# Service difficulty reports: N488UA

A list on [N488UA](https://openairdocs.org/aircraft/N488UA.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 · 105 reports

- [SDR CALA2026081418631](https://openairdocs.org/sdr/CALA2026081418631.md): Battery · discharged · Aug 13, 2026 · N488UA · Airbus A320232 · Emergency Equipment
  > COCKPIT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. REMOVED AND REPLACED COCKPIT EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-65-98.
- [SDR CALA2026032714859](https://openairdocs.org/sdr/CALA2026032714859.md): Skin · contaminated · Mar 24, 2026 · N488UA · Airbus A320232 · Elevator Structure
  > LH TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 12 INCHES FROM I/B EDGE AND 14 INCHES FROM T/E DEFECT IS 1 INCH DIA. IN SI ZE. REPAIRED L/H ELEVATOR TOP SKIN 12IN FROM I/B 14IN FROM T/E 1.38I N DIG ZONE A IAW SRM 55-21-11-300-004 CATEGORY A REPAIR.
- [SDR CALA2026032314762](https://openairdocs.org/sdr/CALA2026032314762.md): Skin · damaged · Mar 22, 2026 · N488UA · Airbus A320232 · Horizontal Stabilizer, Plate/Skin
  > LEFT TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 154.5 INCH ES FROM INBD EDGE AND 9 INCHES FROM T/E. DEFECT IS 1 INCH DIA. IN SIZE. REPAIRED LT ELEVATOR TOP SKIN 154.5 IN FROM INBD 9IN FROM T/E 1. 25IN DIA ZONE A IAW SRM 55-21-11-300-004, CATEGORY A RE
- [SDR CALA2026031914685](https://openairdocs.org/sdr/CALA2026031914685.md): Door Sill · corroded · Mar 16, 2026 · N488UA · Airbus A320232 · Fuselage Main, Structure
  > AFT MAIN CABIN FLOOR STRUCTURE R-2 DOOR SILL CORROSION BETWEEN G IRT BAR FITTINGS. REMOVED AND REPLACED R2 DOOR SHAPE SILL (CENTER) IAW SRM 51 -42-11.
- [SDR CALA2026040114989](https://openairdocs.org/sdr/CALA2026040114989.md): Door Sill · corroded · Mar 12, 2026 · N488UA · Airbus A320232 · Fuselage Main, Structure
  > R2 DOOR SILL AT FR68 HAS CORROSION AROUND NUTPLATE FASTENER HOLE. GENERATED BY V061680 ON AAR LCQ NR 9296398/24398 ESFR COMPLETED REPAIRED DOOR SILL AT FR68 R2 DOOR IAW A320 SRM 53-41-14-300-001 ACMP BY MECH V061742 INSP BY V077960 RII INSP C/W AAR QC LC-30
- [SDR CALA2026030514337](https://openairdocs.org/sdr/CALA2026030514337.md): Shear Panel · corroded · Mar 2, 2026 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN LT SHEAR WEB AT FR 69 - FR 70 WAS CORRODED. REPLACED THE LT SHEAR WEB IAW SRM 51 -72-11, AND SRM 51-42-11.
- [SDR CALA2026030514335](https://openairdocs.org/sdr/CALA2026030514335.md): Floor Support · corroded · Mar 2, 2026 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN FLOOR STRUCTURE CORRODED RT FLOOR SUPPORT, Y -1162.5 AT FR 66. REMOVED AND REPLACED RT FLOOR SUPPORT IAW SRM 51-72-11-911-001.
- [SDR CALA2026030314242](https://openairdocs.org/sdr/CALA2026030314242.md): Door Frame · cracked · Feb 28, 2026 · N488UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT FWD EMERGENCY EXIT DOOR VERTICAL FRAME, FOUND SEVERAL CRACKS IAW AAR LCQ N/R 9296297/24297. REMOVED AND INSTALLED THE VERTICAL FRAME IAW SRM AND DWG 1I D522-79040.
- [SDR CALA2025120511785](https://openairdocs.org/sdr/CALA2025120511785.md): Battery Pack · no test · Dec 3, 2025 · N488UA · Airbus A320232 · Emergency Lighting
  > DURING THE EMERGENCY LIGHTING TEST USING PTP 110RH, RECIEVED FAULT EPSU UNIT FWD LT. REPLACED EPSU BATTERY AT L1 DOOR IAW AMM 33-51-38. OP CHECKED GOOD.
