# Service difficulty reports: N815UA

A list on [N815UA](https://openairdocs.org/aircraft/N815UA.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 · 93 reports

- [SDR CALA2026061117003](https://openairdocs.org/sdr/CALA2026061117003.md): Skin · dented · Jun 8, 2026 · N815UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DAMAGE APPROX 21 INCHES AFT OF FWD AVIONICS DOOR. DENT MEASURES 1"W X 1"L X.030" DEEP. AT FR 16R AND 2 RIVETS UP FROM STGR 36R. DENT IS OUT OF LIMITS, IN RESTRICTED AREA REF. SRM 53-11-11-283-012, FRAME 16 INBETWEEN STRINGER 32 AND 31. DENT IS ON RH FRAME
- [SDR CALA2025081407735](https://openairdocs.org/sdr/CALA2025081407735.md): Fuel Cap · missing · Aug 13, 2025 · N815UA · Airbus A319131 · Fuel Storage
  > AIRCRAFT ARRIVED WITH FUEL CAP MISSING. REF GMM 02-30-95. REF FUEL CAP CDL LOG PAGE 5902678.
- [SDR CALA2025070706263](https://openairdocs.org/sdr/CALA2025070706263.md): Battery · no test · Jul 3, 2025 · N815UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY BATTERY CAPACITY TEST FAILED. EMER R BATTERY REQUIRES REPLACEMENT. REMOVED R EMER EPSU BATTERY PER AMM 33-51-38-000-002-A. INSTALLED R EMER EPSU BATTER PER AMM 33-51-38-400-002-A. BITE CHECK GOOD.
- [SDR CALA2025041703926](https://openairdocs.org/sdr/CALA2025041703926.md): Light Sys · malfunctioned · Apr 16, 2025 · N815UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY "EXIT" LIGHTED SIGNS ILLUMINATED AT DOORS 1L, 1R, O/W LH, AND O/W RH REGARDLESS OF SWITCH POSITION. REMAINDER OF LIGHTS OFF W/ SWITCH IN OFF OR ARM. RESET AIRCRAFT POWER. REF AMM 33-51-00, ALL LIGHTS ILLUMINATE AND EXTINGUISH AS NORMAL DEPENDING ON S
- [SDR CALA2025032103049](https://openairdocs.org/sdr/CALA2025032103049.md): Slide · expired · Mar 18, 2025 · N815UA · Airbus A319131 · Escape Slide
  > FORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - REPLACEMENT OF SLIDE PERFORMED ON TASK 31-2562-1-3803.
- [SDR CALA2025032103048](https://openairdocs.org/sdr/CALA2025032103048.md): Slide · expired · Mar 17, 2025 · N815UA · Airbus A319131 · Escape Slide
  > AFT DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0021}. REPLACEMENT ACCOMPLISHED TASK CARD 31-2562-1-3804.
- [SDR CALA2024081300419](https://openairdocs.org/sdr/CALA2024081300419.md): Unknown · damaged · Aug 12, 2024 · N815UA · Airbus A319131 · Fuselage Structure (General)
  > 25APR SFO CF -T:MAJOR REPAIR AT FR12 STR 6L. REPAIR WAS INSTALLED ON 08-26-2008 AT HMV2 LAKE CITY ON NR D8344Z PER SRM 5 3-11-11 FIG 212. REPAIR IS INACTIVE AND SUPERSEDED BY AND IS IN ACCORDANCE WITH SRM 53-00-11 FIG 232. INSPECTION INSTRUCTION REF IIR IS 53
- [SDR CALA2024081300418](https://openairdocs.org/sdr/CALA2024081300418.md): Unknown · damaged · Aug 12, 2024 · N815UA · Airbus A319131 · Fuselage Structure (General)
  > 25APR SFO CF -T:MAJOR REPAIR AT FR34 STR 10R REPAIR WAS IN STALLED ON 08-26-2008 AT HMV2 ON NR D8346Z PER SRM 53-21-11 FIG 214. REPAIR IS INACTIVE AND SUPERSEDED BY AND I N ACCORDANCE WITH SRM 53-00-11 FIG 232.REPAIR CATEGORY B INSPECT ION INSTRUCTION REF IIR
- [SDR CALA2022091202343](https://openairdocs.org/sdr/CALA2022091202343.md): Eec · inoperative · Sep 12, 2022 · N815UA · Airbus A300* · Engine Exhaust System
  > PILOT REPORTS E1 REV FAULT. DIVERSION INTO BNA. THRUST REVERSER HAS BEEN DEACTIVATED AND SECURED IN THE FWD THRUST (STOWED AND LOCKED) POSITION. REMOVED AND REPLACED #1 ENGINE EEC. ACCP IDT INSPECTION OF EEC INSTALLATION SAFETY AND SECURITY. IDT EEC OP CHK PAS
- [SDR CALA2022020200295](https://openairdocs.org/sdr/CALA2022020200295.md): Fuel Cap · missing · Feb 1, 2022 · N815UA · Airbus A319131 · Aircraft Fuel System
  > FUEL CAP LANYARD MISSING CREW APPLIED CDL 28A. CAP LNAYARD MISSING. STICKER INSTALLED DISPATCH DESK: 14 NAME: MB DATE: 30-JAN-22- DEFERRED DIRECTLY BY TOMC INSTALLED NEW LANYARD.
