# Service difficulty reports: N434UA

A list on [N434UA](https://openairdocs.org/aircraft/N434UA.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 · 132 reports

- [SDR CALA2026100520100](https://openairdocs.org/sdr/CALA2026100520100.md): Fuel Cap · missing · Sep 28, 2026 · N434UA · Airbus A320232 · Fuel Storage
  > FOUND MISSING IAW GMM 02-30-95 FUEL CAP MISSING ON ARRIVAL REF LP 3521127 FOR TERMINATING ACTION. REPLACED FUEL CAP.
- [SDR CALA2026022414030](https://openairdocs.org/sdr/CALA2026022414030.md): Slide · unwanted deploy · Feb 21, 2026 · N434UA · Airbus A320232 · Escape Slide
  > SLIDE DEPLOYMENT ATDOOR 1L FLIGHT ATTENDANT DEPLOYED SLIDE ACCIDENTALLY AT DOOR 1L NO INJURIES REMOVED DOOR 1L SLIDE ASSY, REF AMM 25-62-44-000-002 INSTALLED DOOR 1 LEFT SLIDE ASSY REF AMM 25-62-44. SLIDE RENDER CHECKLIST FOLLOWED AND USED. OBSERVED THE REM
- [SDR CALA2025121512129](https://openairdocs.org/sdr/CALA2025121512129.md): Fuel Cap · missing · Dec 11, 2025 · N434UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING ON ARRIVAL COS, FLT 2670. DOCUMENTED PER GMM 02-30-95, INSTALLED REFUEL/DEFUEL COUPLING-CAP LANYARD-ASSEMBLY OR CHAIN AS PER AMM 28-25-41-400-007-A.
- [SDR CALA2025090408462](https://openairdocs.org/sdr/CALA2025090408462.md): Light · malfunctioned · Sep 3, 2025 · N434UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTSARE ILLUMINATED WITH EMER EXIT LT SWITCH IN OFF AND ARMED POSITION WITH CREW ASSISTANCE CYCLED BREAKERS H06, H05 AND V07. CYCLED NO SMOKING AND EMER SWITCHES, LIGHTS OPS NORMAL. AMM33-51-00.
- [SDR CALA2025080107209](https://openairdocs.org/sdr/CALA2025080107209.md): Control Servo · leaking · Jul 31, 2025 · N434UA · Airbus A320232 · Drag Control System
  > HYD Y ENG 2 PUMP LOW PRESSURE. REF GMM 04-20-16, PTU INOPERATIVE, CARGO DOOR INOPERATIVE, Y ELECT PUMP INOPERATIVE, Y ENG 2 PUMP INOPERATIVE, INSTALLLED NR 4. SPOILER SERVO CONTROL IAW AMM 27-64-52-400-003-A. OPS & LEAK CHK GOOD. OK TO RETURN TO SERVICE.
- [SDR CALA2025061005416](https://openairdocs.org/sdr/CALA2025061005416.md): Filter · clogged · Jun 7, 2025 · N434UA · Airbus A320232 · Air Distribution System
  > PLANE HAS STRONGODORTHANKSWITH PACKS ON THE AIR DISTRIBUTION SENDING A STRONG PUNGENT SMELL IN CABIN MORE CONCENTRATED AT LEFT AND RIGHT OVERWING SECTION, REF FIM05-50-00-810-831-A ALSO FIM 05-51-10-200-801-C-1. FOLLOWING DECISION TABLE IN TSM 05-50-00-810-
- [SDR CALA2025060905366](https://openairdocs.org/sdr/CALA2025060905366.md): Ecs · contaminated · Jun 5, 2025 · N434UA · Airbus A320232 · Cabin Cooling System
  > STRONG DIRTY SOCKS/TOXIC FUMES SMELL ATGATE WHILE RUNNING APU.SM ELLED THROUGHOUT A/C ACPED ECS DECONTAMINATION TEST TASK 21-00-00-615-802-A NO TOXID FUMES OR ODERS NOTED. REMOVED AND REPLACED RECIRCULATION FILTERS.21-21-41-400-001-A.
