# Service difficulty reports: N484UA

A list on [N484UA](https://openairdocs.org/aircraft/N484UA.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 · 91 reports

- [SDR CALA2026060116684](https://openairdocs.org/sdr/CALA2026060116684.md): Fuel Cap · missing · May 26, 2026 · N484UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS CAP IS MISSING REQUESTING CDL FOR MISSING FUEL CAP. CONFIRMED NO LEAKS PRESENT. INSTALLED CAP ASSY REF IPC 28-25-41-02B
- [SDR CALA2026050515982](https://openairdocs.org/sdr/CALA2026050515982.md): Power Supply · faulted · May 1, 2026 · N484UA · Airbus A320232 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING SYS CHECK, SYSTEM OK LIGHT NEVER CAME ON. EPSU UNIT L MESSAGE FOUND AFT LH EPSU UNIT TO BE FAULTY. REPLACED BATTERY PACK AND REPERFORMED CABIN EMERGENCY LIGHT SYSTEM CHECK AT PTP. SYS TEST OK.
- [SDR CALA2025082708164](https://openairdocs.org/sdr/CALA2025082708164.md): Elec Connector · disconnected · Aug 23, 2025 · N484UA · Airbus A320232 · Light System Wiring
  > ROW 38 ABC ON SEAT EMERGENCY LIGHT INOP FOUND CONNECTOR ON SEAT DISCONNECTED, RECONNECTED & PERFORM EMERGENCY LIGHTING TEST PER AMM 33-51-00-710-804-A, OPS TEST GOOD
- [SDR CALA2025072106798](https://openairdocs.org/sdr/CALA2025072106798.md): Probe · faulted · Jul 18, 2025 · N484UA · Airbus A320232 · Fuel Control/Reciprocating Engines
  > REJECTD T/O 50-60 KIAS DUE TO SPLIT POWER SETTING W/ NO ECAM ITEM UPDATED WITH CURRENT P2T2 SENSOR. ENG #2 REPLACED AT ENG #2, P2T2 SENSOR PER AMM 73-22-11/401 CONFIG 13. ALL TEST OK.
- [SDR CALA2025052204910](https://openairdocs.org/sdr/CALA2025052204910.md): Engine · damaged · May 18, 2025 · N484UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > PDA 2 REF LP #4882215 NO 6 STRUT FAIRING PANEL ASSEMBLY MISSING OUTBOARD SIDE. PANEL, FAIRING, NO. 6 STRUT, ASSEMBLY OF POST SBE72-0435, #2 ENGINE REPLACED DUE TO SHOUD DAMAGE AT 6 O'CLOCK POITION #2 ENGINE REPLACED DUE TO SHOUD DAMAGE AT 6 O'CLOCK POITION R
- [SDR CALA2025042104037](https://openairdocs.org/sdr/CALA2025042104037.md): Wing · smoke · Apr 19, 2025 · N484UA · Airbus A320232 · Wing Structure
  > RAMP REPORTS SMOKE COMING FROM WINGS, BURNING SMELL. CONTACTED FIRE DEPARTMENT, NO HEAT SHOWN ON THERMAL IMAGING, NO BURNING SMELL, NO EVIDENCE OF HEAT DAMAGE FOUND. DROPPED FLAP/S SLATS ON GROUND REF AMM 27-50-00, INSPECTED, SMOKE APPEARS TO CONDENSATION WI
- [SDR CALA2025032403112](https://openairdocs.org/sdr/CALA2025032403112.md): Battery · faulty · Mar 22, 2025 · N484UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY EMER R INSTALLED SERVICEABLE BATTERY EPSU 12WL REF. AMM 33-51-38-400-002-A. OKAY TO CONTINUE.PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2025030702623](https://openairdocs.org/sdr/CALA2025030702623.md): Light · malfunctioned · Mar 4, 2025 · N484UA · Airbus A320232 · Emergency Lighting
  > EMER LIGHTS FLICKERED WITH ASSOC FAULTS PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT IN REF TO AMM 33-51-00. OPS CHECK NORMAL. COULD NOT DUPLICATE FAULT.
