRCRAFT CYCLES. REVISION OF ECRA 5311-02974 ON OR BEFORE THE AIRCRAFT REACHES
- [SDR CALA2023042101202](https://openairdocs.org/sdr/CALA2023042101202.md): Fitting · corroded · Apr 20, 2023 · N813UA · Airbus A319131 · Fuselage Main, Frame
  > R-1 DOOR CUTOUT FR 20 JUST ABOVE GIRT BAR FITTING HAS CORROSION PER HAECO LCQ N/R 9298512/40512 GEN BY V926223 WEB FACE AT Z-520 FLOOR LEVEL PER PART 3 OF THE LATEST REVISION AIRCRAFT FLIGHT CYCLES OF ECRA 5311-02975 ON OR BEFORE THE AIRCRAFT REACHES 50984 TOT
- [SDR CALA2023042101201](https://openairdocs.org/sdr/CALA2023042101201.md): Flange · cracked · Apr 20, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > FR 68 STR 22 RH HAS CRACK AT FLANGE LOWER RADIUS BEGINS AT IB RADIUS AND EXTENDS OB APPROX.70" PER HAECO LCQ N/R 9298470/4047 0 GEN BY V892444 FR68 STR22RH PER PART 2A OF THE LATEST REVISION OF ECRA CYCLES. PERFORM REPEAT INSPECTIONS NOT TO EXCEED NTERVALS OF
- [SDR CALA2023033100940](https://openairdocs.org/sdr/CALA2023033100940.md): Fitting · cracked · Mar 30, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD RH CONTINUITY FITTING HAS CRACK INDICATION ON UPPER LEG.400 OB OF ADJACENT FRAME PER HAECO LCQ N/R 9298650/40650 GEN BY V892444 REMOVED AND REPLACED CONTINUITY FITTING AT FR 4 R/H SIDE WINDSHI ELD IAW A319 ECRA 5310-08136 CAT A REPAIR NO FURTHER IN
- [SDR CALA2023033100939](https://openairdocs.org/sdr/CALA2023033100939.md): Fitting · cracked · Mar 30, 2023 · N813UA · Airbus A319131 · Fuselage Main, Structure
  > RH FR 68 LOWER AFT CORNER FITTING HAS 2EA CRACK INDICATIONS IN THIRD HOLE FROM THE TOP PER HAECO LCQ N/R 9298667/40667.
- [SDR CALA2023033100938](https://openairdocs.org/sdr/CALA2023033100938.md): Stringer · corroded · Mar 30, 2023 · N813UA · Airbus A319131 · Fuselage Structure (General)
  > RH MAIN CABIN AFT WET AREA ON STGR 24R AT FR 70 HAS CORROSION PER HAECO LCQ N/R 9298766/40766.
- [SDR CALA2023031700776](https://openairdocs.org/sdr/CALA2023031700776.md): Floor Support · corroded · Mar 16, 2023 · N813UA · Airbus A319131 · Fuselage Structure (General)
  > AFT WET AREA R/H DOOR SILL FR 66 HAS CORROSION PER HAECO LCQ N/R 9298480/40480 GEN BY V926223 REMOVED CORROSION ON THE DOOR SILL AT FR66 AFT WET AREA FOUND TO BE OUT OF LIMITS PERFORMED REPAIR IAW A319 SRM 53-41-14-283-002 53-41-14-300-001 REPAIR CAT A NO FURT
- [SDR CALA2023031700775](https://openairdocs.org/sdr/CALA2023031700775.md): Floor Support · corroded · Mar 16, 2023 · N813UA · Airbus A319131 · Fuselage Structure (General)
  > AFT WET AREA L/H DOOR SILL FR 68 HAS CORROSION PER HAECO LCQ N/R 9298478/40478 GEN BY V926223 REMOVED CORROSION ON THE DOOR SILL AT FR68 AFT WET AREA FOUND TO BE OUT OF LIMITS PERFORMED REPAIR IAW A319 SRM 53-41-14-283-002 53-41-14-300-001 REPAIR CAT A NO FURT
- [SDR CALA2023031700774](https://openairdocs.org/sdr/CALA2023031700774.md): Plate · bent · Mar 16, 2023 · N813UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO DOOR CUT OUT AT SILL BENT FROM FR25-FR27 PER HAECO LCQ N/R 9298378/40378 GEN BY V926223 RMVD AND RPLD PLATE SEAL BUTT AND BRACKET AT FWD CARGO DOOR CUT OUT DOOR SILL FROM FR25 TO FR27 IAW A319 SRM 51-42-11-001 TREATE D PRIMED AND TOP COAT AREA SRM 51
- [SDR CALA2022103102993](https://openairdocs.org/sdr/CALA2022103102993.md): Actuator · fault message · Oct 30, 2022 · N813UA · Airbus A319131 · Compressor Bleed Valve
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. - ENG ENG 1 ON INITIAL TO ROLL PERFORMED FADEC 1A&B BITE AND FOUND CHA AND CHB VSV ACT/HC/EEC1 REMOVED #1 ENG VSV ACTUATOR AS PER AMM 75-32-41-000-010-A. INSTALLED VSV ACTUATOR PER AMM 75-32-41-400-010..NEED TO P
- [SDR CALA2022090502276](https://openairdocs.org/sdr/CALA2022090502276.md): Fuel Cap · missing · Sep 5, 2022 · N813UA · Airbus A300* · Aircraft Fuel System
  > PDA 3 CREW REPORTS FUEL CAP MISSING CREW APPLIED CDL 28A. FUEL CAP MISSING PER CDL. INSTALLED FUEL CAP UNDER R/H WING. OPS GOOD.