- [SDR CALA2025091608963](https://openairdocs.org/sdr/CALA2025091608963.md): None · no discrepancy · Sep 12, 2025 · N488UA · Airbus A320232 · Standard Practices/Structures
  > BIRDSTRIKE ON T/O LEFT WINDSCREEN HOT BRAKES FROM RTO 440 DEGREES. ACP BIRDSTRIKE PER AMM 05-51-14-200-803. ACP'D BIRDSTRIKE INSP OF AIRFRAME AND ENGS PER AMM 05-51-14. NO DAMAGE NOTED.
- [SDR CALA2025090908667](https://openairdocs.org/sdr/CALA2025090908667.md): Battery · no test · Sep 8, 2025 · N488UA · Airbus A320232 · Emergency Lighting
  > CABIN EMER LIGHTING OPS CHK FAIL REPLACE LT EPSU BATTERY REPLACED LT EPSU IAW 33-51-38-400-002-A OPS CHK PASSED.
- [SDR CALA2025043004341](https://openairdocs.org/sdr/CALA2025043004341.md): Bottle · none · Apr 28, 2025 · N488UA · Airbus A320232 · Escape Slide
  > DOOR 2L SLIDE PRESSURE INDICATOR SHOWING LOW PRESSURE. CHECK DOOR 2L SLIDE PRESSURE INDICATOR AT DOOR. NEEDLE IS ON THE LINE DIVIDING AREA A AND AREA B. THE NEEDLE IN AREA B, WHICH IS HALF THE RANGE OF AREA A, SHOWS A PRESSURE LEVEL THAT CAN BE ACCEPTED PER
- [SDR CALA2025021902379](https://openairdocs.org/sdr/CALA2025021902379.md): Slide · faulty · Feb 16, 2025 · N488UA · Airbus A320232 · Escape Slide
  > REPLACED DOOR 2 LEFT EVACUATION SLIDE ASSY PER JOB CARD 31-2561-9-0015 REPLACED DOOR L2 EVACUATION SLIDE ASSY. SER # OFF 7468. SER# ON 7104. REF AMM 25-62-44.PARTS USED: 31-2561-9-0015, QTY:1. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1565986 SN OFF 7468.SLI
- [SDR CALA2025012702057](https://openairdocs.org/sdr/CALA2025012702057.md): Bypass Valve · faulted · Jan 25, 2025 · N488UA · Airbus A320232 · Cabin Temperature Control System
  > LOST/CABIN TEMP CONTROL TALKED TO INBOUND FLIGHT CREW, THERE WAS NO ISSUES WITH BLEED AIR OR AIR FLOW FROM VENTS AND GASPERS. CREW UNABLE TO CONTROL TEMPERTURE WITH ZONE SELECT SWITCHES. ACCOMPLISHED TSM 21-61-00-810-905-A NO ISSUES, SEE LOG PAGE 3659407. FOUN
- [SDR CALA2025010301771](https://openairdocs.org/sdr/CALA2025010301771.md): Lanyard · out of position · Jan 1, 2025 · N488UA · Airbus A320232 · Emergency Equipment
  > DOOR 1L/INDICATOR ON FLO OR POSSIBLY NOT GETTING TO FULL ARM PO SITION. FOUND LANYARD MATERIAL OBSTRUCTING GIRT BART TRAVEL. STOWED LANYARD IN PLACE. CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES. ARMED AND DISARMED DOOR SEVERAL TIMES ALSO. DOOR INDICATION NORMAL
- [SDR CALA2023120103506](https://openairdocs.org/sdr/CALA2023120103506.md): Relay · faulty · Nov 28, 2023 · N488UA · Airbus A320232 · Flight Control System
  > SIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL RESETTING SECS AND GRD SCAN CHECKS OK. TSM CALLS OUT TO CHANGE RELAYS 47CE1 AND 47CE2. SECOND HIT AND DOES HAVE SEC HISTORY. SEE TSM 27-92-00-810-830AH FLT WAS RTO. FO FLYING AND HAD STICK NOSE DOWN AN
