# Service difficulty reports: N824UA

A list on [N824UA](https://openairdocs.org/aircraft/N824UA.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 · 128 reports

- [SDR CALA2026100920246](https://openairdocs.org/sdr/CALA2026100920246.md): Frame · cracked · Oct 8, 2026 · N824UA · Airbus A319131 · Fuselage Main, Frame
  > RIGHT FRAME 16 DOUBLE JOGGLE AREA HOLE 5, HAS A CRACK INDICATION IN CORNER DOUBLER LAYER AT 6 OCLOCK DIRECTION 100%. ACCOMPLISHED A REPAIR IAW REO L26059, REV IR, AND ECRA 5311-03084, REV A.
- [SDR CALA2026060916953](https://openairdocs.org/sdr/CALA2026060916953.md): Battery Pack · faulted · Jun 7, 2026 · N824UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMER R FAULT. REMOVED AND REPLACED EMRGENCY POWERSUPPLY BATTERY IAW AMM CH 33-51-38-400-002-A 33-51-38-000-002-A. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2025110911015](https://openairdocs.org/sdr/CALA2025110911015.md): Light · inoperative · Nov 8, 2025 · N824UA · Airbus A319131 · Emergency Lighting
  > 35ABC EMERGENCY BOTTOM LIGHT INOPERATIVE. FOUND EMERGENCY LIGHT DISCONNECTED RECONNECTED. OPS CK GOOD.
- [SDR CALA2025110310830](https://openairdocs.org/sdr/CALA2025110310830.md): Power Supply · inoperative · Nov 1, 2025 · N824UA · Airbus A319131 · Emergency Lighting
  > EPSU UNIT FWD L FAULT AFTER BITE TEST. T/S IAW TSM 33-51-00-810-801-A, PERFORMED BITE TEST OF EMERGENCY LIGHT SYS & CONFIRMED EPSU UNIT FWD LT, FAULT WAS PRESENT. PERFORMED OPS TEST OF THE EEL & ALL LIGHTS WERE OPERATIONAL. REPLACED LT FWD EPSU 10WL. PERFORM
- [SDR CALA2025100209525](https://openairdocs.org/sdr/CALA2025100209525.md): Light · malfunctioned · Oct 2, 2025 · N824UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT SIGNS ILLUMINATED. PERFORMED AN EMERGENCY LIGHT TEST IAW AMM 33-51-00, OPS CHECK GOOD IAW SDM 33-51-00/001, CONFIG 00. THE EMERGENCY LIGHTS COME ON AUTOMATICALLY WHEN NO SMOKING SWITCH 190RH IS IN THE ON POSITION. THEY ALSO COME ON, WHEN NO S
- [SDR CALA2025092909391](https://openairdocs.org/sdr/CALA2025092909391.md): Idg · faulty · Sep 25, 2025 · N824UA · Airbus A319131 · AC Generator-Alternator
  > ELEC IDG 1 LO OIL PR AT50 KNOTS. COMPLIED WITH MEL 2420E, PRIOR TO CLEARING THIS MEL AND RESTORING THE INOP IDG TO SERVICE PYLON MOUNTED IDG CONNECTORS MUST BE VISUALL INSPECTED FOR ARCING CONDITIONS REF AMM 24-21-43-210-048C1 AND AD 2011-19-01-R1. NO HISTO
- [SDR CALA2025073107148](https://openairdocs.org/sdr/CALA2025073107148.md): Seal · unsecure · Jul 28, 2025 · N824UA · Airbus A319131 · Passenger/Crew Doors
  > CLIMBING THRU FL200, LOUD RUMBLING WITH STRONG VIBRATION IN COCKPIT FLOOR. PRESSURIZED ACFT IAW AMM 05-53-00-780-003-A, CHECKED L1 DOOR, NO LEAKS NOTED. UPON ARRIVAL AT LCQ FOUND L1 DOOR SEAL LOOSE FROM RETAINER, REMOVED SEAL AND REINSTALLED L1 DOOR SEAL
- [SDR CALA2025072806980](https://openairdocs.org/sdr/CALA2025072806980.md): Plate · cracked · Jul 26, 2025 · N824UA · Airbus A319131 · Passenger/Crew Doors
  > L1 DOOR, UPPER AREA HAS CRACK AFT CORNER OF COVER PLATE. REMOVED/REPLACED L1 DOOR COVER PLATE IAW SRM 51-72-11-911-0 01.
