# Service difficulty reports: N831UA

A list on [N831UA](https://openairdocs.org/aircraft/N831UA.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 4 · 153 reports

- [SDR CALA2026102120482](https://openairdocs.org/sdr/CALA2026102120482.md): Unknown · odor · Oct 19, 2026 · N831UA · Airbus A319131 · Air Distribution System
  > FUMES THROUGHOUT ACFT AFTER SHUTDOWN OF NR 2 ENGINE AND OPENING APU BLEED. RAN APU & BLEED TO VERIFY ODOR IN CABIN, ACCOMPLISHED INSPECTION IAW AMM 05-50-00-810-831-A. OPS APU FOR EXTENDED PERIOD & PACKS USING APU BLEED. NO ODORS NOTED DURING OPS.
- [SDR CALA2026102120493](https://openairdocs.org/sdr/CALA2026102120493.md): Flashlight · no discrepancy · Oct 17, 2026 · N831UA · Airbus A319131 · Emergency Equipment
  > AFT FLASHLIGHT NEAR FLIGHT ATTENDANT JUMPSEAT BATTERY FLASHING RED INOP STICKER INSTALLED ON THE AFFECTED FLASHLIGHT BY THE CAPTAIN. AFT OTBD FLASHLIGHT WORKING NORMAL. NO RED LIGHT, TESTING FUNCTION PRODUCES GREEN LIGHT CONSISTENT WITH OTHER FLASHLIGHTS. INO
- [SDR CALA2026090319212](https://openairdocs.org/sdr/CALA2026090319212.md): Panel · damaged · Sep 2, 2026 · N831UA · Airbus A319131 · Aerodynamic Fairings
  > FAIRING PANEL 192DT RAMP DISCOVERED PANEL 192 DT DAMAGED ON WALK AROUND. NO LARGE PORTIONS OF PANEL DEPARTED AIRCRAFT. PANEL WAS TORN FROM LEADING EDGE AROUND 2 FT TOWARD THE BACK.
- [SDR CALA2026062217221](https://openairdocs.org/sdr/CALA2026062217221.md): Fuel Cap · missing · Jun 19, 2026 · N831UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING UNDER RIGHT WING. PDA AND SDR GENERATED FOR MISSING FUEL CAP. FOUND FUEL CAP AT DEN STATION, INSTALLED FUEL CAP IN REF TO AMM TASK 28-25-41-400-007-A.
- [SDR CALA2026050816077](https://openairdocs.org/sdr/CALA2026050816077.md): Blanking Plate · missing · May 7, 2026 · N831UA · Airbus A319131 · Main Landing Gear Attach Section
  > LEFT GEAR BEARING BLANKING PLUG MISSING. ROUND PURPLE PLUG TOP AFT OF LEFT LANDING GEAR STRUT MISSING TOMC APPROVED, QC REVIEWED PERMANENT REPAIR PER PART 3 INSTRUCTIONS WITHIN 25 FH. PERFORMED PART 1 INTER REPAIR REF ECRA 3211-01346. MUST ACCOMPLISH DAILY IN
- [SDR CALA2026042815805](https://openairdocs.org/sdr/CALA2026042815805.md): Spoiler Sys · faulted · Apr 26, 2026 · N831UA · Airbus A319131 · Drag Control System
  > FLIGHT CREW REPORTS VIA DISPATCH ARINC F/CTL SPLR FAULT WITH CFDS L SPLR1 POS ERROR 31CE1. SPOILER PAIR IS EXTENDED PER CAPTAIN. FOUND NR 1 LT SPOILER (31CE1) SERVO ACTUATOR IN BYPASS MODE IAW AMM 27-60-00-866-002-A. PLACED SERVO BACK INTO NORMAL OPS. NOW U
- [SDR CALA2026030214208](https://openairdocs.org/sdr/CALA2026030214208.md): Wire · shorted · Feb 26, 2026 · N831UA · Airbus A319131 · Landing Gear System Wiring
  > BRAKES ECAM, AUTO BRAKE FAULT BRAKE. PERFORMED OPERATINAL CHECK AND INSPECTION ON THE BRAKE 3 AND 4. PISTONS ARE MOVING WHILE PRESSING BRAKES. PERFORMED BITE TEST ON BSCU IAW TASK 32-46-00-740-001-A. CHAN 1 AND CHAN 2 NORMAL BRAKING TEST SHOWS TACHOMETER3 (
- [SDR CALA2025090108321](https://openairdocs.org/sdr/CALA2025090108321.md): Post · worn · Aug 23, 2025 · N831UA · Airbus A319131 · Fuselage Main, Structure
  > FWD CARGO, FWD BULKHEAD VERTICAL POSTS WORN AT UPPER ATTACH POINT. ACCOMPLISHED SPLICE RPR ON Y254 VERT MEMBER AT FWD CARGO BULK HEAD FR24 IAW SRM 53-21-29-300-003. REQUIRES INSP AT 15000 FC/30 000 FH/ 72 MONTHS.
