# Service difficulty reports: N843UA A list on [N843UA](https://openairdocs.org/aircraft/N843UA.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 2 · 85 reports - [SDR CALA2026032714865](https://openairdocs.org/sdr/CALA2026032714865.md): Battery · no test · Mar 26, 2026 · N843UA · Airbus A319131 · Emergency Lighting > EPSU BATTERY AFT L FAULT R/R EMER LIGHT BATTERY AT FIN 13WL EPSU REF AMM 33-51-38, OPS CHECKS OK - [SDR CALA2026032714864](https://openairdocs.org/sdr/CALA2026032714864.md): Battery · no test · Mar 26, 2026 · N843UA · Airbus A319131 · Emergency Lighting > RECIEVED EPSU EATTERY EMER R MSG R/R EMER LIGHT BATTERY AT FIN 12WL EPSU REF AMM 33-51-38, OPS CHECKS OK - [SDR CALA2025081207646](https://openairdocs.org/sdr/CALA2025081207646.md): Fuel Cap · missing · Aug 8, 2025 · N843UA · Airbus A319131 · Fuel Storage > FUEL CAP MISSING ON ARRIVAL TOMC HAS BEEN NOTIFIED REFFER LP 5846636 FOR CDL. - [SDR CALA2025080407257](https://openairdocs.org/sdr/CALA2025080407257.md): Girt Bar · faulted · Jul 31, 2025 · N843UA · Airbus A319131 · Emergency Equipment > DOOR 2R SLIDE/DOOR SHOWS ARMED ON THE GROUND BUT NOT INFLIGHT UNLESS HAN DLE IS PUSHED. REINSTALLED GIRT BAR INDICATION TAB BACK INTO PLACE AS REQUIRED. ALL DOOR OPENING AND CLOSING FUNCTIONS ARE NORMAL REF AMM 52-10-00 PB710. - [SDR CALA2025021002266](https://openairdocs.org/sdr/CALA2025021002266.md): Battery · no test · Feb 8, 2025 · N843UA · Airbus A319131 · Emergency Lighting > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - LEFT EPSU BATTERY FAILED TEST. REPLACED EPSU BATTERY WITH SERVICEABLE ONE FROM STOCK. OPS CHECK GOOD PARTS USED: 18-3351-3-0001,QTY:1 - [SDR CALA2025012702072](https://openairdocs.org/sdr/CALA2025012702072.md): Handle · inoperative · Jan 23, 2025 · N843UA · Airbus A319131 · Passenger/Crew Doors > R1 DOOR SLIDE WOULD NOT ARM.ACCIDENTALLY BLEW EMERGENCY SLIDE WHILE TRYING TO FIX ISSUE UPDATED TO RII DEPLOYED SLIDE REMOVED P/N D31516-617, S/N A6547 IAW AMM 25-62-44. COMPLETED STEPS 1-4(A)3 OF R1 DOOR SLIDE IAW AMM 25-62-44-400-802-A R1 DOOR DOOR DAMPER DI - [SDR CALA2024120601418](https://openairdocs.org/sdr/CALA2024120601418.md): Girt Bar · out of adjust · Dec 5, 2024 · N843UA · Airbus A319131 · Emergency Equipment > DOOR 1R WILL NOT ARM. ADJUSTED GIRT BAR TRAVEL PER AMM 52-11-22-820-001-A OPS CHECK GOOD SLIDE INDICATION IS NORMAL IN FLIGHT DECK PREFORMED TSM 52-11-00-810-801-A TEST FOR ON LIGHT ON DOOR TO ILLUMINATE. OPS NORMAL ACP RII INSPECTION FOR R-1 DOOR SLIDE GIRT - [SDR CALA2024041501082](https://openairdocs.org/sdr/CALA2024041501082.md): Fuel Cap · missing · Apr 7, 2024 · N843UA · Airbus A319131 · Fuel Storage > PDA 2 FUEL COUPLING CAP DEFERRED ON L/P 7587591 MISSING CAP DEFERRED. REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NO TED. UPDATED MAA CODE FIX USINGCHECK FOR LEAKS CHECK FOR LEAKS MAC METER INITIATED RELATED WORK ORDER 000000003101610 AND D - [SDR CALA2024041101037](https://openairdocs.org/sdr/CALA2024041101037.md): Fuel