# Service difficulty reports: N829UA

A list on [N829UA](https://openairdocs.org/aircraft/N829UA.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 · 154 reports

- [SDR CALA2026041615417](https://openairdocs.org/sdr/CALA2026041615417.md): Wire · broken · Apr 14, 2026 · N829UA · Airbus A319131 · Landing Gear System Wiring
  > BRAKES AUTO BRK FAULT DISPLAYED DURING CLIMB. ASSOCIATED CFDS MESSAGE TACHOMETER4(22GG)/ BSCU(10GG). LOCKING LOG PAGE. MAINTENANCE TECHNICIAN TO DISCUSS FINDINGS WITH MAINTENANCE CONTROLLER BEFORE CLEARING THIS ITEM. TACHOMETER FAULT IS NON DEFERRABLE. PERFORM
- [SDR CALA2025092409197](https://openairdocs.org/sdr/CALA2025092409197.md): Battery · no test · Sep 22, 2025 · N829UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY FWD L MESSAGE SHOWN AFTER EMERGENCY LIGHTS TEST REMOVED AND REPLACED EPSU BATTERY PER AMM 33-51-38. OPS CHECK GOOD
- [SDR CALA2025072506908](https://openairdocs.org/sdr/CALA2025072506908.md): Light · loose · Jul 25, 2025 · N829UA · Airbus A319131 · Emergency Lighting
  > TEST SHOW EPSU INT LOAD AFT L MSG ---PROCEDURE - PERFORMED VISUAL CHECK OF THE CABIN EMERGENCY-LIGHT SYSTEM REF AMM 33-51-00-710-009-A. FOUND L2 AND R2 OVER DOOR LIGHTS INTERMITTENT. LIGHT IS NORMALLY OFF BUT ILLUMINATES AND STAYS ON AFTER LIGHT PRESSURE IS A
- [SDR CALA2025072506907](https://openairdocs.org/sdr/CALA2025072506907.md): Light · loose · Jul 25, 2025 · N829UA · Airbus A319131 · Emergency Lighting
  > TEST SHOWS EPSU INT LOAD EMER R MSG---PROCEDURE - PERFORMED VISUAL CHECK OF THE CABIN EMERGENCY-LIGHT SYSTEM REF AMM 33-51-00-710-009-A. FOUND OVERWING EXIT-FWD AISLE LIGHT INTERMITTENT. LIGHT IS NORMALLY OFF BUT ILLUMINATES AND STAYS ON AFTER LIGHT PRESSURE
- [SDR CALA2025012900231](https://openairdocs.org/sdr/CALA2025012900231.md): Frame · cracked · Jan 28, 2025 · N829UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED TASK AD 2016-14-03 FR35 STGR 28-30 REPAIR BEFORE FURT HER FLIGHT LEFT FR 35 BOTTOM CORNER HOLE HAS A CRACK INDICATION IN THE FRAME LAYER AT 8 O''CLOCK AND 2 O''CLCOK POSITION 100%+ SCR EEN GEN BY V062335 ON HAECO LCQ NR 9297014/21014 REAMED HOLE AT
- [SDR CALA2025012400193](https://openairdocs.org/sdr/CALA2025012400193.md): Plate · worn · Jan 21, 2025 · N829UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > RH PYLON HYDRAULIC BULKHEAD PLATE IS WORN PER HAECO LCQ N/R 9296854/20854.
- [SDR CALA2025012100163](https://openairdocs.org/sdr/CALA2025012100163.md): Plate · corroded · Jan 20, 2025 · N829UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > LH PYLON SPIGOT FITTING CORRODED ON INNER BEARING SURFACE. REMOVED AND REPLACED LH PYLON SPIGOT FITTING PLATE IAW A319 SRM 54-51-12-300-002.