- [SDR CALA2022032100702](https://openairdocs.org/sdr/CALA2022032100702.md): Connector · damaged · Mar 19, 2022 · N813UA · Airbus A300* · Air Conditioning System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022032100702 SUBMITTED ON 21/03/22.FOUND BLOWER FAN 20HQ CONNECTOR WIRING WITH DAMAGED SHEATHING.REF ESPM 20 53 20, OUTER MATERIAL THAT WAS WRITTEN UP IS A COLOR COAT WHICH HAS NO EFFECT ON INSULA
- [SDR CALA2021120602253](https://openairdocs.org/sdr/CALA2021120602253.md): None · cracked · Dec 5, 2021 · N813UA · Airbus A319131 · Nacelle/Pylon Structure
  > PDA 2 #1 ENG INBOARD T-R TO PYLON FLEX SEAL SEGMENT ((SECOND FROM AFT)) CRACKED AND MISSING -- SEE PHOTO AND ACCOMPLISH PERMANENT REPAIR PER PART 3 WITHIN 50 FLIGHT HOURS. REF ECRA 5450-02357 REV-B FIG 3 ITEM 110 CRACKED AND MISSING. PERFORMED INTERIM REPAIR P
- [SDR CALA2019040500534](https://openairdocs.org/sdr/CALA2019040500534.md): Mount · cracked · Apr 4, 2019 · N813UA · Airbus A319131 · Engine Mount Section
  > METAL IS CRACKING AT INBOARD PYLON ENGINE ATTACH POINT ON NO.1ENG INE. TAPED ITEM 110 (MISSING) REF ECRA 5450-02357 PART 1D.
- [SDR CALA2018060531355](https://openairdocs.org/sdr/CALA2018060531355.md): Battery · discharged · May 24, 2018 · N813UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY, AFT LEFT 13WL FAILED AN EMERGENCY LIGHTS OPS TEST. REMOVED AND REPLACED THE BATTERY 13WL IAW AMM 33-51-38-4 00-008A. ACCOMPLISHED AN OPERATIONAL TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-001A, TESTED OK.
- [SDR CALA2017101303578](https://openairdocs.org/sdr/CALA2017101303578.md): Outflow Valve · malfunctioned · Oct 13, 2017 · N813UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > VENT SKIN VALVE FAULT ON ECAM. PRESSURIZATION ISSUE. EMERGENCY DECLARED. REPLACED SKIN AIR OUTLET VALVE REF. MM 21-26-53. OPERATIONAL CHECKED GOOD IAW MM 21-26-00.
- [SDR CALA2017091803220](https://openairdocs.org/sdr/CALA2017091803220.md): Unknown · odor · Sep 18, 2017 · N813UA · Airbus A319131 · Air Distribution System
  > BURNING ELECTRICAL ODOR THGROUGH OUT AIRCRAFT. HAPPEN DURING DECENT. INSPECTED THE CARGO BAYS, AVIONIC COMPARTMENTS, GALLEYS AND CABIN. HAD CREW RUN BOTH ENGINES IDLE AT GATE WITH PACKS ON. NO ELECTRICAL ODOR NOTICED AFTER GROUND AIR WAS REMOVED. ACFT OK
- [SDR CALA2017082502896](https://openairdocs.org/sdr/CALA2017082502896.md): Connector · faulty · Aug 25, 2017 · N813UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE AT ROWS 12A AND 23A. R & R THE CONNECTORS AT SEATS 12A AND 23A. OPS CHECKED GOOD.