- [SDR CALA2025082508083](https://openairdocs.org/sdr/CALA2025082508083.md): Plate · corroded · Aug 22, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > INTERNAL FUSELAGE UNDER FLOOR STRUCTURE FR68 14DU DRAIN MAST "F" HAS CORROSION AROUND SURROUNDING STRUCTURE GEN BY V798788 ON HA ECO LCQ NR 9296689/20689 ESFR INFORMATION UPDATE REMOVED AND REPLACED ANGLE SUPPORT AT INTERNAL FUSELAGE UNDER FL OOR STRUCTURE FR6
- [SDR CALA2025090108312](https://openairdocs.org/sdr/CALA2025090108312.md): Frame · cracked · Aug 6, 2025 · N831UA · Airbus A319131 · Fuselage Main, Frame
  > FR35, S30L, FRAME FWD FACE HAS CRACK INDICATION AT FASTENER ADJACENT TO HOLE 2. CRACK EXTENDING APPROX.050 FROM FASTENER IN THE 10 OCLOCK DIRECTION. ACCOMPLISHED PART 1: INTERIM REPAIR IAW REO-L25490, REV IR. MAJOR REPAIR. COMPLIED WITH RII INSPECTION
- [SDR CALA2025090108313](https://openairdocs.org/sdr/CALA2025090108313.md): Spar · gouged · Aug 1, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT PYLON UPPER SPAR UPPER SURFACE AT RIB 4-RIBS HAS GOUGE AREA. ACCOMPLISHED PART 1, INTERIM REPAIR PER REO-L25512 REV IR. PER EC 5451-0500. ACCOMPLISH A PERMANENT REPAIR AT RH PYLON REAR UPPER SPAR UPPER SURFACE BETWEEN RIBS 4 & 5 PER PART 3 IAW ECRA 54
- [SDR CALA2025080407241](https://openairdocs.org/sdr/CALA2025080407241.md): Profile · corroded · Aug 1, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH FR 35 BULKHEAD LOWER PROFILE CORRODED STR 35-38L. REMOVED AND REPLACED PROFILE PANEL AT FWD CARGO FR 35, S35-38L IAW SRM 51-42-11-00.
- [SDR CALA2025080407234](https://openairdocs.org/sdr/CALA2025080407234.md): Panel · cracked · Jul 31, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 56 LSTR 32-35 PROFILE PANEL IS CORRODED AND BROKEN. REMOVED AND REPLACED DISCREPANT FR56 L/H STR 32-35 PROFILE IAW A 319 SRM 51-42-11-001.
- [SDR CALA2025080407233](https://openairdocs.org/sdr/CALA2025080407233.md): Profile · corroded · Jul 31, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY FR34 PROFILE PNL HAS CORROSION STR 38 LH-RH. REMOVED AND REPLACED PROFILE PANEL AT FWD CARGO FR 34 STR 38 L/H -R/H IAW A319 SRM 51-42-11-001.
- [SDR CALA2025081407728](https://openairdocs.org/sdr/CALA2025081407728.md): Bolt · cracked · Jul 30, 2025 · N831UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 68, STR 22 HAS CRACK INDICATION AT LOWER SIDE OF FLANGE ABOVE DOOR STOP FASTENERS NR 3.
- [SDR CALA2025081107554](https://openairdocs.org/sdr/CALA2025081107554.md): Fitting · corroded · Jul 25, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > NUMBER 1 PYLON SPIGOT BEARING LOWER FITTING HAS CORROSION. R & R THE NR 1 PYLON SPIGOT BEARING LOWER FITTING IAW SRM 54-51-12-300-002.