- [SDR CALA2023090802738](https://openairdocs.org/sdr/CALA2023090802738.md): Slide · unwanted deploy · Aug 25, 2023 · N488UA · Airbus A320232 · Escape Slide
  > DEPLOYED OVERWING SLIDE ON AIRCRAFT LEFT. PICS OF DEPLOYED SLIDE. REMOVED LH OFFWING SLIDE INFLATION RESERVOIR REF AMM 25-62-46-000-001-A. INFLATION RESERVOIR REMOVED PLACED IN AFT CGO PIT LT O/W WING SLIDE REMOVED REF AMM 25-62-42-000-002-A. BOTTLE, ASSY, O O
- [SDR CALA2023082102595](https://openairdocs.org/sdr/CALA2023082102595.md): Stringer · corroded · Aug 20, 2023 · N488UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CRG LH SIDE FR59- STRG-30 CORRODE, REQUIRES FURTHER EVALUATION. AS NOTED ON LTPR NR#5001249722-0010. HEET 2. WORK PERFORMED ON LTPR NR# 5001249722-0010. THIS REPAIR 205-001, TABLE 004. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR SUBSEQUENT INSPECTION AT I
- [SDR CALA2023081602516](https://openairdocs.org/sdr/CALA2023081602516.md): Battery · no test · Aug 14, 2023 · N488UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250321-0010. BATTERY REPLACEMENT OF (13WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-3-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INFO
- [SDR CALA2023081602515](https://openairdocs.org/sdr/CALA2023081602515.md): Battery · no test · Aug 14, 2023 · N488UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250432-0010. BATTERY REPLACEMENT OF (12WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INF
- [SDR CALA2023081602514](https://openairdocs.org/sdr/CALA2023081602514.md): Battery · no test · Aug 14, 2023 · N488UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250322-0010. BATTERY REPLACEMENT OF (10WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INF
- [SDR CALA2023081602513](https://openairdocs.org/sdr/CALA2023081602513.md): Battery · no test · Aug 14, 2023 · N488UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250423-0010. BATTERY REPLACEMENT OF (11WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INF
- [SDR CALA2023050801411](https://openairdocs.org/sdr/CALA2023050801411.md): Unknown · unknown · May 8, 2023 · N488UA · Airbus A320232 · Flight Control System
  > C/B TRIPPED R ELEC BAY FOUND 16CE2 ELAC 2 STBY SPLY ON 105VU POPPED.RESET C.B. UPDATED LABOR HOURS TOMC REQUESTED TO HAVE CB REPLACED AS A PRECAUTION. BREAKER P/N REF AMM 27-93-00, PERFORMED OPERATIONAL CHECK OF ELAC 2. C.B. EN2995-004A7A5A M&E # 18-2424-3-00
- [SDR CALA2022060201422](https://openairdocs.org/sdr/CALA2022060201422.md): Tube · loose · Jun 2, 2022 · N488UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > HYDRAULIC QUANTITY LOW LEFT OR GREEN SYSTEM GREEN LO LVL ON ARRIVAL FOUND B NUT AT BOTTOM OF GREEN ACCUMULATOR LEAKING AS INDICATED BY MISS ALLIGNED WITNESS STRIPE. TIGHTENED B NUT, SERVICED HYDRAULICS. OPERATED HYDRAULIC SYSTEM. NO LEAKS NOTED.