- [SDR CALA2025031302764](https://openairdocs.org/sdr/CALA2025031302764.md): Skin · damaged · Mar 11, 2025 · N434UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > 4634 FR35 STGR30RH PREVIOUS REPAIR MULTIPLE FASTENER HOLE DISCREPANCIES FOUND DURING RE-INSPECTION OUTLINED IN ECRA 5330-06963. REF LOG PAGE 8992357. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5330-07480 WITH NO DEVIATION. ACCOMPLISH A PERMANENT REPAIR ON THE FR35 S
- [SDR CALA2025031302763](https://openairdocs.org/sdr/CALA2025031302763.md): Crossbeam · cracked · Mar 11, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 16 RH CROSSBEAM HOLE #H3 HAS CRACK INDICATIONS IN BOTH LAY ERS AT 9 AND 5 OCLOCK 100% S.H. (AD 2024-04-04) PER NON ROUTINE 9296355/44355. ORIGINAL ACCOMPLISHED INTERIM REPAIR PART 1 TO FRAME 16 RH CROSSBEAM HOLE #H3 PER ECRA5311-03343 WITH NO DEVIATION
- [SDR CALA2025031302766](https://openairdocs.org/sdr/CALA2025031302766.md): Crossbeam · cracked · Mar 9, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 16 RH CROSSBEAM HOLE #H4 HAS CRACK INDICATION IN BOTH LAYE RS AT 6 OCLOCK 100% S.H. (AD 2024-04-04) PER HAECO LCQ NON ROUTI NE 9296351/44351 ACCOMPLISHED INTERIM REPAIR PART 1 TO FRAME 16 RH CROSSBEAM HOLE #H4 PER ECRA5311-03343 WITH NO DEVIATIONS. ACC
- [SDR CALA2025031302765](https://openairdocs.org/sdr/CALA2025031302765.md): Crossbeam · cracked · Mar 9, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 16 RH CROSSBEAM HOLE #H2 HAS CRACK INDICATION IN BOTH LAYE RS AT 4 OCLOCK 100% S.H. (AD 2024-04-04) PER HAECO LCQ NON ROUTI NE 9296353/44353 GENERATED BY V892444 ACCOMPLISHED INTERIM REPAIR AT FRAME 16 RH CROSSBEAM HOLE #H2 PER PART 1 OF ECRA5311-03343 W
- [SDR CALA2025031102705](https://openairdocs.org/sdr/CALA2025031102705.md): Skin · cracked · Mar 9, 2025 · N434UA · Airbus A320232 · Passenger/Crew Doors
  > SECONDARY FINDING. L1 DOOR EXTERIOR SKIN UPPER AFT CORNER CRACKED. ESFR ENTRY GENERATED REMOVED AND REPLACED L1 DOOR UPPER EXTERNAL SKIN IAW A320 SRM 51 -72-11-911-001.
- [SDR CALA2025031002661](https://openairdocs.org/sdr/CALA2025031002661.md): Crossbeam · cracked · Mar 7, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 16 RH CROSSBEAM HOLE #H6 HAS CRACK INDICATION IN BOTH LAYE RS AT 12 OCLOCK 100% S.H. AD 2024-04-04. REAMED HOLE #6 AT FRAME 16 RH AT.2500 (6.35MM) NO DEFECTS NOTED. COLDWORKED AS REQ'D FINAL REAMED AT.2780(7.061MM) INSTALLED N EW FASTENER. ALL WORK
- [SDR CALA2025031302767](https://openairdocs.org/sdr/CALA2025031302767.md): Fuel Panel · damaged · Mar 6, 2025 · N434UA · Airbus A320232 · Wing Main, Frame Structure
  > LEFT WING LOWER FUEL PANEL LAND 540JB HAS IRREGULAR HOLE. ACCOMPLISHED REPAIR OF IRREGULAR HOLE#595 ON FUEL PANEL LAND 540 JB IAW SRM 57-21-11-300-002. REAMED AND COLD WORKED HOLE. FABRIC ATED AND INSTALLED BUSHING OD=.4054IN. FABRICATED AND INSTALLED BRIDGIN
- [SDR CALA2025031002649](https://openairdocs.org/sdr/CALA2025031002649.md): Crossbeam · damaged · Mar 4, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > WHILE SURVEYING THE UPPER TWO ROWS AT L/H FR20 CROSSBEAM FRAME S PLICING IT WAS FOUND THAT THERE WERE NON-ORIGINAL TYPE FASTENERS INSTALLED. REPAIRED LH FR20 CROSSBEAM FRAME SPLICING UPPER TWO ROWS FASTENE RS IAW UAL EA 5310-06784-001.