- [SDR CALA2025072806968](https://openairdocs.org/sdr/CALA2025072806968.md): Bushing · corroded · Jul 25, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > NR 2 PYLON SPIGOT BEARING AND SLEEVE HAVE CORROSION. INSTALLED SERVICEABLE #2 SPIGOT BEARING AND SLEEVE IAW A319 AMM 54-51-41-400-001-A AND 57-26-12-400-002-A.
- [SDR CALA2025072806965](https://openairdocs.org/sdr/CALA2025072806965.md): Fitting · corroded · Jul 25, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > NUMBER 2 PYLON SPIGOT LOWER FITTING HAS CORROSION. REMOVED AND REPLACED NR 2 PYLON SPIGOT BEARING LOWER FITTING IAW SRM 54-51-12-300-002. REMOVED AND REPLACED #2 PYLON SPIGOT BEARING LOWER FITTING IAW SRM 54-51-12-300-002.
- [SDR CALA2025072806964](https://openairdocs.org/sdr/CALA2025072806964.md): Bushing · corroded · Jul 25, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > #1 PYLON SPIGOT BEARING AND SLEEVE HAVE CORROSION. INSTALLED NEW #1 PYLON SPIGOT BEARING AND SLEEVE IAW A319 AMM 54-51-41-400-001-A AND AMM 57-26-12-400-002-A. INSTALLED NEW #1 PYLON SPIGOT BEARING AND SLEEVE IAW A319 AMM 54 -51-41-400-001-A AND 57-26-12-4
- [SDR CALA2025072106756](https://openairdocs.org/sdr/CALA2025072106756.md): Shear Tie · gouged · Jul 18, 2025 · N831UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > INBD AND OTBD FWD UPPER SKIN SUPPORT FLANGES HAVE PREVIOUS GOUGES PR ESENT AND REQUIRE REPLACEMENT. REMOVED AND REPLACED I/B AND O/B FWD UPPER SKIN SUPPORT ANGLES I AW A319 SRM 51-42-11-01.
- [SDR CALA2025071506579](https://openairdocs.org/sdr/CALA2025071506579.md): Skin · dented · Jul 14, 2025 · N831UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AIRCRAFT FUSELAGE DENTED NEAR A REPAIR DOUBLER AT APPROXIMANTELY FR26 STR40L PER HAECO LCQ NON ROUTINE 9296899/20899 GENERATED B Y V075078 ESFR COMPLETED REMOVED/FABRICATED/INSTALLED SOUBLER AT FR26 BELLY BETWEEN STGR 40L TO STGR40R IAW A319 SRM 53-21-11-300-0
- [SDR CALA2025071506578](https://openairdocs.org/sdr/CALA2025071506578.md): Seat Track · corroded · Jul 14, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y765 SEAT TRACK FR 47-64 FOUND OUT OF LIMITS AND REQUIRES REPAIR. SEAT TRACK Y765 FR 47-64 REMOVED AND REPLACED IAW A319 SRM 51-42 -11/001 AND 51-72-11-911-002.
- [SDR CALA2025071506577](https://openairdocs.org/sdr/CALA2025071506577.md): Seat Track · corroded · Jul 14, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y-1292 SEAT TRACK FR 47-64 FOUND OUT OF LIMITS AND REQUIRES REPAIR. REMOVED AND REPLACED Y-1292 SEAT TRACK AT MAIN CABIN FR 47-64 IA W A319 SRM 51-42-11-001.
- [SDR CALA2025071106468](https://openairdocs.org/sdr/CALA2025071106468.md): Floor Panel · corroded · Jul 10, 2025 · N831UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO ENTRY DOOR FLOOR HAS CORROSION SPOTS ON UPPER SURFACE. REMOVED AND REPLACED DOOR SILL AT AFT CARGO DOOR IAW A319 SRM 51 -42-11-001.
