# Service difficulty reports: N850UA

A list on [N850UA](https://openairdocs.org/aircraft/N850UA.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 · 79 reports

- [SDR CALA2026040715132](https://openairdocs.org/sdr/CALA2026040715132.md): Battery · no test · Apr 6, 2026 · N850UA · Airbus A319131 · Emergency Lighting
  > CIDS EMERGENCY LIGHT SYSTEMS TEST FAILED. FAULT LIGHT EPSU BATTERY AFT L. 33-51-38 REPLACED EPSU BATTERY AFT L 13WL PER AMM 33-51-38-400-002-A. BITE TEST OP CHECKS GOOD.
- [SDR CALA2026031014453](https://openairdocs.org/sdr/CALA2026031014453.md): Unknown · odor · Mar 5, 2026 · N850UA · Airbus A319131 · Air Distribution System
  > AFTER LIGHTNING STRIKE, BURNING ODOR THROUGH OUT FLIGHT DECK AND CABIN. LASTED 8-10 MINUTES. RAN BOTH ENGS. NO FUMES OR SMOKE IDENTIFIED. ALL SYSTEMS NORMAL, NO MAINT MESSAGES OR FAULTS. CYCLED GALLEY OVENS AND COFFEE MAKERS ALL NORMAL IAW AMM 05-51-10-200
- [SDR CALA2026021013649](https://openairdocs.org/sdr/CALA2026021013649.md): Light · inoperative · Feb 9, 2026 · N850UA · Airbus A319131 · Emergency Lighting
  > SEAT 30C EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LIGHT ASSY IAW AMM 33-51-19, OPS CHKD GOOD.
- [SDR CALA2026011412967](https://openairdocs.org/sdr/CALA2026011412967.md): Nozzle · faulted · Jan 12, 2026 · N850UA · Airbus A319131 · Engine Collector/Tailpipe/Nozzle
  > AT 11 OCLOCK POSITION IN AFT SECTION OF NR 2 ENG A PIECE OF LINE R APPEARS TO BE MISSING. DIMENSIONS OF DAMAGED AREA ARE ROUGHLY 10"X8". REMOVED & REPLACED NR 2 ENGINE COMMON NOZZLE ASSEMBLY IAW AMM TASK 78-11-11-400-010-A. ALL CHECKS GOOD.
- [SDR CALA2025100709743](https://openairdocs.org/sdr/CALA2025100709743.md): Battery Pack · inoperative · Oct 6, 2025 · N850UA · Airbus A319131 · Emergency Lighting
  > WHILE PERFORMING EPSU BITE REF AMM 33-51-00-710-001-A, RECIEVED A EPSU EMER R BATTERY MESSAGE REMOVED AND REPLACED THE RIGHT EMERGENCY EXIT EPSU BATTERY REF AMM 33-51-38/401. OPS CHECK GOOD, ALL INSTALL TESTS PASS WITH NO FAULT MESSAGES PRESENT.
- [SDR CALA2025100609662](https://openairdocs.org/sdr/CALA2025100609662.md): Battery · inoperative · Oct 5, 2025 · N850UA · Airbus A319131 · Emergency Lighting
  > WHEN PERFORMING EMERGENCY LIGHT TEST FROM COCKPIT OR F/A TEST SWITCH OVERHEAD EXIT LAMPS AT DOORS 1L & 1R FAIL TO ILLUMINATE. FAILURE OCCURS WHEN SYSTEM IS IN ARMED MODE, AND AC POWER IS REMOVED. ALSO FAILS WITH NO POWER, AND ON SELECTED ON EMERG LIGHT SWITCH.
- [SDR CALA2025013002128](https://openairdocs.org/sdr/CALA2025013002128.md): Battery Pack · no test · Jan 29, 2025 · N850UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD R EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST REMOVED AND REPLACED FWD R EMERGENCY LIGHT BATTERY AS PER AMM 33-51-38. OPS CHECK, GOOD.
