# Service difficulty reports: N458UA

A list on [N458UA](https://openairdocs.org/aircraft/N458UA.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 · 150 reports

- [SDR CALA2026010612706](https://openairdocs.org/sdr/CALA2026010612706.md): Fuel Cap · missing · Jan 3, 2026 · N458UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTED THAT THE FUEL CAP IS MISSING. NO LEAKS NOTED FROM COUPLING. REPLACED FUEL CAP. OK FOR SVC.
- [SDR CALA2025112011366](https://openairdocs.org/sdr/CALA2025112011366.md): Actuator · faulted · Nov 19, 2025 · N458UA · Airbus A320232 · Trailing Edge Flap Actuator
  > F/CTL FLAPS FAULT ON APPROACH SLATS 1 / FLAPS 0 LOCKED FOR FIX, FLAPS STILL RETRACTED, PERFORMED DETAILED INSPECTION OF ALL MECHANICAL ITEMS, FOUND FLAP ACTUATOR #1 RT TORQUE LIMITER TRIPPED IAW TSM 27-51-00-810-810-A, PERFORMED RESET OF TORQUE LIMITER IAW A
- [SDR CALA2025091608958](https://openairdocs.org/sdr/CALA2025091608958.md): Slide · deployed · Sep 16, 2025 · N458UA · Airbus A320232 · Standard Practices/Structures
  > DOOR 1L SLIDE DEPLOYED. REPLACED DOOR 1L SLIDE. REF AMM 25-62-44-400-006-A. REPLACED DIAPHRAGM IN THE PERCUSSION MECHANISM. REF AMM 52-10-00-610-001-A. CHARGED THE EMERGENCY OPERATION CYLINDER. REF AMM 52-10-00-614-001-A. ALL OPS CHECK GOOD. AMM 25-62
- [SDR CALA2025091008726](https://openairdocs.org/sdr/CALA2025091008726.md): Fan · faulted · Sep 8, 2025 · N458UA · Airbus A320232 · Air Distribution Fan
  > NOTICED BURNING SMELL COMING FROM UPPER VENT BY COCKPIT ENTRY DOOR AND AMBER 'FAN' WARNING ON AIRCONDITIONING ECAM PAGE COMPLETED CABIN TEMP CONTROL TEST REF AMM TASK 21-21-00-710-052-B AND TEST FAILED. RECIEVED 'RECIRC FAN 2 OR SUPPLY' MESSAGE CREATED SEPERAT
- [SDR CALA2025073107127](https://openairdocs.org/sdr/CALA2025073107127.md): Rib · cracked · Jul 27, 2025 · N458UA · Airbus A320232 · Wing, Rib/Bulkhead
  > RIGHT MAIN LANDING GEAR SUPPORT RIB 5 FORWARD LUG INSPECTION FOUND CRACK ON RT MLG SUPPORT RIB 5 FORWARD LUG. AFT SIDE REF AVO14715, ACP STEPS 1,2 AND 3. CRACKED AS INDICATED. NO DAMAGE FOUND WITH 10X ON SURROUNDING AREAS AT RADII AND SURFACES. C/W FPI IAW NT
- [SDR CALA2025072806979](https://openairdocs.org/sdr/CALA2025072806979.md): Shroud · cracked · Jul 26, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CRACK ON REAR SKIN INBOARD UPPER SIDE OF RIGHT WING SHROUD BOX. REPAIR ACCOMPLISHED ON AEROMAN NR 2025-373234 IAW AEM EA 57-0073-25 AND EC/RA 5751-01579. REPAIR ACCOMPLISHED ON AEROMAN NON ROUTINE 20 25-373234 PER ECRA 5751-01579. NO REPEAT INSPECTIONS ARE
- [SDR CALA2025020200253](https://openairdocs.org/sdr/CALA2025020200253.md): Stringer · corroded · Jan 28, 2025 · N458UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO LEFT SIDE HAS CORRSION ON STRINGER 43 AT FRAME 59. FOUND STRINGER 43L FR54 TO FR60 TO BE OUT OF LIMITS AFTER CORROS CORROSION REMOVAL ACCOMPLISHED IAW A320 SRM 51-73-08. RESTORED S ION REMOVAL IAW A320 SRM 53-41-13-283-002 FIG.1 SHEET 1, AND A32 TR
- [SDR CALA2025020200254](https://openairdocs.org/sdr/CALA2025020200254.md): Skin · dented · Jan 27, 2025 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LOWER FUSE HAS 2EA DENTS AT APPROX 43-STR38R FR27 A3NB-05-3-6003
- [SDR CALA2025013000245](https://openairdocs.org/sdr/CALA2025013000245.md): Skin · damaged · Jan 27, 2025 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FR61 STR42R HAS SET MARK AT RIVET (A3NB-05-3-6003) PER HAECO LCQ NON ROUTINE 9298879/32879 INSPECTION IAW SRI 53-41-11-205-048 BY 20500 FC OR 41000 FH WITH 4600 FH. ORIGINAL DISCREPANCY FOUND ON LCQ NR 9298879. 4600 FH. ORIGINAL DISCREPANCY FOUN
- [SDR CALA2025012400192](https://openairdocs.org/sdr/CALA2025012400192.md): Skin · damaged · Jan 21, 2025 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FR 21 STR42 HAS ILLEGAL LIGHTNING STRIKE REPAIR 2 EA HI-LOCKS WI TH NO SPACING A3NB-05-3-6003.
