# Service difficulty reports: N459UA

A list on [N459UA](https://openairdocs.org/aircraft/N459UA.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 · 139 reports

- [SDR CALA2026072317960](https://openairdocs.org/sdr/CALA2026072317960.md): Fuel Cap · missing · Jul 19, 2026 · N459UA · Airbus A320232 · Fuel Storage
  > AIRCRAFT CAME IN WITH MISSING FUEL CAP. NO FUEL LEAKING FROM COUPLING. INSTALLED A SERVICEABLE FUEL CAP AND LANYARD ASSY.
- [SDR CALA2026070717600](https://openairdocs.org/sdr/CALA2026070717600.md): Battery Pack · no test · Jun 29, 2026 · N459UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY - REPLACED ON A-CHECK. REQUIRES 4 BATTERIES, REMOVED AND REPLACED ALL 4 EPSU BATTERIES 10WL, 11WL, 12WL, 13WL REF AMM 33-51-38-400-001-A OPS CHECKED GOOD, NO FAULTS FOUND AT THIS TIME.
- [SDR CALA2026042215597](https://openairdocs.org/sdr/CALA2026042215597.md): Fuel Cap · missing · Apr 19, 2026 · N459UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISING APPLIED PLACARD AND VERIFIED COUPLING SEAL NOT LEAKNG FUEL TOMC PENDING DISPATCH DESK: 14 NAME: AS DATE: 19-APR-26- OK TO APPLY CDL 28A....TOMC SMITH PLACED ON CDL NO LEAKING NOTED
- [SDR CALA2025101309969](https://openairdocs.org/sdr/CALA2025101309969.md): Elec Connector · broken · Oct 12, 2025 · N459UA · Airbus A320232 · Light System Wiring
  > AISLE PATHWAY LIGHTING AT SEAT 38C HAS BROKEN WIRE AT CONNECTOR. REPLACED CONNECTOR AT 38C ESPM 20-56-21. REF AMM 33-51-00 VERIFIED OPERATION OF LIGHT.
- [SDR CALA2025080707436](https://openairdocs.org/sdr/CALA2025080707436.md): Battery Pack · no test · Aug 6, 2025 · N459UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY AFT LT FAILED CAP CHECK. REMOVED AND REPLACED EPSU BATTERY PER AMM 33-51-38-000-002-A. OP CHECK OK
- [SDR CALA2025052704970](https://openairdocs.org/sdr/CALA2025052704970.md): Unknown · smoke · May 23, 2025 · N459UA · Airbus A320232 · Instrument Panel
  > SMOKE COMING FROM BEHIND PANEL BEHIND PFD CREW REPORTED SMOKE COMING FROM 500VU PANEL (FO'S DISPLAY BRIGHTNESS AND SPEAKER VOLUME PANEL) VISSUALLY CK'D PANEL AND COMPONENTS AND PFD AND ND CONNECTOR DID NOT SEE ANY ABNORMALITIES. COULD NOT DUPLICATE,PULLED DISP
- [SDR CALA2025050504440](https://openairdocs.org/sdr/CALA2025050504440.md): Chiller · faulted · May 2, 2025 · N459UA · Airbus A320232 · Buffet/Galleys
  > GALLEY FOUR CHILLER GETTING HOT SMELL SMOKE WHEN TURNED ON REQUEST NEF 2522AG FOR GALLEY FOUR CHILLER INOP.OKAY TO DEFER CHILLER PER MEL 2522AG PLACED GALLEY FOUR CHILLER ON NEF 2522AG FOR INOP FOUND CHILLER G41 SN 568 EXHAUST OUTLET COVERPLATE INSTALLED IN TH
- [SDR CALA2025042304161](https://openairdocs.org/sdr/CALA2025042304161.md): Skin · chafed · Apr 21, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REF. N/R 39049 (REWORK PER E/A 5300-02120 OP1 STEP 4.1) AREA REW ORKED ON N/R 39049 RQUIRES EVALUATION OF LIMITS AND REPAIR. REPAIRED CHAFE MARK ON FUSELAGE EXT SKIN FR 34 STGR 43L-43R. REC EIVED ECRA 5321-02162 THAT PROVIDES PERMANENT REPAIR INSTRUCTION S FO
- [SDR CALA2025042204111](https://openairdocs.org/sdr/CALA2025042204111.md): Doubler · corroded · Apr 14, 2025 · N459UA · Airbus A320232 · Trailing Edge Flaps
  > LH WING O/B FLAP RIB 5-6, TRACK 3 SUPPORT, INTERNAL DOUBLER FOUND CORROSION AROUND SEVERAL FASTENERS.