- [SDR CALA2017050101222](https://openairdocs.org/sdr/CALA2017050101222.md): Power Supply · inoperative · May 1, 2017 · N813UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED AT PTP PANEL. REPLACED THE EPSU AT 11WL IAW AMM 33-51-38 PB401. OK FOR SERVICE
- [SDR CALA2017022000439](https://openairdocs.org/sdr/CALA2017022000439.md): Power Supply · inoperative · Feb 20, 2017 · N813UA · Airbus A319131 · Emergency Lighting
  > BATTERY EMERG POWER SUPPLY ON RT INOP. REPLACED BATTERY EMERG POWER SUPPLY IAW AMM 33-51-38-000-001-A, AND 33-51-38-400-001-A. OPERATIONAL TEST OK.
- [SDR CALA2017010600020](https://openairdocs.org/sdr/CALA2017010600020.md): Fire Warning · false activation · Jan 6, 2017 · N813UA · Airbus A319131 · Fire Detection
  > ENG START AND IGN PYLON PEDESTAL INTERMITTENTLY ILLUMINATING FIRE NO FIRE WARNING OR ECAM DEFERRED DIRECTLY BY TOMC FIRE LIGHT ON NR 1 ENG CONTROL PANEL INTERMITTENT INOP. ACCOMPLISH FIM TASK 26-21-00-810-819-B FOR POSSIBLE ENGINE NOR1 FIRE, OR ENGINE NR 1 FIR
- [SDR CALA2016101995816](https://openairdocs.org/sdr/CALA2016101995816.md): Door Sill · corroded · Oct 17, 2016 · N813UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CORROSION AT R1 DOOR SILL FWD GIRT BAR HOLES AT FR 16, STR 23 AND AFT GIRT BAR HOLES AT FR 20, STR 23. REPAIRED IAW SRM 53-11-14 FIG 108.
- [SDR CALA2016090895724](https://openairdocs.org/sdr/CALA2016090895724.md): Door · damaged · Sep 6, 2016 · N813UA · Airbus A319131 · Fuel Storage
  > FUEL PANEL DOOR SUSTAINED DAMAGE DUE TO CONTACT WITH LE SLAT ON RETRACTION. REPLACED FUEL PANEL DOOR IAW MM 57-41-37.
- [SDR CALA2016072295573](https://openairdocs.org/sdr/CALA2016072295573.md): Doubler · not reported · Jul 20, 2016 · N813UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LEFT AIRFONE ANTENNA REQUIRES DOUBLER REPAIR FR 63-64 STR 41L-42L FABRICATED, LOCATED & DRI LLED & INSTALLED REPAIR DOUBLER IAW SRM 53-00-11-201 FIG 230
- [SDR CALA2016071895564](https://openairdocs.org/sdr/CALA2016071895564.md): Door Sill · corroded · Jul 15, 2016 · N813UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CORROSION AT R1 DOOR SILL FWD GIRT BAR HOLES AT FRAME 16, STR 23 AND AFT GIRT BAR HOLES AT FR 20, STR 23. REPAIRED IAW SRM 53-11-14 FIG.108.
- [SDR CALA2016071895563](https://openairdocs.org/sdr/CALA2016071895563.md): Skin · contaminated · Jul 14, 2016 · N813UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION, 53 INCHES FROM INBD, 4.5 INCHES FROM TE, 2.75 INCHES DIAMETER. REPAIRED IAW ECRA 5520-01491.
- [SDR CALA2016071895562](https://openairdocs.org/sdr/CALA2016071895562.md): Skin · contaminated · Jul 14, 2016 · N813UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN PANEL HAS TRAPPED WATER INDICATION, 163 INCHES FROM INBD, 13 INCHES FROM TE, 2 INCHES IN DIAMETER. REPAIRED IAW ECRA 5520-01490.
- [SDR CALA2016020995096](https://openairdocs.org/sdr/CALA2016020995096.md): Button · dirty · Feb 6, 2016 · N813UA · Airbus A319131 · Fire Detection
  > EXTERIOR POWER PANEL APU FIRE LIGHT STICKS ON & OTHER LIGHTS ARE INOPERATIVE. CLEANED PUSH TO TEST BUTTON & RELAMPED OTHER LIGHTS.
- [SDR CALA2014090992094](https://openairdocs.org/sdr/CALA2014090992094.md): Battery · not seated · Sep 6, 2014 · N813UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED ON 2 SVC. RESEATED EPSU BATTERY AT AFT LT IAW AMM 33-51-38, EMER LIGHT TEST NOW PASSES.
- [SDR CALA2014030390503](https://openairdocs.org/sdr/CALA2014030390503.md): Connector · loose · Mar 1, 2014 · N813UA · Airbus A319131 · Engine Fuel System Wiring
  > NR 1 FUEL VLV FAULT DISPLAYED ON UPPER ECAM. ECAM CAME ON AT ENG START BUT STARTED NORMAL. FAULT CLEARED BUT CAME BACK AT CRUISE, POSSIBLE FMU. ACCOMPLISHED COMPLETION OF FMU INSTALLATION, SECURED CANON PLUGS & CLAMP.