- [SDR CALA2025012200171](https://openairdocs.org/sdr/CALA2025012200171.md): Door Sill · corroded · Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > MAIN CABIN, R-2 ENTRY SILL, AT FR 68 HAS CORROSION. REMOVED AND REPLACED R-2 DOOR SILL IAW A320 SRM 51-72-911-001-00 2.
- [SDR CALA2025012200170](https://openairdocs.org/sdr/CALA2025012200170.md): Stiffener · cracked · Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Main, Structure
  > RH FWD EMERGENCY EXIT HATCH AFT VERTICAL STIFFNER IS CRACKED. REMOVED AND REPLACED AFT VERTICAL STIFFENER ON RH FWD EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.
- [SDR CALA2025012200172](https://openairdocs.org/sdr/CALA2025012200172.md): Stiffener · cracked · Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH FORWARD EMERGENCY EXIT HATCH FWD VVERTICAL STIFNER IS CRACKED. REMOVED AND REPLACED FWD VERTICAL STIFFENER ON RH FWD EMERGENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11.
- [SDR CALA2025012100165](https://openairdocs.org/sdr/CALA2025012100165.md): Stiffener · cracked · Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH AFT EMERGENCY EXIT HATCH FWD VERTICAL STIFFNER IS CRACKED. REMOVED AND REPLACED VERT STIFFENER ON L/H AFT EMERGENCY EXIT IA W SRM A320 51-72-911-001.
- [SDR CALA2025012100164](https://openairdocs.org/sdr/CALA2025012100164.md): Stiffener · cracked · Jan 17, 2025 · N458UA · Airbus A320232 · Fuselage Main, Structure
  > LH AFT OVER WING EXIT AFT VERTICAL STIFFENER IS CRACKED. REMOVED AND REPLACED VERTICAL STIFFENER ON L/H OVER WING EXIT IA W A320 SRM 51-72-911-001. ACMP BY MECH V934190 INSP BY V935513
- [SDR CALA2025010700049](https://openairdocs.org/sdr/CALA2025010700049.md): Intercostal · cracked · Jan 6, 2025 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R/H FR16 DOOR STOP 1 HOLE NUMBER 3 HAS A CRACK INDICATION AT THE 9 O''CLOCK POSITION IN THE INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL AT FR 16 DOOR STOP #2 IAW A320 AMM 52-11-31-400-002-A.
- [SDR CALA2024123003184](https://openairdocs.org/sdr/CALA2024123003184.md): Skin · contaminated · Dec 27, 2024 · N458UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT FOLLOWING LOCATIONS 27 INCH INBOARD, 18 INCH TRAILING EDGE, 2 INCH DIAMETER "REPAIR BEFORE N EXT FLIGHT". REPAIRED ALL ELEVATOR LIQUID INGRESS @ LOCATION UPPER SKIN IAW A 320 SRM 55-21-11-300-005.