- [SDR CALA2025042204110](https://openairdocs.org/sdr/CALA2025042204110.md): Doubler · corroded · Apr 14, 2025 · N459UA · Airbus A320232 · Trailing Edge Flaps
  > RH WING O/B FLAP RIB 5-6, TRACK 3 SUPPORT, INTERNAL DOUBLER FOUN D CORROSION AROUND FASTENERS. INSTALLED FLAP.
- [SDR CALA2025041603887](https://openairdocs.org/sdr/CALA2025041603887.md): Frame · cracked · Apr 14, 2025 · N459UA · Airbus A320232 · Fuselage Main, Frame
  > WHILE PERFOMING REINSPECT OF RH FR35 STR 30 FOUND PREVIOSLY REPAIRED HOLE #2 TO BE CRACKED. ACCOMPLISHED IMPROVED INTERIM REPAIR PER ECRA 5331-02334 REV B. PART 1A STEP 1. REF LPS 9144384 ASSOCIATED DIP LIMITS.
- [SDR CALA2025042304162](https://openairdocs.org/sdr/CALA2025042304162.md): Door Frame · cracked · Apr 13, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > RIGHT AFT DOOR CUTOUT FR68 STRG 8 HAS A CRACK INDICATION IN THE RADIUS 10MM LONG. RIGHT AFT DOOR CUTOUT, FR 68 STRG 8 HAS A CRACK INDICATION. ESFR COMPLETE RIGHT AFT DOOR CUTOUT FR68 STRG 8 HAS A CRACK INDICATION IN THE RADIOS 10MM LONG ESFR ENTRY INTERIM REPA
- [SDR CALA2025042304164](https://openairdocs.org/sdr/CALA2025042304164.md): Doubler · damaged · Apr 12, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > TEMP DOUBLER NEEDS PERMANENT REPAIR LOCKING FOR FERRY FLT. UNLOCKING FOR MX. ESFR COMPLETED INTERIM REPAIR COMPLETED WITH NO DEVIATIONS IAW ECRA 5311-03350. ACCOMPLISH A PERMANENT REPAIR ON THE LH FWD FUSELAGE SKIN BETWEEN FR13 AND FR14 ABOVE Z-520 PER PART 3
- [SDR CALA2025041403785](https://openairdocs.org/sdr/CALA2025041403785.md): Skin · corroded · Apr 7, 2025 · N459UA · Airbus A320232 · Wing, Plate/Skin
  > RH WING FUEL TANK RIBS 18-19 PANEL LAND FASTENER HOLES ELONGATED PER HAECO LCQ N/R 9290923/38923 GEN BY V798788SFR COMPLETED ESFR COMPLETED ESFR COMPLETED IDENTIFIED RH WING FUEL TANK PANEL 640NB ELONGATED HOLES P, K, F, B, C, G, L, Q, U, M, AND E. REAMED HOL
- [SDR CALA2025041403784](https://openairdocs.org/sdr/CALA2025041403784.md): Skin · corroded · Apr 7, 2025 · N459UA · Airbus A320232 · Wing, Plate/Skin
  > RH WING FUEL TANK RIBS 17-18 PANEL LAND FASTENER HOLES ELONGATED EVIDENCE OF CORROSION PER HAECO LCQ N/R 9290922/38922 GEN BY V798788ESFR COMPLETED IDENTIFIED RH WING FUEL TANK PANEL 640MB ELONGATED HOLES F, G, K, AND P. REAMED HOLES TO DIA:.328?, REPAIRED F
- [SDR CALA2025040803639](https://openairdocs.org/sdr/CALA2025040803639.md): Support Angle · cracked · Apr 6, 2025 · N459UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FR 34 R/H PNL SUPPORT FRAME ANGLE CRACKED. R & R PNL SUPPORT FRAME ANGLE AT FR34 R/H IAW A320 SRM 51-7 2-11.