- [SDR CALA2025062305793](https://openairdocs.org/sdr/CALA2025062305793.md): Apu · faulted · Jun 19, 2025 · N824UA · Airbus A319131 · APU Oil System
  > DUE TO REPEAT DISCREPENCY FOR DIRTY SOCK SMELL IN CABIN, THIS REQUIRES FURTHER TROUBLESHOOTING. REF L/P 5247674 AND 5245675 FOR PREVIOUS WORK PERFORMED. REMOVED APU BLEED DUCT AND PERFORMED VISUAL INSPECTION OF ANY FOD OR DEBRIS. FOUND BLEED DUCT TO BE SERVICE
- [SDR CALA2025061805655](https://openairdocs.org/sdr/CALA2025061805655.md): Unknown · odor · Jun 17, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > ODOR IN FLT DECK ON DEPARTURE. STARTED AT GEAR RETRACTION, ENDED PASSING THRU 10000.
- [SDR CALA2025052204900](https://openairdocs.org/sdr/CALA2025052204900.md): Unknown · odor · May 20, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > AC MUSTY SMELL BELOW10K FEET. ATTEMPTED TO ACCOMPLISH TASK 21-00-00-615-802-A AT THE REQUEST OF UAL MANAGEMENT AND TOMC, REQUIRED ENGINE PRESSURE AND TEMPERATURE IN STEP 4B4A ARE UNATTAINABLE AT IDLE THRUST SETTING ON THE GATE. ACCOMPLISHED MAINT TASK AMM 21-0
- [SDR CALA2025050104378](https://openairdocs.org/sdr/CALA2025050104378.md): Oil System · leaking · Apr 28, 2025 · N824UA · Airbus A319131 · Turbine Engine Oil System
  > WITHIN 3 CYCLES, DUE TO REPEAT OILY SMELL IN COCKPIT ON DESCENT (ONLY, NO ODORS IN CABIN), COMPLETE TROUBLE SHOOTING PER THE TSM 71-00-00-810-801-A. NOTE DUE TO REPORT OF COCKPIT ODOR ONLY START WITH THE LT ENGINE AND PACK FIRST.DOCUMENT ALL FINDINGS.CARRIE
- [SDR CALA2025043004346](https://openairdocs.org/sdr/CALA2025043004346.md): Unknown · odor · Apr 27, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > CREW REPORTED STRONG DIRTY SOCK SMELL IN FLIGHT DECK ONLY ON DESCENT. OCCURRED AT 8,000' LASTED ABOUT THREE MINUTES. CABIN CREW REPORTED NO FUMES OR DIRTY SOCK SMELL. NOTICED ODOR WHEN INCREASING POWER FROM IDLE, ONLY IN-FLIGHT DECK. PERFORMED INSPECTION RE
- [SDR CALA2025042104040](https://openairdocs.org/sdr/CALA2025042104040.md): Unknown · odor · Apr 20, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > PACS MAKING A WET SOCK SMELL INBOUND CAPT STATED MUSTY SMELL WAS IN FLT USING ENG BLEEDS, APU WAS OFF, AND HE DID NOT NOTICE ANY ODOR BEFORE DEPARTURE USING APU BLEED, THE INBOUND CABIN CREW IN FRONT AND REAR OF CABIN ALL SAID NO ODORS WERE NOTICED BY THEM OR
- [SDR CALA2025042104035](https://openairdocs.org/sdr/CALA2025042104035.md): A/C Pack · odor · Apr 16, 2025 · N824UA · Airbus A319131 · Cabin Cooling System
  > MUSTY SMELL COMING FROM PACKS PERF. AIR CABIN RECIRCULATION TEST. RUNN PACK FOR 20MIN. & COULDNT DUPLICATED MUSTY SMELL FROM PACKS.. OK FOR SVC.