- [SDR CALA2024123003185](https://openairdocs.org/sdr/CALA2024123003185.md): Skin · contaminated · Dec 27, 2024 · N458UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT FOLLOWING LOCATIONS 45 INCH I NBOARD, 8 AND A HALF INCH TRAILING EDGE, 1 AND A HALF INCH DIAME TER "REPAIR BEFORE NEXT FLIGHT". DRILLED WITNESS HOLE @LOCATION ON UPPER SKIN FOUND NO LIQUID REP AIRED HOLE IN UPPER SKIN OF LH
- [SDR CALA2024102900946](https://openairdocs.org/sdr/CALA2024102900946.md): Autothrottle Sys · faulted · Oct 27, 2024 · N458UA · Airbus A320232 · Auto Throttle System
  > AUTO FLIGHT AUTO THRUST OFF ON ECAM DURING TAKEOFF ROLL. - CREW NOTED TAKEOFF ROLL REJECTED AROUND 40 KNOTS DUE TO ECAM. EMERGENCY BRAKE APPLICATION CHECK NOT APPLICABLE FOR CURRENT BRAKE TEMPS. NO ASSOCIATED FAULTS IN CFDS. NO MAINTENANCE ACTION NECESSARY PER
- [SDR CALA2024093000712](https://openairdocs.org/sdr/CALA2024093000712.md): Eec · failed · Sep 25, 2024 · N458UA · Airbus A320232 · Fuel Controlling System
  > E2 ESN V10226 - PLEASE R&R THE EEC DUE TO THE RECENT A/R, REF LP 9370004 & 9370032. REPORT FINDINGS AND ACTIONS WITHIN THIS LP. ESCPP@UNITED.COM, 847-700-8324 OP.4. CARRIED BY ELB REMOVED AND REPLACED #2 ENGINE EEC PER AMM 73-22-34. ALL OPS CKS NORMAL.PARTS US
- [SDR CALA2024050801391](https://openairdocs.org/sdr/CALA2024050801391.md): Pump · leaking · May 4, 2024 · N458UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > ECAM CAUTION MESSAGE - Y ENG PUMP LO PR MESSAGE INOP - HYD Y ENG PUMP LO PR. SD INDICATES LOW HYD QTY WHEN AIRCRAFT ARRIVED AT GATE NO YELLOW SYSTEM FLUID ON ECAM AND HYDRAULIC SERVICE PANNEL, FLUID LEAKING FROM #2 ENGINE. REF TSM 29-00-00-280-006-A-01, FOUN
- [SDR CALA2023122003667](https://openairdocs.org/sdr/CALA2023122003667.md): Idg · overtemp · Dec 16, 2023 · N458UA · Airbus A320232 · AC Generator-Alternator
  > DURING CRUISE NO.1 IDG OIL TEMP SPIKED TO 175.ECAM ELEC IDG OIL L O PR OVHT. OFF AND DISCONNCT RECONNECTED LEFT ENG IDG, OIL LEVEL CK NORMAL DPI NOT EXTENDED. ACCOMPLISH LEFT ENG IDLE RUN LEFT GENERATOR OPERATION NORMAL. STARTED TSM TASK 28-16-00-810-801-A FOR
- [SDR CALA2023040401039](https://openairdocs.org/sdr/CALA2023040401039.md): Flange · cracked · Apr 4, 2023 · N458UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE PERFORMING EA5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. 22 INNER CAP AND WEB HORIZONTAL FLANGE PER THE LATEST REVISION 22 INNER CAP AND WEB HORIZONTAL FLANGE PER THE LATEST
- [SDR CALA2023040401038](https://openairdocs.org/sdr/CALA2023040401038.md): Flange · cracked · Apr 4, 2023 · N458UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 31-SEPT-2023. EXPECTED TO BECOME A PERMANEN
- [SDR CALA2023040401037](https://openairdocs.org/sdr/CALA2023040401037.md): Flange · cracked · Apr 4, 2023 · N458UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > WHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 O REACHES 49,948 TOTAL FLIG
- [SDR CALA2023040401025](https://openairdocs.org/sdr/CALA2023040401025.md): Frame · cracked · Apr 4, 2023 · N458UA · Airbus A320232 · Fuselage Main, Frame
  > WHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 31-SEPT-2023. EXPECTED TO BECOME A PERMANEN
- [SDR CALA2023040401024](https://openairdocs.org/sdr/CALA2023040401024.md): Frame · cracked · Apr 4, 2023 · N458UA · Airbus A320232 · Fuselage Main, Frame
  > WHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 O REACHES 49,948 TOTAL FLIG
- [SDR CALA2023032000799](https://openairdocs.org/sdr/CALA2023032000799.md): Escape Hatch · cracked · Mar 17, 2023 · N458UA · Airbus A320232 · Emergency Exits
  > RH AFT EMERGENCY ESCAPE HATCH FWD PROFILE HAS CRACKS AT FASTENER HOLES. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-42-11 AND 51 1-72-11. CRACK LENGTH: 5.4IN. P/N: D5227902620451 BATCH# 0004068 83, TOP COAT WILL BE APPLIED USING JOB CARD# 53072, ATTACH
- [SDR CALA2022121203368](https://openairdocs.org/sdr/CALA2022121203368.md): Line · loose · Dec 12, 2022 · N458UA · Airbus A320232 · Hydraulic Pressure Indicator
  > GREEN HYD QTY LOW SERVICED GREEN SYSTEM HYD. OPERATED HYD SYSTEM FOR LEAK CHECK. NO LEAKS NOTED. RAN #1 ENGINE AND FOUND SUPPLY LINE ON EDP LOOSE. SECURED LINE AND NO LEAKS NOTED AT THIS TIME.