Cap · missing · Apr 7, 2024 · N843UA · Airbus A319131 · Fuel Storage > PDA 2 FUEL CAP FOUND MISSING ON ARRIVAL YVR SEE LOG PAGE 7587591 FOR CDL. REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NO TED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK FOR LEAKS. CHECK - [SDR CALA2023090102674](https://openairdocs.org/sdr/CALA2023090102674.md): Fuel Cap · missing · Aug 30, 2023 · N843UA · Airbus A319131 · Fuel Storage > FUEL CAP MISSING WHEN A/C ARRIVED. PICTURE OF MISSING FUEL CAP. REF LOG PAGE 5603595 MISSING FUEL CAP PLACED ON CDL ON THAT LOG PAGE. FUEL CAP IS MISSING.PLACE MISSING FUEL CAP ON CDL28A. VERFIED NO FUEL LEAKING FROM FUEL HOSE ATTACH POINT WHERE CAP GOES ON. C - [SDR CALA2023050901429](https://openairdocs.org/sdr/CALA2023050901429.md): Slide · partial deploy · May 8, 2023 · N843UA · Airbus A319131 · Emergency Locator Beacon > DOOR 1L SLIDE PARTIALLY DEPLOYED DUE TO OPENING IN ARMED POSITION CHECKING SDR FOR SLIDE FOUND DOOR 1L STUCK IN CLOSED POSITION WITH HANDLE IN OPEN POSITION, UNABLE TO OPEN DOOR. RELEASED PRESSURE ON DOOR ASSIST BOTTLE REF MT 52-002. OPNED DOOR 1L AND INSPECTE - [SDR CALA2022092802526](https://openairdocs.org/sdr/CALA2022092802526.md): None · corroded · Sep 28, 2022 · N843UA · Airbus A300* · Brake > BRAKE ACCUMULATOR BLEEDING OFF WITH PARKING BRAKE SET. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V926493 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK ACCUM MAC RELATED WORK ORDER 000000003057621 AND PRTR N - [SDR CALA2022091202331](https://openairdocs.org/sdr/CALA2022091202331.md): None · cracked · Sep 10, 2022 · N843UA · Airbus A300* · Fuselage Structure (General) > LH FR 35 PRESS PANEL AREA, HAS CRACK INDICATION IN HOLES 2 AND 4 IN THE PRESSURE PANEL LAYER. GENERATED BY V892444 ON HAECO LCQ NR 9296406/26406 IAL INSPECTION AT LH FR35-36 PRESSURE PANEL HOLES #1 THROUGH #15 02952 ON OR BEFORE 75,932 TOTAL AIRCRAFT FLIGHT CY - [SDR CALA2022082902194](https://openairdocs.org/sdr/CALA2022082902194.md): Cleat · corroded · Aug 26, 2022 · N843UA · Airbus A300* · Fuselage Miscellaneous Structure > AFT PIT: CLEAT AT FR57 STR 41-42L CORRODED A3NB-53-4-6179 PER HA ECO LCQ N/R 9296573/26573 GEN BY V079881 REMOVED AND REPLACED CLEAT AT FR 57 STR 41-42L IAW A319 SRM 51-4 2-11 BY MECH V052030 INSP BY V061771 - [SDR CALA2022082602191](https://openairdocs.org/sdr/CALA2022082602191.md): None · corroded · Aug 25, 2022 · N843UA · Airbus A300* · Fuselage Miscellaneous Structure > AFT CARGO PIT STR39R AT FR 64-65 CORRODED A3NB-53-4-6179 PER HAE CO LCQ N/R 9296634/26634 GEN BY V079881 - [SDR CALA2022082602190](https://openairdocs.org/sdr/CALA2022082602190.md): None · corroded · Aug 25, 2022 · N843UA · Airbus A300* · Fuselage Main, Structure > STRINGER 31R BETWEEN FR 65 AND FR 66 HAS EXFOLIATION CORROSION ( JUST BELOW OUTFLOW VALVE). GENERATED BY V061626 ON HAECO LCQ NR 9296597/26597 REMOVED AND REPLACED STRINGER 31R BETWEEN FR 65-66 IAW A319 SRM 