- [SDR CALA2024072600285](https://openairdocs.org/sdr/CALA2024072600285.md): Fuel Cap · missing · Jul 25, 2024 · N484UA · Airbus A320232 · Fuel Storage
  > PDA 2 REFUEL CAP MISSING FROM RIGHT WING
- [SDR CALA2024030800667](https://openairdocs.org/sdr/CALA2024030800667.md): Panel · missing · Mar 6, 2024 · N484UA · Airbus A320232 · Wing, Plate/Skin
  > PDA 2 LEFTWING LEADING EDGE PANEL MISSING. ON ARRIVAL FROM SJD, TECH FOUND PANEL 522WB (L/H WING) MISSING WHEN PERFORMING EXTERIOR GVI INSTALLED NEW COVER ASSY ON BLOWOFF PANEL REF IPC 57-41-37.
- [SDR CALA2023050101299](https://openairdocs.org/sdr/CALA2023050101299.md): Bulb · inoperative · Apr 29, 2023 · N484UA · Airbus A320232 · Emergency Lighting
  > SEAT LAMP RED LIGHT BULB (1EA) INOP AT ROW 21ABC. REMOVED AND REPLACED 1 EPL BULB AT ROW 21ABC IAW A320 AMM 33-51-18-00/400-002-A OPS CHECK GOOD PER STS N0031. R & R 1 EPL BULB AT ROW 21ABC IAW A 320 AMM 33-51-18-000/400-002-A. OPS CHECK GOOD
- [SDR CALA2023050101298](https://openairdocs.org/sdr/CALA2023050101298.md): Bulb · inoperative · Apr 29, 2023 · N484UA · Airbus A320232 · Passenger Compartment Lighting
  > SEAT LAMP RED LIGHTBULB (EA) INOP AT ROW 22ABC. REMOVED & REPLACED AFT CARGO COMPARTMENT SKID PLATES IAW A320 EC RA 5322-01050. R & R 1 EPL BULB AT ROW 22ABC IAW A320 AMM 33-51-18-000-400-002-A. OPS CHECK GOOD.
- [SDR CALA2022060201421](https://openairdocs.org/sdr/CALA2022060201421.md): Check Valve · cracked · Jun 2, 2022 · N484UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > ECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD FOUND CRACKED CHECK VALVE ON PTU HP MANIFOLD REF IPC 29-11-15-02 ITEM 150.REPLACED CHECK VALVE PER AIPC 29-11-15-02. LEAK CHECK GOOD
- [SDR CALA2022022800524](https://openairdocs.org/sdr/CALA2022022800524.md): Hydraulic System · depleted · Feb 28, 2022 · N484UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > YELLOW SYSTEM ALMOST DEPLETED. LARGE LEAK NOTICED BEHIND RIGHT GEAR WELL. WAS ABLE TO CLOSE CARGO DOORS MANUALLY BY HAND PUMP. FOUND WEEPING B-NUT ON AUTOMATIC SELECTOR VALVE, TORQUED IN REFERENCE TO AMM 32-42-13 (FIG 31-42-13-991-00100-B ITEM 17). SERVICING A
- [SDR CALA2022010700058](https://openairdocs.org/sdr/CALA2022010700058.md): Stringer · cracked · Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > LH SIDE FRAME 68 AT STR22 INNER CAP AND WEB FLANGEIS CRACKED. CR ACK ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, AFT SIDE, I N AND ABOVE RADIOUS. CRACK APPROX 2.25" WITH ENDS MARKED IN BLAC K. L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE. ACCOMPL
