# Service difficulty reports: N429UA

A list on [N429UA](https://openairdocs.org/aircraft/N429UA.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 · 118 reports

- [SDR CALA2025082007943](https://openairdocs.org/sdr/CALA2025082007943.md): Bottle · low pressure · Aug 16, 2025 · N429UA · Airbus A320232 · Escape Slide
  > SLIDE PRESSURE 2L AND2R ARE LOW BOTH PRESSURES IN THE TOP OF GREEN BAND OK FOR SERVICE.
- [SDR CALA2025081307675](https://openairdocs.org/sdr/CALA2025081307675.md): Slat Valve · no discrepancy · Aug 11, 2025 · N429UA · Airbus A320232 · Escape Slide
  > 2L DOOR SLIDE IN THE RED, PRESSURE INSPECTED AFT L2 DOOR SLIDE NEEDLE IS WITHIN THE GREEN BAND, IT WAS JUST A LITTLE HARD TO AT A ANGLE BUT OK TO CONT
- [SDR CALA2025070906387](https://openairdocs.org/sdr/CALA2025070906387.md): Hydraulic Line · leaking · Jul 7, 2025 · N429UA · Airbus A320232 · Hydraulic System, Main
  > AFTER GEAR EXTENSION, COMPLETE LOSS OF GREEN HYD SYS RESIVOR. FOUND HYDRAULIC HOSE AT THE RIGHT MLG DOOR ACTUATOR LEAKING. FOUND LANDING GEAR DOOR EXTENSION FLEX LINE FAILED REPLACED LINE REF AMM 29-23-11. ALL OPERATIONAL AND LEAK CHECKS OKAY.
- [SDR CALA2025062705978](https://openairdocs.org/sdr/CALA2025062705978.md): Slide · no discrepancy · Jun 24, 2025 · N429UA · Airbus A320232 · Escape Slide
  > DOOR L2 SLIDE PRESSURE BELOW GREEN RANGE IAW AMM 25-62-00-210-001-A. MODEL A GAUGE NEEDLE AT TOP OF GREEN BAND, 2L WAS OPEN IN HEATED ENVIRONMENT FOR CATERING.
- [SDR CALA2025061205479](https://openairdocs.org/sdr/CALA2025061205479.md): None · none · Jun 7, 2025 · N429UA · Airbus A320232 · Standard Practices/Structures
  > 2L SLIDE PRESSURE IN THE RED ZONE INSPECTED SLIDE GAUGE AND FOUND IT TO BE WITHIN NORMAL LIMITS. OKAY FOR CONTINUED SERVICE
- [SDR CALA2025050704519](https://openairdocs.org/sdr/CALA2025050704519.md): Bottle · no discrepancy · May 5, 2025 · N429UA · Airbus A320232 · Passenger/Crew Doors
  > SLIDE 2L SERVICE PRESSURE IN RED ZONE EVALUATE GAUGE AND CONTACT TOMC WITH FINDINGS NEEDLE IS ON THE SPLIT BETWEEN GREEN AND RED, REF AMM25-62-00-810-803-A -GAUGE MODEL A IS INSTALLED AND PRESSURE IS WITHIN LIMITS (ACCEPTABLE UP TO A NEEDLE WIDTH INTO THE R
- [SDR CALA2025032103062](https://openairdocs.org/sdr/CALA2025032103062.md): Warning Light · false activation · Mar 19, 2025 · N429UA · Airbus A320232 · Door Warning System
  > FWD CARGO DOOR OPENINDICATION X 3 ECAM.REPEATEDLY HAPPENING. LOG PAGE 4161341 HAS BEEN REOPENED. VISUALLY CHECKED FORWARD CARGO DOOR IS CLOSED AND LOCKED (REF. AMM 52-70-00-040-001-A) AND INSTALLED INOPERATIVE STICKER ADJACENT TO LOWER ECAM DISPLAY.
- [SDR CALA2025031802912](https://openairdocs.org/sdr/CALA2025031802912.md): Bottle · no discrepancy · Mar 14, 2025 · N429UA · Airbus A320232 · Escape Slide
  > SLIDE PRESSURE ON DOOR2L IS IN THE RED. REF AMM 25-62-00-210-001-A. INSPECTED SLIDE PRESSURE AND NEEDLE IS RIGHT BETWEEN GREEN AND RED BAND. ACCEPTABLE PER AMM INSPECTION REQUIREMENTS FOR MODEL A GUAGE.