- [SDR CALA2025031402841](https://openairdocs.org/sdr/CALA2025031402841.md): Slide · overpressured · Mar 14, 2025 · N824UA · Airbus A319131 · Escape Slide
  > CABIN DOOR 1L SLIDEPRESSURE INDICATOR ISIN THE RED INSPECTED DOOR SLIDE PRESSURE AT DOOR 1L REF AMM 25-62-00, DOOR SLIDE PRESSURE WITHIN GREEN BAND CLOSER TO OVER PRESSURE PORTION. DOOR SLIDE PRESSURE WITHIN LIMITS. A/C OK FOR SERVICE.
- [SDR CALA2025022602474](https://openairdocs.org/sdr/CALA2025022602474.md): Filter · odor · Feb 24, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > AIR CONDITIONING DIRTY SOCK SMELL BELOW 13000 ON DEPARTURE AND A RRIVAL NEED TO DF PACK 1 APPROVED FOR MEL 3152W CREW DID SAY THE SMELL WAS FROM PACK 1 COMPLYED WITH MEL 2152W. DUE TO PREVIOUS HISTORY NEED POSITIVE FIX, NOT JUST AN OPS CHECK *DM* UPDATED M/L
- [SDR CALA2025022502466](https://openairdocs.org/sdr/CALA2025022502466.md): None · none · Feb 22, 2025 · N824UA · Airbus A319131 · Standard Practices/Structures
  > INSTALLED EMERGENCY RELEASE MECHANISM LOCKOUT PIN ON RH OVER WING EXIT HATCH REF AMM 52-21-11-000-001-A REMOVED EMERGENCY RELEASE MECHANISM LOCKOUT PIN ON RH OVERWING EXIT HATCH MX COMPLETE REF MM 52-21-11 VERIFIED REMOVAL OF EMERGENCY RELEASE MECHANISM LOCKOU
- [SDR CALA2025020502213](https://openairdocs.org/sdr/CALA2025020502213.md): Door · broken · Feb 2, 2025 · N824UA · Airbus A319131 · Landing Gear Doors
  > REPLACED LH MLG DOOR. LP CLOSED.LOWER SECTION OF CENTRAL RAMP BROKEN AND DETACHED FROM L MLG DOOR. PUNCTURED ALL THE WAY THROUGH AND IS STICKING OUT 6 INCHES SEE IPC REF 52-81-14-10A ITEM 90 AND PICTURES ATTACHED SEE MORE PICS ATTACHED REMOVED LH MLG DOOR IAW
- [SDR CALA2025010601817](https://openairdocs.org/sdr/CALA2025010601817.md): A/C Pack · odor · Jan 3, 2025 · N824UA · Airbus A319131 · Cabin Cooling System
  > STRONG PUNGENT ODOR COMING FROM PAC1 PER CREW WHILE RUNNGINNG PACKS ON ENGINE BLEED OR APU BLEED SMELL REMAINS ONLY WITH PACK 1 ON. SMELL IS THROUGHOUT AIRCRAFT FROM RECIRCULATING SYSTEM. PACK 1 MEL REOPENED PER LOGPAGE 3404109
- [SDR CALA2025010601794](https://openairdocs.org/sdr/CALA2025010601794.md): Filter · odor · Jan 3, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > NOTE CREW REPORTS PUNGENT (OIL) TYPE SMELL IN COCKPIT FROM LEFT PACK. REPEAT LPS,34041111, 3404109, 3373516. MX REPORTS SMELL IS PRESENT WITH EITHER APU OR ENGINE PROVIDING BLEED AIR. ENG 1 OIL CONSUMPTION IS 0.06 WELL WITH IN LIMITS. TS SMELL. COMPLY WITH
- [SDR CALA2025010301768](https://openairdocs.org/sdr/CALA2025010301768.md): Unknown · odor · Jan 2, 2025 · N824UA · Airbus A319131 · Air Distribution System
  > BAD SMELL IS EMANATING FROM PACK 1. NO SMELL WITH PAC 2 OPERATIONAL, AEVC OPS NORMAL ALL OTHER REQUIREMENTS VERIFIED OK FOR FLIGHT. REQUIRES FURTHER T/S. PREFORMED INSPECTION OF APU, AND RAN PACK #1 ON BOTH APU AND ENGINES TO TRY AND FIND THE SMELL, COULD N