- [SDR CALA2024102300896](https://openairdocs.org/sdr/CALA2024102300896.md): Fan · faulted · Oct 19, 2024 · N850UA · Airbus A319131 · Air Distribution Fan
  > REQUEST INSPECTION FORUNUSUAL BURNING SMELLON FLIGHT DECK STRONG SMELL IN AIRCRAFT. CONFIGURED A/C IN SEVERAL WAYS AND FOUND THE SMELL TO GET STRONGER WITH THE FOLLOWING CONFIGURATION (PACKS OFF, HOT AIR AUTO, CAB FANS AUTO, CARGO VENTS AUTO, AVIONICS BLOWER A
- [SDR CALA2024093000716](https://openairdocs.org/sdr/CALA2024093000716.md): Engine · bird ingestion · Sep 26, 2024 · N850UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > DURING BIRD STRIKE INSPECTION FOUND EVIDENCE OF BIRD REMAINS IN #1 ENGINE INTAKE AND EXHAUST. UPON BIRDSTRIKE BSI OF THE #1 ENGINE PER AMM 72-00-200-010-A FOUND MISALIGNED STAGE 3 CLAPPER TO BE OUT OF LIMITS IAW AMM 72-00-00-200-016-B PARA D.2(4)WHICH IS MORE
- [SDR CALA2024071702052](https://openairdocs.org/sdr/CALA2024071702052.md): Fitting · cracked · Jul 14, 2024 · N850UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT WINDSHIELD LOWER NODE, CONTINUITY FITTING HAS A CRACK INDIC ATION IN HORZ. FLANGE AFT OF INBD FASTENER, APPROX 1" OTBD OF CE NTER OF CENTER POST. REMOVED AND REPLACED L/H AND R/H CONTINUITY FITTINGS AS PER AIB REPAIR DWG R53113426 AS DIRECTED BY REO 2250
- [SDR CALA2024041701113](https://openairdocs.org/sdr/CALA2024041701113.md): Fuel Cap · missing · Apr 14, 2024 · N850UA · Airbus A319131 · Fuel Storage
  > PDA 2 UPON ARRIVAL FUEL CAP FOUND MISSING. PLACED ON CDL INSTALLED FUEL CAP ASSY. REF AMM 28-25-41. OK TO CONTINUE.
- [SDR CALA2024040400978](https://openairdocs.org/sdr/CALA2024040400978.md): Bolt · missing · Apr 1, 2024 · N850UA · Airbus A319131 · Wheel/Ski/Float
  > PDA 2 #2 WHEEL MISSING TIEBOLT REPLACED WHEEL ASSY REF LOG PAGE 7522208
- [SDR CALA2023122103698](https://openairdocs.org/sdr/CALA2023122103698.md): Fuel Cap · missing · Dec 20, 2023 · N850UA · Airbus A319131 · Fuel Storage
  > PDA 2 AIRCRAFT ARRIVED DFW WITH UNDER WING FUEL CAP MISSING SHOULD READ FUEL CAP MISSING APPLIED CDL 28A FOR MISSING FUEL CAP CREATED ESDR REPORT #1034612. PLACED ON MEL PLACED ON CDL AND CREATED ESDR REPORT DISPATCH DESK: 3 NAME: AB DATE: 19-DEC-23- APPROVED
- [SDR CALA2023062802050](https://openairdocs.org/sdr/CALA2023062802050.md): Engine · inoperative · Jun 25, 2023 · N850UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > ENG 2 FAIL. ABRUBT YAWLOUD BANG. FIRST ECAMWAS ENG STALL. THEN ENG2 FAIL. EGT RED. REPLACED #2 ENG.PER W/C 317100-1-4900 GROUND RUN LEAK CHECKED NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1809185 SN OFF 0046. DUE TO ENGINE 2 REPLACEMENT, PERFORMED TEST
- [SDR CALA2022100302655](https://openairdocs.org/sdr/CALA2022100302655.md): Filter · odor · Oct 3, 2022 · N850UA · Airbus A319131 · Cabin Cooling System
  > DURING CRUISE HAD STRONG ODORS IN FLT DECK ANDGALLEY. FOUND NO EVIDENCE OF ODOR. PERFORMED TSM 05-50-00-810-831-A. PERFORMED OPS CHECK OF BOTH PACKS. FOUND #1 PACK TO BE CAUSING ODOR. FOUND #1 PACK TO BE CAUSING ODOR. PERFORMED VISUAL REPLACED RECIRCULATION
- [SDR CALA2022060801465](https://openairdocs.org/sdr/CALA2022060801465.md): Flap System · overspeed · Jun 8, 2022 · N850UA · Airbus A319131 · Trailing Flap Position Indicating System
  > MOMENTARY FLAPS 2 OVERSPEED OF 5 KTS. ITEM LOCKED TO CONFIRM CLEARING ACTION. ITEM UNLOCKED FOR CLEARING ACTION WITH CONCURRENCE OF TOMC SR MANAGER. - TOMC KROWN ACCOMPLISHED FLAP OVER SPEED CHECK REF AMM 05-51-13-200-001-A. MORE THAN 10 SEC - ON BOTH SFCC 1&2
- [SDR CALA2022030700590](https://openairdocs.org/sdr/CALA2022030700590.md): Fitting · cracked · Mar 6, 2022 · N850UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED TASK RH WINDSHIELD SIDE POST AND FR4 HOLE#3 HAVE CRAC K INDICATION CRACKED AT INTERFACE FITTING 5 O''CLOCK POS PER HAEC O LCQ N/R 9290510/38510 GEN BY FLT CYCLES THEREAFTER. NOTE TO EG ALI53-11-35 IS IMPACTED IN RE IMPACTED IN THE REWORKED AREA AND