- [SDR CALA2022010700057](https://openairdocs.org/sdr/CALA2022010700057.md): Stringer · cracked · Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > L/H FR35 STR30L HOLE #3 HAS CRACK INDIACTIONS AT THE 2:00. 3:00, AND 4:00 POSITIONS. REF HAECO N/R 9294150 FOR REFERENCE. #3 FINIAL HOLE SIZE.199". ACCOMPLISH INITIAL INS THE LATEST OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE 59,68 HOURS, WHICHEVER COMES
- [SDR CALA2022010700056](https://openairdocs.org/sdr/CALA2022010700056.md): Frame · cracked · Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Frame
  > L/H FR35 STR 30 HOLES #2 HAS CRACK INDACTIONS AT THE 5:00, 6:00, AND 11:00 POSITIONS CONTACT ENGINEERING FOR REPAIR INSTRUCTION BEFORE NEXT FLIGHT. FOR A REFERENCE FOR #2 HOLE. FINIAL HOLE SIZE.250". ACCOMPLISH OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE
- [SDR CALA2022010700055](https://openairdocs.org/sdr/CALA2022010700055.md): Door Frame · cracked · Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Structure
  > L2 DOOR FRAME 68 DOOR STOP FITTING #1 LOWER INBOARD HOLE IS CRAC KED IN THE FRAME WEB AT 5:00 AND 10:00 POSITION. REO-L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE.#3 HOL REPAIR ON THE FR68 DOOR STOP #1 AND STR 22 FLANGE PER PART 3 OF E START DIA.269"
- [SDR CALA2022010700037](https://openairdocs.org/sdr/CALA2022010700037.md): Frame · cracked · Jan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, Frame
  > LH SIDE FRAME 68 AT STR 22 INNER CAP AND WEB FLANGE IS CRACKED. CRACK LOCATED ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, A FT SIDE, IN AND ABOVE RADIUS. CRACK APPROX 2.25" WITH ENDS MARKE D IN BLACK. L2 DOOR DRAME 68 DOOR STOP FITTING #1 LOWER I/B HOLE I
- [SDR CALA2022010700036](https://openairdocs.org/sdr/CALA2022010700036.md): Frame · cracked · Jan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, Frame
  > L/H FR35 STR30L HOLE #2 HAS CRACK AT THE 5:00, 6:00, AND 11:00 P OSITIONS. HOLE #3 HAS CRACK INDICATIONS AT 2:00, 3:00, AND 4:00. #1 HAS CRACK INDICATIONS AT 5:30 AND 6:30 POSITIONS. PER HAECO LCQ NR 9294149/22149, 9294150/22150, 9294148/22148. GENERATED BY V0
- [SDR CALA2021122902464](https://openairdocs.org/sdr/CALA2021122902464.md): Fitting · corroded · Dec 28, 2021 · N484UA · Airbus A300* · Fuselage Structure (General)
  > MAIN CABIN L2 DOOR SILL AFT CORNER FITTING HAS CORROSION (A3NB-5 3-3-6222) GENERATED BY:N078592 AT HAECO LCQ PER NON ROUTINE 929 273 (22273) REMOVED AND REPLACED CORNER FITTING FR68 L/H DOOR SILL. IAW A320 SRM 51-42-11/001 PARA 2B,F PERFORMED BY:V061630 INSPEC
- [SDR CALA2021122902463](https://openairdocs.org/sdr/CALA2021122902463.md): Door Sill · corroded · Dec 28, 2021 · N484UA · Airbus A300* · Doors
  > MAIN CABIN L2 DOOR SILL FWD GIRT BAR MOUNT POINT HAS 2 AREAS OF CORROSION. (A3NB-53-3-6222) GENERATED BY N078592 AT HAECO LCQ PE R NR 9294271 (22271) REMOVED AND REPLACED L-2 DOOR SILL IAW A320 SRM 51-42-11/001. PE RFORMED BY V061630 INSP BY N078570.
