# Service difficulty reports: N478UA

A list on [N478UA](https://openairdocs.org/aircraft/N478UA.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 2 · 95 reports

- [SDR CALA2026042815744](https://openairdocs.org/sdr/CALA2026042815744.md): Thrust Reverser · damaged · Apr 22, 2026 · N478UA · Airbus A320232 · Engine Thrust Reverser
  > ENG 1 REVERSER FAULT CLEARING THE RUNWAY, NR 1 ENG OTBD REVERSER WILL NOT FULLY STOW DUE TO BROKEN PLATE AND AFT BRACKET BROKE ON OTBD ACTUATOR ROD. LOCKED OUT HYDRAULIC CONTROL UNIT FOR NR 1 ENG THRUST REVERSER IAW AMM 78-30-00-040-013-A. LOWER TR ACTUATOR
- [SDR CALA2025123012528](https://openairdocs.org/sdr/CALA2025123012528.md): Light · damaged · Dec 28, 2025 · N478UA · Airbus A320232 · Emergency Lighting
  > ROW 31 EMERGENCY LIGHT LENS MISSING AND HOUSING CRACKED. REPLACED THE HOUSING IAW AMM 33-51-18. OPS CHKD NORMAL.
- [SDR CALA2025120511797](https://openairdocs.org/sdr/CALA2025120511797.md): Fuel Cap · missing · Dec 3, 2025 · N478UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. DEFERED ON LOG PAGE 7156404 FUEL CAP MISSING DEFERED ON LOG PAGE 7156404
- [SDR CALA2025101610182](https://openairdocs.org/sdr/CALA2025101610182.md): Fuel Cap · missing · Oct 15, 2025 · N478UA · Airbus A320232 · Fuel Storage
  > CREW REPORTED FUEL CAP IS MISSING. UNABLE TO LOCATE FUEL COUPLING CAP. REPLACED CAP REF APPLICABLE STEPS WITHIN AMM TASK 28-25-41.
- [SDR CALA2025090508514](https://openairdocs.org/sdr/CALA2025090508514.md): Lens · missing · Sep 4, 2025 · N478UA · Airbus A320232 · Emergency Lighting
  > FOUND MISSING ESCAPE PATH LIGHT LENS ON SEAT 25ABC. INSTALLED LENS COVER AS REQUIRED IAW AIPC 33-51-19.
- [SDR CALA2025082508081](https://openairdocs.org/sdr/CALA2025082508081.md): Power Supply · no test · Aug 22, 2025 · N478UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTING TESTS SHOWS THE FOLLOWING FAULTS: EPSU COMM FWD L, EPSU COMM AFT L, EPSU ARMED/ON EMER R, EPSU ARMED/ON L. T/S & FOUND FAULTY FWD ESPU 10WL IAW TSM 33-51-00-810-806A. REMOVED & REPLACED ESPU 10WL IAW AMM 3-51-38-000-001A & 33-51-3 4-400-00
- [SDR CALA2025061805652](https://openairdocs.org/sdr/CALA2025061805652.md): Ecs · odor · Jun 16, 2025 · N478UA · Airbus A320232 · Cabin Cooling System
  > BIRD STRIKE FWD OF RIGHT PACK INLET NO EVIDENCE VISIBLE IN PACK INLET DUCT, NEED TO RUN RIGHT PACK OFF APU BLEED TO ENSURE NO ODOR PRESENT REF LOG PAGE 5219952 FOR ECS SYSTEM LEVEL A DECONTAMINATION PER BIRD STRIKE INSPECTION PROCEDURES
- [SDR CALA2025041003674](https://openairdocs.org/sdr/CALA2025041003674.md): Battery · no test · Apr 9, 2025 · N478UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY FWD L MESSAGE ON EMERGENCY LIGHTS TEST REMOVED AND REPLACED ESPU BATTERY REF AMM 33-51-38. OKAY FOR SERVICE.PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024112002907](https://openairdocs.org/sdr/CALA2024112002907.md): Support Angle · damaged · Nov 18, 2024 · N478UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO, AT FR 62 S37L SUPPORT ANGLE HAS VISIABLE DAMAGE ()
- [SDR CALA2024112002906](https://openairdocs.org/sdr/CALA2024112002906.md): Support Angle · damaged · Nov 18, 2024 · N478UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO, AT FR 59 S37L SUPPORT ANGLE HAS VISIABLE DAMAGE.