- [SDR CALA2025032703252](https://openairdocs.org/sdr/CALA2025032703252.md): Skin · corroded · Mar 23, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > AFT CARGO LH FR58, STRG 43L HAS CORROSION. BLENDED CORROSION ON FR58, STRG 43L. DETERMINED TO BE OUT OF LIM ITS IAW SRM 53-41-13-283-002, FIG 1, SHEET 1. MAX REWORK DEPTH B EYOND 10 PERCENT OF NOMINAL THICKNESS. FLOW CHART TAKES YOU TO S RM 53-41-13 BUT FR58 N
- [SDR CALA2025032403144](https://openairdocs.org/sdr/CALA2025032403144.md): Door Frame · cracked · Mar 22, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > RH FR 66 DOORSTOP NO.1, LOWER IB HOLE HAS CRACK INDICATION IN FRAME LAYER @ 5 OCLOCK POSITION, 80% S.H. REMOVED CRACK AND FABRICATED REPAIR WASHER IAW A320 SRM 53-41-12-300-010 AND SRM 53-41-12-300-008 REMOVED CRACK AND INSTALLED REPAIR TO FR66 RH #1 DOORST
- [SDR CALA2025032103058](https://openairdocs.org/sdr/CALA2025032103058.md): Fitting · cracked · Mar 20, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > WINDSHIELD CENTER POST LH CONTINUITY FITTING HAS CRACK APPROX.400 INCH O/B OF CENTER POST PER HAECO LCQ N/R 9290924/38924 GEN BY V892444 REPLACED WITH NEW CONTINUITY FITTING IAW DRWG R53112919 AND SRM 51-42-11.
- [SDR CALA2025032103052](https://openairdocs.org/sdr/CALA2025032103052.md): Skin · contaminated · Mar 20, 2025 · N459UA · Airbus A320232 · Rudder, Plate/Skin
  > L/H AFT SIDE OF RUDDER HAS TRAPPED WATER 2 IN FROM TRAILING EDGE, 103 IN FROM BOTTOM, 8X5 IN DIAMETER, NUMEROUS SPOTS IN AREA. " REPAIR PRIOR TO NEXT FLIGHT". GENERATED BY V061632 ON HAECO LCQ NR 9290745/38745. REPAIR WAS PERFORMED IAW A320 SRM 55-41-13-300-0
- [SDR CALA2025031902942](https://openairdocs.org/sdr/CALA2025031902942.md): Skin · damaged · Mar 18, 2025 · N459UA · Airbus A320232 · Nacelle/Pylon, Plate/Skin
  > #1 ENG PYLON AFT FIXED FAIRING LOWER SKIN PANEL HAS 1EA CHAFED RIVIT HEAD WITH MATERIAL LOSS. ESFR COMPLETE RMVD AND RPLD 1EA RIVET AT #1 ENG AFT FIXED FAIRING LOWER SKIN PNL IAW A320 SRM 51-42-11.
- [SDR CALA2025031902941](https://openairdocs.org/sdr/CALA2025031902941.md): Skin · damaged · Mar 18, 2025 · N459UA · Airbus A320232 · Nacelle/Pylon, Plate/Skin
  > #1 ENG PYLON AFT FIXED FAIRING INBD SIDE SKIN IS CRACKED AND HAS BROKEN/MISSING RIVETS. ESFR COMPLETE RMVD AND RPLD SKIN AT #1 ENG PYLON AFT FIXED FAIRING I/B IAW A320 SRM 54-54-11
- [SDR CALA2025031002667](https://openairdocs.org/sdr/CALA2025031002667.md): Web · cracked · Mar 9, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > FLIGHT DECK FLOOR WEB HAS CRACK FR 11 RBL 30. REMOVED & REPLACED CRACKED WEB AT FLIGHT DECK FR11 RBL 30 IAW A3 20 SRM 51-72-11-911-001.
- [SDR CALA2025031302754](https://openairdocs.org/sdr/CALA2025031302754.md): Skin · gouged · Mar 6, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO COMP FLOOR STRUCTURE GOUGE IN SKIN APROX 6 INCHES FWD OF FWD OF FR 26 BETWEEN STR 41L AND STR 42L. GENERATED BY V89904 5 ON HAECO LCQ NR 9290788 / 38788. ESFR COMPLETED
- [SDR CALA2025031302753](https://openairdocs.org/sdr/CALA2025031302753.md): Frame · corroded · Mar 6, 2025 · N459UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO FR 58 LST 43 HAS CORROSION PER HAECO LCQ N/R 9290766/ 38766.