- [SDR CALA2022071501765](https://openairdocs.org/sdr/CALA2022071501765.md): None · missing · Jul 15, 2022 · N458UA · Airbus A320232 · Steering Unit
  > PDA 3 ONE SPRING CLIP BROKEN/MISSING ON NOSE GEAR ELECT BOX TOWING LEVER...SEE PHOTO PHOTO ADDED PARTS ADDED REF IPC 32-51-12-01E REPLACED SPRING CLIP ON TOWING LEVER.. REF IPC 32-51-12-01E.
- [SDR CALA2022061701529](https://openairdocs.org/sdr/CALA2022061701529.md): Fuel Cap · missing · Jun 14, 2022 · N458UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL REPORT SUBMITTED ON 6/17/22. PDA 3 FUEL CAP MISSING ON ARRIVAL PLACED ON CDL.REPLACED CAP COUPLING REFUEL OK FOR SERVICE.
- [SDR CALA2021020800132](https://openairdocs.org/sdr/CALA2021020800132.md): Fitting · worn · Feb 5, 2021 · N458UA · Airbus A320232 · Landing Gear Doors
  > LH MLG DOOR FWD HINGE AT KEEL BEAM HAS WEAR FROM DOOR FITTING A3 NB-06-3-6001 PER NR 9294246 HAECO NR 20246 GEN BY V892442. RMVD AND RPLD LH MLG DOOR FWD HINGE AT KEEL BEAM IAW A320 SRM 51 -42-11-801 PG.20 AND REPAIR DWG R53370500F BY MECH V903765 INSP BY V077
- [SDR CALA2020100901170](https://openairdocs.org/sdr/CALA2020100901170.md): Display · inoperative · Oct 9, 2020 · N458UA · Airbus A320232 · Central Display
  > CAPT'S NAVIGATION DISPLAY (ND), UNIT INOPERABLE. EIS CAPT ND INOPERABLE W/DIAGONAL LINE ACROSS ATTEMPTED RESET, PER QRH. UNSUCCESSFUL, REPLACED NR 1 DMC, REF AMM TASK 31-63-34-000-001-A. PEERFORMED OPE RATIONAL TEST OF THE LAND CAT III CAPABILITY, NO FAULTS
- [SDR CALA2020050200886](https://openairdocs.org/sdr/CALA2020050200886.md): Unknown · malfunctioned · May 1, 2020 · N458UA · Airbus A320232 · Fixed Inner Doors
  > AT CRZ ALT COCKPIT DOORHANDLE WILL NOT TURN TOOPEN DOOR-FEELS JA MMED CREW REPORTS UNABLE TO OPEN COCKPIT DOOR A CRUISE. TRIED SEVERAL TIMES DID NOT WANT TO BREAK ANYTHING. ON DECENT AT A LOWER CABIN PSI DOOR WOULD OPEN NORMALLY. INSPECTED THE COCKPIT DOOR HAN
- [SDR CALA2019011300087](https://openairdocs.org/sdr/CALA2019011300087.md): Seal · damaged · Jan 11, 2019 · N458UA · Airbus A320232 · Leading Edge Devices
  > LT WING NR 1 SLAT OB EDGE SEAL LWR FASTENER HOLE AND LEADING EDGE HAS DAMAGE SUPPORT TASK PER NR NO.9295226 REPAIRED LT WING NR 1 SLA OB EDGE SEAL IAW SRM 57-42-21-300 -004.