- [SDR CALA2021121702379](https://openairdocs.org/sdr/CALA2021121702379.md): Stringer · corroded · Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO LWR SILL WEB PLATE FR26 TO FR28 UPPER SURFACE HAS SEV ERAL AREAS OF CORROSION (A3NB-53-3-6105) GENERATED BY N078592 AT HAECO LCQ PER NON ROUTINE 9294405 (22405) REMOVED CORRODED FWD CARGO SILL WEB PLATE AND INSTALLED NEW WEB PLATE IAW A320 SRM 51-42-
- [SDR CALA2021121702378](https://openairdocs.org/sdr/CALA2021121702378.md): Stringer · corroded · Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO PIT STRINGER 41RT BETWEEN FRAME 61-62 HAS CORROSION O N VERTICAL FLANGE (SUPPORT TASK) GENERATED BY V052030 AT HAECO L CQ PER NR 9294337 (22337) REMOVED AND REPLACED STRINGER 41RT AFT CARGO. IAW A320 SRM 51-72 -11. PERFORMED BY V052030 INSP BY V06133
- [SDR CALA2021121702377](https://openairdocs.org/sdr/CALA2021121702377.md): Stringer · corroded · Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO PIT STRINGER 42 LEFT HAS CORROSION AT FRAME 57LT AND F R59 LEFT (SUPPORT TASK) GENERATED BY V052030 @HAECO LCQ PER NR 9 294340 (22340) REMOVED AND REPLACED STRINGER 42L IN AFT CARGO. IAW A320 SRM 51- 72-11. PERFORMED BY V052030 INSP BY V061334
- [SDR CALA2021121702376](https://openairdocs.org/sdr/CALA2021121702376.md): Stringer · corroded · Dec 15, 2021 · N484UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO PIT BETWEEN FR63-64 STRINGER 42R HAS CORROSION SPOTS O N UPPER SURFACE GENERATED BY V919150 AT HAECO LCQ PER NR # 9294507 (22507) REMOVED CORRODED STRINGER 42R AT FR63-64 AND INSTALLED NEW STRIN GER IAW A320 SRM 51-42-11 PERFORMED BY V913406 INSP BY
- [SDR CALA2021121202342](https://openairdocs.org/sdr/CALA2021121202342.md): Fitting · corroded · Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > MAIN CABIN R2 DOOR SILL HAS (2EA) AREAS OF CORROSION ON UPPER SU RFACE CENTER SHAPE SILL ONLY. GENERATED BY N078592 PER HAECO LCQ NR 9294286/22286 REMOVED AND REPLACED R-2 DOOR SILL SHAPE SILL IAW A320 SRM 51-42 -11/001 PARA 6 DOT REMOVED KC50 BY MECH V061630
- [SDR CALA2021121202341](https://openairdocs.org/sdr/CALA2021121202341.md): Fitting · corroded · Dec 10, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > R2 DOOR SILL FWD CORNER FITTING HAS CORROSION. GENERATED BY N078 592 PER HAECO LCQ NR 9294287. REMOVED AND REPLACED CORNER FITTING AT R2 DOOR SILL IAW A320 SRM 51-42-11/001 PARA 6 B,F DOT REMOVED KC51 BY MECH V061630 INSP BY V919150
- [SDR CALA2021120602247](https://openairdocs.org/sdr/CALA2021120602247.md): Plate · corroded · Dec 4, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > CARGO PIT IB TORSION BOX COVER SHEET HAS CORROSION AROUND TIE DO WN FITTINGS PER NR9294383/22383 GEN BY V052030. RMVD AFT CARGO PIT INBD TORSION BOX COVER SHEET AND INSTALLED NE W TORSION BOX COVER SHEET IAW SRM 53-41-49-283-004. APPLIED TOP COAT IAW SRM 51-75
- [SDR CALA2021120102212](https://openairdocs.org/sdr/CALA2021120102212.md): Intercostal · cracked · Nov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FR 16 DOOR STOP FITTING #7, INBD UPPER HOLE HAS A CRACK IND ICATION AT 5 O''CLOCK POSITION AT FRAME TO INTERCOSTAL LAYER. (AD 2019-20-10). GENERATE BY V061671 AT HAECO LCQ PER NR 9294263 (2 2263) REMOVED AND REPLACED L/H FRAME 16 DOOR STOP #7 INTERCOSTAL
- [SDR CALA2021120102211](https://openairdocs.org/sdr/CALA2021120102211.md): Intercostal · cracked · Nov 30, 2021 · N484UA · Airbus A320232 · Fuselage Main, Frame