- [SDR CALA2025021900381](https://openairdocs.org/sdr/CALA2025021900381.md): Profile · corroded · Feb 17, 2025 · N434UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FUSELAGE INTERNAL AREA AT FR 67 LST42-RST42 HAS EXFOLIATION. REMOVED AND REPLACED CORRODED FRAME PROFILE AT FR67 WITH A NEW F RAME PROFILE AT FR 67 IAW A320 SRM 51-42-11-001 PARA F.
- [SDR CALA2025022400419](https://openairdocs.org/sdr/CALA2025022400419.md): Structure · corroded · Feb 13, 2025 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > FUSELAGE INTERNAL FR 69 AFT LAV EXHAUST VENT STRUCTURE HAS CORROSION. REMOVED AND REPLACED AFT LAC EXHAUST VENT INTERNAL DOUBLER IAW A 320 SRM 51-72-11-911-001.
- [SDR CALA2025022000387](https://openairdocs.org/sdr/CALA2025022000387.md): Door Sill · corroded · Feb 13, 2025 · N434UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN L2 DOOR ENTRY SILL HAS CORROSION. GEN BY V798788 ON HA ECO LCQ NR 9296327/44327 REPAIRED THE L2 DOOR SILL IAW A320 SRM 53-41-14-300-001 REPAIR P RINCIPLE 5 H IS A CATEGORY A REPAIR PERMANENT. NO FURTHER ACTION REQUIRED.
- [SDR CALA2025021800378](https://openairdocs.org/sdr/CALA2025021800378.md): Door Sill · corroded · Feb 13, 2025 · N434UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R2 DOOR ENTRY SILL HAS CORROSION. GEN BY V798788 ON HA ECO LCQ NR 9296326/44326
- [SDR CALA2025010101733](https://openairdocs.org/sdr/CALA2025010101733.md): Unknown · odor · Dec 31, 2024 · N434UA · Airbus A320232 · Air Distribution System
  > STRONG HYDRAULIC ODOR NOTICED FROM PASSENGER IN THE BACK OF THECAB IN UPON TAXI TO GATE. PERFORMED TSM 05-50-00-810-813-A. PERFORMED SMELL CHECK ON APU BLEED, ENGINE BLEED WITH CREW RUNNING AIRCRAFT. NO SMELL NOTED ON BOTH BLEED SOURCES. ALSO, INSPECTION OF A
- [SDR CALA2024042201165](https://openairdocs.org/sdr/CALA2024042201165.md): Lgciu · inoperative · Apr 19, 2024 · N434UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > LGCIU 2 ECAM LOST REV 2 AND MAIN GALLEY POWER AND LAVS ALSO AIRCRAFT WAS REPOSITIONED DOWN TO MAINT AREA AND WAS POWERED DOWN. POWERED AIRCRAFT UP AND ALL FAULTS CLEARED. PERFORMED CFDS TEST FOR LGCIU 1 AND 2 NO FAULTS. POST FLIGHT SHOWED NO DATA LGCIU 2. SUGG
- [SDR CALA2023072102291](https://openairdocs.org/sdr/CALA2023072102291.md): Clamp · corroded · Jul 19, 2023 · N434UA · Airbus A320232 · Water and Waste System
  > OBSERVED LK FROM BILGE DRAIN AT CENTER OF AIRCRAFT, AFTER INVESTIGATION FOUND LK FWD OF GRAY WATER HOLDING TANK.PERFORM CLEANUP AS PER ECRA 2011-01000 DUE TO GRAY WATER LEAK FOUND. COMPLETED SPILL CLEAN UP THROUGH STEP 2 B (13) ECRA 2011-01000. ADD EMP:U411446