- [SDR CALA2025030702612](https://openairdocs.org/sdr/CALA2025030702612.md): Door Frame · cracked · Mar 6, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > RH AFT EMERGENCY DOOR AFT CENTER FRAME HAS CRACK. REMOVED AND REPLACED FRAME AT AFT CENTER OF RH AFT EMERGENCY EXI T DOOR IAW A320 SRM 51-42-11, SRM 51-72-11.
- [SDR CALA2025030702611](https://openairdocs.org/sdr/CALA2025030702611.md): Door Frame · cracked · Mar 6, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > RH FWD EMERGENCY EXIT AFT FRAME CRACKED. REMOVED AND REPLACED FRAME AT RH FWD EMERGENCY EXIT DOOR AFT SEC TION IAW A320 SRM 51-42-11, SRM 51-72-11.
- [SDR CALA2025030702610](https://openairdocs.org/sdr/CALA2025030702610.md): Door Frame · cracked · Mar 6, 2025 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > RH AFT EMERGENCY DOOR FWD CENTER FRAME HAS CRACK. REMOVED AND REPLACED FRAME AT FWD CENTER OFRH AFT EMERGENCY ENT DOOR IAW A320 SRM 51-42-11, SRM 51-72-11.
- [SDR CALA2025031302762](https://openairdocs.org/sdr/CALA2025031302762.md): Skin · contaminated · Mar 5, 2025 · N459UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 116 IN FROM I/B END 12 IN FROM TRAILING EDGE 1 1/2 IN DIAMETER PER HAECO LCQ N/R 9290931/38931 GEN BY V061632 ENTERED SFR INFORMATION REPAIRED LH ELEVATOR IAW A320 SRM 55-21-11-300-005.
- [SDR CALA2025031302752](https://openairdocs.org/sdr/CALA2025031302752.md): Skin · gouged · Mar 5, 2025 · N459UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO COMP FLOOR STRUCTURE GOUGE IN SKIN APROX 6 INCHES FWD OF FR 26 BETWEEN STR 43L AND STR 44L.
- [SDR CALA2025022000396](https://openairdocs.org/sdr/CALA2025022000396.md): Seat Track · corroded · Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN RT SIDE I/B SEAT TRACK CORRODED AT FR 20. REMOVED AND REPLACED SEAT TRACK AT FWD CABIN RT SIDE I/B FROM FR 12 TO FR24 IAW A320 SRM 51-42-11, SRM 51-72-11. SFR NO.1038443.
- [SDR CALA2025021800377](https://openairdocs.org/sdr/CALA2025021800377.md): Floor Support · corroded · Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN CTR AREA FLOOR SUPPORT Y254 CORRODED AT FR 20 PER HAECO LCQ N/R 9290686/38686 GEN BY. REMOVED AND REPLACED FLOOR BEAM AT FWD CABIN CTR AREA FROM FR 20 -24 IAW A320 SRM 51-72-11.
- [SDR CALA2025021800379](https://openairdocs.org/sdr/CALA2025021800379.md): Seat Track · corroded · Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN RT SIDE O/B SEAT TRACK AT FR 20 CORRODED. REMOVED AND REPLACED SEAT TRACK AT FWD CABIN RT SIDE O/B FROM FR 12 TO FR24 IAW A320 SRM 51-42-11,SRM 51-72-11.
- [SDR CALA2024123001721](https://openairdocs.org/sdr/CALA2024123001721.md): Chiller · faulted · Dec 28, 2024 · N459UA · Airbus A320232 · Buffet/Galleys
  > POPPING NOISE CB PANEL AFT GALLEY TURNED IT OFF SMELL OF BURNING RUBBER CREW STATED SOURCE IS CHILLER CONTROL 401, 402. DEFER AFT GALLEY CHILLER C41 INOP IAW NEF 2522AG. PULL & COLLARED C/B INOP STICKER APPLIED. TOMC APPROVES NEF 2522AG. LOCAL FBO VERIFIED
- [SDR CALA2024111101090](https://openairdocs.org/sdr/CALA2024111101090.md): Valve · leaking · Nov 11, 2024 · N459UA · Airbus A320232 · Hydraulic Power System
  > FLUID RUNNING DOWN AFTBELLY BELOW CARGO DOOR PER AMM 29-00-00-790-001-A 10 DROPS PER MINUTE IS GOOD SUSPECT DOOR CONTROL VALVE. REF A319AMM 52-36-15/401 CONFIG 00 REMOVED AND REPLACED AFT CARGO DOOR MANUAL SELECTOR VALVE (2504MJ). LEAK CHECK OPS CHECK GOOD.