- [SDR CALA2019011300085](https://openairdocs.org/sdr/CALA2019011300085.md): Skin · gouged · Jan 11, 2019 · N458UA · Airbus A320232 · Wing, Plate/Skin
  > RT WING TOP SKIN INBD LE AT NUMBER ONE SLAT NUMBER ONE SLAT NUMBER ONE TRACK HAS GOUGE IN SKIN SPEC NR A3NB-57-3-6156 GEN BY NR 9294974. BLENDED GOUGE AND FOUND TO BE 0.022" DEEP AND OUT OF LIMITS IAW SRM 57-41-11-283-001. REPAIRED GOUGED SKIN IAW SRM 57-41-1
- [SDR CALA2019010700051](https://openairdocs.org/sdr/CALA2019010700051.md): Stringer · corroded · Jan 7, 2019 · N458UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO BILGE BETWEEN FR30 AND FR31 AT STR41L HAS CORROSION ON STRINGER A3NB-53-3-6105 PER NON ROUTINE 9295359 GENERATED BY V080285 BLENDED CORROSION BETWEEN FR30 & 31 ON STR 41L. FOUND TO BE OUT OF LIMITS PER AB DRWG 053231206 AS REF IN SRM 53-21-13-001. CU
- [SDR CALA2019010700047](https://openairdocs.org/sdr/CALA2019010700047.md): Stringer · not reported · Jan 7, 2019 · N458UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD PIT STR42R BETWEEN FR33 AND FR34 REQ''S REPAIR SUPPORT TASK AT PER REF NO.9295419. FABRICATED AND INSTALLED STR REPAIR IN FWD PIT STR 42R BWT FR33 AND FR 34 IAW SRM 53-21-13-300-004. THID REPAIR REQUIRES RE CURRENT INSPECTION AT 60,000 FC 120,000 FH WHICHE
- [SDR CALA2019010700046](https://openairdocs.org/sdr/CALA2019010700046.md): Cleat · corroded · Jan 7, 2019 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FR26 BETWEEN STRINGERS 42R-43R CLEAT HAS E LONGATED FASTENER HOLES AND SIGNS OF CORROSION UNDER FACE A3NB-5 3-3-6105 GENERATED ON NR 9295281 REPLACED CLEAT IAW SRM 53-21-12-001 AND REPAIRED ELONGATED HOLES IAW 53-00-11-300-022.THIS RPR RE
- [SDR CALA2019010700043](https://openairdocs.org/sdr/CALA2019010700043.md): Skin · cracked · Jan 6, 2019 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > IT IS MADE TO COMPLY WITH CFT 121.1109 PER AMM TASK 51-00-80-200 -801C1. EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN FR 25-26 S TGR 41L-43L A3NB-51-4-6001 GENERATED ON NR 9294204 REMOVED AND REINSTALLED NEW DOUBLER REPAIR IAW SRM 53-00-11 -300-042. THIS REPA
- [SDR CALA2019010600040](https://openairdocs.org/sdr/CALA2019010600040.md): Skin · corroded · Jan 5, 2019 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO BILGE BETWEEN FR30 AND FR31 AT STR41L HAS CORROSION ON STRINGER A3NB-53-3-6105. BLENDED CORROSION BETWEEN FR30 & 31 ON STR 41L. FOUND TO BE OUT OF LIMITS PER AB DRWG 053231206 AS REF IN SRM 53-21-13-001. CUT OUT DAMAGED AREA AND ACCOMPLISHED STRINGER
- [SDR CALA2019010600016](https://openairdocs.org/sdr/CALA2019010600016.md): Hinge Fitting · worn · Jan 3, 2019 · N458UA · Airbus A320232 · Landing Gear Doors
  > MLG RT MAIN DOOR FWD HINGE FITTING INNER FACE HAS WEAR MARKS. REMOVED AND REPLACED MGL RT MAIN DOOR FWD HINGE FITTING IAW SRM 51-42-11-001 AND SRM 51-44-11-001AND SRM 5172-11-911-001.