- [SDR CALA2024070500145](https://openairdocs.org/sdr/CALA2024070500145.md): Thermostat · intermittent · Jul 3, 2024 · N478UA · Airbus A320232 · Engine Bleed Air System
  > AIR ENG2 BLEED ABNORM PR PFR AND BMC 2 BITE SHOWING: PRESS REG-V 4001HA2 OR SOL 10HA2 OR SENSE LINE. T/S REF TSM 36-11-00-810-810-A. PERFORMED LEAK CHECK ON THE #2 ENG PRV BRAIDED SENSE LINE AND RIGID LINES. NO LEAKS NOTED. PERFORMED HEALTH CHECK ON PRV 4001HA
- [SDR CALA2024052401577](https://openairdocs.org/sdr/CALA2024052401577.md): Fuel Cap · missing · May 22, 2024 · N478UA · Airbus A320232 · Fuel Storage
  > RAMP REPORTED FUEL CAP MISSING. NOTED TO TOMC. REF LP 8038451 - FUEL CAP LOCATED AND RE-INSTALLED.
- [SDR CALA2024011900155](https://openairdocs.org/sdr/CALA2024011900155.md): Fuel Cap · missing · Jan 14, 2024 · N478UA · Airbus A320232 · Fuel Storage
  > AIRCRAFT CAME IN WITH NO FUEL CAP. PLANE CAME IN WITH NO FUEL CAP. PLACE ON CDL 28A. AIRCRAFT CAME IN WITH NO FUEL CAP. PLACE ON CDL 28A. DISPATCH DESK: 8 NAME: BK DATE: 14-JAN-24- OK TO DEFER PER CDL 28A CAP, COUPLING R OFF 31-2825-9-0001 1481 ON 31-2825-9-00
- [SDR CALA2023021600468](https://openairdocs.org/sdr/CALA2023021600468.md): Safety Valve · unknown · Feb 16, 2023 · N478UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > GEAR WOULD NOT EXTENDNORMALLY. GRAVITY EXTPER ECAM. REPLACED PRIORITY VALVE, GREEN SYSTEM REF AMM 29-11-33. LEAK CHECKED NO HELP. GEARS AND GEAR DOORS WOULD NOT RETRACT. REPLACED HYD SYTEM SAFETY VALVE. NEED OPERATIONAL TEST. ACCOMPLISHED RII INSPECTION. REPLA
- [SDR CALA2022061701525](https://openairdocs.org/sdr/CALA2022061701525.md): Servo Control · failed · Jun 17, 2022 · N478UA · Airbus A320232 · Drag Control System
  > DIVERTED TO IAD DUE TO DCA HAVING AVAILABLE RUNWAY BELOW MINIMUM REQUIREMENT FOR MEL 2764R. SR MGR MC NEELEY NOTIFIED. SPOILER 3 INOP PLACED ON MEL. HAS HISTORY. DDP COMPLIED WITH. ADD EMP:U244875 PLACE NUMBER THREE SPOILER ON MAL. DDP COMPLIED WITH THIS IS
- [SDR CALA2022051801282](https://openairdocs.org/sdr/CALA2022051801282.md): None · cracked · May 18, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > (AD2020-20-05) DURING ROTO PROBE OF RH FR16 FOUND HOLES #A #B #C #8 & #9 WITH CRACK INDICATION ON THE FRAME LAYER REPAIR BEFORE NEXT FLIGHT. () REPAIRED RH FR16 HOLES A,B,C, 8 & 9 BY OVERSIZING & BUSHING INST ALLATION IAW EC/RA 5311-02807. ACCOMPLISHED BY EMP#
- [SDR CALA2022051601254](https://openairdocs.org/sdr/CALA2022051601254.md): None · cracked · May 15, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > (AD2020-20-05) DURING ROTO PROBE OF RH FR16 FOUND HOLES #A #B #C #8 & #9 WITH CRACK INDICATION ON THE FRAME LAYER REPAIR BEFORE NEXT FLIGHT. ()
- [SDR CALA2022051601248](https://openairdocs.org/sdr/CALA2022051601248.md): Skin · corroded · May 15, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > DURING HMV-3 CHECK AT VTMAE BFM CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LH S18 UPPER FUSELAGE SKIN BETWEEN FR69 & 70 STGR 1L & 2L. ECRA 5331-02902. WORK ACCOMPLISHED BY VTMAE EMP V934143. UPON AN INSPECTION OF THE UPPER SURFACE OF THE LH S18 UPPER FUSE