  > AD 2019-20-10; RIGHT FR 16 DOOR STOP FITTING #7, INBD LOWER HOLE HAS A CRACK INDICATION AT 7 O''CLOCK POSITION AT FRAME TOTO INTE RCOSTAL LAYER GENERATED BY V061671 ON HAECO LCQ NR 9294264 (2226 4) REMOVED AND REPLACED R/H FRAME 16 DOOR STOP FITTING #7 INTERCO
- [SDR CALA2021112202143](https://openairdocs.org/sdr/CALA2021112202143.md): None · corroded · Nov 19, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO FR32 STR44 HAS CORROSION ON FWD FACE OF SHEAR TIE (A3N B-53-3-6105). GENERATED BY N078592 AT HAECO LCQ PER NR 9294415 ( 22415). REMOVED AND REPLACED FWD CARGO SHEAR TIE AT FR32 STR44 IAW A320 SRM 51-72-11-911-001. PERFORMED BY V061765 AND INSP BY V06
- [SDR CALA2021112202139](https://openairdocs.org/sdr/CALA2021112202139.md): Angle · corroded · Nov 18, 2021 · N484UA · Airbus A320232 · Fuselage Structure (General)
  > MAIN CABIN R2 DOOR SILL FR68 HAS CORROSION AT FASTENER HOLE (A3N B-53-3-6222)GENERATED BY N078592 AT HAECO LCQ PER NR 9294284 (22 284) PERFORMED MAIN CABIN R2 DOOR SILL REPAIR AT FRAME 68 IAW A320 SR M 53-41-14-300-001, REPAIR PRINCIPLE #5.PERFORMED BY V913406
- [SDR CALA2020012000216](https://openairdocs.org/sdr/CALA2020012000216.md): Fuel Cap · missing · Jan 20, 2020 · N484UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. INSTALLED A NEW CAP.
- [SDR CALA2019061400944](https://openairdocs.org/sdr/CALA2019061400944.md): Shear Panel · corroded · Jun 13, 2019 · N484UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA LEFT LATERAL SHEAR PLATE HAS A CORROSION AROUND FASTENER HOLES BETWEEN FR69 AND FR70 STA Y1732 REMOVED AND REPLACED SHEAR PLATE AT AFT WET AREA LEFT LATERAL BETWEEN FR69 AND FR70 Y1732 IAW A320 SRM 51-42-11 & 51-72-11-911 -001
- [SDR CALA2019061400943](https://openairdocs.org/sdr/CALA2019061400943.md): Shear Plate · corroded · Jun 13, 2019 · N484UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA RIGHT LATERAL SHEAR PLATE HAS CORROSION AROUND FAST ENER HOLES BETWEEN FR 69 AND FR 70 STA -Y1732 DATA WAS TRANSCRIBED FROM PAPER DOCUMENT:AAR N/R 9593890 WORK REMOVED AND REPLACED AFT WET AREA RIGHT LATERAL SHEAR PLATE BETW EEN FR 69 AND FR 70
- [SDR CALA2019041200562](https://openairdocs.org/sdr/CALA2019041200562.md): Fuel Cap · missing · Apr 9, 2019 · N484UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING.
- [SDR CALA2017120104286](https://openairdocs.org/sdr/CALA2017120104286.md): Battery · faulty · Dec 1, 2017 · N484UA · Airbus A320232 · Emergency Lighting
  > EPSU BATT EMERGENCY L FAILED SYS TEST. RPL EPSU BATT EMERGENCY L. OPS CHK OK.
- [SDR CALA2017111204047](https://openairdocs.org/sdr/CALA2017111204047.md): Battery · discharged · Nov 12, 2017 · N484UA · Airbus A320232 · Lighting System
  > EMERGENCY LIGHTING POWER SUPPLY BATT FAIL. R&R BATT. OP-CHECK GOOD. AMM 33-51-000-002-A, AMM 33-51-38-400-002-A.
- [SDR CALA2017082502897](https://openairdocs.org/sdr/CALA2017082502897.md): Cradle · broken · Aug 25, 2017 · N484UA · Airbus A320232 · Emergency Equipment
  > REAR EMERGENCY FLASHLIGHT HOUSING BROKEN AT 2L JUMPSEAT. REPLACED BROKEN HOUSING
- [SDR CALA2016081195626](https://openairdocs.org/sdr/CALA2016081195626.md): Battery Pack · no test · Jun 26, 2016 · N484UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED WITH EPSU BATTERY FWD LEFT FAULT. REPLACED EPSU BATTERY, OPS CHECKED NORMAL.