- [SDR CALA2025011400114](https://openairdocs.org/sdr/CALA2025011400114.md): Window Frame · cracked · Jan 13, 2025 · N829UA · Airbus A319131 · Fuselage Main, Structure
  > L/H WINDSHIELD FRAME I/B HOLE HAS A CRACK INDICATION 100% SCREEN HEIGHT PER HAECO LCQ N/R 9296891/20891 GEN BY V061632
- [SDR CALA2025011300111](https://openairdocs.org/sdr/CALA2025011300111.md): Skin · cracked · Jan 7, 2025 · N829UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FR 35 STR 30 RH HOLE #2 HAS CRACK INDICATION APPEARS TO BE IN AFT SKIN LAYER AT 60%SH. PERFORMED REPAIR OF HOLE #2 AT FR 35 STR 30 R IAW ECRA 5330-0737 THERE IS NO TERMINATING ACTION FOR THESE REPETITIVE INSPECTION R 1/ HAECO REO L25265 REV IR PART1 THE REPA
- [SDR CALA2025011400113](https://openairdocs.org/sdr/CALA2025011400113.md): Frame · cracked · Jan 6, 2025 · N829UA · Airbus A319131 · Fuselage Main, Frame
  > LH DOUBLE JOGGLE FR 16 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER. REPAIRED FR16 L/H DOUBLE JOGGLE HOLE #6 FRAME LAYER BY REAMING TO REMOVE CRACK IAW A319 SRM 53-11-12-300-012 PER ECRA 5311- 03320.
- [SDR CALA2025010700051](https://openairdocs.org/sdr/CALA2025010700051.md): Beam · damaged · Jan 6, 2025 · N829UA · Airbus A319131 · Fuselage Main, Structure
  > FWD CARGO FWD WALL VERTICAL MEMBER ASSYS UPPER ATTACH FITTINGS HAVE ELONGATED HOLES (3) EA. REMOVED & REPLACED 3EA VERTICAL MEMBERS AT FR24 FWD BULKHEAD IN FWD PIT IAW A319 AMM 25-54-81-400-801-A,
- [SDR CALA2025010700050](https://openairdocs.org/sdr/CALA2025010700050.md): Door Frame · gouged · Jan 6, 2025 · N829UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT FWD LIP HAS GOUGE AND BENT APROX 6 INCHES ABOVE LOWER FWD CORNER. REMOVED & REPLACED AFT CARGO DOOR CUTOUT FWD LIP IAW A319 SRM 53 -41-49-283-002. RESTORED SURFACE PROTECTION IAW A319 SRM 51-21-1 1.
- [SDR CALA2025010200011](https://openairdocs.org/sdr/CALA2025010200011.md): Window Frame · cracked · Dec 20, 2024 · N829UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK OF 0.218" APPROX OF LENGTH ON LH HORIZONTAL UPPER STIFFENER AT COCKPIT WINDOW FR 4.
- [SDR CALA2025011500121](https://openairdocs.org/sdr/CALA2025011500121.md): Doubler · corroded · Dec 18, 2024 · N829UA · Airbus A319131 · Trailing Edge Flaps
  > LH WING O/B FLAP INTERNAL DOUBLER AT RIB 5 HAS CORROSION AROUND 2 FASTENERS. R & R LT WING O/B FLAP IAW A319 AMM 27-54-62-400-001-A 27-54-62-000-001-A RIG AND OPS GOOD.
- [SDR CALA2025011300094](https://openairdocs.org/sdr/CALA2025011300094.md): Doubler · corroded · Dec 18, 2024 · N829UA · Airbus A319131 · Trailing Edge Flaps
  > RH WING I/B FLAP INTERNAL DOUBLER AT L/E RIBS 9 AND 10 HAS CORROSION AROUND FEW FASTENERS. REMOVED AND REPLACED RW IB FLAP IAW A319 AMM 27-54-01-000-001-A, 27-54-61-400-001-A. OPS CHECK GOOD.
- [SDR CALA2025011300095](https://openairdocs.org/sdr/CALA2025011300095.md): Doubler · corroded · Dec 18, 2024 · N829UA · Airbus A319131 · Trailing Edge Flaps
  > RH WING O/B FLAP INTERNAL DOUBLER AT RIBS 5 AND 6 HAS CORROSION AROUND SEVERAL FASTENERS PER HAECO LCQ N/R 9296639/20639. REMOVED AND REPLACED R/W O/B FLAP IAW AMM 319 27-54-62-000-001-A AND 27-54-62-400-001-A(RIG LOPS CHECK GOOD).