- [SDR CALA2021110402033](https://openairdocs.org/sdr/CALA2021110402033.md): Plate · corroded · Nov 3, 2021 · N815UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO PIT FR24-FR28 UPPER TORQUE BOX WEB HAS CORRODED AREAS PER HAECO LCQ NR 9292521/36521 GENERATED BY V061704 REMOVED AND REPLACED TORQUE BOX COVER SHEET AT FWD CARGO PIT BET WEEN FR 24 AND FR 28 IAW A319 SRM 51-72-11-911-001 AND SRM 51-72 -11-911-002 AN
- [SDR CALA2021102901989](https://openairdocs.org/sdr/CALA2021102901989.md): Plate · cracked · Oct 27, 2021 · N815UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN BETWEEN FR69-70 STRINGER 23R FLOOR SUPPORT HAS CRACK O N SHEAR PLATE. PER HAECO LCQ NR 9292351/36351 GENERATED BY V9191 50 REMOVED AND REPLACED SLEAR PLATE IN AFT CABIN BETWEEN FR 67-70 S TR 23R IAW A319 SRM 51-72-11-911-001 REMOVED DOT M111
- [SDR CALA2021102901987](https://openairdocs.org/sdr/CALA2021102901987.md): Plate · corroded · Oct 27, 2021 · N815UA · Airbus A319131 · Fuselage Main, Floor Beam
  > R-2 DOOR SILL I/B UPPER SKIN HAS SPOTS OF CORROSION DOT M110. PE R HAECO LCQ NR 9292347/36347 GENERATED BY V919150
- [SDR CALA2018100102011](https://openairdocs.org/sdr/CALA2018100102011.md): Stop Fitting · cracked · Sep 27, 2018 · N815UA · Airbus A319131 · Fuselage Main, Structure
  > A CRACK INDICATION R1 DOOR STOP FITTING NR 7 HOLE NR 3 AT FR 1 6 AT 7 O’CLOCK POSITION AD 2017-22-03 ON LCQ REF 9290259 S PEC A3NB-53-4-6304 GENERATED BY V923744 ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECR A 5311-02017 ON OR BEFORE THE AIR
- [SDR CALA2018100102010](https://openairdocs.org/sdr/CALA2018100102010.md): Intercostal · cracked · Sep 27, 2018 · N815UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L-1 DOOR CUTOUT FRAME 16 STOP FITTING NR 1 LOWER INBOARD HOLE IS CRACKED IN WEB & INTERCOSTAL FITTING AT 6 O’CLOCK AD 2017-22-0 3 ON LCQ REF 9290063 SPEC A3NB-53-4-6304 GENERATED BY V061 633 ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS PER PART 2 ECRA 5 311-
- [SDR CALA2018092801999](https://openairdocs.org/sdr/CALA2018092801999.md): Stop Fitting · cracked · Sep 27, 2018 · N815UA · Airbus A319131 · Service Doors
  > R1 DOOR CUTOUT FRAME 20 STOP FITTING NO. 1 LOWER INBOARD HOLE IS CRACKED IN WEB & IN INTERCOCSTAL FITTING AT 6 O''CLOCK AD 2017-2 2-03 ON HAECO LCQ REF 9290062 SPEC A3NB-53-4-6304 GENERATED BY V 061633 REPAIRED PER EC/RA 5311-02017 R-1 DOOR FR20 #1HOLE. ACCOMP
- [SDR CALA2018092801998](https://openairdocs.org/sdr/CALA2018092801998.md): Stop Fitting · cracked · Sep 27, 2018 · N815UA · Airbus A319131 · Passenger/Crew Doors