53-41-19-283-002. ACMP BY MECH V052030 INSP BY V06177 - [SDR CALA2022082602189](https://openairdocs.org/sdr/CALA2022082602189.md): None · corroded · Aug 25, 2022 · N843UA · Airbus A300* · Fuselage Miscellaneous Structure > AFT PIT TORSION BOX UPPER SURFACE WEB AT FR55 -10 STGR 38R-37R C ORRODED ON BOTTOM SURFACE (A3NB-53-4-6179). GENERATED BY V079881 AT HAECO LCQ PER NR 9296571 (26571). REMOVED AND REPLACED AFT CARGO PIT TORSION BOX COVER SHEET IAW A 319 SRM 81-42-11. GENERATED - [SDR CALA2022082602188](https://openairdocs.org/sdr/CALA2022082602188.md): Fitting · none · Aug 25, 2022 · N843UA · Airbus A300* · Fuselage Main, Frame > L/H FR16 DOOR STOP #7 HAS CRACK INDICATIONS IN HOLE #1 AT 3 O''CL OCK IN THE INTERCOSTAL PER HAECO LCQ N/R 9296133/26133 GEN BY V0 61632 - [SDR CALA2022082402171](https://openairdocs.org/sdr/CALA2022082402171.md): Stringer · corroded · Aug 22, 2022 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > AFT CARGO PIT: STR40L+6 CORRODED C FR64 -A3NB-53-4-6179 GENERATE D BY V079881 AT HAECO LCQ PER NR 9296633 (26633) REMOVED AND REPLACED CORRODED STRINGER STR40L+6 AT FRAME 64 IAW A319 SRM 51-42-11/001 PERFORMED BY V940604 - [SDR CALA2022081602091](https://openairdocs.org/sdr/CALA2022081602091.md): Door Sill · corroded · Aug 13, 2022 · N843UA · Airbus A319131 · Fuselage Main, Floor Beam > R2 DOOR SILL FWD OF FWD GIRT BAR FITTING CORRODED GENERATED BY V 892285 AT HAECO LCQ PER NR 9296275 (26275) A3NB-53-3-6222 REMOVED AND REPLACED R-2 DOOR SILL IAW A319 SRM 51-22-11-911-001 (CATEGORY A- NO FURTHER ACTION REQUIRED) PERFORMED BY V061630 IN SP BY V - [SDR CALA2022081602085](https://openairdocs.org/sdr/CALA2022081602085.md): Shear Plate · corroded · Aug 12, 2022 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > AFT CABIN LH LATERAL SHEAR PLATE AT FR70 CORRODED. GENERATED BY V929087 ON HAECO LCQ NR 9296657/26657 REMOVED AND REPLACED AFT CABIN L/H LATERAL SHEAR PLATE AT FR70 I AW A319 SRM 51-72-11-911-001 PERFORED BY V901486 INSP BY N078570 - [SDR CALA2022081602070](https://openairdocs.org/sdr/CALA2022081602070.md): Door Sill · corroded · Aug 12, 2022 · N843UA · Airbus A319131 · Fuselage Main, Floor Beam > L2 DOOR SILL @ FR68 AFT OF GIRT BAR FITTING CORRODED GENERATED B Y V079881 AT HAECO LCQ PER NR 9296291 (26291) A3NB-53-3-6222 REMOVED AND REPLACED L-2 DOOR SILL AT FR 66-68 PART #D5348004320 601 PO:#1116536.1 IAW A319 SRM 51-72-11-911-001 AND SRM 51-42-11 -001 - [SDR CALA2022081202038](https://openairdocs.org/sdr/CALA2022081202038.md): Shear Plate · corroded · Aug 10, 2022 · N843UA · Airbus A319131 · Fuselage Main, Floor Beam > AFT CABIN RH LATERAL SHEAR PLATE @ FR70 CORRODED A3NB-53-3-6222 GENERATED BY V079881 AT HAECO LCQ PER NR 9296281 (26281) REMOVED AND REPLACED RH LATERAL SHEAR PLATE IAW A319 SRM 51-72-1 1/001 DOT REMOVED PERFORMED BY V915807 INSP BY N078570 - [SDR CALA2022081002034](https://openairdocs.org/sdr/CALA2022081002034.md): Shear Web · corroded · Aug 9, 2022 · N843UA · Airbus