- [SDR CALA2025010200009](https://openairdocs.org/sdr/CALA2025010200009.md): Door Sill · corroded · Dec 18, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO ENTRY TOP SILL BOX HAS CORROSION AROUND MULTIPLE FASTENERS HEADS. FWD CARGO ENTRY TOP SILL BOX WAS FOUND TO BE OUT OF LIMITS. REPL ACED FWD CARGO ENTRY TOP SILL BOX IAW A319 SRM 51-42-11. TOP COA TED FASTENERS IAW A319 SRM 51-23-11.
- [SDR CALA2024121603077](https://openairdocs.org/sdr/CALA2024121603077.md): Threshold · corroded · Dec 13, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP CORROSION AT AFT CARGO DOOR THRESHOLD MT LOCATION S BETWEEN 55 + FR 59. RMVD CORROSION AND EVALUATED THRESHOLD FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-49-283-004 RMVD AND RPLD THRESHOLD IN AFT CAR GO DOOR BETWEEN FR55-59 IAW A319 51-42-11.
- [SDR CALA2024121803117](https://openairdocs.org/sdr/CALA2024121803117.md): Frame · cracked · Dec 9, 2024 · N829UA · Airbus A319131 · Fuselage Main, Frame
  > RH DOUBLE JOGGLE FR16 HOLE #6 HAS CRACK INDICATION IN FRAME LAYER. PERFORMED BUSHING REPAIR AT FR16 HOLE. PERFORMED BUSHING REPAIR AT FR16 HOLE #6 IAW SRM 53-11-12-300-012. REPAIR REQUIRES INITIAL INSPECTION #6 IAW SRM 53-11-12-300-012. REPAIR REQUIRES INITIA
- [SDR CALA2024120303008](https://openairdocs.org/sdr/CALA2024120303008.md): Floor Support · corroded · Dec 2, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > ON TOP OF FLOOR SUPPORT +Y765 BETWEEN FR67 AND FR68 HAS CORROSION AROUND 2 FASTENER HOLES. RMVD AND RPLD FLOOR SUPPORT AT +Y765 LH BETWEEN FR67 AND FR68 IAW A319 SRM 51-72-11-911-001 REPLACEMENT OF STRUCTURAL COMPONENTS
- [SDR CALA2024120202999](https://openairdocs.org/sdr/CALA2024120202999.md): Door Frame · cracked · Nov 27, 2024 · N829UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 16 LH DOOR STOP 7 HOLE 3 HAS CRACK INDICATION IN INTER COSTAL LAYER O''CLOCK DIRECTION 80% S.H. PER HAECO LCQ N/R 9296726/20726 RMVD AND RPLD INTERCOSTAL AT L/H FR16 DOOR STOP 7 IAW A319 SRM 53-11-12 AND 51-72-11.
- [SDR CALA2024120202988](https://openairdocs.org/sdr/CALA2024120202988.md): Channel · corroded · Nov 27, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > EVIDENCE OF CORROSION ON AFT CARGO COMPARTMENT CONNECTING PLATE BETWEEN DOOR THRESHOLD AND TORSION BOX COVER. REWORKED CORROSION ON AFT CARGO CONNECTING PLATE BTWN DOOR THRES HOLD AND TORSION BOX AND WAS FOUND TO BE OUT OF LIMITS RMVD AND RPLD CONNECTING PLAT
- [SDR CALA2024112902981](https://openairdocs.org/sdr/CALA2024112902981.md): Floor Support · corroded · Nov 27, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN RT SIDE Y-765 CORRODED AT FR68 PER HAECO LCQ N/R 9296821/20821
- [SDR CALA2024112902980](https://openairdocs.org/sdr/CALA2024112902980.md): Seat Track · corroded · Nov 27, 2024 · N829UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN RT SIDE I/B SEAT TRACK CORRODED AT FR20 Y-1292 PER HAECO LCQ N/R 9296814/20814 GEN BY V061642
- [SDR CALA2024112702965](https://openairdocs.org/sdr/CALA2024112702965.md): Beam · corroded · Nov 25, 2024 · N829UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CABIN RT SIDE TRIPLE BEAM CORRODED AT FR68 RMVD AND RPLD AFT CABIN RT SIDE TRIPLE BEAM IAW A319 SRM 51-72- 11-911-002.