  > A CRACK INDICATION L1 DOOR STOP FTG NO. 7 HOLE NO. 3 FR16 AT 5 O ''CLOCK POSITION AD RELATED TASK (2017-22-03) ON HAECO LCQ REF 92 90261 SPEC A3NB-53-4-5304 GENERATED BY V923744 REPAIRED HOLE 3 IAW ECRA 5311-02018.CREATE DTA LOGPAGE TO ACCOMP LISH THE INITIAL
- [SDR CALA2018092801997](https://openairdocs.org/sdr/CALA2018092801997.md): Stop Fitting · cracked · Sep 27, 2018 · N815UA · Airbus A319131 · Passenger/Crew Doors
  > A CRACK INDICATION R1 DOOR STOP FTG NO. 7 HOLE NO. 3 AT FR20 AT 5 O''CLOCK POSITION AD 2017-22-03 ON HAECO LCQ REF 9290260 SPEC A 3NB-53-4-6304 GENERATED BY V923744 REPAIRED PER EC/RA 5311-02017 R/H FR16 DOOR STOP #7 HOLE #3, FR2 0 DOOR STOP 1 HOLE #3, FR20 DO
- [SDR CALA2018011300178](https://openairdocs.org/sdr/CALA2018011300178.md): Filter · dirty · Jan 13, 2018 · N815UA · Airbus A319131 · Air Distribution System
  > STRONG WET SOCK ODOR IN THE FLT DECK DURING CLIMB. DID IT ON 2 LEGS. REMOVED AND REPLACED BOTH CABIN RECIRCULATIION AIR FILTERS IAW AMM 21-21-41-400--001-A.
- [SDR CALA2017122804631](https://openairdocs.org/sdr/CALA2017122804631.md): Unknown · odor · Dec 28, 2017 · N815UA · Airbus A319131 · Air Distribution System
  > DURING DESCENT, CABIN AIR QUALITY POOR HAD A WET SOCK ODOR. PERFORMED 05-50-00-810-831-A. RAN PACKS, NO NOTICIBLE ODORS AND NO HISTORY. OK TO CONTINUE.
- [SDR CALA2017111003987](https://openairdocs.org/sdr/CALA2017111003987.md): Unknown · odor · Nov 10, 2017 · N815UA · Airbus A319131 · Air Conditioning System
  > DURING DESCENT,.AC SYSTEM SMELLED LIKE OLD GYM SOCKS.. PERFORMED TSM 05-50-00-810-831-A, NO ODOR COMING OUT OF PACK SYSTEM, NO EVIDENCE OF ANY OIL LEAKAGE.
- [SDR CALA2017081402703](https://openairdocs.org/sdr/CALA2017081402703.md): Light · intermittent · Aug 14, 2017 · N815UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS GOING ON AND OFF UNCOMMANDED. RESET THE SYSTEM, OPS OK IAW MM 33-51-00
- [SDR CALA2017073002452](https://openairdocs.org/sdr/CALA2017073002452.md): Light · intermittent · Jul 30, 2017 · N815UA · Airbus A319131 · Emergency Lighting
  > EXIT PATH LIGHTING IS FLICKERING PERFORMED CIDS EMERGENCY SYS LIGHT TEST, NO FAULTS, RESET CIDS A S A PRECAUTION. OK FOR SERVICE.
- [SDR CALA2017051901485](https://openairdocs.org/sdr/CALA2017051901485.md): Lens · broken · May 19, 2017 · N815UA · Airbus A319131 · Emergency Lighting
  > AFT LAV AISLE EEL LIGHT BROKEN. REPLACED LENS. OPS NORMAL REF MM 33-51-19.