- [SDR CALA2016040495250](https://openairdocs.org/sdr/CALA2016040495250.md): Fluid · low · Mar 31, 2016 · N484UA · Airbus A320232 · Hydraulic System, Main
  > YELLOW HYD SYS ECAM MSG, ZERO INDICATION. SERVICED YELLOW HYD QTY AS REQUIRED, NO LEAKS NOTED.
- [SDR CALA2015120894866](https://openairdocs.org/sdr/CALA2015120894866.md): Stringer · corroded · Dec 2, 2015 · N484UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 31R AT C65 FRAME IN AREA AFT OF AFT CARGO COMPARTMENT UNDER OUTFLOW VLV, LOWER FWD CORNER. R & R STRINGER 31R, FRAME 64 - 67 IAW SRM 51-42-11 PAR 7.
- [SDR CALA2015092194380](https://openairdocs.org/sdr/CALA2015092194380.md): Battery · discharged · Sep 20, 2015 · N484UA · Airbus A320232 · Emergency Lighting
  > REFERENCE 2 SERVICE, EMER LIGHTS FAIL TEST. R & R LT FWD EPSU BATTERY, BATTERY ONLY, IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHECKED OK.
- [SDR CALA2014060991250](https://openairdocs.org/sdr/CALA2014060991250.md): Aileron · malfunctioned · Jun 9, 2014 · N484UA · Airbus A320232 · Aileron Control System
  > RIGHT AILERON DEFLECTED DOWN 2 - 3 SCALE WITH ASSOCIATED ROLL OBSERVED.
- [SDR CALA2014050690961](https://openairdocs.org/sdr/CALA2014050690961.md): Unknown · faulty · May 5, 2014 · N484UA · Airbus A320232 · Crew Oxygen System
  > O2 SERVICED TO FULL IN DENVER, SHOWED 1500 AT DULLES. NOW SHOWING 1360 IN FLT. BOTTLE PRE-SERVICE READING WAS 1600 PSI, SERVICE TO 2000 PSI. COCKPIT INDICATION SHOWED 1900 PSI. CREW WILL MONITOR PRESS INFLIGHT.
- [SDR CALA2014041490821](https://openairdocs.org/sdr/CALA2014041490821.md): Adapter · corroded · Apr 13, 2014 · N484UA · Airbus A320232 · Fuel Storage
  > LEFT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED CORROSION & MEASURED THE AREA.
- [SDR CALA2014041490820](https://openairdocs.org/sdr/CALA2014041490820.md): Adapter · corroded · Apr 13, 2014 · N484UA · Airbus A320232 · Fuel Storage
  > RIGHT WING MANUAL REFUELING ADAPTER APERTURE HAS PITTING CORROSION RIB 19 - RIB 20. BLENDED THE AREA & MEASURED REMAINING THICKNESS.
- [SDR CALA2014041490819](https://openairdocs.org/sdr/CALA2014041490819.md): Stringer · corroded · Apr 13, 2014 · N484UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FRAME 63 - FRAME 64 & STRINGER 42L HAS CORROSION IN AFT CARGO COMPARTMENT. BLENDED CORROSION & FOUND THE AREA BEYOND LIMITS IAW SRM 51-72-11 PG 11. CUT OUT CORRODED AREA OF STRINGER & INSTALLED STRINGER REPAIR & SPLICE ON STRINGER 42L FROM FRAME 62.5 - FRAME
- [SDR CALA2014040890782](https://openairdocs.org/sdr/CALA2014040890782.md): Skin · saturated · Apr 5, 2014 · N484UA · Airbus A320232 · Elevator, Plate/Skin
  > RIGHT ELEVATOR UPPER SKIN SURFACE HAS A WATER INGRESS INDICATION 39 INCHES FROM INBD END, 3 INCHES FROM TE, 3.5 INCHES DIAMETER. REPAIRED RT ELEVATOR UPPER SKIN AT LOCATION NOTED. DRILLED WITNESS HOLES & FOUND WATER. CUT OUT, SANDED AREA & REMOVED WATER. AP

Next page: https://openairdocs.org/aircraft/N484UA/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 = 'N484UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N484UA/reports

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