A319131 · Fuselage Internal Mounting Structure > AFT SHEAR WEB CORRODED @ FR70 A3NB-53-3-622 GENERATED BY V079881 AT HAECO LCQ PER NR 9296340 (26340) REMOVED AND REPLACED RH SHEAR WEB IAW A319 SRM 51-72-11-001 PERF ORMED BY V915851 INSP BY N078570 - [SDR CALA2022081002015](https://openairdocs.org/sdr/CALA2022081002015.md): Stringer · corroded · Aug 8, 2022 · N843UA · Airbus A319131 · Fuselage Main, Structure > 7 TO 10" AFT OF FR65 TOP SIDE OF STRINGER 43L HAS SURFACE CORROSION (A3ND-53-3-6185) GENERATED BY V061626 AT HAECO LCQ PER NR 92 96595 (26595) REPAIRED STRINGER 43L AFT OF FR65 7 TO 10" IAW A319 SRM 53-41-13 -300-004 PG5 FIGURE 001 PERFORMED BY V061737 INSP BY - [SDR CALA2022072901912](https://openairdocs.org/sdr/CALA2022072901912.md): Door Frame · cracked · Jul 29, 2022 · N843UA · Airbus A319131 · Fuselage Main, Frame > RH FR66 DOOR STOP #1 HOLE #3 HAS A CRACK INDICATION AT 6 O''CLOCK IN FRAME. GENERATED BY V061632 ON HAECO LCQ NR 9296134/26134 300-010. IAW SRM 53-41-12-300-008 D1=.3755, D2=.2495, D3=.2495, IAW SRM 53-41-12-300-008 FIG 002 STEP REAMED THE R2 DOOR STOP #1 #3=. - [SDR CALA2020032700733](https://openairdocs.org/sdr/CALA2020032700733.md): Slide · partial deploy · Mar 27, 2020 · N843UA · Airbus A319131 · Escape Slide > DOOR 1R SLIDE PARTIALLY DEPLOYED BY SCRUB WILL NEED SLIDE CHANGE. SHOULD READ DR 1L REMOVED SLIDE PACK FROM DR 1L. - [SDR CALA2019053100866](https://openairdocs.org/sdr/CALA2019053100866.md): Power Supply · failed · May 31, 2019 · N843UA · Airbus A319131 · Emergency Lighting > (A3NB-23-3-6018) REMOVE AND REPLACE THE FWD CABIN EMERGENCY POWER SUPPLY. REFER TO N/R: 9619191. CHANGED DUE TO A FAILED BITE TEST. REMOVED AND REPLACED THE FWD CABIN EMERGENCY POWER SUPPLY. REFER TO N/R: 9619191. WORK ACCOMPLISHED. ROTABLE PARTS CHANGE WAS IN - [SDR CALA2016090195711](https://openairdocs.org/sdr/CALA2016090195711.md): Power Supply · malfunctioned · Sep 1, 2016 · N843UA · Airbus A319131 · Emergency Lighting > EMERGENCY LIGHT TEST FAILED. FOUND TWO FAULT MESSAGES FOR EPSU INT LOAD AFT L, AND EPSU COMM FWD L, AFTER EMERGENCY LIGHT TEST. TROUBLESHOT AND TESTED IAW TSM 33-51-00-810-807-A - [SDR CALA2016081195619](https://openairdocs.org/sdr/CALA2016081195619.md): Battery Pack · failed · Jun 23, 2016 · N843UA · Airbus A319131 · Emergency Lighting > EPSU BATTERY FAULT LIGHT DURING TEST. REPLACED AFT EMERGENCY BATTERY IAW 33-51-38. - [SDR CALA2014030390505](https://openairdocs.org/sdr/CALA2014030390505.md): Blanking Plate · damaged · Mar 1, 2014 · N843UA · Airbus A319131 · Pitot/Static System > STATIC PORT BLANKING PLATE RT SIDE FWD OF NLG DOORS HAS BLENDING & PITTING MARKS. REPLACED BLANKING PLATE. - [SDR CALA2014022590431](https://openairdocs.org/sdr/CALA2014022590431.md): Sill · corroded · Feb 21, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > AFT CABIN L2 DOOR SILL BEAM HAS CORROSION FRAME 68 Y 1292 FRAME 68. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR IAW A319 SRM 51-42-11 PARA 7. - [SDR CALA2014022590430](https://openairdocs.org/sdr/CALA2014022590430.md): Sill · corroded · Feb 21, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > R2 DOOR SILL FWD & AFT GIRT BAR PLATE ATTACH AREA HAS CORROSION. R & R DOOR SILL IAW SRM51-42-11. - [SDR CALA2014022190407](https://openairdocs.org/sdr/CALA2014022190407.md): Fitting · corroded · Feb 18, 2014 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > AFT CABIN CROSS BEAM RT END FITTING HAS CORROSION AT FRAME 70, STRINGER 23. ORIGINAL THICKNESS WAS 0.300 & REMAINING THICKNESS AFTER CORROSION REMOVAL IS 0.200. MATERIAL LOSS IS 0.100. OUT OF LIMITS IAW A319 SRM 51-73-11, PAGE 11. REMOVED DAMAGED FITTING & - [SDR CALA2014011390123](https://openairdocs.org/sdr/CALA2014011390123.md): Latch · defective · Jan 11, 2014 · N843UA · Airbus A319131 · Passenger Oxygen System > OXYGEN MASKS DEPLOYED 34 ABC, STOWED MASK, O2 DOOR WILL NOT LATCH, SECURED O2 DOOR. SEATS 34 ABC NOT USEABLE, COMPLIED WITH MEL. - [SDR CALA2013122693959](https://openairdocs.org/sdr/CALA2013122693959.md): Servo Control · inoperative · Dec 25, 2013 · N843UA · Airbus A319131 · Drag Control System > REPLACED 2L SPOILER SERVO CONTROL COULD NOT GET IT TO ACTIVATE & FOUND THE MAINTENANCE DEVICE INOPERATIVE FROM STOCK. REPLACED 2L SPOILER SERVO CONTROL. - [SDR CALA2013122693940](https://openairdocs.org/sdr/CALA2013122693940.md): Spoiler · inoperative · Dec 23, 2013 · N843UA · Airbus A319131 · Drag Control System > NR 2 SYMMETRICAL SPOILER SURFACES INOPERATIVE, RETRACTED & DEACTIVATED. SPOILER 2 FAULT, HAS BEEN RESET SEVERAL TIMES. REPLACED SERVO IAW MM, NO HELP. - [SDR CALA2013112593224](https://openairdocs.org/sdr/CALA2013112593224.md): Oxygen System · low pressure · Nov 22, 2013 · N843UA · Airbus A319131 · Crew Oxygen System > CREW OXY SYS LOW RECORD PRESS PRIOR TO SERVICING. SERVICED CREW OXY IAW AMM 12-14-35 OXY FLOW NORMAL. OK FOR SERVICE. - [SDR CALA2013111893014](https://openairdocs.org/sdr/CALA2013111893014.md): Hydraulic Line · leaking · Nov 14, 2013 · N843UA · Airbus A319131 · Hydraulic System, Main > HYDRAULIC LEAK BELLY AFT CARGO DOOR AREA, YELLOW SYSTEM SERVO LINE. - [SDR CALA2013100191625](https://openairdocs.org/sdr/CALA2013100191625.md): Valve · out of position · Sep 30, 2013 · N843UA · Airbus A319131 · Aircraft Fuel Distribution System > CREW REPORTED FUEL LEAKING FROM WATER DRAIN VALVE ON LT WING. UNABLE TO FUEL. REPOSITIONED VALVE NO LEAKS. - [SDR CALA2013082690732](https://openairdocs.org/sdr/CALA2013082690732.md): Panel · damaged · Aug 23, 2013 · N843UA · Airbus A319131 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT PANEL BEHIND BOTTOM DOOR SILL HAS METAL STICKING UP. PERFORMED INTERIM REPAIR IAW ECRA 5322-01050 PART 1. GENERATED CF FOR REPAIR BEFORE NEXT 'C' CHECK IAW IPC 53-42-04-22X ITEM 62. - [SDR CALA2013081990542](https://openairdocs.org/sdr/CALA2013081990542.md): Wire Harness · unknown · Aug 18, 2013 · N843UA · Airbus A319131 · Window System