- [SDR CALA2017021200334](https://openairdocs.org/sdr/CALA2017021200334.md): Power Supply · faulty · Feb 12, 2017 · N815UA · Airbus A319131 · Emergency Lighting
  > EMER LIGHTS FAIL SYS TEST. REPLACE EMER LIGHT AFT POWER SUPPLY. OPS CK GOOD. REF AMM 33-51-38-400-001-A & IPC 33-51-04-07
- [SDR CALA2016121901123](https://openairdocs.org/sdr/CALA2016121901123.md): Unknown · malfunctioned · Dec 19, 2016 · N815UA · Airbus A319131 · Emergency Lighting
  > EMER EXIT LIGHT ON CONSTANTLY. CYCLED SWITCH NO HELP. NOTED FASTEN SEATBELT SWITCH ON, SWITCHED OFF. EMERGENCY EXIT LIGHTS ARE OFF NOW.
- [SDR CALA2016081595649](https://openairdocs.org/sdr/CALA2016081595649.md): Pump · failed · Aug 12, 2016 · N815UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > AIR RETURN FOR ECAM CAUTION MESSAGE B HYD RESERVOIR OVEHEAT. R & R BLUE SYSTEM ELECTIC HYD PUMP, CASE DRAIN FILTER, LP FILTER. SERVICED. OPS NORMAL
- [SDR CALA2015091894367](https://openairdocs.org/sdr/CALA2015091894367.md): Stator Vane · lack of lube · Sep 16, 2015 · N815UA · Airbus A319131 · Compressor Bleed Control
  > EXPERIENCED A FADEC B FAULT & ECAM STALL MSG. CREW REPORTS THAT ACFT YAWED SEVERAL TIMES ALONG WITH STALL ECAM & EGT INCREASED. POWER WAS REDUCED & PARAMETERS RETURNED TO NORMAL & ENG REMAINED RUNNING FOR DURATION OF FLIGHT. DECLARED EMER & AIR RETURNED. B
- [SDR CALA2015071594117](https://openairdocs.org/sdr/CALA2015071594117.md): Secu · faulty · Jul 13, 2015 · N815UA · Airbus A319131 · Drag Control System
  > SPOILER CONTROL FAULT DISPLAYED ON UPPER ECAM SCREEN. CREW REPORT, HAD VIBRATION & BOTH NR 3 SPOILERS WERE FLOATING UP. LANDED UNDERWEIGHT. R & R THE NR 1 SEC IAW MM 27-94-34-000-001-A & 400-001A. PERFORMED OPERATIONAL TEST IAW 27-94-00-710-00 2. ACFT OK
- [SDR CALA2015060893873](https://openairdocs.org/sdr/CALA2015060893873.md): Actuator · faulty · Jun 7, 2015 · N815UA · Airbus A319131 · Passenger Oxygen System
  > PASSENGER O2 MASKS DO NOT DEPLOY IN AFT LAVATORY. REPLACED DOOR ACTUATOR. DROP CHECK, CHECKED GOOD.
- [SDR CALA2015050693662](https://openairdocs.org/sdr/CALA2015050693662.md): Door Frame · corroded · Apr 27, 2015 · N815UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT AFT ENTRY DOOR CUT OUT AFT FRAME FWD FACE HAS ONE CORRODED FASTENER HOLE, 3 INCHES ABOVE FLOOR LINE & 4 INCHES INBD OF FUSELAGE. EXCESSIVE MATERIAL LOSS DURING CORROSION REMOVAL. REQUIRED INSTALLING DOUBLER IAW SRM 53-41-12-201 FIG 201.
- [SDR CALA2015050693656](https://openairdocs.org/sdr/CALA2015050693656.md): Door Frame · corroded · Apr 27, 2015 · N815UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT AFT ENTRY DOOR CUT OUT AFT FRAME FWD FACE HAS ONE CORRODED FASTENER HOLE, 3 INCH ABOVE FLOOR LINE & 4 INCH INBD OF FUSELAGE. EXCESSIVE MATERIAL LOSS DURING CORROSION REMOVAL. REQUIRED INSTALLING DOUBLER IAW SRM 53-41-12-201 FIG 201.