- [SDR CALA2025011301874](https://openairdocs.org/sdr/CALA2025011301874.md): Door · open · Jan 11, 2025 · N429UA · Airbus A320232 · Cargo/Baggage Doors
  > FWD CARGO DOOR UNLOCKED INDICATION ECAM UPON CLIMB THRU APPROX 20 00MSL. FOUND FWD CARGO DOOR NOT FULLY STOWED POSITION. OPS CHK FWD CARGO DOOR. VERIFIED THE FWD CARGO GREEN INDICATIONS APPEAR IN THE INSPECTION WINDOW. FLIGHT DECK INDICATION OF FWD CARGO
- [SDR CALA2024122001590](https://openairdocs.org/sdr/CALA2024122001590.md): Slat System · stuck · Dec 18, 2024 · N429UA · Airbus A320232 · Leading Edge Slat Control System
  > FLAP INDICATOR SHOWINGXXFLAP AND SLATS STUCK AT.5 AND 2.5 FLIGHT CREW ADVISED, SET FLAP LEVER TO POSITION 1, FLAPS AND SLATS WENT HALF WAY. SET FLAP LEVER TO POSITION 2 AND FLAP AND SLATS WENT TO POSITION 2, THEN SET FLAP LEVER TO POSITION 3, FLAPS AND SLATS W
- [SDR CALA2025091008753](https://openairdocs.org/sdr/CALA2025091008753.md): Aoa · faulty · Aug 23, 2024 · N429UA · Airbus A320232 · Stall Warning System
  > EG HAS BEEN NOTIFIED BY THE FAA THAT THIS AIRCAFT IS REPORTING HIGHER THAN EXPECTED RVSM ALTITUDES EG IS REQUESTING TO ACCOMPLIS H (ASE) ALTIMETRY SYSTEM ERROR CHK. 1. PERFORM AIRBUS SRM 51-11 -00 SECTION 4,A AND SRM 53-00-11 SECTION 4.B SKIN WAVINESS. 2. PERF
- [SDR CALA2023120603574](https://openairdocs.org/sdr/CALA2023120603574.md): Unknown · unknown · Nov 30, 2023 · N429UA · Airbus A320232 · Doors
  > DOOR L1 SLIDE WILL NOT ARM MAIN CABIN DOOR SHOWING NOT ARMED ON ECAM WITH DOOR CLOSED AND COMPLIED WITH THE REQUIREMENTS OF MEL 2560B. DOOR VERIFIED SMOOTHLY AS 1RH DOOR ARM LEVER. ARMED. CLOSED AND ARMED. ADD FAULT: 2500 ADD FAULT: 2560 DISPATCH DESK: S32 NA
- [SDR CALA2023112203449](https://openairdocs.org/sdr/CALA2023112203449.md): Fitting · cracked · Nov 19, 2023 · N429UA · Airbus A320232 · Fuselage, Door Hinge
  > LH MLG DOOR FWD HINGE FITTINGS, FWD HALF HAS CRACK INDICATION AT CONNECTING PLATE LOWER FASTENER. GEN BY V892444 ON NR# 9292461/ 40461 REMOVED AND REPLACED LH MLG DOOR FWD HINGE FITTING IAW AIRBUS RE PAIR INSTRUCTION R53370500F. ACMP BY V061619 INSP BY V892285
- [SDR CALA2023112003435](https://openairdocs.org/sdr/CALA2023112003435.md): Hinge Fitting · cracked · Nov 18, 2023 · N429UA · Airbus A320232 · Fuselage, Door Hinge
  > RH MLG DOOR FWD HINGE FITTING, BOTH FWD AND AFT HINGE HALF HAVE CRACK INDICATIONS AT CONNECTING PLATE LOWER FASTENER. REMOVED AND REPLACED RH MLG DOOR FWD HINGE FITTING IAW AIRBUS RE PAIR INSTRUCTION R53370500F.