- [SDR CALA2021092801719](https://openairdocs.org/sdr/CALA2021092801719.md): Fuel Cap · missing · Sep 28, 2021 · N488UA · Airbus A320232 · Aircraft Fuel System
  > PDA 1 LANYARD MISSING FROM FUEL CAP. OPBLM CHRISTIANSEN ITEM ENTEREDIN CCL 28A. OPBLM CHRISTIANSEN
- [SDR CALA2021092801718](https://openairdocs.org/sdr/CALA2021092801718.md): Lanyard · missing · Sep 28, 2021 · N488UA · Airbus A320232 · Aircraft Fuel System
  > RIGHT SIDE FUEL CAPLANYARD MISSINGFUEL CAP SECURE CURTIS, ZACHERY (V927339)VERIFIED NO LEAKS AT SPR COUPLING PER CDL 28A PROCEDURES.OPBLM CHRISTIANSEN. DISPATCH DESK: 01 NAME: CR DATE: 26-SEP-21- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE F
- [SDR CALA2021081601344](https://openairdocs.org/sdr/CALA2021081601344.md): Handle · binding · Aug 15, 2021 · N488UA · Airbus A320232 · Trailing Edge Flap Control System
  > FLAP HANDLE BINDING ON FLAP RETRACTION. REMOVED AND REPLACED FLAP AND SLAT CONTROL LEVER REF AMM 27-51-43. OPS CHECK GOOD REMOVED AND REPLACED FLAP/SLAT COMMAND SENSOR UNIT REF AMM 27-51-17. OPS CHECK GOOD ROTABLE PARTS CHANGE WAS INDICATED - TT # 1999483 SN
- [SDR CALA2021080901304](https://openairdocs.org/sdr/CALA2021080901304.md): Cover · missing · Aug 9, 2021 · N488UA · Airbus A320232 · Trailing Edge Flaps
  > PDA 3 LEFT WING #4 FLAP FAIRING 533CB MISSING BOLT COVER ON I/B SIDE. SEE PHOTO. REQUEST CDL. DISPATCH DESK: 34 NAME: SB.DATE: 07-AUG-21- APPROVED CDL 27AD APPLIED CDL. SEE AMM 57-55-11-400-001-A. STEP 4. B. (7) (E). RETAINER 59 AND PUSH-FIT COVER 45. REQUI
- [SDR CALA2021080401256](https://openairdocs.org/sdr/CALA2021080401256.md): Valve · failed · Aug 4, 2021 · N488UA · Airbus A320232 · Turbine Engine Oil System
  > ENG2 BEARING 4 OIL SYSHI PRESS ECAM ON CLIMBOUT OF ORD.ECAM WENT AWAYAFTER A FEW MINUTES. RELATED CLM ARE "CHECK HARNESS OR CHANGE VALVE 4006EN (ENG 2)" AND "CHECK N4 BRG SCAV PRESSXMTR2 CITCUIT 4005 EN. AS WELL AS A RELATED "ENG 2 EIU" FAULT. TROUBLESHOOT PER
- [SDR CALA2021070501020](https://openairdocs.org/sdr/CALA2021070501020.md): Skin · corroded · Jul 3, 2021 · N488UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE CROWN IN AREA COVERED BY VERT LWR L/E FAIRING AT BASE O F VERT STAB (2 EA) COAX CABLES CORROSION AT SKIN ON HAECO LCQ RE F 9294543/24543 A3NB-53-3-6208. NR GENERATED BY N079592 REPAIR AT FUSELAGE CROWN BASE OF VERT STAB FR69-70 STR 2R-2L ACC OMPLISHED
- [SDR CALA2021070101014](https://openairdocs.org/sdr/CALA2021070101014.md): Frame · cracked · Jul 1, 2021 · N488UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FRAME 35 AT S30L NR 2 HOLE CRACK INDICATION A3NB-53-3-6315 PER HA ECO LCQ NR 9294502/24502. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5331-02733. REAMED THE LH FRAME 35 AT STR30 #2 HOLE TO.4687. ACCOMPLISH INITIAL INSPECTION AT LH FR35 STR30 HOLE #
- [SDR CALA2021070101009](https://openairdocs.org/sdr/CALA2021070101009.md): Skin · cracked · Jun 30, 2021 · N488UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > AFT PIT LT FRAME 61 CRACK INDICATION NOTED IN THE VERTICAL WEB OF THE FRAME AT LT STRINGER 37. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01251. REAMED THE EFFECTED HOLE IN THE AFT PIT LH FRAME 61 VERTICAL WEB OF THE FRAME AT LH STRINGER 37 TO.190. A
- [SDR CALA2021062300940](https://openairdocs.org/sdr/CALA2021062300940.md): Stop Fitting · cracked · Jun 22, 2021 · N488UA · Airbus A320232 · Fuselage Main, Structure