- [SDR CALA2024112702963](https://openairdocs.org/sdr/CALA2024112702963.md): Floor Support · corroded · Nov 25, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CABIN RT SIDE FLOOR BEAM CORRODED AT FR21 Y-189. RMVD AND RPLD FLOOR BEAM (RAIL) FROM FR20-FR24 Y-189 IAW A319 SRM 51-72-11-911-001 AND SRM 51-42-11/001
- [SDR CALA2024120403016](https://openairdocs.org/sdr/CALA2024120403016.md): Floorbeam · corroded · Nov 24, 2024 · N829UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN LH SIDE FLOOR BEAM Y 464 AT FR 66 HAS CORROSION. GEN B Y V798788 ON HAECO LCQ NR 9296434 / 20434 REMOVED & REPLACED FLOOR BEAM Y464 ST FR66 IAW A319 SRM 51-42-11 /001, SRM 51-72-11-911-001. ACMP BY MECH V942264 INSP BY V899260
- [SDR CALA2024112702968](https://openairdocs.org/sdr/CALA2024112702968.md): Floor Support · corroded · Nov 24, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SURVEILANCE INSP, L2 DOOR LOWER CENTER SHAPE SILL SECTION IS COR RODED AT FR67+12" STR23L. GEN BY V892429 ON HAECO LCQ NR 9296887 / 20887 REMOVED AND REPLACED CENTER SHAPE SILL AT L-2 DOOR IAW A319 SRM 51-42-11/001 AND SRM 51-72-11-911-001. ACMP BY MECH V94437
- [SDR CALA2024112702967](https://openairdocs.org/sdr/CALA2024112702967.md): Channel · cracked · Nov 24, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP PROFILE PANEL CRACKED IN (2) LOCATIONS AT FR 63 S TR 32L GEN BY V899045 ON HAECO LCQ NR 9296743/20743 REMOVED AND REPLACED PROFILE PANEL IN AFT CARGO AT FR63 STR32L I AW A319 SRM 51-42-11 ACMP BY MECH V899047 INSP BY V917055
- [SDR CALA2024112502936](https://openairdocs.org/sdr/CALA2024112502936.md): Panel · cracked · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP PROFILE PANEL CRACKED FR63 STR 32R PER HAECO LCQ N/R 9296744/20744 RMVD AND RPLD PROFILE PANEL FROM FR63 STR32 THROUGH FR59 STR 34R IAW A319 SRM 51-42-11/001
- [SDR CALA2024112502935](https://openairdocs.org/sdr/CALA2024112502935.md): Transition Panel · corroded · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FR51-FR52 STRG 38L TRANSITION PANEL HAS SURFACE CORROSION PER HAECO LCQ N/R 9296909/20909 RMVD AND RPLD TRANSITION PANEL AT STR38L FR51-FR52 IAW SRM 51-42 -11/001
- [SDR CALA2024112502934](https://openairdocs.org/sdr/CALA2024112502934.md): Panel · cracked · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO FR 25 TO FR 28 STR 38 PROFILE PANEL HAS A CRACK AT FR 26-27 FASTENER HOLE PER HAECO LCQ N/R 9296360/20360 RMVD AND RPLD FWD CARGO FR25 TO FR28 L/H STR 38 PROFILE PANEL IAW A319 SRM 51-42-11 TOP COATED PROFILE PANEL IAW A319 SRM 51- 23-11
- [SDR CALA2024112502933](https://openairdocs.org/sdr/CALA2024112502933.md): Panel · cracked · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO FR 25 TO FR 28 STR 38 PROFILE PANEL HAS A CRACK AT FR 26-27 FASTENER HOLE PER HAECO LCQ N/R 9296360/20360 RMVD AND RPLD FWD CARGO FR25 TO FR28 L/H STR 38 PROFILE PANEL IAW A319 SRM 51-42-11 TOP COATED PROFILE PANEL IAW A319 SRM 51- 23-11
- [SDR CALA2024112502930](https://openairdocs.org/sdr/CALA2024112502930.md): Panel · cracked · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMP PROFILE PANEL CRACKED AT FR59 STR 34R PER HAECO LCQ N/R 9296747/20747 RMVD AND RPLD PROFILE PANEL FROM FR63 STR 32 THROUGH FR59 STR 34 R IAW A319 SRM 51-42-11/001.