- [SDR CALA2023050101295](https://openairdocs.org/sdr/CALA2023050101295.md): Actuator · unknown · Apr 28, 2023 · N434UA · Airbus A320232 · Hydraulic Power System
  > HYD RAT FAULT ON DECK.IN AIR GREEN RAT OUT MEMO. SOLID GREEN ARR OW ON HYD PAGE. PICTURE UPDATE TSM 29-22-00-810-801-A REQUIRES AVIONICS 104 TROBLESHOOTING PILOT MSG HYD RAT FAULT ON DECK IN AIR GREEN RAT OUT MEMO SOLID GREEN ARR OW ON HYD PAGE RETRACTED AND S
- [SDR CALA2022121203367](https://openairdocs.org/sdr/CALA2022121203367.md): Fuel Cap · missing · Dec 12, 2022 · N434UA · Airbus A320232 · Fuel Storage
  > PDA 1 FUEL CAP MISSING WAS ALLREADY REPORTED, ON CDL. FOUND FUEL CAP INSTALLED, OKAY FOR SERVICE.
- [SDR CALA2022070601651](https://openairdocs.org/sdr/CALA2022070601651.md): None · cracked · Jul 6, 2022 · N434UA · Airbus A300* · Fuselage Main, Plate/Skin
  > RH FRAME 35 STR 30 RH HOLES #1 AND #2 HAVE CRACK INDICATIONS. PERMANENT RPR AT FR 35 STR 30 RH PER PART 3 OF THE LATEST REV OF 9290225 AND 9290224 IAW ECRA 5330-06963 PART 1.2. ECRA 5330-06963 ON OR BEFORE 30-DEC-22.ALL WORK ACMP ON HAECO NR ACMP INTERIM RPR A
- [SDR CALA2022070601662](https://openairdocs.org/sdr/CALA2022070601662.md): Frame · cracked · Jul 5, 2022 · N434UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > RH FRAME 35 STR 30 RH HOLES #1 AND #2 HAVE CRACK INDICATIONS. PERMANENT RPR AT FR 35 STR 30 RH PER PART 3 OF THE LATEST REV OF 9290225 AND 9290224 IAW ECRA 5330-06963 PART 1.2. ECRA 5330-06963 ON OR BEFORE 30-DEC-22.ALL WORK ACMP ON HAECO NR ACMP INTERIM RPR A
- [SDR CALA2022070601660](https://openairdocs.org/sdr/CALA2022070601660.md): Fitting · cracked · Jul 5, 2022 · N434UA · Airbus A320232 · Fuselage Main, Frame
  > FR 68 HAS CRACK INDICATION AT LH STR 22 IN RADIUS OF HORIZONTAL FLANGE ADJACENT TO LOWER IB DOOR STOP BOLT. GENERATED AT HAECO L CQ PER NR 9290219 (26219) BY V892444 {SUPPORT TASK} 1 WITH NO DEVIATIONS. A DIP IS REQUIRED PER PART 2 TO ACCOMPLIS ILLET RADII AT
- [SDR CALA2022070601654](https://openairdocs.org/sdr/CALA2022070601654.md): Fitting · none · Jul 4, 2022 · N434UA · Airbus A300* · Fuselage Structure (General)
  > LH SIDEWALL KEEL BEAM HOLE L13 HAS ELONGATED HOLE THROUGH THE FI TTING AND KEEL BEAM PER NR 9290570/26570 GEN BY V080280 INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06955.SEE LOG PAGE 896 0036 FOR REPAIR DETAILS AND DIP LIMITS.