- [SDR CALA2025072506899](https://openairdocs.org/sdr/CALA2025072506899.md): Panel · cracked · Jul 8, 2025 · N831UA · Airbus A319131 · Service Doors
  > R-1 DOOR EXTERNAL SURFACE UPPER PANEL AFT AREA HAS CRACK. GEN BY /N078570 ON HAECO LCQ NR 9296187/20187 ESFR COMPLETED REMOVED & REPLACED PLATE @ R-1 UPPER DOOR I/A/W A319 SRM 51-42-1 1/001 SFR#1329 PER MECH V936069 INSP V935513 RII COMPLIED WITH BY HAECO LCQ
- [SDR CALA2025082007967](https://openairdocs.org/sdr/CALA2025082007967.md): Bushing · out of limits · Jul 6, 2025 · N831UA · Airbus A319131 · Elevator Structure
  > R/H ELEVATOR HAS 2EA PREVIOUSLY OVERSIZED PLAIN BUSHINGS WITH WO RN I/D AT HINGES 5 OUTBOARD AND 6 INBOARD. PERFORMED OVERSIZING REPAIR AT R/H ELEVATOR HINGE #5 AND #6 IAW A319 SRM 55-26-41-300-004 THIS REINSPECT AT 6 YEARS FROM REPAIR EMBODIMENT WITH SUB IN
- [SDR CALA2025072506898](https://openairdocs.org/sdr/CALA2025072506898.md): Floorbeam · corroded · Jul 6, 2025 · N831UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CARGO AT FR 55, LSTR43 AND UNDERFLOOR BEAM BRACKETS, HAS COR ROSION. REMOVED AND REPLACED CLIP AFT CARGO AT FR55 STGR 43L IAW A319 SR M 51-42-11-001.
- [SDR CALA2025070906374](https://openairdocs.org/sdr/CALA2025070906374.md): Bracket · worn · Jul 1, 2025 · N831UA · Airbus A319131 · Wing Miscellaneous Structure
  > R/H AFT FLAP STRUT SENSOR BRACKET PLATE BEARING HAS EXCESSIVE PLAY. REMOVED AND REPLACED DICREPANT R/H AFT FLAP STRUT SENSOR BRACKET IAW A319 SRM 51-42-11-001.
- [SDR CALA2025070306187](https://openairdocs.org/sdr/CALA2025070306187.md): Seat Track · corroded · Jun 30, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN BETWEEN FR12-24 FLOOR SEAT TRACK BEAM Y254(L/H) HAS CORROSION ON UPPER SURFACE AROUND FASTERNER HOLE. REMOVED AND REPLACED Y254 FLOOR SEAT TRACK BEAM LH AT CABIN BETWEEN FR 12-24 IAW A319 SRM 51-42-11-001.
- [SDR CALA2025070306186](https://openairdocs.org/sdr/CALA2025070306186.md): Floor Support · corroded · Jun 30, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN BETWEEN FR12-24 FLOOR SUPPORT Y-254(R/H) HAS COR OSION ON UPPER SURFACE AROUND FASTENER HOLE. REMOVED AND REPLACED Y254 SUPPORT BEAM RH AT MAIN CABIN BETWEEN FR 12-24 IAW SRM 51-42-11-001.
- [SDR CALA2025063006071](https://openairdocs.org/sdr/CALA2025063006071.md): Panel · corroded · Jun 27, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 58 LSTR 38-RSTR 41 PROFILE PANEL IS CORRODED AND LO OSE. GENERATED BY V798788 ON HAECO LCQ NR 9296674 / 20674 ESFR INFORMATION UPDATE REMOVED AND REPLACED PROFILE FROM AFT CARTGO FR58 STR38-STR41 IA W A319 SRM 51-42-11-001 ACMP BY MECH V932196 INS
- [SDR CALA2025063006067](https://openairdocs.org/sdr/CALA2025063006067.md): Floor Support · corroded · Jun 27, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO LH PROFILE FR 25-28 CORRODED. REMOVED AND REPLACED PROFILE PANEL AT FWD CARGO FR25-28 LH IAW A 319 SRM 51-42-11-001.
- [SDR CALA2025063006062](https://openairdocs.org/sdr/CALA2025063006062.md): Seat Track · corroded · Jun 26, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y-765 SEAT TRACK FR 35-36 FOUND OUT OF LIMITS AND REQUIRES REPLA CEMENT. REMOVED AND REPLACED DISCREPANT Y-765 FR35-36 SEAT TRACK IAW A31 9 SRM 51-42-11-001.