- [SDR CALA2022051601247](https://openairdocs.org/sdr/CALA2022051601247.md): None · cracked · May 15, 2022 · N478UA · Airbus A320232 · Fuselage Main, Structure
  > (AD2016-14-03) DURING ROTO PROBE OF FR35 STRINGER 28-31 FOUND LH S HOLE #2 CRACKED AND HOLE #4 WITH REJECTABLE DAMAGE. CONTACT EN GNEERING FOR REPAIR INSTRUCTIONS BEFORE FURTHER FLIGHT (REPAIR I AW R DWG & ECRA)
- [SDR CALA2022051301223](https://openairdocs.org/sdr/CALA2022051301223.md): None · none · May 12, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > AD2022-02-11 DURING ROTO PROBE LH FR16 DOOR STOP #7 FOUND HOLES #1 & #3 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYER. R EPAIR BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUIRE D) REPAIRED L/H FR16 DOOR STOP #7 HOLES #1 & #3 BY INTERCOSTAL REP
- [SDR CALA2022050901167](https://openairdocs.org/sdr/CALA2022050901167.md): None · corroded · May 6, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR53/FR59 STRG 42LH HAS CORROSION. DOT 52-43. () REMOVED CORROSION AT AFT CARGO PIT BETWEEN FR53-FR59 IAW SRM 51- 002. REMOVE AND REPLACED STRG 42LH BETWEEN FR53-FR60 IAW SRM 51- 74-00 AREA 1 BETWEEN FR53-5
- [SDR CALA2022050601154](https://openairdocs.org/sdr/CALA2022050601154.md): None · cracked · May 5, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > DURING HMV-3 CHECK AT VT MAE, PRODUCTION REPORTED CRACK INDICATION AT PRESSURE PANEL LAYER (LHS) ON HOLES #24 AND #26, ADDITIONALLY HOLES #5 THRU #12 WERE FOUND CRACKED. ON OR BEFORE AIRCRAFT 4278 ACCUMULATES 80,400 TOTAL FLIGHT CENTER FUSELAGE PRESSURE DECK M
- [SDR CALA2022042701090](https://openairdocs.org/sdr/CALA2022042701090.md): Structure · cracked · Apr 27, 2022 · N478UA · Airbus A320232 · Fuselage Floor Panel
  > (A3NB-52-4-6031) MIDDLE FUSELAGE, EMERGENCY EXIT AFT RH, INTERNA L STRUCTURE HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT 132-93 () REMOVED AND REPLACED DAMAGED SEGMENT ANGLE P/N D5227902620551 BA TCH #0003925895 IAW SRM 57-42-11, & DWG 52279010. ACCOMPLISHED
- [SDR CALA2022042701081](https://openairdocs.org/sdr/CALA2022042701081.md): Angle · cracked · Apr 26, 2022 · N478UA · Airbus A320232 · Fuselage Floor Panel
  > (A3NB-52-4-6031) MIDDLE FUSELAGE, EMERGENCY EXIT AFT RH, INTERNA L STRUCTURE HAS CRACK AT RH LOAD TRANSMITTING PROFIL. DOT 132-93 () REMOVED AND REPLACED DAMAGED SEGMENT ANGLE P/N D5227902620551 BA TCH #0003925895 IAW SRM 57-42-11, & DWG 52279010. ACCOMPLISHED
- [SDR CALA2022042101042](https://openairdocs.org/sdr/CALA2022042101042.md): Stringer · corroded · Apr 20, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKED
- [SDR CALA2022042101041](https://openairdocs.org/sdr/CALA2022042101041.md): Frame · cracked · Apr 20, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > (AD2022-02-11) DURING ROTO PROBE RH FR20 DOOR STOP #7 FOUND HOLE #1 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYERS. REPAI R BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUIRED) REPAIRED RH FR20 DOOR STOP #7 HOLE #1 BY INTERCOSTAL REPLACEMENT &