- [SDR CALA2022022800510](https://openairdocs.org/sdr/CALA2022022800510.md): Plate · corroded · Feb 25, 2022 · N850UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO DOOR SILL MULTIPLE AREAS OF SURFACE CORROSION FR55A-FR 59 (A3NB-05-3-6023) PER HAECO LCQ NON ROUTINE 9290318/38318 GENE RATED BY V061629 REMOVED AND REPLACED ONE COVER ASSY AFT CARGO FR55-59 STR39R IAW A319 SRM 51-42-11,51-44-11/001 AND 51-42-11 PARA
- [SDR CALA2022021400379](https://openairdocs.org/sdr/CALA2022021400379.md): Fitting · cracked · Feb 14, 2022 · N850UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 68 FITTING #1 I/B LOWER HOLE IS CRACKED AT FRAME AT 10 AND 4 O''CLOCK POS. EA 5340-01724 002 PER HAECO LCQ NON ROUTINE/9290 455 GENERATED BY V061682 12-300-008, FIG 002 & 003 WHERE D1 IS.5968" AND D2, D3, D4 = FINAL REPAIR INSTRUCTIONS. SRM53-41-12-300
- [SDR CALA2022021400371](https://openairdocs.org/sdr/CALA2022021400371.md): Stringer · corroded · Feb 13, 2022 · N850UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT FR61-FR64, STGR41R IS CORRODED. GENERATED BY V925324 ON HAECO LCQ NR 9290293/38293 REMOVED AND REPLACED WITH NEW STRINGER AT FR61-FR64 STGR 41R P/N D5347643320000 P.O. 1108106.1 IAW A319 SRM 51-42-11/001 AND IAW A319 SRM 51-72-11-911-001
- [SDR CALA2022020800347](https://openairdocs.org/sdr/CALA2022020800347.md): Joint · corroded · Feb 8, 2022 · N850UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN LEFT DOOR SILL CORRODED AT FR66. PER NR 9290354/38354 GENERATED BY V892285. REMOVED 2 OLD SPLICED AT AFT CABIN LEFT COOR SILL FR66 INSTALLED PERFORMED BY V913393 INSP BY V892442 NEW 2 SPLICED AT NR 38551 IAW A319 SRM 51-42-11-001 AND SRM 319 53-41-14
- [SDR CALA2022020800346](https://openairdocs.org/sdr/CALA2022020800346.md): Fitting · cracked · Feb 8, 2022 · N850UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 68 FITTING #1 I/B LOWER HOLE IS CRACKED AT FRAME AT 10 AND 4 O''CLOCK POS. EA 5340-01724 002 PER HAECO LCQ NON ROUTINE/9290 455 GENERATED BY V061682
- [SDR CALA2022020400314](https://openairdocs.org/sdr/CALA2022020400314.md): Frame · corroded · Feb 3, 2022 · N850UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO FR30 STGR41R-STGR40R CLEAT CORRODED(A3NB-53-3-6105)G ENERATED BY:V061629 @HAECO LCQ PER NON ROUTINE 9290301 (38301) REMOVED AND REPLACED CLEAT WITH NEW PART P/N:D532351320002, PO:1 PERFORMED BY: V932428 INSP BY:V892285 0728623 ON FWD CARGO COMPARTMEN
- [SDR CALA2022020100292](https://openairdocs.org/sdr/CALA2022020100292.md): Intercostal · cracked · Feb 1, 2022 · N850UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR16 DOOR STOP #7 HOLE #1 AND 3 CRACKED AT INTERCOSTAL EA 531 1-02164 AD RELATED PER HAECO LCQ NON ROUTINE 9290419/38419 GENER ATED BY V061682
- [SDR CALA2022020100289](https://openairdocs.org/sdr/CALA2022020100289.md): Cleat · corroded · Feb 1, 2022 · N850UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO FR30 STGR41R-STGR40R CLEAT CORRODED(A3NB-53-3-6105)G ENERATED BY:V061629 @HAECO LCQ PER NON ROUTINE 9290301 (38301) REMOVED AND REPLACED CLEAT WITH NEW PART P/N:D532351320002, PO:1 PERFORMED BY: V932428 INSP BY:V892285 0728623 ON FWD CARGO COMPARTMEN
- [SDR CALA2022012600239](https://openairdocs.org/sdr/CALA2022012600239.md): Intercostal · cracked · Jan 25, 2022 · N850UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR16 DOOR STOP #7 HOLE #1 AND #3 CRACKED AT INTERCOSTAL, HOLE #2 CRACKED AT FRAME. GENERATED BY V061682 ON HAECO LCQ NR 92904 18/38418 REMOVED AND REPLCED INTERCOASTAL FITTING AT FR16 STOP #7 IAW A31 9 AIRBUS DWG R53113118 PERFORMED BY 061680 INSP BY V89228
- [SDR CALA2019071501193](https://openairdocs.org/sdr/CALA2019071501193.md): Floor Support · corroded · Jul 12, 2019 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LT AFT CABIN CORNERR FLOOR SUPPORT UNDER SHEAR WEB IS CORRODED PER NR LP 9290299 REMOVED AND REPLACED DISCREPANT FLOOR SUPPORT AT LT AFT CORNERR FR69-70 IAW SRM 51-72-11-911-001 AND 51-42-11-001 PARA E.