- [SDR CALA2023081102489](https://openairdocs.org/sdr/CALA2023081102489.md): Pressure Switch · faulty · Aug 8, 2023 · N429UA · Airbus A320232 · Hydraulic System, Main
  > HYD G RSVR LO LVL.ACCOMPLISHED ECAM/QRH.MANUALLY LOWERED GEAR. DEBRIEFED CREW - ALONG WITH HYD RES LOW LEVEL LOST HYD PRESSURE ON GREEN SYSTEM. NO VISIBLE LEAKS AND HYD QTY IN GREEN SYSTEM IS HIGH. REMOVED GREEN HYDRAULIC POWER ACCUMULATOR PER AMM 29-11-42 PER
- [SDR CALA2023040601059](https://openairdocs.org/sdr/CALA2023040601059.md): Reservoir · low · Apr 6, 2023 · N429UA · Airbus A320232 · Hydraulic System, Main
  > G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD SERVICED GREEN HYD FLUID AND HEAD PRESSURE TO SERVICABLE LIMIT REF AMM 12-12-00. NO FAULTS NOTED
- [SDR CALA2022100702742](https://openairdocs.org/sdr/CALA2022100702742.md): Eiu · inoperative · Oct 7, 2022 · N429UA · Airbus A320232 · Fuel Control/Reciprocating Engines
  > ENG 1 FUEL VALVE FAULT ON CLIMBOUT UPDATED PICTURES UNABLE TO POWER UP FADEC 1 ON CHANNEL A OR B ALSO LOWER ECAM SWAPPED ENGINE EIU AND #1 ENGINE PARAMETERS WENT TO NORMAL AND ENGINE PAGE SHOWING BOTH A AND B IGNITION ON WITH ENGINE MASTER ABLE TO ACCESS #1 E
- [SDR CALA2022061001479](https://openairdocs.org/sdr/CALA2022061001479.md): None · leaking · Jun 10, 2022 · N429UA · Airbus A320232 · Hydraulic Pressure Indicator
  > ECAM CAUTION MESSAGE - Y ENG PUMP LO PR MESSAGE INOP - HYD REPLACED PTU MANIFOLD QUICK DISCONNECT FITTING O-RING M&E SERVICED YELLOW STSTEM HYD. 40-0595-3-1983, LEAK CHECK OK, MOTOR ENGINE PUMP PRESSURE NORMAL, CHECK ALL DPI AT FILTERS OK REF AMM 29-00-00-28
- [SDR CALA2021060200783](https://openairdocs.org/sdr/CALA2021060200783.md): Lock · inoperative · Jun 2, 2021 · N429UA · Airbus A320232 · Cargo/Baggage Doors
  > FWD CARGODOOR SHOWING OPEN LOCKED FOR POSITIVE FIX DO THE FUNCTIONAL CHECK OF FWD CARGO DOOR REF AMM 52-31-00-720-001A. UNLOCKING FOR FIX FORWARD CARGO DOOR INDICATION OPERATION CHECKED OK AFTER REPLACING DOOR LOCK PIN AND ADJUSTING LOCK PER WRITE UP 6391178(R
- [SDR CALA2019070801171](https://openairdocs.org/sdr/CALA2019070801171.md): Transceiver · malfunctioned · Jul 8, 2019 · N429UA · Airbus A320232 · Weather Radar System
  > WR R/T ERROR WHEN RADAR ON. TILT OFF 0.5 DEGBETWEEN CA AND FO REPLACED WX RADAR R/T IAW AMM 34-41-37, OP CKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1118613 SN OFF 3495 TRANSCEIVER, WX OFF 31-2311-9-0001 3495 ON 31-2311-9-0001 1225.
- [SDR CALA2019062401054](https://openairdocs.org/sdr/CALA2019062401054.md): Light · inoperative · Jun 23, 2019 · N429UA · Airbus A320232 · Escape Slide
  > R1 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A320 AMM 25-62-44- 000-802 AND 25-62-44-400-802.
- [SDR CALA2019062210988](https://openairdocs.org/sdr/CALA2019062210988.md): Skin · corroded · Jun 17, 2019 · N429UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > CORROSION ON STRUCTURE BETWEEN FR12-FR13, STR41L-39L AFTER REMOVAL OF SURFACE CORRISION ON SKIN THE REMAINING THICKNESS FOUND TO BE NOMINAL.079" IAW A320 SRM 53-11-11-283-001, REMOVED FABRICATED AND REPLACED STR 39L BETWEEN FR12-13 AND THE FWD GUSSET AT FR13
- [SDR CALA2019062210987](https://openairdocs.org/sdr/CALA2019062210987.md): Pressure Panel · cracked · Jun 17, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > LH AND RH SIDE PRESSURE PANELS BETWEEN FR 35 AND 36 HAVE MULTIPL E CRACKS IN FASTENER HOLES. INTERIM REPAIR ACCOMPLISHED TO LH AND RH FR 35-36 PRESSURE PANEL S PER ECRA 5331-02397 PART 1.