- [SDR CALA2022042101039](https://openairdocs.org/sdr/CALA2022042101039.md): Frame · cracked · Apr 20, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > (AD2022-02-11) DURING ROTO PROBE RH FR16 DOOR STOP #7 FOUND HOLE S #1 & #3 WITH CRACK INDICATIONS IN INTERCOSTAL AND FRAME LAYERS REPAIR BEFORE NEXT FLIGHT (REPAIR IAW R53113118 & ECRA AS REQUI RED) REPAIRED RH FR16 DOOR STOP #7 HOLE''S 1 & 3 BY INTERCOSTAL RE
- [SDR CALA2022042101038](https://openairdocs.org/sdr/CALA2022042101038.md): Beam · corroded · Apr 20, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN BEAM STRUCTURE HAS CORR OSION BETWEEN FR 17 & 18 Y254 DOT 132-96 () REMOVED FLOOR BEAM AND REPLACED P/N D5311281820401, BATCH 003938 281 IAW SRM 51-42-11, AND RESTORE SURFACE PROTECTION IAW 51-21-1 1. ACCOMPLISHED BY EM
- [SDR CALA2022041801014](https://openairdocs.org/sdr/CALA2022041801014.md): Frame · corroded · Apr 18, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR64/FR65 STRG 43RH HAS CORROSION. DOT 52-36 () REMOVED CORROSION IAW 320 SRM 51-74-00 AND FOUND OUT OF LIMITS I BY EMP#V933870 AT BFM ST AEROSPACE MOBILE. NR#0027407 AW SRM 53-41-13-300-004 FIG 001 CHECKED
- [SDR CALA2022041801010](https://openairdocs.org/sdr/CALA2022041801010.md): Bonding Plate · broken · Apr 17, 2022 · N478UA · Airbus A320232 · Elevator Control System
  > (A3NB-55-3-6005) LH HORIZONTAL STABILIZER, ELEVATOR HINGE FITTIN G N.5 HAS PLATE BONDING BROKEN. DOT 132-134() REMOVED BONDING PLATE IAW SRM 51-42-11. FABRICATED NEW BONDING P.07 MILLIOHMS IAW AMM 20-28-00 T91450. ACCOMPLISHED BY EMP#V9347 LATE IAW DRAWING #D
- [SDR CALA2022041100952](https://openairdocs.org/sdr/CALA2022041100952.md): Frame · cracked · Apr 10, 2022 · N478UA · Airbus A320232 · Fuselage Main, Frame
  > (EA 5340-01724 REV C) FRAME 68 LH DOOR STOP FITTING #1 LOWER I/B HOLE CRACK INDICATION AT 6 O''CLOCK IN THE FRAME. () WASHER, THIS TASK IS CATEGORY B. I AW SRM 53-41-12-300-010. REI W SRI 53-41-12-205-009 INSP THRESHOLD FROM TIME OF ADL/REPAIR EM TERVALS 1070
- [SDR CALA2022040600906](https://openairdocs.org/sdr/CALA2022040600906.md): Seat Track · corroded · Apr 6, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN SEAT TRACK HAS CORROSIO N AT FR 20 -Y765 DOT 132-99() EVALUATED BLENDING OUT IAW SRM 51-42-15 FOUND TO BE OUT OF LIMIT S AND REMOVED AND INSTALL NEW SEAT TRACK -Y765 FR20 ON FLOOR CAB IN IAW SRM 51-42-11/001. ACCOMPLISH
- [SDR CALA2022040600905](https://openairdocs.org/sdr/CALA2022040600905.md): None · corroded · Apr 6, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN STRUCTURE HAS CORROSION AT FR20 DOT 132-98() BLEND OUT AREA AT MAIN CABIN STR FR20 -Y1588 ORG. THICKNESS 0.07 6 AND INSTALLED FLOOR CABIN WEB IAW SRM 51-42-1144-008. ACCOMPLI 1", MAT REMOVED 0.020, MAT REMAINING 0.051"
- [SDR CALA2022040400871](https://openairdocs.org/sdr/CALA2022040400871.md): Floor Support · corroded · Apr 3, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN STRUCTURE HAS CORROSION AT FR20 DOT 132-98() BLEND OUT AREA AT MAIN CABIN STR FR20 -Y1588 ORG. THICKNESS 0.07 6 AND INSTALLED FLOOR CABIN WEB IAW SRM 51-42-1144-008. ACCOMPLI 1", MAT REMOVED 0.020, MAT REMAINING 0.051"