- [SDR CALA2017123104715](https://openairdocs.org/sdr/CALA2017123104715.md): Circuit Breaker · tripped · Dec 31, 2017 · N850UA · Airbus A319131 · Emergency Lighting
  > C/B TRIPPED ON OVERHEAD PANEL ECAM. EMER LIGHTS CABIN RESET C/B EMERGENCY LIGHTS CHECK OK.
- [SDR CALA2016041195265](https://openairdocs.org/sdr/CALA2016041195265.md): Skin · gouged · Apr 8, 2016 · N850UA · Airbus A319131 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HAS SKIN GOUGE UPPER AFT AREA. INSTALLED DOUBLER REPAIR IAW SRM52-31-00-201 FIG 209.
- [SDR CALA2014061391256](https://openairdocs.org/sdr/CALA2014061391256.md): Hydraulic Line · chafed · Jun 12, 2014 · N850UA · Airbus A319131 · Hydraulic System, Main
  > FOUND HYD LEAK COMING FROM RT LG UPPER FWD BEHIND BEAM FOUND YELLOW SYS PRESS LINE LEAKING CHAFED ON SUCTION LINE IAW IPC 29-13-05-04C ITEM 23 & 24. ALL LINE CLAMPS REMOVED STOWED IN PART BAGS AT POSITIONS REMOVED YELLOW SYS HEAD PRESS REMOVED. INSTALLED & S
- [SDR CALA2014032490675](https://openairdocs.org/sdr/CALA2014032490675.md): Structure · corroded · Mar 24, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.
- [SDR CALA2014031290598](https://openairdocs.org/sdr/CALA2014031290598.md): Fitting · corroded · Mar 11, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.
- [SDR CALA2014031290588](https://openairdocs.org/sdr/CALA2014031290588.md): Fitting · corroded · Mar 11, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN L1 & L2 FWD & AFT GIRT BAR FITTINGS HAS LIGHT CORROSION UNDER FITTING AROUND BOLT HOLES.
- [SDR CALA2014031090563](https://openairdocs.org/sdr/CALA2014031090563.md): Fastener · damaged · Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 9 APPROXIMATELY 9 INCHES RT OF TOP CTR LINE. R & R FASTENERS IAW SRM 53-11-11-FG 208.
- [SDR CALA2014031090562](https://openairdocs.org/sdr/CALA2014031090562.md): Fastener · damaged · Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 12 APPROXIMATELY 10 INCHES RT OF TOP CTR LINE, R & R FASTENERS IAW SRM 53-11-11-FG 208.
- [SDR CALA2014031090561](https://openairdocs.org/sdr/CALA2014031090561.md): Fastener · damaged · Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 13 APPROXIMATELY 10 INCHES RT OF TOP CTR LINE. R & R FASTENERS.
- [SDR CALA2014031090560](https://openairdocs.org/sdr/CALA2014031090560.md): Fastener · damaged · Mar 8, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LIGHTNING STRIKE DAMAGE AT RIVET AREA FRAME 8 APPROXIMATELY 9.5 INCHES RT OF TOP CTR LINE. R & R FASTENER.
- [SDR CALA2014030790545](https://openairdocs.org/sdr/CALA2014030790545.md): Stringer · corroded · Mar 5, 2014 · N850UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT FUSELAGE STRINGER 26R AT FRAME 64 HAS CORROSION. R & R STRINGER IAW A-319 SRM 51-42-71 PG 25 PARA 7.