- [SDR CALA2024111201112](https://openairdocs.org/sdr/CALA2024111201112.md): Fuel Cap · missing · Nov 9, 2024 · N824UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP REPORTED MISSING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSP FUEL COUPLING FOR LEAKS AND CONTACT TOMC TO APPLY CDL 28A, DD 34 KU ADVISED MAC METER INITIATED. CONFIRMED NO LEAKS FROM COUPLIN
- [SDR CALA2024031800773](https://openairdocs.org/sdr/CALA2024031800773.md): Proximity Sensor · faulty · Mar 16, 2024 · N824UA · Airbus A319131 · Landing Gear Position and Warning
  > L/G SYS DISAGREE ECAM ON LANDING REMOVED SENSOR 23GA, LEFT MAIN GEAR EXTENDED SENSOR REF AMM 32-31-73-000-001-A INSTALLED NEW LEFT MAIN GEAR EXTENDED AENSOR 23GA REF AMM 32-31-73-400-001-A, STEPS 1 UP TO AND INCLUDING 4F. PARTS USED: 31-3231-3-0007,QTY:1 20-3
- [SDR CALA2023101603079](https://openairdocs.org/sdr/CALA2023101603079.md): Skin · dented · Oct 6, 2023 · N824UA · Airbus A319131 · Rudder, Plate/Skin
  > (SUPPORT TASK) RUDDER RH LOWER SIDE HAS A DENT. W/C:69985 REPAIRED RH LOWER SIDE IAW SRM 55-41-13-300-024 PARA 2 STEP 2. W /C:69985 STA:STENGBFM INSPECTIONS ACCOMPLISHED ON ST ENGINEERING NRC#69985 AT STA:STENGBFM
- [SDR CALA2023100602962](https://openairdocs.org/sdr/CALA2023100602962.md): Fitting · cracked · Oct 3, 2023 · N824UA · Airbus A319131 · Fuselage Main, Structure
  > (AD2020-17-03) DURING HFEC SURFACE INSPECTION, CRACK WAS FOUND AT RH CONTINUITY FITTING WITH A CRACK LENGTH OF 0.165". END MARKED IN RED. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT. W/C:69929 ACCOMPLISHED REPAIR IAW UAL EC/RA 5311-03076 REV
- [SDR CALA2023091102757](https://openairdocs.org/sdr/CALA2023091102757.md): Panel · damaged · Sep 10, 2023 · N824UA · Airbus A319131 · Rudder, Plate/Skin
  > DURING THERMOGRAPHIC INSPECTION OF THE L/H RUDDER SIDE PANEL, NDT NOTES WATER INGRESS AT THE 12TH FASTENER FROM TOP AT 6.75" FROM THE TRAILING EDGE. INDICATION MEASURES AT 3.5" X 3.0". () LH RUDDER SIDE PNL REPAIRS COMPLETED AS REQUIRED SRM 55-41-13-30 0-025 C
- [SDR CALA2023091102755](https://openairdocs.org/sdr/CALA2023091102755.md): Panel · damaged · Sep 10, 2023 · N824UA · Airbus A319131 · Rudder, Plate/Skin
  > DURINGTHERMOGRAPIC INSPECTION OF THE L/H RUDDER SIDE PANEL, NDT NOTES WATER INGRESS AT THE 11TH FASTENER FROM THE TOP AT 6.25" F ROM THE TRAILING EDGE. INDICATION MEASURES AT 4.75 X 3.25" () LH RUDDER SIDE PNL REPAIRS COMPLETED AS REQUIRED- SMR 55-41-13-3 00-0
- [SDR CALA2023091102756](https://openairdocs.org/sdr/CALA2023091102756.md): Panel · damaged · Sep 10, 2023 · N824UA · Airbus A319131 · Rudder, Plate/Skin