- [SDR CALA2024112502929](https://openairdocs.org/sdr/CALA2024112502929.md): Stringer · corroded · Nov 22, 2024 · N829UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMP CORROSION AT TRANSITION PANEL AT STR 38L BETWEEN FR56 AND FR57 PER HAECO LCQ N/R 9296733/20733. RMVD AND RPLD TRANSITION PANEL AT STR 38L BETWEEN FR56-FR57 IAW A319 SRM 51-42-11/001
- [SDR CALA2024121303067](https://openairdocs.org/sdr/CALA2024121303067.md): Shear Plate · corroded · Nov 20, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN LT SIDE SHEAR PLATE CORRODED AT FR70. REMOVED + REPLACED SHEAR PLATE AT AFT CABIN LH SIDE BUST FR69 TO 70 IAW A319 SRM 51-42-11/001.
- [SDR CALA2024112502948](https://openairdocs.org/sdr/CALA2024112502948.md): Floor Support · corroded · Nov 20, 2024 · N829UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN R2 DOOR FLOOR SILL ATTACH BEAM AT FR 68 HAS CORROSION. PERFORMED ANGLE REPAIR ON AFT R2 DOOR FLOOR SILL AT FR68 IAW A31 9 SRM 53-41-14-300-001 CAT A 53-41-14-283-002.
- [SDR CALA2024112702964](https://openairdocs.org/sdr/CALA2024112702964.md): Skin · gouged · Nov 19, 2024 · N829UA · Airbus A319131 · Passenger/Crew Doors
  > L1 DOOR OUTER SURFACE HAS A GOUGE ON FWD EDGE.
- [SDR CALA2024112602953](https://openairdocs.org/sdr/CALA2024112602953.md): Seat Track · corroded · Nov 18, 2024 · N829UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN RT SIDE O/B SEAT TRACK CORRODED AT FR20 Y-765 PER HAECO LCQ N/R 9296815/20815 GEN BY V061642
- [SDR CALA2024111701169](https://openairdocs.org/sdr/CALA2024111701169.md): Seat Track · worn · Nov 17, 2024 · N829UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN LH SIDE FLOOR BEAM Y1292 AT FR66 HAS CHAFFING PER HAECO LCQ N/R 9296433/20433.
- [SDR CALA2024111601168](https://openairdocs.org/sdr/CALA2024111601168.md): Floorbeam · corroded · Nov 16, 2024 · N829UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN LH CENTER FLOOR BEAM Y160 FR 70 HAS CORROSION PER HAECO LCQ N/R 9296432/20432
- [SDR CALA2024111802889](https://openairdocs.org/sdr/CALA2024111802889.md): Floorbeam · corroded · Nov 16, 2024 · N829UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT CABIN LH CENTER FLOOR BEAM Y160 FR 70 HAS CORROSION PER HAECO LCQ N/R 9296432/20432. REMOVED AND REPLACED LH CENTER FLOOR BEAM Y160 IAW A319 SRM 51-4 2-11 AND 51-72-11 CAT A.
- [SDR CALA2024111802888](https://openairdocs.org/sdr/CALA2024111802888.md): Seat Track · chafed · Nov 16, 2024 · N829UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN LH SIDE FLOOR BEAM Y1292 AT FR66 HAS CHAFING PER HAECO LCQ N/R 9296433/20433 REMOVED AND REPLACED AFT CABIN LH SIDE FLOOR BEAM Y-1292 AT FR66 IAW A319 SRM 51-72-11 AND SRM 51-42-11 CAT A.