- [SDR CALA2013121993804](https://openairdocs.org/sdr/CALA2013121993804.md): Connector · defective · Dec 18, 2013 · N813UA · Airbus A319131 · Landing Gear System Wiring
  > LGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. R & R CONNECTOR 22GA ON RT MAIN LG. IAW ASM 32-31-04. PERFORMED LAND TEST IAW AMM 22-97-00, ALL TEST PASSED. PLACARD REMOVED.
- [SDR CALA2013102992486](https://openairdocs.org/sdr/CALA2013102992486.md): Unknown · odor · Oct 29, 2013 · N813UA · Airbus A319131 · Air Distribution System
  > HEAVY MUSTY, ACRID & MOLDY SMELL FROM AC SYSTEM IN LOW & HIGH FLOW.
- [SDR CALA2013102992485](https://openairdocs.org/sdr/CALA2013102992485.md): Tube · leaking · Oct 28, 2013 · N813UA · Airbus A319131 · APU Oil System
  > APU OIL TUBE LEAKING 5 DROPS PER MINUTE. ITEM 60 IS THE TUBE THAT IS LEAKING. REPLACED TUBE IAW IPC 49-21- 04-51A. LEAK CHECKED GOOD, CLEANED EFFECTED AREAS IN APU COMPARTMENT.
- [SDR CALA2013102892411](https://openairdocs.org/sdr/CALA2013102892411.md): Line · leaking · Oct 25, 2013 · N813UA · Airbus A319131 · APU Oil System
  > OIL ODOR IN CABIN. ON ARRIVAL, NOTICED STREAM OF SMOKE COMING FROM REAR TURBINE SECTION OF APU, FOUND OIL LINE AT 11 O'CLOCK POSITION AFT LEAKING. FWD LOOSE AT FITTING, OIL DRIPPING TO TURBINE CASE. SECURED FITTING, CLEANED EXCESS OIL, RAN APU FOR 30 MINUT
- [SDR CALA2013101692105](https://openairdocs.org/sdr/CALA2013101692105.md): Drain Mast · damaged · Oct 15, 2013 · N813UA · Airbus A319131 · Water Line Anti-Ice System
  > HOT WATER DRAIN MAST DAMAGE AFT FUSELAGE. AFT DRAIN MAST DAMAGE FOUND ON ARRIVAL. REPLACED AFT DRAIN MAST ASSEMBLY.
- [SDR CALA2013093091587](https://openairdocs.org/sdr/CALA2013093091587.md): Vhf Comm · inoperative · Sep 28, 2013 · N813UA · Airbus A319131 · VHF Communications System
  > VHF 1 INOPERATIVE, RING OUT WIRING BETWEEN AMU BENCH PLUG AA POS 1A, 1B, 1E, 1D, 1F, & 1H TO VHF 1 BENCH PLUG 1A,1B,1C,13A,13B,15,15B, IAW ASM 23-51-06. ALSO CHECKED SHIELD GROUNDS.
- [SDR CALA2013093091565](https://openairdocs.org/sdr/CALA2013093091565.md): Control Panel · faulty · Sep 28, 2013 · N813UA · Airbus A319131 · VHF Communications System
  > VHF1 FAULTS. DUE TO REPEAT LOGS FOR VHF 1 TX & RX FAULTS REF ASM 23-51-02 CHECK WIRING CONTINUITY FROM CONNECTION AA (9D,9E,9H,9G,10F,10G,10E,10D,9J,9K,12D,12E,12H,12G,13F,13G,13E,13D,12J,12K). ALSO CHECK WIRING CONTINUITY FROM CONNECTION AB (11B,12B,13B,14B,1
- [SDR CALA2013092791519](https://openairdocs.org/sdr/CALA2013092791519.md): Amu · faulty · Sep 26, 2013 · N813UA · Airbus A319131 · VHF Communications System
  > VERY HIGH FREQUENCY RADIO 1 INOPERATIVE. R & R AMU IAW A319 AMM & OPERATIONS CHECKED GOOD & TESTED OK.
- [SDR UALA2013072505233](https://openairdocs.org/sdr/UALA2013072505233.md): Computer · faulty · Jul 24, 2013 · N813UA · Airbus A319131 · Flight Control System
  > FLIGHT CONTROL ELAC 2 FAULTED. LOSS OF THE RECEPTION OF ELAC 2 DISCRETES BY 1 FAC OR 1 FMGC. REPLACED FCDC2 AND TESTED IAW MM 27-95-34-400-001-A, NO FAULTS NOTED.

Next page: https://openairdocs.org/aircraft/N813UA/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 = 'N813UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N813UA/reports

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