  > DURING THERMOGRAPHIC IINSPECTION OF THE L/H RUDDER SIDE PANELS, NDT NOTES WATER INGRESS AT THE 4TH FASTENER FROM TOP AT 6.5"FROM THE TRAILING EDGE. INDICATION MEASURES AT 4.0" X 3.25". () LH RUDDER SIDE PNL''S REPAIRED AS REQUIRED IAW SRM''S 55-41-13-300 -025/
- [SDR CALA2023091102750](https://openairdocs.org/sdr/CALA2023091102750.md): Skin · unknown · Sep 8, 2023 · N824UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHY INSPECTION OF THE R/H ELEVATOR, NDT NOTED INDICATION OF A POTENTIAL REPAIR OF THE TOP PANEL LOCATED APPROXIMATELY 63.5" FROM THE I/B EDGE AND 10.75" FROM THE AFT ED GE. AREA OF CONCERN IS LABELED AS INDICATION "7". W/C:69750 REPAIRED R/H EL
- [SDR CALA2023090802734](https://openairdocs.org/sdr/CALA2023090802734.md): Fitting · corroded · Sep 7, 2023 · N824UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6185) RH AFT DOOR SILL CENTER FITTING CORRODED. DOT #110-64. W/C:69698 REPLACED AFT DOOR CENTER FITTING IAW SRM 51-72-911-001. W/C:6969 8 EMP:V934614 STA:STENGBFM
- [SDR CALA2023091402784](https://openairdocs.org/sdr/CALA2023091402784.md): Skin · damaged · Sep 6, 2023 · N824UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHY INSPECTION OF THE R/H ELEVATOR, NDT NOTED INDICATION OF A POTENTIAL REPAIR OF THE TOP PANEL LOCATED APPROXIMATELY 99" FROM THE I/B EDGE AND 137.75" FROM THE AFT EDGE. AREA OF CONCERN IS LABELED AS INDICATION "11". W/C:697 54 REPAIRED DAMAGE
- [SDR CALA2023090802744](https://openairdocs.org/sdr/CALA2023090802744.md): Panel · unknown · Sep 6, 2023 · N824UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHY INSPECTION OF THE R/H ELEVATOR, NDT NOTED INDICATION OF A POTENTIAL REPAIR OF THE TOP PANEL LOCATED APPROXIMATELY 63.5" FROM THE I/B EDGE AND 10.75" FROM THE AFT ED GE. AREA OF CONCERN IS LABELED AS INDICATION "7". W/C:69750 REPAIRED R/H EL
- [SDR CALA2023090802743](https://openairdocs.org/sdr/CALA2023090802743.md): Skin · damaged · Sep 6, 2023 · N824UA · Airbus A319131 · Elevator, Plate/Skin
  > DURING THERMOGRAPHY INSPECTION OF THE R/H ELEVATOR, NDT NOTED INDICATION OF A POTENTIAL REPAIR OF THE TOP PANEL LOCATED APPROXIMATELY 99" FROM THE I/B EDGE AND 137.75" FROM THE AFT EDGE. AREA OF CONCERN IS LABELED AS INDICATION "11". W/C:697 54 REPAIRED DAMAGE
- [SDR CALA2023092002821](https://openairdocs.org/sdr/CALA2023092002821.md): Door Sill · corroded · Sep 3, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) RH AFT DOOR SILL CORRODED AROUND FWD GIRTBAR FITTING DOT#110-62. W/C:69696 REPLACED AFT DOOR SILL RH IAW SRM 51-72-911-001. W/C:69696 EMP:V934614 STA:STENGBFM
- [SDR CALA2023090802740](https://openairdocs.org/sdr/CALA2023090802740.md): Door Sill · corroded · Sep 3, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) RH AFT DOOR SILL CORRODED AROUND FWD GIRTBAR FITTING DOT#110-62. W/C:69696 REPLACED AFT DOOR SILL RH IAW SRM 51-72-911-001. W/C:69696 EMP:V934614 STA:STENGBFM