  > R1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBOARD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING AT 6:00. INTERIM REPAIR ACCOMPLISH IAW PART 1 OF ECRA 5311-02584. REPLACED THE R1 DOOR FRAME STOP #7 INTERCOASTAL FITTING IAW ECRA 5311-02584. ACCOMPLISH INIT
- [SDR CALA2021062000904](https://openairdocs.org/sdr/CALA2021062000904.md): Intercostal · cracked · Jun 18, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > PER NR 9294472/24472 L1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING. "REPAIR BEFORE NEXT FLIGHT", CONTACT ENGINEERING FOR APPROVED REPAIR IN STRUCTIONS. GENERATED BY V061633. REPAIR ON LH FR16 DOOR STOP FITTI
- [SDR CALA2021061800891](https://openairdocs.org/sdr/CALA2021061800891.md): Floor Support · corroded · Jun 17, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > PER NR 9294698/24698. AFT PUT BETWEN FR63-64 LEFT STR42L HAS CORROSION. REPLACED DAMAGED SECTION OF S42L BETWEEN FR 62-64 IAW SRM 53-00-13-300-001. SUPPLEMENTAL INSPECTIONS REQUIRED IAW SRI 53-00-13-205-001 BEGINNING AT 60000FC OR 120000FH FROM REPAIR EMBODI
- [SDR CALA2021061500883](https://openairdocs.org/sdr/CALA2021061500883.md): Stringer · corroded · Jun 15, 2021 · N488UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT PUT BETWEN FR63-64 LEFT STR42L HAS COR ROSION. REPLACED DAMAGED SECTION OF S42L BETWEEN FR 62-64 IAW SRM 53-00-13-300-001. SUPPLEMENTAL INSPECTIONS REQUIRED IAW SRI 53-00-13-205-001 BEGINNING AT 60000FC OR 120000FH FROM REPAIR.
- [SDR CALA2021060400788](https://openairdocs.org/sdr/CALA2021060400788.md): Shear Tie · corroded · Jun 3, 2021 · N488UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > PER NR 9294611/24611. AFT CABIN SHEAR TIE FR70 STGR 23R HAS CORR OSION. GENERATED BY N078570. UPON EVAL OF SHEAR TIE AT FR70 STR 23-25R FOUND TO BE OUT OF LIM ITS. REMOVED, FABRICATED AND ISNTALLED SHEAR TIE IAW A320 SRM 51 -72-11, 51-44-11, 51-42-11. MECH V06
- [SDR CALA2021060400787](https://openairdocs.org/sdr/CALA2021060400787.md): Shear Panel · corroded · Jun 2, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH SHEAR PLATE IS CORRODED. A3NB-53-3-6222 ON HAECO LCQ NR 92944 40/24440. REMOVED AND REPLACED LH SHEAR PLATE IAW A320 SRM 51-42-11 AND SR M 51-72-11. SDR.
- [SDR CALA2021060400785](https://openairdocs.org/sdr/CALA2021060400785.md): Door Sill · corroded · Jun 2, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION. A3NB-53-3-6222 GENERATED BY V892442 ON HAECO LCQ NR 9294450/24450 L-2 DOOR SILL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DO OR SILL IAW A320 SRM 51-42-11 AND 53-41-14-283-002. ACCOMPLISHED BY MECH V061673 INSP BY N078570
- [SDR CALA2021060200777](https://openairdocs.org/sdr/CALA2021060200777.md): Door · corroded · May 31, 2021 · N488UA · Airbus A320232 · Service Doors
  > R2 DOOR SILL HAS CORROSION (A3NB-53-3-6222). REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2021053100748](https://openairdocs.org/sdr/CALA2021053100748.md): Shear Web · corroded · May 28, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SHEAR WEB AT FR 70 LOWER SURFACE HAS CORROSION AND UPPER SURFACE HAS TOOL MARK A3NB-53-3-6222. GENERATED BY N078570 ON NR 9294610/HAECO NR 24610 REMOVED AND REPLACED CORRODED SHEAR WEB AT FR 70-69 LOWER SURFAC E IAW A320 SRM 51-42-11-001 SDR. ACCO
- [SDR CALA2021052800743](https://openairdocs.org/sdr/CALA2021052800743.md): Shear Panel · corroded · May 26, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH SHEAR PLATE IS CORRODED. REMOVED AND REPLACED SHEAR PLATE RH FR 69-70 IAW SRM 51-42-11-001 AND SRM 51-72-11-911-001.