- [SDR CALA2025063006056](https://openairdocs.org/sdr/CALA2025063006056.md): Seat Track · corroded · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y-765 SEAT TRACK FR 36-42 FOUND OUT OF LIMITS AND REQUIRES REPLA CEMENT. R & R CABIN SEAT TRACK Y-765 FR 36-42 IAW A319 SRM 51-42 -11/001.
- [SDR CALA2025062706000](https://openairdocs.org/sdr/CALA2025062706000.md): Skin · damaged · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > REMOVE DAMAGED DOUBLER, MAP OUT DAMAGE OF SKIN PANEL. REMOVED DAMAGED DOUBLER IAW SRM 51-42-11/001 FABRICATED NEW REPAIR DOUBLER AS DIRECTED BY RFTS 60004 PG2 A319 SRM 53-21-11- 300-093. INSTALLED REPAIR DOUBLER IAW A319 SRM 51-42-11/001.
- [SDR CALA2025062705999](https://openairdocs.org/sdr/CALA2025062705999.md): Panel · corroded · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > BULK CARGO FR 63-65 RSTR38 PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED PROFILE PNL IN BULK CARGO FR63-65 RSTR 63 I NSTALLED NEW IAW SRM 51-42-11/001.
- [SDR CALA2025062705998](https://openairdocs.org/sdr/CALA2025062705998.md): Panel · corroded · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 58-59 LSTR32 PROFILE PANEL HAS EVIDENCE OF CORROSIO N AND IS LOOSE. REMOVED DAMAGED (FOUND WITH EVIDENCE OF CORROSION AND LOOSE FIT) INSTALLED NEW PROFILE PANEL AT FR58-59 LSTR32 IAW SRM 51-42-11/ 001.
- [SDR CALA2025062705997](https://openairdocs.org/sdr/CALA2025062705997.md): Panel · corroded · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 56 LSTR38-RSTR41 PROFILE PANEL IS CORRODED AND LOOSE. REMOVED AND REPLACED PROFILE PNL AT FR56 LSTR38-RSTR41 IN AFT CA RGO IAW SRM 51-72-11-911-002 / SRM 51-42-11/001.
- [SDR CALA2025062705995](https://openairdocs.org/sdr/CALA2025062705995.md): Seat Track · corroded · Jun 25, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y-1292 SEAT TRACK FR 24-35 CORRODED OUT OF LIMITS. REMOVED AND REPLACED DISCREPANT SEAT TRACK AT Y-1292 FR24-35 IAW A319 SRM 51-42-11-001.
- [SDR CALA2025062605906](https://openairdocs.org/sdr/CALA2025062605906.md): Plate · corroded · Jun 23, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 47/51 - FR 52 RSTR 38 PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED R/H PROFILE PANEL AT FR47 TO 52 IAW A319 SR M 51-42-11 PG 5,6.
- [SDR CALA2025062605900](https://openairdocs.org/sdr/CALA2025062605900.md): Seat Track · corroded · Jun 23, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y1292 SEAT TRACK FR 47-64 FOUND OUT OF LIMITS OVER ENTIRE LENGTH AND REQUIRES REPLACEMENT. SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-42-11. REMOVED ADN REPLACED Y1292 SEAT TRACK AT MAIN CABIN BETWEEN FR47 -67 L/H IAW A319 SRM 51-42-11-001.
- [SDR CALA2025062605899](https://openairdocs.org/sdr/CALA2025062605899.md): Floor Support · corroded · Jun 23, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT RT BETWEEN FR52-56A AT STRINGER 38R HAS C ORROSION SPOTS ON FLOOR SUPPORT PROFILE UPPER SURFACE. FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-42-11.