- [SDR CALA2024101400828](https://openairdocs.org/sdr/CALA2024101400828.md): Fuel Cap · missing · Oct 12, 2024 · N829UA · Airbus A319131 · Fuel Storage
  > PDA 2 UNDERWING REFUEL CAP MISSIN REPLACED MISSING REFUEL CAP PER AMM 28-25-41 PARTS USED: 31-2825-9-0001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1379537 SN OFF 2450 CAP, COUPLING R OFF 31-2825-9-0001 2450 ON 31-2825-9-0001 2933
- [SDR CALA2024062700106](https://openairdocs.org/sdr/CALA2024062700106.md): Ring · missing · Jun 24, 2024 · N829UA · Airbus A319131 · Fuel Storage
  > REFUEL CAP LANYARD MISSING KEYRING REQUESTING CDL 28A DISPATCH DESK: 31 NAME: SS DATE: 24-JUN-24- / OK TO DEFER PER CDL 28A C/W MAINTENANCE DDP. REMOVED FUEL CAP AND REPLACED CABLE ASSEMBLY REF AMM 28-25-41. REINSTALLED FUEL CAP. NO PARTS
- [SDR CALA2024062701909](https://openairdocs.org/sdr/CALA2024062701909.md): Ring · missing · Jun 24, 2024 · N829UA · Airbus A319131 · Fuel Storage
  > REFUEL CAP LANYARD MISSING KEYRING REQUESTING CDL 28A C/W MAINTENANCE DDP. DISPATCH DESK: 31 NAME: SS DATE: 24-JUN-24- OK TO DEFER PER CDL 28A REMOVED FUEL CAP AND REPLACED CABLE ASSEMBLY REF AMM 28-25-41. REINSTALLED FUEL CAP. NO PARTS DEPARTED AIRCRAFT.
- [SDR CALA2023111503349](https://openairdocs.org/sdr/CALA2023111503349.md): Contactor · faulty · Nov 11, 2023 · N829UA · Airbus A319131 · Fuel System Wiring
  > FUEL TRAPPED IN CENTERTANK. MEL PROCEDURE DIDNOT WORK. BOTH FUEL PUMPSHOW FAULT. AFTER GET THE CREW INFO THEY CONFIRM COMPLY WITH MEL BUT STILL PUMPS SHOW FAULT,PERFORMED FUEL TRANSFER PER AMM 28-25-00 FROM CENTER TANK TO RIGHT TANK FUEL PUMPS SHOW FAULT FOUN
- [SDR CALA2023111403335](https://openairdocs.org/sdr/CALA2023111403335.md): Gfi · unknown · Nov 8, 2023 · N829UA · Airbus A319131 · Fuel Indicating System
  > CTR TK PUMPS LO PR DISPLAYED ON UPPER ECAM SCREEN. - FUEL UPPER ECAM FUEL CTR TKPUMPS ALSO BOTH OVRHDCTR PUMP SWITCHES HA VEFAULT LIGHTS YYC MECHANIC GUPTA, RITESH (V937228) FOUND 420 LBS IN CENTER TANK AUTOMATIC FUEL FEED SYSTEM REQUIRES FURTHER TROUBLESHOOT
- [SDR CALA2023071002212](https://openairdocs.org/sdr/CALA2023071002212.md): Control Unit · inoperative · Jul 7, 2023 · N829UA · Airbus A319131 · Landing Gear Brake System
  > ABORTED T/O BRAKES SYS 1FAULT.ALREADY RESET ANTISKID ON TAXI OUT. 40KTS. LOCKING FOR BSCU REPLACEMENT. ADDED POST FLIGHT REPORT OK TO UNLOCK R&R THE BSCU IAW AMM 32-42-34-400-001-A. OPS AND BITE CHECK GOOD. REQUIRES A LAND VERIFY TEST. ROTABLE PARTS CHANGE
- [SDR CALA2023071002198](https://openairdocs.org/sdr/CALA2023071002198.md): Control Unit · faulty · Jul 6, 2023 · N829UA · Airbus A319131 · Landing Gear Brake System
  > BRAKES SYS 1 FAULTBRAKES SYS 2 WAS ALREADY RESET ON TAXI OUT TS PER TSM 32-51-00-810-815-A, MULTIPLE FAULTS OF BSCU 2 OVER THE LAST SEVERAL DAYS. GROUND SCAN SHOWS NO FAILURES AT THIS TIME. BSCU AOG... NIS IN EWR REMOVED AND AND REPLACED BSCU PER AMM 32-42-34-

Next page: https://openairdocs.org/aircraft/N829UA/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 = 'N829UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N829UA/reports

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