- [SDR CALA2014060291203](https://openairdocs.org/sdr/CALA2014060291203.md): Indication Sys · unknown · May 29, 2014 · N815UA · Airbus A319131 · Landing Gear Position and Warning
  > AIR RETURN TO ORD FOR POSSIBLE GEAR INDICATION ISSUE.
- [SDR CALA2014050690955](https://openairdocs.org/sdr/CALA2014050690955.md): Skin · cracked · May 4, 2014 · N815UA · Airbus A319131 · Engine Collector/Tailpipe/Nozzle
  > NR 2 ENG CHANGE, EXHAUST CONE SKIN HAS A CRACK EXCEEDING SIX INCHES AT THE 530 POSITION. REPLACED IAW MM-78-11-12- 400-010-A13.
- [SDR CALA2013123093999](https://openairdocs.org/sdr/CALA2013123093999.md): Plug · faulty · Dec 28, 2013 · N815UA · Airbus A319131 · Spark Plug/Igniter
  > ENG 2 START MALFUNCTION AUTO ABORT IGNITION 2 FAULT. R & R IGNITER PLUGS, OPERATIONS CHECKED OK.
- [SDR CALA2013122393895](https://openairdocs.org/sdr/CALA2013122393895.md): Wire · loose · Dec 21, 2013 · N815UA · Airbus A319131 · Light System Wiring
  > EMERGENCY EXIT LIGHT 12C INOPERATIVE. REPAIRED LOOSE WIRE TO LIGHT.
- [SDR CALA2013112093143](https://openairdocs.org/sdr/CALA2013112093143.md): Coffeemaker · dirty · Nov 19, 2013 · N815UA · Airbus A319131 · Buffet/Galleys
  > THE INBOUND CABIN CREW REPORTED TO CUSTOMER SVC THERE WAS AN ELECTRICAL BURNING SMELL IN THE CABIN. NO LOCATION & NO WRITE UP WITH NO SMOKE IN CABIN REPORT INITIATED. THE FLIGHT ATTENDANT WHO REPORTED THE BURNING SMELL RETURNED TO THE ACFT TO POINT OUT THE L
- [SDR CALA2013111893013](https://openairdocs.org/sdr/CALA2013111893013.md): Tab · out of position · Nov 15, 2013 · N815UA · Airbus A319131 · Passenger Compartment Equipment
  > RED PLASTIC HANGING OUT OF CEILING AT 25B MAY BE OXYGEN MASK PROBLEM. SECURE TAB, FOUND O2 DOOR CLOSED.
- [SDR CALA2013110892761](https://openairdocs.org/sdr/CALA2013110892761.md): Liner · loose · Nov 7, 2013 · N815UA · Airbus A319131 · Engine Thrust Reverser
  > NR 2 ENG INBD TR INNER LINER. ACCOMPLISH INSPECTION OR RECHECK REQUIRED. WHEN COMPLETE, SIGN OFF THIS MF ITEM ONLY, DO NOT SIGN OFF. NR 2 ENG INBD TR INNER LINER HAS WIRE MESH COMING LOOSE. APPLIED SPEED TO TR INNER SLEEVE 9 TO 6 O'CLOCK POSITION.
- [SDR CALA2013103092530](https://openairdocs.org/sdr/CALA2013103092530.md): Contactor · failed · Oct 29, 2013 · N815UA · Airbus A319131 · Electrical Power System Wiring
  > BEFORE PUSHBACK BCL 1 FAULT. REPLACED CONTACTOR IAW MM 24-38-55-000-001-A. MESSAGE CLEARED, BCL CFDS TEST PASSED.
- [SDR CALA2013110192569](https://openairdocs.org/sdr/CALA2013110192569.md): Warning System · activated · Oct 29, 2013 · N815UA · Airbus A319131 · DC Indicating System
  > BCL 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, ELECTRICAL. CAME ON 15 MIN AFTER PUSH BACK ITEM ROLLED FORWARD. CFDS REPORTS ELECTRICAL BCL 1 FAULT & PREVIOUS REPORT HIT FUSE 4PB11 PCN 562-3969 & FOLLOW TSM 24-38-00-810-807. R & R BATTERY SHUNT 3PB1 IAW AMM 2
- [SDR CALA2013081990520](https://openairdocs.org/sdr/CALA2013081990520.md): Window · faulty · Aug 18, 2013 · N815UA · Airbus A319131 · Flight Compartment Windows
  > RT WINDOW DISPLAYED ON UPPER ECAM. REMOVED WINDOW AND INSTALLED NEW ONE. COMPLETED RT WINDOW INSTALLATION, OPS CHECKED GOOD.
