# Service difficulty reports: N455UA

A list on [N455UA](https://openairdocs.org/aircraft/N455UA.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 4 · 173 reports

- [SDR CALA2026051216190](https://openairdocs.org/sdr/CALA2026051216190.md): Engine · smoke · May 11, 2026 · N455UA · Airbus A320232 · Engine Oil System (Airframe Furnished)
  > GRND PERSONNEL REPORTED WHITE SMOKE OUT OF THE LEFT ENGINE WHILE TAXING TO THE GATE. ACCOMPLISHED GENERAL VISUAL INSPECTION FOR ANY FUEL OR OIL LEAKS AND NONE FOUND. OIL QTY IS NORMAL, SUSPECT RESIDUAL FUEL IN BURNER CAN AREA BEING THE CAUSE. ACCOMPLISHED 3 M
- [SDR CALA2025122112275](https://openairdocs.org/sdr/CALA2025122112275.md): Fan · faulted · Dec 19, 2025 · N455UA · Airbus A320232 · Air Distribution Fan
  > NOISE COMING FROM AVION ICS BAY WITH LIGHT PUNGENT SMELL REQUEST MEL 2126AC APPROVED. MEL 2126AC REJECT TO CLEAR REMOVED AND REPLACED BLOWER FAN PER AMM 21-26-51-400-001-A OPS CHECK GOOD. NO FAULTS FOUND.
- [SDR CALA2025102210410](https://openairdocs.org/sdr/CALA2025102210410.md): Fuel Cap · missing · Oct 22, 2025 · N455UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISSING PLACED ON CDL 28A REF LP 6707105.
- [SDR CALA2025042104097](https://openairdocs.org/sdr/CALA2025042104097.md): Door · not closed · Apr 19, 2025 · N455UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR NOT SHOWING LOCKED INDICATION. CLOSED THE L1 DOOR AND ARMED THE SLIDE. DOOR LOCKED INDICATION NOW VISIBLE. REF AMM 52-10-00. CLOSED THE L1 DOOR AND ARMED THE SLIDE. DOOR LOCKED INDICATION NOW VISIBLE. REF AMM 52-10-00.
- [SDR CALA2025042104039](https://openairdocs.org/sdr/CALA2025042104039.md): Unknown · odor · Apr 19, 2025 · N455UA · Airbus A320232 · Air Distribution System
  > SMELL OF FUEL IN AFT CABIN. REPORTED BY FLIGHT ATTENDANTS ON LAN DING TOUCHDOWN RUN APU AND TESTED BOTH PACKS WITH APU BLEED ON, NO SMELL NOTED. PREFORMED TSM 05-50-00-810-831-A0, THE PARAMETERS GIVEN BY PILOT & TOMC REPORTING SHEET #1 PER DECISION TABLE SHOWS
- [SDR CALA2025021700369](https://openairdocs.org/sdr/CALA2025021700369.md): Pressure Blkhd · cracked · Feb 12, 2025 · N455UA · Airbus A320232 · Fuselage Main, Bulkhead
  > CRACK OF 0.350" APROX LENGTH COMING OUT FROM FASTENER AT LH SIDE FR35 FWD SURFACE TO THE PRESSURE BULKHEAD BELOW STR 30 LH. ACCOMPLISH A PERMANENT REPAIR AT LH FR35 STGR30LH FRAME WEB LATEST REVISION OF ECRA 5330-07424 ON OR BEFORE 11-AUG-25 PER HOLES #A AND
- [SDR CALA2025021400351](https://openairdocs.org/sdr/CALA2025021400351.md): Retainer · cracked · Feb 11, 2025 · N455UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > R/H ENGINE PYLON FWD END OF CORE FIRE SEAL RETAINER CRACKED I/B AND O/B SIDE REMOVED AND REPLACED DISCREPANT I/B AND O/B FIRE SEAL RETAINER A T R/H ENGINE PYLON FWD END OF CORE IAW A320 SRM. SFR NO. 1038395
- [SDR CALA2025020400275](https://openairdocs.org/sdr/CALA2025020400275.md): Skin · damaged · Jan 30, 2025 · N455UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FR34 STRG 43 HAS A REWORK AREA THAT IS OUT OF L IMITS CATECORY C.