Wiring > LEFT WINDOW DISPLAYED ON UPPER ECAM SCREEN. R & R WINDOW HEAT WIRE HARNESS THAT ATTACHES TO THE WINDOW IAW AMM & STANDARD PRACTICES. - [SDR CALA2013081490439](https://openairdocs.org/sdr/CALA2013081490439.md): Coffeemaker · odor · Aug 14, 2013 · N843UA · Airbus A319131 · Buffet/Galleys > MELTED PLASTIC ELECTRICAL ODOR IN FWD GALLEY. REPLACED COFFEEMAKER. NO FURTHER ODOR OR ELECTRICAL SMELL IN FWD GALLEY. - [SDR UALA2013052303591](https://openairdocs.org/sdr/UALA2013052303591.md): Actuator · out of adjust · May 21, 2013 · N843UA · Airbus A319131 · Elevator Control System > RT ELEVATOR DURING GROUND CONTROL CHECK IN FULL UP POSITION SAGGED BUT WAS STILL IN BOX. CREW ALSO REPORTED ENROUTE, RT ELEVATOR NOW BELOW LEVEL BOX. PLANE FLYS NORMAL. COMPLIED WITH DDP. INDICATION PROBLEM ONLY. FOUND RIGHT ELEVATOR IS SAGGING, WHEN GREEN HY - [SDR UALA2013042202759](https://openairdocs.org/sdr/UALA2013042202759.md): Tape · peeling · Apr 19, 2013 · N843UA · Airbus A319131 · Vertical Stabilizer Miscellaneous Structure > TAPE ON VERTICAL STAB IS PEELING BACK. CUT OFF LOOSE TAPE AND INSPECTED GFRP. NO DAMAGE IS PRESENT. - [SDR UALA2013022601157](https://openairdocs.org/sdr/UALA2013022601157.md): Girt Bar · binding · Feb 22, 2013 · N843UA · Airbus A319131 · Emergency Equipment > L2 DOOR WOULD NOT ARM. ARMING HANDLE BINDING. CLEANED DEBIS FROM UNDER SLIDE HOOK. OP'S CHECKED GOOD. - [SDR UALA2012112906851](https://openairdocs.org/sdr/UALA2012112906851.md): Slat · damaged · Nov 29, 2012 · N843UA · Airbus A319131 · Leading Edge Devices > CREW REPORT: BIRD STRIKE, ACP BIRD STRIKE INSP PER AMM 05-51-14. FOUND LEFT NR 2 SLAT WITH DAMAGE SEE LOG 4 NO OTHER DAMAGE NOTED ON AIRCRAFT OR ENGINES. - [SDR UALA2012111606627](https://openairdocs.org/sdr/UALA2012111606627.md): Oxygen Bottle · low pressure · Nov 15, 2012 · N843UA · Airbus A319131 · Crew Oxygen System > COCKPIT OXYGEN STARTED FLIGHT AT 930 PSI. READING 690 PSI NOW AT 0100Z AT FL 370. SERVICED OXYGEN BOTTLE TO 1700 PSI. PRESSURE IS HOLDING AND STEADY. CHECKED ALL FOUR MASK ASSYS AND BOTTLE ASSY FOR LEAKS, NONE NOTED. - [SDR UALA2012081604569](https://openairdocs.org/sdr/UALA2012081604569.md): Oxygen Mask · leaking · Aug 16, 2012 · N843UA · Airbus A319131 · Crew Oxygen System > COCKPIT OXYGEN BOTTLE - LOW. PRESSURE SLOWLY DROPPING. MAY HAVE A SLOW LEAK MAINT TEXT: AIRCRAFT ARRIVED WITH CREW OXYGEN PRESS AT 270 PSI. REPLACED FIRST OFFICERS MASK ASSY THAT WAS LEAKING AND SERVICED CREW BOTTLE TO 1730 PSI. NO LEAKAGE NOTED. - [SDR UALA2012080704262](https://openairdocs.org/sdr/UALA2012080704262.md): Plug · damaged · Aug 6, 2012 · N843UA · Airbus A319131 · Leading Edge Devices > RT INBOARD INNER MOST FLAP HOIST POINT NYLON PLUG DAMAGED. INSTALLED NEW PLUG. Next page: https://openairdocs.org/aircraft/N843UA/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 = 'N843UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N843UA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.