- [SDR CALA2019061400955](https://openairdocs.org/sdr/CALA2019061400955.md): Wire · broken · Jun 14, 2019 · N429UA · Airbus A320232 · Light System Wiring
  > EEPL HARNES, CONNECTOR 7260VC8, CONNECTING 31, 32, 34ABC, HAS BROKEN WIRES 6 IN. FROM SEAT CONNECTOR. REFER TO AA R N/R: 9819958. REMOVED AND REPLACED EEPL HARNESS CONNECTOR 7260VC8 IAW A-320 AM M 33-51-22-400-802-C. THRU STEP 4.(4)(E). PERFORMED OPS CHECK IA
- [SDR CALA2019060700904](https://openairdocs.org/sdr/CALA2019060700904.md): Flap · worn · Jun 6, 2019 · N429UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR OUTER DOOR HANDLE FLAP WORN. REFER TO AAR N/R: 9819940. REMOVED AND REPLACED L1 DOOR OUTER HANDLE FLAP I/A/W A320 CMM 52 -11-15-400-805, AND AMM''S 52-11-21-000-001, 52-11-21-400-001. HA NDLE ADJUSTMENTS ARE GOOD. DATA TRANSCRIBED FROM PAPER DOCUMENT A
- [SDR CALA2019060700898](https://openairdocs.org/sdr/CALA2019060700898.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMER EXIT HATCHES R AFT INTERIOR CRACKS ON R VE RT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT ON R/H AFT EMERGENCY E XIT DOOR, AND RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11- 911-001 AND ER 5100R01017 REV E.
- [SDR CALA2019060700897](https://openairdocs.org/sdr/CALA2019060700897.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMER EXIT HATCHES L AFT INTERI OR CRACK ON R VERT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT ON L/H AFT EMERGENCY E XIT DOOR, AND RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11- 911-001 AND ER 5100R01017 REV E.
- [SDR CALA2019060700895](https://openairdocs.org/sdr/CALA2019060700895.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMERGENCY EXIT DOORS, L/H AFT INTERIOR CRACKS ON L/H VERT FRAMES OTBD WINDOWS. REMOVED AND REPLACED L/H BEAM AND SEGMENT ON L/H AFT EMERGENCY E XIT DOOR, RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11-911- 001 AND ER 5100R01017 REV E.
- [SDR CALA2019060700894](https://openairdocs.org/sdr/CALA2019060700894.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMERGENCY EXIT DOORS L/H FWD INTERIOR CRACKS ON L/H VERT FRAMES OTBD WINDOW. REMOVED AND REPLACED L/H BEAM AND SEGMENT ON L/H FWD EMERGENCY E XIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECT ION IAW ER 5100R01017 REV E.
- [SDR CALA2019060700893](https://openairdocs.org/sdr/CALA2019060700893.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMER EXIT HATCHES L FWD INTERIOR CRACKS ON R VE RT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT L/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V923083
- [SDR CALA2019060700892](https://openairdocs.org/sdr/CALA2019060700892.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMER EXIT HATCHES, R FWD INTERI OR CRACKS ON R VERT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT R/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V903758
- [SDR CALA2019060700891](https://openairdocs.org/sdr/CALA2019060700891.md): Door Frame · cracked · Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, Structure
  > EMERGENCY EXIT DOORS R/H FWD I NTERIOR CRACK ON L/H VERT. FRAMES OTBD WINDOWS. REMOVED AND REPLACED L/H BEAM AND SEGMENT R/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V903758
- [SDR CALA2019060400880](https://openairdocs.org/sdr/CALA2019060400880.md): Skin · corroded · Jun 2, 2019 · N429UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > CORROSION FOUND I NSIDE SKIN AT FR 20 STR 28,29 RIGHT. REPAIRED CORROSION ON SKIN AT FR20 STR 28-29 RIGHT IAW ECRA 5331 -02395. THIS A PERMANINENT REPAIR NO FURTHER ACTION REQUIRED.