- [SDR CALA2022070601652](https://openairdocs.org/sdr/CALA2022070601652.md): Fitting · corroded · Jul 4, 2022 · N434UA · Airbus A300* · Fuselage Structure (General)
  > RH FR68 FWD FACE AND STR23 APROX. HAVE A HOLE WITH CORROSION. FA BRICATE RH FR68 STR23 EXTEND REPAIR FITTING AS REQUIRED PER HAEC O LCQ NON ROUTINES 9291028/27028 AND 9291071/27071 PER HAECO LCQ GENERATED BY V061682/V061742 STR22 RH - 23 RH PER PART 2 OF THE L
- [SDR CALA2022070401641](https://openairdocs.org/sdr/CALA2022070401641.md): Stringer · corroded · Jul 4, 2022 · N434UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > RH FR68 FWD FACE AND STR23 APROX. HAVE A HOLE WITH CORROSION. FABRICATE RH FR68 STR23 EXTEND REPAIR FITTING AS REQUIRED.REPEAT INSP NOT TO EXCEED INTERVALS OF 20,200 FC THEREAFTER. IAW ON OR BEFORE THE ACFT REACHES 51,264 TOTAL ACFT FC.THEREAFTER TOMC APPROVED
- [SDR CALA2022062901603](https://openairdocs.org/sdr/CALA2022062901603.md): Skin · dented · Jun 28, 2022 · N434UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > UAL QC DISCOVERY DURING STORAGE, EXISTING DENT AND SCRATCH BETWEEN FRAMES 61 AND 62 JUST LEFT OF CENTER ON BELLY AFTER SMOOTHING PAINT SCRATCH STILL EXISTS, WILL REQUIRE ADDITIONAL EVALUATION IMENSIONS OF DENT: 2.4" L X 1.7" W X 0.42" D. FOUND TO BE OUT OF USE
- [SDR CALA2022062901602](https://openairdocs.org/sdr/CALA2022062901602.md): Stringer · corroded · Jun 28, 2022 · N434UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STRINGER 43L SPLICE BETWEEN FR55-56 HAS CO RROSION A3NB-05-3-6023 PER HAECO LCQ NON ROUTINE 9290727/26727 G ENERATED BY V077960 REMOVED AND REPLACED AFT CARGO COMPARTMENT STRINGER 43L FR54-FR6 0 IAW A320 SRM 51-42-11-001 TREATED, PRIMED &
- [SDR CALA2022062701579](https://openairdocs.org/sdr/CALA2022062701579.md): Fitting · cracked · Jun 25, 2022 · N434UA · Airbus A320232 · Fuselage, Door Hinge
  > RH AFT FR 68 DOOR STOP FITTING #1 BOTTOM I/B HOLE HAS CRACK INIC ATION AT APPROX THE 5:0CLOCK POS (2018-03-12) PER HAECO LCQ N/R 9290312/26312 GEN BY V062 GEN BY V062335 IS ''D1=.6280", D2=.2485", D3=.2485",D4=.2485", WITH EDGE HOLE T W SRI53-41-12-205-010 @ 3
- [SDR CALA2022062201553](https://openairdocs.org/sdr/CALA2022062201553.md): Torsion Box · corroded · Jun 21, 2022 · N434UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > AFT CARGO COMPARTMENT TORSION BOX UPPER SURFACE HAS MULTIPLE ARE A OF CORROSION SPEC # A3NB-05-3-6022 PER NR9290743/26743 GEN BY V077960 RMVD AND RPLD AFT CARGO COMPARTMENT TORSION BOX COVER IAW SRM 53 -41-49-283-004 FOUND TO BE OUT OF LIMITS MAX MAT. LOSS.01
- [SDR CALA2022062201552](https://openairdocs.org/sdr/CALA2022062201552.md): Door Sill · corroded · Jun 21, 2022 · N434UA · Airbus A320232 · Fuselage Structure (General)
  > R2 DOOR SILL AND FWD FR68 AROUND GIRT BAR FITTING HAVE 2 AREAS W ITH CORROSION RED MARKED GEN BY V061682 NR9291027/27027 RMVD AND RPLD R2 DOOR SILL FR68 IAW SRM 51-72-12 BY MECH V061742 INSP BY V061334