- [SDR CALA2019011200053](https://openairdocs.org/sdr/CALA2019011200053.md): Fitting · damaged · Jan 2, 2019 · N458UA · Airbus A320232 · Fuselage, Landing Gear Attach Fittings
  > LH MLG DOOR AFT UPPER ACTUATOR FITTING HAS GOUGE AT L09 HOLE 18- 0553-8-0008; FCD 5330-05575 AT PER REF NR 9295249. REMOVED AND REPLACED LH MLG AFT UPPER ACT FITING IAW 51-42-11 AND SB A320-53-1158.
- [SDR CALA2019011200052](https://openairdocs.org/sdr/CALA2019011200052.md): Stringer · corroded · Jan 1, 2019 · N458UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > A3NB-53-4-6179 AFT CARGO COMPT STR42R AT FR52+4 HAS CORROSION AT HAECO LCQ PER REF NO. 9295332. REMOVED CORROSION IAW SRM 74-00-001. HFEC INSP BLENDED AREA AND AROUND (3) OPEN HOLES. NO CORROSION OR CRACKS FOUND. HFEC ROTARY SCAN OF (3) HOLES. ALL HOLES ARE OU
- [SDR CALA2019010200011](https://openairdocs.org/sdr/CALA2019010200011.md): Fitting · preloaded · Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FOUND KEELBEAM RT FWD ACTUATOR FITTINGS PRELOADED ON REF 9295350 SUPPORT TASK. REMOVED AND REPLACED RT KEELBEAM FWD ACT FITTING IAW SRM 51-72-11-911-001.
- [SDR CALA2019010200009](https://openairdocs.org/sdr/CALA2019010200009.md): Skin · not reported · Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-51-4-6001; IT IS MADE TO COMPLY WITH CFR 121.1109 PER AMM T ASK 51-00-80-200-801C1. EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN FR64-65 STR 26L, 28L AT PER REF NO.9294208 REMVED AND REPLACED EXTERNAL FUSELAGE REPAIR DOUBLER AT FR64-65L IAW SRM 53-41-11-
- [SDR CALA2019010200008](https://openairdocs.org/sdr/CALA2019010200008.md): Intercostal · cracked · Dec 31, 2018 · N458UA · Airbus A320232 · Emergency Exits
  > A3NB-05-3-6165 RT AFT EMERGENCY EXIT HATCH FWD VERT INTERCOASTAL CRACKED BETWEEN RIVET TAILS. REMOVED AND REPLACED RT AFT EMER EXIT HATCH FWD VERT INTERCOASTAL IAW 52-21-18-960-003-A.
- [SDR CALA2019010200007](https://openairdocs.org/sdr/CALA2019010200007.md): Fitting · preloaded · Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > FOUND KEELBEAM RT AFT ACTUATOR FITTING PRELOADED ON REF 9295351 SUPPORT TASK. REMOVED AND REPLACED RT AFT ACTUATOR FITTING IAW SRM 51-72 -11-001, SRM 51-42-11-001 & 51-44-11-001.
- [SDR CALA2019010200006](https://openairdocs.org/sdr/CALA2019010200006.md): Plate · worn · Dec 31, 2018 · N458UA · Airbus A320232 · Landing Gear Doors
  > RT MLG DOOR FORWARD UPPER FITTING CONNECTING PLATE HAS WORKING FASTENERS ON REF 9294821 SUPPORT TASK. NR GENERATED REMOVED AND REPLACED RT MLG DOOR FWD UPPER FITTING CONNECTING PLATE IAW SRM 51-42-11-001 & 51-44-11-001, 51-72-11-911-00.
- [SDR CALA2019010200005](https://openairdocs.org/sdr/CALA2019010200005.md): Fitting · corroded · Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FORWARD CARGO PIT, FWD DOOR CUTOUT FITTING INBOARD OF CORNER FITTING CORRODED SPEC NO. A3NB-05-3-6013. REMOVED AND REPLACED FITTING INBD OF CORNER FITTING PER SRM 51-72-11-911-001 PAR 2A.

Next page: https://openairdocs.org/aircraft/N458UA/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 = 'N458UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N458UA/reports

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