- [SDR CALA2022040400870](https://openairdocs.org/sdr/CALA2022040400870.md): Beam · corroded · Apr 3, 2022 · N478UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6049) MAIN CABIN, FLOOR CABIN SEAT TRACK HAS CORROSIO N AT FR 20 -Y765 DOT 132-99() EVALUATED BLENDING OUT IAW SRM 51-42-15 FOUND TO BE OUT OF LIMIT S AND REMOVED AND INSTALL NEW SEAT TRACK -Y765 FR20 ON FLOOR CAB IN IAW SRM 51-42-11/001. ACCOMPLISH
- [SDR CALA2022033100825](https://openairdocs.org/sdr/CALA2022033100825.md): None · none · Mar 29, 2022 · N478UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR56/FR57 STRG 40RH HAS CORROSION. REPLACED AFT CARGO PIT BETWEEN FR56 TO FR58 STR 40RH IAW A320 SR M 51-42-11 AND SRM 51-72-11-911-001. P/N:D5347552623400 BTCH:000 3865486 AT BFM ST AEROSPACE MOBILE. NR#00
- [SDR CALA2022032800810](https://openairdocs.org/sdr/CALA2022032800810.md): Stringer · corroded · Mar 28, 2022 · N478UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (A3NB-53-4-6179) AFT CARGO PIT UNDERFLOOR BAY BETWEEN FR56/FR57 STRG 40RH HAS CORROSION. REPLACED AFT CARGO PIT BETWEEN FR56 TO FR58 STR 40RH IAW A320 SR M 51-42-11 AND SRM 51-72-11-911-001. P/N:D5347552623400 BTCH:000 3865486 AT BFM ST AEROSPACE MOBILE. NR#00
- [SDR CALA2022032800802](https://openairdocs.org/sdr/CALA2022032800802.md): Bonding Plate · damaged · Mar 28, 2022 · N478UA · Airbus A320232 · Elevator Control System
  > (A3NB-55-3-6005) LH HORIZONTAL STABILIZER, ELEVATOR HINGE FITTIN G N.5 HAS PLATE BONDING BROKEN. DOT 132-134() REMOVED BONDING PLATE IAW SRM 51-42-11. FABRICATED NEW BONDING P.07 MILLIOHMS IAW AMM 20-28-00 T91450. ACCOMPLISHED BY EMP#V9347 LATE IAW DRAWING #D
- [SDR CALA2019120302133](https://openairdocs.org/sdr/CALA2019120302133.md): Battery · failed · Nov 28, 2019 · N478UA · Airbus A320232 · Emergency Lighting
  > DURING TEST FND ESPU BATT 13WL LOW VOLTAGE. REPLACED 13WL ESPU BATTERY PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33-51-38-000-002 REV.103, AMM 33-51-38-400-002 REV103 AMM 33-51-00-710-001 REV.103.
- [SDR CALA2019120302132](https://openairdocs.org/sdr/CALA2019120302132.md): Battery · failed · Nov 28, 2019 · N478UA · Airbus A320232 · Emergency Lighting
  > DURING TEST FND ESPU BATT 12WL LOW VOLTAGE REF ROUTINE NO. 9491373 - ORIGINATED BY EMP V924351, SPEC NO.A3NB-33-3-6012 PERFORMED BY EMP V924351, PERFORMED REPLACEMENT OF 12WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33
- [SDR CALA2019120302131](https://openairdocs.org/sdr/CALA2019120302131.md): Battery · failed · Nov 28, 2019 · N478UA · Airbus A320232 · Emergency Lighting
  > CAB ESPU 10WL BATTERY FOUND LOW VOLTAGE REF ROUTINE NO.9490827 - ORIGINATED BY EMP V905504, SPEC NO.A3NB-24-3-6062. PERFORMED BY EMP V924351, REPLACED 10WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33 -51-38-000-002 REV
- [SDR CALA2019120302130](https://openairdocs.org/sdr/CALA2019120302130.md): Battery · failed · Nov 28, 2019 · N478UA · Airbus A320232 · Emergency Lighting
  > DURING TEST FND ESPU BATT 11WL LOW VOLTAGE REF ROUTINE NO. 9491372 - ORIGINATED BY EMP V924351, SPEC NO.A3NB-33-3-6012. PERFORMED BY EMP V924351,REPLACED 11WL ESPU BATT PACK AND PERFORMED BITE TEST OF ESPU THE RESULT FND ''SATIS'' AS PER AMM 33 -51-38-000-002