- [SDR CALA2022062001532](https://openairdocs.org/sdr/CALA2022062001532.md): Door Sill · corroded · Jun 17, 2022 · N434UA · Airbus A320232 · Fuselage Structure (General)
  > L-2 DOOR SILL I/B FR 68 AREA HAS EVIDENCE OF CORROSION. GENERATE D BY V052040 ON HAECO LCQ NR 9290696/26696 REMOVED AND REPLACED L-2 DOOR SILL FR 66-68 IAW A320 SRM 51-72-1 1 ACMP BY MECH V080280 INSP BY V061682
- [SDR CALA2022062001531](https://openairdocs.org/sdr/CALA2022062001531.md): Stringer · corroded · Jun 17, 2022 · N434UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STRINGER 42R HAS CORROSION FWD AND AFT FR 62. GENERATED BY V077960 ON HAECO LCQ NR 9290744/26744 REMOVED AND REPLACED STRINGER 42R AFT CARGO FR 60 TO FR 64 IAW A 320 SRM 51-72-11-911-001. ACMP BY MECH V080280 INSP BY V061629
- [SDR CALA2022062001530](https://openairdocs.org/sdr/CALA2022062001530.md): Support Angle · cracked · Jun 17, 2022 · N434UA · Airbus A320232 · Emergency Exits
  > AFT RH EMERGENCY EXIT DOOR FWD, AFT SUPPORT ANGLE CRACKED PER NR 9291044/27044 GEN BY V061771 RMVD DAMAGED FWD & AFT SEGMENTS & REPLACED WITH NEW FIND AND NEW AFT SEGMENTS IAW SRM 51-42-11/001 AND 52-21-00-01-A APPLIED C.I C AS REQUIRED TO INTERNAL SURFACES/ST
- [SDR CALA2022050901184](https://openairdocs.org/sdr/CALA2022050901184.md): Intercostal · cracked · May 8, 2022 · N434UA · Airbus A320232 · Doors
  > AFT RH EMERGENCY EXIT HATCH FWD INTERCOSTAL APPEARS TO BE CRACKE D PER NR9290231/26231 GEN BY V052040 RMVD DAMAGED SEGMENT IAW SRM 51-25-11-911-001 AND AIRBUS DWG#152 2-79610 BY MECH V061742 INSP BY V892442
- [SDR CALA2022050901183](https://openairdocs.org/sdr/CALA2022050901183.md): Skin · punctured · May 8, 2022 · N434UA · Airbus A320232 · Elevator, Plate/Skin
  > (CR-INBOUND HAIL DAMAGE) RIGHT ELEVATOR HAS ONE PUNCTURE DUE TO HAIL DAMAGE. 1) 123 INCHES FROM INBOARD EDGE 9 INCHES FROM TRAIL ING EDGE.75 INCHES DIAMETER PER HAECO LCQ N/R 9290136/26136 GEN BY V061742 REPAIRED RH ELEVATOR 123 IN I/B 9 IN FROM T/E 1 IN DIA
- [SDR CALA2022050901182](https://openairdocs.org/sdr/CALA2022050901182.md): Skin · punctured · May 8, 2022 · N434UA · Airbus A320232 · Elevator, Plate/Skin
  > (CR-INBOUND HAIL DAMAGE) LEFT ELEVATOR HAS ONE PUNCTURE DUE TO H AIL DAMAGE.1) 90 INCHES FROM OUTBOARD EDGE 11 INCHES FROM TRAILI NG EDGE 1 INCH DIAMETER PER HAECO LCQ N/R 9290137/26137 GEN BY V 061742 REPAIRED LH ELEVATOR 90 INCH FROM O/B EDGE 11 INCHES FROM
- [SDR CALA2019042200623](https://openairdocs.org/sdr/CALA2019042200623.md): Fuel Cap · missing · Apr 20, 2019 · N434UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISSING IN YVR CDL 28A APPLIED ON LOG PAGE 3033680
- [SDR CALA2017122804641](https://openairdocs.org/sdr/CALA2017122804641.md): Light · malfunctioned · Dec 28, 2017 · N434UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS CAME ON DURING LANDING AND WOULD NOT GO OFF. RESET THE NO SMOKING SWITCH.