- [SDR CALA2023083002672](https://openairdocs.org/sdr/CALA2023083002672.md): Door Sill · damaged · Aug 29, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) RH SIDE FR67, FORMER HAS DAMAGE, DISCOVERED UPON REMOVAL OF DOOR SILL (R&R) W/C:69903 REMOVED AND REPLACED FORMER AT RH SIDE FR 67 IAW SRM 51-42-11. W/C:69903 EMP:V935975 STA:STENGBFM
- [SDR CALA2023082502630](https://openairdocs.org/sdr/CALA2023082502630.md): Floorbeam · corroded · Aug 23, 2023 · N824UA · Airbus A319131 · Fuselage Main, Floor Beam
  > SUPPORT TASK: CABIN FWD WET AREA FLOOR BEAM Y1732 FRAME 20 STR 23 LH UPPER SURFACE HAS CORROSION. W/C:69841 NO ESTABLISHED LIMITS IN SRM FOUND TO BE OUT OF LIMITS, REMOVED WEB IAW SRM 51-42-11, RECEIVED NEW WEB P/N 531278520200 BATCH 0001904070, INSTALLED NEW
- [SDR CALA2023082102589](https://openairdocs.org/sdr/CALA2023082102589.md): Skin · dented · Aug 19, 2023 · N824UA · Airbus A319131 · Trailing Edge Flaps
  > SUPPORT TASK- R/H WING I/B FLAP I/B LOWER SURFACE DENTS DOT 49-0 19. W/C:69171 REPAIRED R/H WING I/B FLAP I/B LOWER SURFACE IAW SRM 57-52-00-30 0-095 FIG 1. W/C:69171
- [SDR CALA2023081602538](https://openairdocs.org/sdr/CALA2023081602538.md): Flap · dented · Aug 13, 2023 · N824UA · Airbus A319131 · Trailing Edge Flaps
  > SUPPORT TASK- R/H WING I/B FLAP I/B LOWER SURFACE DENTS DOT 49-0 19. W/C:69171 REPAIRED R/H WING I/B FLAP I/B LOWER SURFACE IAW SRM 57-52-00-30 0-095 FIG 1. W/C:69171
- [SDR CALA2023081102487](https://openairdocs.org/sdr/CALA2023081102487.md): Floor Support · corroded · Aug 10, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6321) FLOOR SUPPORT AT Y 1292 CORODDED AT FR 16. DOT# 110-86. W/C:69736 BLENDED AREA FLOOR SUPPORT Y1292 FR 16 IAW SRM 53-11-14-283-007, Y1292 IAW SRM 51-42-11. W/C:69736 EMP:V936636 STA:STENGBFM FOUND TO BE OUT OF LIMITS MAX 0,003,:/ 0,049" (T91554
- [SDR CALA2023081102485](https://openairdocs.org/sdr/CALA2023081102485.md): Floorbeam · corroded · Aug 10, 2023 · N824UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-05-3-6059 FR 66 FLOOR BEAM CENTER AREA HAS SURFACE CORROSION. W/C:69494 EVALUATED FLOOR BEAM AND FOUND OUT OF LIMITS IAW A319 SRM 53-41- DAMAGED BEAM IAW A319 SRM 51-42-11 AND INSTALLED NEW FLOOR BEAM 14-283-009 AND FABRICATED NEW FLOOR BEAM OF MATERIAL P
- [SDR CALA2023081102484](https://openairdocs.org/sdr/CALA2023081102484.md): Seat Track · corroded · Aug 10, 2023 · N824UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6321) SEAT TRACK AT -Y1292 CORRODED AT FR20 DOT #110-81. W/C:69730 REMOVED AND REPALCED SEAT TRACK -Y1292 AT FR 12 TO FR 24 IAW SRM 51-42-11. W/C:69730 EMP:V935975 STA:STENGBFM