- [SDR CALA2013081990516](https://openairdocs.org/sdr/CALA2013081990516.md): Controller · faulty · Aug 16, 2013 · N815UA · Airbus A319131 · Windshield/Door Rain/Ice Removal
  > RT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI-ICE RT WINDSHIELD ECAM. REPLACED IAW TSM 30-42-00-810-831, SENSORS CHECKED NORMAL. REPLACED CONTROLLER IAW MM. OPS CHECKED NORMAL FR 078 REMOVED, REV TSM TO 30-42-00-810-804-A.
- [SDR UALA2013070504699](https://openairdocs.org/sdr/UALA2013070504699.md): Sign · damaged · Jul 3, 2013 · N815UA · Airbus A319131 · Emergency Lighting
  > BROKEN PIECE ON PAX LOADING DOOR. SECURE PANEL HOLDING EXIT SIGN BETWEEN F/A SEAT AND L1 DOOR. OP TESTED EXIT SIGN AFTER SECURING PANEL.
- [SDR UALA2013053003752](https://openairdocs.org/sdr/UALA2013053003752.md): Shroud · cracked · May 29, 2013 · N815UA · Airbus A319131 · Water Line Anti-Ice System
  > AFT DRAIN MAST OUTER SHROUD CRACK.
- [SDR UALA2013041802693](https://openairdocs.org/sdr/UALA2013041802693.md): Headset · broken · Apr 17, 2013 · N815UA · Airbus A319131 · Audio Integrating System
  > COCKPIT OBSERVERS HEADSET IS BROKEN. RIGHT EAR PIECE COMES OFF. REPLACED OBS HEADSET.
- [SDR UALA2013041602610](https://openairdocs.org/sdr/UALA2013041602610.md): Trim Panel · unsecure · Apr 15, 2013 · N815UA · Airbus A319131 · Passenger Compartment Equipment
  > AFT GALLEY FLOOR TRIM BY AFT ROW OF CARTS IS COMING UP HARD TO PULLOUT CARTS. SECURED TRANSITION STRIP DOWN PER EC-RA# 2525-01497. ECRA COMPLIED WITH. (TRANSITION PART NOT AVAIL FOR REPLACEMENT)
- [SDR UALA2013032701954](https://openairdocs.org/sdr/UALA2013032701954.md): Eec · faulty · Mar 25, 2013 · N815UA · Airbus A319131 · Fuel Control/Turbine Engines
  > CREW REPORTS: AT FLAP RETRACTION AFTER TAKEOFF, GOT STATUS MSG ON LOWER ECAM, WHEN SLATS OUT. ENGINE 2 AT IDLE ON GROUND. ENGINE 2 MAX PWR-IDLE. INOP SYS SHOWS REV 2 AND ENGINE 2 THR. REPLACED NR 2 ENGINE EEC REFERENCE MM 73-22-34, OPS CHECK NORMAL.
- [SDR UALA2013022601144](https://openairdocs.org/sdr/UALA2013022601144.md): Bottle · faulty · Feb 25, 2013 · N815UA · Airbus A319131 · Portable Oxygen System
  > OXYGEN BOTTLE MISSING - USED AT LOCATION NOT SPECIFIED CREW COMMENTS: ONE O2 BOTTLE USED AND ONE THE KNOB TO START THE FLOW OF O2 WOULD NOT TURN. REPLACED BOTH O2 BOTTLES.
- [SDR UALA2013022001012](https://openairdocs.org/sdr/UALA2013022001012.md): Light · damaged · Feb 19, 2013 · N815UA · Airbus A319131 · Emergency Lighting
  > AISLE EMERGENCY PATHWAY LIGHT DAMAGED AT SEAT 12C, 30C, AND 32C. RELAMPED ABOVE REFERENCED LIGHTS PER AMM, IPC 33-51-04, BR9644-21.

Next page: https://openairdocs.org/aircraft/N815UA/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 = 'N815UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N815UA/reports

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