- [SDR CALA2019053100856](https://openairdocs.org/sdr/CALA2019053100856.md): Actuator · failed · May 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew Doors
  > (A3NB-52-3-6091) L-50 NO DOT--R1 DOOR DAMPER ACTUATOR FAILS DAMPING TEST REMOVED AND REPLACED R1 DOOR DAMPER CYLINDER ACTUATOR IAW MM''S 52-11-14-000-001, AND 52-11-14-400-001. CLEARANCE AND ADJUSTMENT OF PERCUSSION BELL CRANK FINGER ARE GOOD. PART TRANSACTION
- [SDR CALA2019053100855](https://openairdocs.org/sdr/CALA2019053100855.md): Actuator · failed · May 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew Doors
  > (A3NB-52-3-6091) L-28 NO DOT- R2 DOOR DAMPER ACTUATOR FAILED DAMPING CHECK REMOVED AND REPLACED R2 DOOR DAMPER ACTUATOR CYLINDER IAW A MM''S 52-13-14-000-001, AND 52-13-14-400-001. CLEARANCES AND ADJUSTMENT OF BELL CRANK FINGER ARE GOOD. PART TRANSACTION WAS A
- [SDR CALA2019053100854](https://openairdocs.org/sdr/CALA2019053100854.md): Actuator · failed · May 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew Doors
  > (A3NB-52-3-6091) L-28 NO DOT- L2 DOOR DAMPER ACTUATOR FAILS DAMPING CHECK REMOVED AND REPLACED L2 DOOR DAMPER ACTUATOR OR CYLINDER IAW AMM 52-13-14-000-001, AND 52-13-14-400-001. CLEARANCE AND BELL CRANK FINGER ADJUSTMENT ARE GOOD. THE PART TRANSACTION WAS ACC
- [SDR CALA2019051300768](https://openairdocs.org/sdr/CALA2019051300768.md): Wire Harness · damaged · May 13, 2019 · N429UA · Airbus A320232 · Light System Wiring
  > (SUPPORT TASK) THE EEPL HARNESS FOR SEAT ROWS 12 TO 22 IS DAMAGED. REFER TO N/R: 9819035. REMOVED AND REPLACED HARNESS FROM RACEWAY ON ROWS 12 TO 22 IAW AMM 33-51-22-000-801C1. OPS CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD NR 18-3351-1-4705 SEQ 545. WORK ACCOM
- [SDR CALA2019051300765](https://openairdocs.org/sdr/CALA2019051300765.md): Connector · damaged · May 13, 2019 · N429UA · Airbus A320232 · Light System Wiring
  > (SUPPORT TASK) THE EEPL HARNESS THAT CONNECTS TO 7260VC9 IS DAMAGED. REFER TO N/R: 9819037. REMOVED AND REPLACED CONNECTORS ON EEPL HARNESS 7260VC9 IAW ESPM 20-53-51 PB0201 CONFIG 01. OPS TEST TO BE ACCOMPLISHED ON CUSTOMER WORK CARD NR 18-3351-1-4705 SEQ 545.
- [SDR CALA2019051300763](https://openairdocs.org/sdr/CALA2019051300763.md): Wire Harness · damaged · May 13, 2019 · N429UA · Airbus A320232 · Light System Wiring
  > (SUPPORT TASK) THE EEPL HARNESS THAT CONNECTS TO 7260VC7 IS DAMAGED. REFER TO N/R: 9819036. REMOVED AND REPLACED HARNESS FROM RACEWAY THAT GOES TO 7260VC7 IAW AMM 33-51-22-000-801C1. OPS CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD NR 18-3351-1-4705 SEQ 545. DATA
- [SDR CALA2018120702503](https://openairdocs.org/sdr/CALA2018120702503.md): Oven · contaminated · Dec 3, 2018 · N429UA · Airbus A320232 · Buffet/Galleys
  > ACRID ELECTRICAL SMELLTHROUGHOUT CABIN AFTERTAKEOFF. RAN CHEKLI STRETURND TOAIRPORT PERFORMED SMOKE/ODOR IN CABIN INSPECTION REF AMM 05-51-10-200-801C. CREW COMPLETED SMOKE/ODOR FORM AND INFORMED M/X THAT SMELL BEGAN DURING TAKEOFF. PERFORMED IDENTIFICATION C
- [SDR CALA2018012600347](https://openairdocs.org/sdr/CALA2018012600347.md): Connector · not seated · Jan 26, 2018 · N429UA · Airbus A320232 · Light System Wiring
  > WHILE PERFORMING EMERGENCY SYSTEM TEST, RECEIVED AN EPSU BATTERY MESSAGE. RESEATED BATTERY CONNECTOR. TESTED GOOD.