- [SDR CALA2021032600379](https://openairdocs.org/sdr/CALA2021032600379.md): Battery · no test · Mar 26, 2021 · N488UA · Airbus A320232 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPS. CHK. RIGHT BATTERY AT FLOOR LEVEL OVER WING SEAT ROW 21F FAILED TEST. REPLACED BATTERY PACK AT RIGHT OW SEAT ROW 21F, OPS. CHK''S. GOOD, IAW AMM 33-51-38-00-002-AO.
- [SDR CALA2021032600378](https://openairdocs.org/sdr/CALA2021032600378.md): Battery · no test · Mar 26, 2021 · N488UA · Airbus A320232 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPS. CHK. FWD LEFT BATTERY FAILED TEST. REPLACED FWD ELL BATTERY PACK ABOVE FWD ENTRY DOOR 1L, OPS. CHK''S GOOD, IAW AMM 33-51-38-00-002-AO.
- [SDR CALA2021012500092](https://openairdocs.org/sdr/CALA2021012500092.md): Power Supply · failed · Jan 25, 2021 · N488UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT EMERGENCY L MESSAGE PRESENT REPLACED EPSU, REF AMM 33-51-38-000-001-A & 33-51-38-400-001-A. ALSO REPLACED BATTERY PACK REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPERATIONS CHECKED OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249021 SN OFF
- [SDR CALA2020012600226](https://openairdocs.org/sdr/CALA2020012600226.md): Shear Tie · gouged · Jan 20, 2020 · N488UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO FRAME 27, STRINGER 43R - 44R CLEAT GOUGED. REMOVED AND REPLACED THE CLEAT IAW SRM 51-72-1 1-911-001 PARA S, D 1.
- [SDR CALA2020012300197](https://openairdocs.org/sdr/CALA2020012300197.md): Skin · dented · Jan 17, 2020 · N488UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REPAIR REQUIRED AT FR.27, BETWEEN STR. 43R AND STR. 44 AT CENTER FUSELAGE. PER TASK CARD: 5273678/4216 (CUSTOMER REQUEST) (SUPPOR T TASK) PER HAECO LCQ N/R 9290201 GENERATED BY V061737 REF TERMINATING ACTION FOR DENT LOCATED AT FR27 BETWEEN S43R AND S44 FROM
- [SDR CALA2020012000194](https://openairdocs.org/sdr/CALA2020012000194.md): Plate · corroded · Jan 17, 2020 · N488UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR TORSION BOX SILL PLATE CORROSION AT FR54 (A3NB-05 -3-6012) PER N/R 9290354 GENERATED. RMVD & RPLCD W/NEW TORSION BOX COVER PLATE AT AFT CARGO DOOR ENTRY PER SRM 53-41-49-283-004 & SRM 51-42-11-801. PERFORMED BY MECH, INSP.
- [SDR CALA2019081601367](https://openairdocs.org/sdr/CALA2019081601367.md): Servo · leaking · Aug 14, 2019 · N488UA · Airbus A320232 · Hydraulic System, Main
  > POSITION FERRY MADE AIR RETURN DUE TO LOSS OF YELLOW HYDS. SPOILER #4 LEAK. REMOVED #4 SPOILER REF M.M. 27-64-44-000-001-A. FOUND #4 RIGHT SPOILER ACT LEAKING. REMOVED AND REPLACED #4 SPL ACT. REF AMM 27-64-51-400-004-A, 27-64-00-820-001-C, 27-64-00-710-001-A.
- [SDR CALA2018110502299](https://openairdocs.org/sdr/CALA2018110502299.md): Contactor · warning message · Nov 5, 2018 · N488UA · Airbus A320232 · Electrical Power System Wiring
  > DC ESS BUS SHED DISPLAYED ON UPPER ECAM SCREEN. - EL EC REF TSM 24-60-00-710-801. BERG TOMC. REPLACED DC SHED ESSENTIAL BUS CONTACTOR, CKS OK, REF AMM24-62-5 5.

Next page: https://openairdocs.org/aircraft/N488UA/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 = 'N488UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N488UA/reports

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