- [SDR CALA2024111101091](https://openairdocs.org/sdr/CALA2024111101091.md): Hydraulic Line · leaking · Nov 10, 2024 · N459UA · Airbus A320232 · Hydraulic System, Main
  > REF LOG PAGE 9748634, ECRA 2011-01000 MUST BE COMPLIED WITH FOR HYD FUILD SPILL IN AFT PIT ACCOMPLISHED ECRA 2011-01000 PART A, IMMEDIATE CLEAN UP OF HYD FUILD SPILL IN THE AFT PIT, REMOVED PIT FLOORBOARD 151LF IAW AMM 53-42-17, CLEANED LOWER FUSELAGE SKIN FRO
- [SDR CALA2024020900372](https://openairdocs.org/sdr/CALA2024020900372.md): Smoke Detector · faulted · Feb 7, 2024 · N459UA · Airbus A320232 · Smoke Detection
  > SMOKE DETECTOR FAULT FOUND 3WH SMOKE DETECTOR FAULTING. REPLACED SMOKE DETECTOR AND OPS CK REF AMM TASK 26-16-15-400-001-A TESTS PASS PARTS USED: 31-2610-3-0001,QTY:1.
- [SDR CALA2024012900246](https://openairdocs.org/sdr/CALA2024012900246.md): Anti-Ice Valve · low pressure · Jan 25, 2024 · N459UA · Airbus A320232 · Airfoil Anti/De-ice System
  > WING A.ICE R WING LO PR. WING A.ICE SYS FAULT AND WING A.ICE R WING LO PR. REMOVED AND REPLACED THE RIGHT HAND WING ANTI ICE VALVE, AND RELAY AT LOCATION 5DL. OPS CHECK GOOD LEAK CHECK GOOD.
- [SDR CALA2023050801390](https://openairdocs.org/sdr/CALA2023050801390.md): Frame · cracked · May 6, 2023 · N459UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR 68 STR 22 HAS CRACK INDICATION IN FLANGE RADIUS BEGINNING AT IB CAP RADIUS AND EXTENDING OB APPROX 1.00 INCH PER HAECO LCQ NR 9290240/36240 GENERATED BY V892444 CYCLES. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED ECRA5341-01390 ON OR BEFORE
- [SDR CALA2023050801388](https://openairdocs.org/sdr/CALA2023050801388.md): Stringer · cracked · May 5, 2023 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > LH FR 68 STR 22 HAS CRACK INDICATION IN FLANGE RADIUS BEGINNING AT IB CAP RADIUS AND EXTENDING OB APPROX.75 INCH PER HAECO LCQ NR 9290241/36241 GENERATED BY V892444 01391 ON OR BEFORE 49921 TOTAL FLIGHT CYCLES. PERFORM REPEAT INS OF ECRA 5341-01391 ON OR BEFO
- [SDR CALA2023050101293](https://openairdocs.org/sdr/CALA2023050101293.md): Frame · cracked · Apr 28, 2023 · N459UA · Airbus A320232 · Fuselage Main, Frame
  > FR43 FOOT LH FASTENER HOLE HAS A CRACK LIKE INDICATION AT 12 OCL OCK AND 1 OCLOCK IN FRAME LAYER. REMOVED AND REPLACED CRACKED FR43 LH FRAME AND FRAME FOOT IAW A3 20 SRM 51-72-11-911-001 AIRBUS REPAIR DWG 53370232 AND EA 5330-0 6692-003 AND A320 SRM 51-72-11-
- [SDR CALA2023050101292](https://openairdocs.org/sdr/CALA2023050101292.md): Beam · cracked · Apr 28, 2023 · N459UA · Airbus A320232 · Fuselage Main, Structure
  > FR43 FOOT RH FASTENER HOLE HAS A CRACK INDICATION AT 1 OCLOCK AN D 11 OCLOCK IN FRAME LAYER. REPLACED RH FR 43 FRAME AND FRAME FOOT IAW A320 AIRBUS DWG #533 70232 ISSUE D AND A320 SRM 51-72-11-911-001.