- [SDR CALA2025062005735](https://openairdocs.org/sdr/CALA2025062005735.md): Seat Track · corroded · Jun 19, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > Y1292 SEAT TRACK FR 42-47 FOUND OUT OF LIMITS AND REQUIRES REPLA CEMENT. REMOVED AND REPLACED T1292 SEAT TRACK BETWEEN FR 42 AND FR 47 V936069 IAW SRM 51-42-11-001 RMVD AND RPLD Y1292 SEAT TRACK AT CABIN BETWEEN FR42 AND FR 47 IAW A319 SRM 51-42-11/001
- [SDR CALA2025061205497](https://openairdocs.org/sdr/CALA2025061205497.md): Seat Track · corroded · Jun 11, 2025 · N831UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN O/B SEAT TRACK BEAM Y-765 RT) HAS CORROSION SPOTS AT FR20 R/H A3NB-53-3-6038 ESFR CORRECTION FROM LOCATION RH TO LH ESFR ENTERED CORRECTION RH BETWEEN FR12 AND FR24 LBL 20 REMOVED AND REPLACED SEAT TRACK-BEAM Y-765 AT MAINN CABIN R/H BT W FR12-24 IA
- [SDR CALA2025061105463](https://openairdocs.org/sdr/CALA2025061105463.md): Angle · corroded · Jun 10, 2025 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO ENTRY DOORSILL TORSION BOX HAS CORROSION SPOTS ON UPPER SKIN A3NB-53-4-6332. INSTALLED ANGLE AT FR59 AFT CARGO IAW SRM 51-42-11/001 AND INSTA LLED NEW COVER SHEED FOR AFT CARGO LOWER ENTRY AREA IAW SRM 51-4 2-11/001.
- [SDR CALA2025031802915](https://openairdocs.org/sdr/CALA2025031802915.md): None · none · Mar 15, 2025 · N831UA · Airbus A319131 · Standard Practices/Structures
  > INSTALLED RH SLIDE SAFETY LOCKPIN IAW AMM TASK 25-62-00 REMOVED RH OFF-WING SLIDE SAFETY LOCK PIN IAW AMM TASK 25-62-00. C/W RII FOR THE REACTIVATION OF THE RT OVERWING SLIDE PER THE GMM
- [SDR CALA2025021902378](https://openairdocs.org/sdr/CALA2025021902378.md): Proximity Sensor · out of tolerance · Feb 16, 2025 · N831UA · Airbus A319131 · Door Warning System
  > FORWARD CARGO DOOR PROXIMITY SWITCH INSPECTION {A3NB-52-3-0008} - FWD CARGO DOOR J2 SENSOR CLEARANCE OUT OF TOLERANCE. ADJUSTED J2 SENSOR CLEARANCE. REF AMM 52-35-13-400-002-A. CLEARANCE WITHIN TOLERANCE.
- [SDR CALA2025021902372](https://openairdocs.org/sdr/CALA2025021902372.md): Battery · no test · Feb 16, 2025 · N831UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - BATTERY TEST UNSATISFIED. EPSU LOCATED AT FWD L AND AFT L NEED REPLACEMENT UPDATED PART INFO. BATTERY NIS IN SEA NEEDS A NEW BATTERY PACK FORWARD L / H SIDE. P / N: AD3214-31. S /
- [SDR CALA2024122603160](https://openairdocs.org/sdr/CALA2024122603160.md): Floor Support · damaged · Dec 9, 2024 · N831UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LAV DOOR WON''T OPEN OR CLOSE AT FWD CAB LT LAV A FOUND LAV DOOR BINDING AT LOWER AFT SIDE ON FLOOR WHEN SOMEONE IS SITTING IN FA JUMPSEAT AND AFT WALL APPEARS TO HAVE A SEPERATION BUT UNABLE TO CONFIRM DUE TO WALLPAPER. UPLOADED PICTURE OF AREA. LOCKED FOR MA
- [SDR CALA2024090600579](https://openairdocs.org/sdr/CALA2024090600579.md): Fuel Cap · missing · Sep 4, 2024 · N831UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELER REPORTS FUEL CAP MISSING FROM AIRCRAFT UPON ARRIVAL. PLACED ON CDL 28A. DISPATCH DESK: 13 NAME: JG DATE: 04-SEP-24- CDL 28A APPROVED. PLACED ON CDL 28A. FUEL CAP M&E 31-2825-9-0001 IPC 28-25-41-02B ITEM 001B. FUEL CAP M&E 31-2825-9-0001 IPC 28-

Next page: https://openairdocs.org/aircraft/N831UA/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 = 'N831UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N831UA/reports

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