- [SDR CALA2014030790543](https://openairdocs.org/sdr/CALA2014030790543.md): Sill · corroded · Mar 5, 2014 · N850UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL BEAM CORRODED AT FRAME 66 & FRAME 68. R & R SILL BEAM IAW A319 SRM 51-42-11 PARA 6 & 7.
- [SDR CALA2014022790485](https://openairdocs.org/sdr/CALA2014022790485.md): Stringer · corroded · Feb 25, 2014 · N850UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CORROSION ON RT BULK CARGO COMPARTMENT STRINGER 31R AT FRAME 65.
- [SDR CALA2014010290022](https://openairdocs.org/sdr/CALA2014010290022.md): Nose Cowl · dented · Dec 31, 2013 · N850UA · Airbus A319131 · Engine Cowling System
  > DENT & SCRATCH AT THE 5 O-CLOCK POSITION ON THE RT HAND ENG INLET COWL 6 INCHES LONG & A DENT 1 INCH DEEP. INLET COWL MR71212 PCN 115-9100 MUST BE REPAIRED OR REPLACED WITHIN 2 CYCLES, WORK ACCOMPLISHED BY LCL MAINT.
- [SDR CALA2013121993806](https://openairdocs.org/sdr/CALA2013121993806.md): Flap · dented · Dec 18, 2013 · N850UA · Airbus A319131 · Trailing Edge Flaps
  > FOUND DENT IN LT INBD FLAP. DENT APPROXIMATELY.75 W X.062 DEEP, LOCATION 7 1-4 IN FROM TE 64 1-2 IN FROM INBD EDGE OK TO CF FOR 2C FOR EDDY CURRENT IAW ECRA 572101360.
- [SDR CALA2013121293637](https://openairdocs.org/sdr/CALA2013121293637.md): Wire Harness · faulty · Dec 11, 2013 · N850UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT TEST FAILED, INTERIOR LOAD AFT LT. REPLACED WIRE HARNESS FOR SEAT 34C, EMERGENCY LIGHT TEST IS OKAY.
- [SDR CALA2013112193188](https://openairdocs.org/sdr/CALA2013112193188.md): Paint · chipped · Nov 17, 2013 · N850UA · Airbus A319131 · Aerodynamic Fairings
  > RADOME HAS NUMEROUS PAINT CHIPS.
- [SDR CALA2013100491741](https://openairdocs.org/sdr/CALA2013100491741.md): Panel · cracked · Oct 3, 2013 · N850UA · Airbus A319131 · Nacelle/Pylon, Plate/Skin
  > CRACK ON TOP OF NR 1 ENGINE PYLON JUST FWD OF LEADING FLAP LE. REPLACED PANEL IAW AMM.
- [SDR CALA2013090490994](https://openairdocs.org/sdr/CALA2013090490994.md): Starter · failed · Sep 2, 2013 · N850UA · Airbus A319131 · Engine Starter
  > DURING NR 1 ENGINE START FIRE SPARK BITS CAME OUT OF THE ENGINE. REPLACED LT ENGINE STARTER.
- [SDR CALA2013082090604](https://openairdocs.org/sdr/CALA2013082090604.md): Cover · missing · Aug 19, 2013 · N850UA · Airbus A319131 · Fuel Indicating System
  > UNDERWING FUEL PANEL FILL VALVE LENS COVER MISSING. REPLACED LENS COVER.
- [SDR UALA2013061904263](https://openairdocs.org/sdr/UALA2013061904263.md): Floor Panel · damaged · Jun 18, 2013 · N850UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PANEL BY DOOR HAS SHARP EDGE. PERFORMED INTERIM REPAIR PART 1 OF ECRA 5322-01050.
- [SDR UALA2013042902953](https://openairdocs.org/sdr/UALA2013042902953.md): Floor Panel · delaminated · Apr 27, 2013 · N850UA · Airbus A319131 · Fuselage Floor Panel
  > FORWARD CARGO BAY FLOOR PANEL 131AF IS DELAMINATED AND HAS TOP SURFACE PERFORATION. REPLACED FLOOR PANEL IAW 53-22-14.
- [SDR UALA2013030701367](https://openairdocs.org/sdr/UALA2013030701367.md): Oxygen Mask · no test · Mar 6, 2013 · N850UA · Airbus A319131 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK DOES NOT TEST CORRECTLY WITH PRESS TO TEST BUTTON. REPLACED MASK & STOWAGE BOX IAW MM 35-12-41-000-001A AND MM 35-12-41-400-001-A AND REPLACED FULL FACE QUICK DONNING O2 MASK IAW MM 35-12-41- 400-002-A. LEAK AND OPS CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N850UA/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 = 'N850UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N850UA/reports

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