- [SDR CALA2017111004019](https://openairdocs.org/sdr/CALA2017111004019.md): Wire · unsecure · Nov 10, 2017 · N429UA · Airbus A320232 · Light System Wiring
  > AISLE EMERGENCY LIGHT AT SEAT 30C HAS A WIRE EXTENDING INTO THE AILSEWAY. SECURED THE WIRING. OK FOR SERVICE.
- [SDR CALA2017110303926](https://openairdocs.org/sdr/CALA2017110303926.md): Connector · loose · Nov 3, 2017 · N429UA · Airbus A320232 · Light System Wiring
  > 30C EMERGENCY LITE CONNECTOR LOOSE REPAIRED LOOSE CONNECTOR AT SEAT 30C EMERGENCY LIGHT OPS CK NORMAL REF SWPM 20-42-01. VERIFIED REPAIR AT CONNECTOR AT SEAT 30C EMERGENCY LIGHT REF SWP M 20-42-01 AND GMM-09-10-05.
- [SDR CALA2017102303768](https://openairdocs.org/sdr/CALA2017102303768.md): Battery · failed · Oct 23, 2017 · N429UA · Airbus A320232 · Emergency Lighting
  > LEFT AND AFT EMERGENCY LIGHT BATTERYS FAIL CAPACITY CHECK. REMOVED AND REPLACED LEFT AND AFT EMERGENCY LIGHT BATTERYS REF AMM 33-51-38 PB401 OPS CHECK OK.
- [SDR CALA2017071402244](https://openairdocs.org/sdr/CALA2017071402244.md): Power Supply · faulty · Jul 14, 2017 · N429UA · Airbus A320232 · Emergency Lighting
  > EEPL ON SEATS, CENTER CABIN, ARE FLICKERING,. TROUBLESHOT, FOUND EPSU 11WL & OVERWING EMER LIGHT ASSY 60WL REMOVED AND REPLACED BOTH IAW MM 33-51-15-000-001A, 33-51-15-4 00-001A, 33-51-38-000-001A, 33-51-38-400-001A SYSTEM OPS CHECK GOOD IAW MM 33-51-00-710-00
- [SDR CALA2017081402663](https://openairdocs.org/sdr/CALA2017081402663.md): Skin · corroded · Jul 10, 2017 · N429UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE EXT SKIN AROUND LAVATORY E, EXHAUST HAS CORROSION. BLENDED CORROSION AROUND LAVATORY EXHAUST VENT, FOUND TO BE OUT OF LIMITS ORIGINAL.063 REMAINING.052 LOSS OF.011. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-41-11-300-004, PG 1-6,
- [SDR CALA2017071002123](https://openairdocs.org/sdr/CALA2017071002123.md): Door Sill · corroded · Jul 9, 2017 · N429UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN UNDER FLOOR STRUCTURE WITH LIGHT CORROSION AT R2 DOOR SILL BEAM UPPER FACE FRAME 69-2 INCHES AND STRINGER 23. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001, AND 51-42-11-001, REV 118.
- [SDR CALA2017051201381](https://openairdocs.org/sdr/CALA2017051201381.md): Wire Harness · loose · May 12, 2017 · N429UA · Airbus A320232 · Light System Wiring
  > FOUND EMERGENCY LIGHT HARNESS HANGING DOWN SEAT 38 ABC. REPLACED SEAT ROW HARNESS, SECURED HARNESS. OPS CHK GOOD FOR LIGHT ASSY.
- [SDR CALA2017020600292](https://openairdocs.org/sdr/CALA2017020600292.md): Battery · discharged · Feb 6, 2017 · N429UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED AT PTP PANEL. REPLACED BATTERY AT EPSU 10WL REF AMM 33-51-38 PB401, NOW OK FOR SERVICE.
- [SDR CALA2015111794839](https://openairdocs.org/sdr/CALA2015111794839.md): Pump · leaking · Nov 13, 2015 · N429UA · Airbus A320232 · Turbine Engine Oil System
  > ENGINE 2 SHUTDOWN DUE TO OIL LOSS. BEGAN AT FL340, PUT TO IDLE. AT 3 QTS ECAM, ENG SHUTDOWN. FOUND AREA AROUND OIL PUMP VERY WET. R & R ENG 2 OIL PRESS PUMP. OPERATIONS & LEAK CHECKED GOOD.

Next page: https://openairdocs.org/aircraft/N429UA/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 = 'N429UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N429UA/reports

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