- [SDR CALA2023041901153](https://openairdocs.org/sdr/CALA2023041901153.md): Unknown · corroded · Apr 17, 2023 · N459UA · Airbus A320232 · Fuselage Structure (General)
  > R2 PAX DOOR SILL HAS CORROSION MULTIPLE SPOTS. GEN BY V937268 ON HAECO LCQ NR 9290267/36267 REPAIRED AREA ON R-2 DOOR SILL IAW A320 SRM 53-41-14-300-001 ACM P BY MECH V077956 INSP BY V892442
- [SDR CALA2022092802529](https://openairdocs.org/sdr/CALA2022092802529.md): Fastener · missing · Sep 28, 2022 · N459UA · Airbus A300* · Aileron Control System
  > PDA 3 FASTENER MISSING ON LEFT LOWER AILERON TRAILING EDGE. SEE PHOTO. ADDED PHOTO. UPON FURTHER INVESTIGATION LOWER AILERON HAVE FASTENER INSTALLED. NO DEFLECT FOUND
- [SDR CALA2022090702292](https://openairdocs.org/sdr/CALA2022090702292.md): None · none · Sep 7, 2022 · N459UA · Airbus A300* · Horizontal Stabilizer Structure
  > RETURN TO GATE REF REJECTED TAKE OFF ACP CHECK OF BRAKES REF AMM 05--51-16-200-001. CREW REPORTS BRAKE TEMP IN THE MID 400 DEGREES. BRAKES CK OK, NO DAMAGE NOTED PER CREW REJECTED T-O OCCURRED DUE TO FLEX T-O TEMPERATURE CLOSE TO STATION OAT
- [SDR CALA2022042501060](https://openairdocs.org/sdr/CALA2022042501060.md): None · inoperative · Apr 23, 2022 · N459UA · Airbus A300* · Engine Oil System (Airframe Furnished)
  > CREW REPORTS OIL QTY DROPPED TO ZERO THEN CAME BACK TO 1.5 TO 2.0 FLUX, CURRENTLY READING 18.0 CREW ELECTED TO RETURN TO DEN, MX TO MEET AND DEBRIEF CREW VERIFIED ENG 1 OIL QTY FULL. NO LEAKS. APPLIED MEL. VERIFIED ENG 1 OIL QTY FULL. NO LEAKS. APPLIED MEL. TO
- [SDR CALA2021092801724](https://openairdocs.org/sdr/CALA2021092801724.md): Fuel Cap · missing · Sep 28, 2021 · N459UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 FUEL CAP MISSING FROM AIRCRAFT INSTALLED NEW FUEL CAP. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1937103 SN OFF 1532 CAP, COUPLING R OFF 31-2825-9-0001 1532 ON 31-2825-9-0001 0332
- [SDR CALA2021092801706](https://openairdocs.org/sdr/CALA2021092801706.md): Fuel Cap · missing · Sep 28, 2021 · N459UA · Airbus A320232 · Aircraft Fuel System
  > FUEL CAP MISSING SEE LOG PAGE 7140736. NO DAMAGE TO AIRCRAFT.
- [SDR CALA2021030100242](https://openairdocs.org/sdr/CALA2021030100242.md): Profile · cracked · Feb 27, 2021 · N459UA · Airbus A320232 · Emergency Exits
  > A3NB-52-4-6031. LEFT FWD EMERGENCY EXIT DOOR, FWD AND AFT LOAD T RANSMITTING PROFILES CRACKED. REF BY PEMCO NR.10589.0324 REPLACED LH FWD EMERGENCY EXIT DOOR FWD AND AFT LOAD TRASMITTING PROFILES IAW A320 IPC 52-21-00-01B, A320 SRM 51-72-11-911-001, AND PEMCO
- [SDR CALA2020051700970](https://openairdocs.org/sdr/CALA2020051700970.md): Transceiver · defective · May 17, 2020 · N459UA · Airbus A320232 · Weather Radar System
  > CREW REPORTED WX RADAR INOP. - TOMC KROWN PFR SHOWES 34-41 NAV PRED W/S DET FAULT WITH ASSOCIATED 34-41-33 WXR1- 1SQ1. REF TSM 34-41-00-810-802-A WXR1-1SQ1 FAILS TEST. RESET NO HELP. SUSPECT BAD WXR TRANSCIVER 1SQ1-P/N 066-50008-04-09 M&E31-2311-9-0001. IPC34-

Next page: https://openairdocs.org/aircraft/N459UA/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 = 'N459UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N459UA/reports

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