- [SDR CALA2023081102476](https://openairdocs.org/sdr/CALA2023081102476.md): Floor Support · corroded · Aug 9, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6321) FLOOR SUPPORT AT Y 765 CORRODED AT FR16. DOT #110-85. W/C:69735 REMOVED CORROSION FLOOR SUPPORT Y765 FOUND OUT OF LIMITS IAW SRM IAW SRM 51-42-11. W/C:69735 STA:STENGBFM 53-11-14-283-001 L=1.8 W=1,2 D= 0,070" (T14717) REMOVED FLOOR S UPPORT Y7
- [SDR CALA2023081102474](https://openairdocs.org/sdr/CALA2023081102474.md): Dummy Rail · corroded · Aug 9, 2023 · N824UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6321) O/B DUMMY RAIL, -Y81, FR12-FR16, CORRODED AT MU TIPLE LOCATIONS DOT#110-83. W/C:69732 REMOVED AND REPLACED DUMMY RAIL FR 12-FR16 IAW SRM 51-42-11/001. W/C:69732
- [SDR CALA2023080902457](https://openairdocs.org/sdr/CALA2023080902457.md): Floor Support · corroded · Aug 8, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) FLOOR SUPPORT AT -Y465 CORRODED AT FR66. DOT#11 0-53. W/C:69689 REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11 P/N: D5347228400800 BTCH:0002723888. W/C:69689 EMP:V934700 STA:STENGB FM
- [SDR CALA2023080702435](https://openairdocs.org/sdr/CALA2023080702435.md): Floor Support · corroded · Aug 4, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) FLOOR SUPPORT AT Y512 CORRODED AT FR66. DOT# 110-56. W/C:69692 REMOVED AND REPLACED FLOOR SUPPORT AT Y512 FR 66 IAW SRM 51-42-1 1-001. W/C:69692 EMP:V934619 STA:STENGBFM
- [SDR CALA2023080702434](https://openairdocs.org/sdr/CALA2023080702434.md): Floor Support · corroded · Aug 4, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) FLOOR SUPPORT AT Y765 CORRODED AT FR68. DOT #110-59. W/C:69693 FLOOR SUPPORT CORRODED REMOVED AND INSTALLED NEW FLOOR SUPPORT P/N D5347219220000 IAW SRM 51-42-11. W/C:69693 EMP:V936191 STA:STENGBFM
- [SDR CALA2023080402425](https://openairdocs.org/sdr/CALA2023080402425.md): Floor Support · corroded · Aug 3, 2023 · N824UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) FLOOR SUPPORT AT Y512 CORRODED AT FR66. DOT# 110-56. W/C:69692 REMOVED AND REPLACED FLOOR SUPPORT AT Y512 FR 66 IAW SRM 51-42-1 1-001. W/C:69692.
- [SDR CALA2023080402424](https://openairdocs.org/sdr/CALA2023080402424.md): Floor Support · corroded · Aug 3, 2023 · N824UA · Airbus A319131 · Fuselage Main, Bulkhead
  > (A3NB-53-3-6185) FLOOR SUPPORT AT Y765 CORRODED AT FR68. DOT #110-59. W/C:69693 FLOOR SUPPORT CORRODED REMOVED AND INSTALLED NEW FLOOR SUPPORT P/N D5347219220000 IAW SRM 51-42-11. W/C:69693

Next page: https://openairdocs.org/aircraft/N824UA/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 = 'N824UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N824UA/reports

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