- [SDR CALA2017100603525](https://openairdocs.org/sdr/CALA2017100603525.md): Power Supply · faulted · Oct 6, 2017 · N434UA · Airbus A320232 · Emergency Lighting
  > OPS CHECK OF THE EMERGENCY LIGHTS, EPSU LT FAULTED. REPLACED POWER SUPPLY AND BATTERY. BITE CHECKED, TESTED OK IAW AMM 33-51-38.
- [SDR CALA2017042801164](https://openairdocs.org/sdr/CALA2017042801164.md): Light · malfunctioned · Apr 28, 2017 · N434UA · Airbus A320232 · Emergency Lighting
  > EMER LIGHTS ARE ON IN THE CABIN NO MATTER WHAT POS THE SWITCH IS IN. TURNED OFF LIGHT AT 2L.
- [SDR CALA2016072295574](https://openairdocs.org/sdr/CALA2016072295574.md): Power Supply · inoperative · Jul 21, 2016 · N434UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED,(UNIT 12WL) FAULTING. REPLACED POWER SUPPLY UNIT 12WL, OPS CHECKED GOOD PER AMM 33-51-38-400-002-A
- [SDR CALA2015060493855](https://openairdocs.org/sdr/CALA2015060493855.md): Skin · damaged · Jun 2, 2015 · N434UA · Airbus A320232 · Wing, Plate/Skin
  > RIGHT WING FUEL TANK ACCESS PANEL LANDING 640HB HAS TWO EACH ELONGATED HOLES. REPAIRED IAW ECRA 5720-02664.
- [SDR CALA2015060293849](https://openairdocs.org/sdr/CALA2015060293849.md): Stringer · corroded · May 30, 2015 · N434UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > RIGHT STRINGER 31 AT FRAME 65 HAS CORROSION. R & R STRINGER 31RT IAW SRM 51-72-11
- [SDR CALA2015060293848](https://openairdocs.org/sdr/CALA2015060293848.md): Stop Fitting · damaged · May 30, 2015 · N434UA · Airbus A320232 · Fuselage Main, Structure
  > AFT R2 DOOR CUT OUT FRAME 66 DOOR STOP FITTINGS AT THE FOLLOWING LOCATION 1ST, 2ND, 3RD, 4TH, 5TH & 6TH FROM BOTTOM OF FLOOR, ALL 4 HOLES IN EACH FITTING OUT OF ROUND. REPAIRED HOLES IAW 53-41-12 PARA 5C D & E SECOND OVER SIZE, ALL HOLES IAW NTM 51-10-01.
- [SDR CALA2015030493184](https://openairdocs.org/sdr/CALA2015030493184.md): Frame · cracked · Mar 2, 2015 · N434UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FRAME 43 CRACKED AT HOLE NR 3. REPAIRED IAW ECRA 5330-05 076 REV A. THIS IS A PERMANENT REPAIR WITH NO INSPECTION REQUIREMENTS.

Next page: https://openairdocs.org/aircraft/N434UA/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 = 'N434UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N434UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.