- [SDR CALA2019053100864](https://openairdocs.org/sdr/CALA2019053100864.md): Release Cable · frayed · May 30, 2019 · N478UA · Airbus A320232 · Emergency Exits
  > REF. N/R: 9459059 LEFT OVERWING EMERGENCY EXIT MANUAL RELEASE CABLE FWD AND AFT HAVE FRAYED WIRES. DATA WAS TRANSCRIBED FROM PAPER DOCUMENT N/R 9459059 WORK ACCOMPLISHED BY MECHANIC INSPECTED BY QC REMOVED AND INSTALLED NEW MANUAL RELEASE SLIDE CABLE ASSY LEFT
- [SDR CALA2018011200174](https://openairdocs.org/sdr/CALA2018011200174.md): Warning Light · false activation · Jan 12, 2018 · N478UA · Airbus A320232 · Door Warning System
  > DOOR AFT EMERGENCY EXIT ECAM ILLUMINATED TWICE WHILE AT CRUISE, 370 AND DISAPPEARED. CABIN PRESSURE FINE, COULD NOT DUPLICATE PROBLEM. PERFORMED A GV INSPECTION OF EXTERIOR AND INTERIOR EMERGENCY HATCH, NO FAULTS FOUND. REMOVED HANDLE COVER AND INSPECTED
- [SDR CALA2017063002062](https://openairdocs.org/sdr/CALA2017063002062.md): Cover · loose · Jun 30, 2017 · N478UA · Airbus A320232 · Emergency Lighting
  > LEFT DOOR FWD EMERGENCY EXIT FOUND LOOSE. SECURED THE EMERGENCY EXIT COVER.
- [SDR CALA2015070994071](https://openairdocs.org/sdr/CALA2015070994071.md): Unknown · malfunctioned · Jul 8, 2015 · N478UA · Airbus A320232 · Emergency Lighting
  > FORWARD EMER LIGHTS FAILED TO COME ON WHEN ACFT LOST POWER AT THE GATE. ACCOMPLISHED BITE OF FWD EPSU IAW AMM 33-51-38. ACCOMPLISHED EMER LIGHT TEST OF ENTIRE CABIN OF ATTENDANT PTP PANEL. EMER LIGHTS TESTS PASSED.
- [SDR CALA2014122692866](https://openairdocs.org/sdr/CALA2014122692866.md): Engine · malfunctioned · Dec 21, 2014 · N478UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > NUMBER 2 ENG OIL QTY LOW & DECREASING EVENTUALLY TO ZERO. PRESS & TEMP GOOD. ENG SHUTDOWN INFLIGHT. SUSPECTED ENG OIL PUMP HOUSING FAILURE. NR 2 ENG R & R. ACCOMPLISHED AMM TASK 72-00-00-200-021-BM INFLIGHT SHUTDOWN PROCEDURE.
- [SDR CALA2014021390372](https://openairdocs.org/sdr/CALA2014021390372.md): Sill · corroded · Feb 12, 2014 · N478UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L1 DOOR SILL BENEATH AFT GIRT BAR ATTACH FITTING HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH TWO EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.
- [SDR CALA2014021390371](https://openairdocs.org/sdr/CALA2014021390371.md): Sill · corroded · Feb 12, 2014 · N478UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R1 DOOR SILL BENEATH FWD & AFT GIRT BAR ATTACH FITTINGS HAS BEEN REPAIRED IAW SRM 53-11-14 FIG 208 WITH FOUR EACH BUSHINGS & REPAIR WASHERS DUE TO CORROSION.
- [SDR CALA2014021090336](https://openairdocs.org/sdr/CALA2014021090336.md): Stringer · corroded · Feb 7, 2014 · N478UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 42 RT HAS CORROSION BETWEEN FRAME 63 &64. REPLACED STRINGER IAW A320 SRM 51-42-11 PG 24 NR 21308.

Next page: https://openairdocs.org/aircraft/N478UA/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 = 'N478UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N478UA/reports

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