- [SDR CALA2025013000247](https://openairdocs.org/sdr/CALA2025013000247.md): Hinge Arm · gouged · Jan 30, 2025 · N455UA · Airbus A320232 · Rudder Structure
  > VERTICAL STABILIZER NO 5 RUDDER HINGE ARM FITTING SPHERICAL BEAR ING BORE INNER DIAMETER GOUGED. GENERATED BY V061070 ON HAECO LC Q NR 9292527/36527
- [SDR CALA2025012900235](https://openairdocs.org/sdr/CALA2025012900235.md): Fitting · cracked · Jan 29, 2025 · N455UA · Airbus A320232 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST UPPER ATTACHMENT, 3RD HOLE AT LOWER FACE MARKED, HAS CRACK INDICATION IN FRAME LAYER. 50% S.H. PERFORMED PERMANENT REPAIR BY GUSSET REPLACEMENT AS DIRECTED BY ECRA 5311-01953.
- [SDR CALA2025013000246](https://openairdocs.org/sdr/CALA2025013000246.md): Web · cracked · Jan 24, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH FLOOR STRUCTURE BETWEEN FR 10 AND 11 WEB IS CRACKED.
- [SDR CALA2025012700205](https://openairdocs.org/sdr/CALA2025012700205.md): Cover · corroded · Jan 22, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO TORSION BOX COVER SHEET UPPER SURFACE HAS SEVERAL SPOT S OF CORROSION BETWEEN FR 53-56. GEN BY N078570 ON HAECO LCQ NR 9293020/37020
- [SDR CALA2025012100162](https://openairdocs.org/sdr/CALA2025012100162.md): Spar · cracked · Jan 20, 2025 · N455UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > R/H PYLON O/B SLIDE SPAR DOUBLER HAS CRACK. R & R R/H PYLON O/B SPAR IAW A320 SRM 51-75-12-911-001.
- [SDR CALA2025012300186](https://openairdocs.org/sdr/CALA2025012300186.md): Floor Support · corroded · Jan 17, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT BULK CARGO FR 58-59 RSTR 38 PROFILE PANEL HAS CORROSION. GEN BY V798788 ON HAECO LCQ NR 9292817 / 36817 REMOVED AND REPLACED PROFILE PANEL AFT CARGO FROM FR 58 - FR59 I AW A320 SRM 51-42-11.
- [SDR CALA2025012300185](https://openairdocs.org/sdr/CALA2025012300185.md): Web · corroded · Jan 17, 2025 · N455UA · Airbus A320232 · Wing Miscellaneous Structure
  > #2 MOVABLE FAIRING INTERNAL WEB CORRODED. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11-001.
- [SDR CALA2025012100154](https://openairdocs.org/sdr/CALA2025012100154.md): Seat Track · corroded · Jan 17, 2025 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK +Y765 CORROSION OUT OF LIMITS FRAME 63. REMOVED SEAT TRACK +Y765 OUT OF LIMITS FRM 61 / FRM 64 IAW A320 SRM 51-42-11/001 REV 151, REPAIRED AREA ON FRM 61 / FRM 64 IAW A 320 SRM 53-41-15-300-003 REV 151 PAR 2.
- [SDR CALA2025012100146](https://openairdocs.org/sdr/CALA2025012100146.md): Cover · corroded · Jan 16, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO TORSION BOX COVER SHEET HAS SEVERAL SPOTS OF CORROSION B/W FR 26-27. REMOVED AND REPLACED TORSION BOX COVER SHEET AT FWD CARGO DOOR F R24-28 IAW A320 SRM 51-72-11-911-001 SRM 51-72-11-911-002 AND SR M 51-42-11-001.
- [SDR CALA2025012100150](https://openairdocs.org/sdr/CALA2025012100150.md): Fitting · corroded · Jan 15, 2025 · N455UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > LEFT PYLON SPIGOT BEARING RETAINER PLATE,RECEPTACLE FITTING AND SLEEVE HAVE CORROSION.. REMOVED & REPLACED #1 PYLON SPIGOT BEARING FITTING IAW A320 SRM 54-51-12-300-002. REPLACED SPIGOT SLEEVE IAW AMM 57-26-12-400-00 2-A.
- [SDR CALA2025012100147](https://openairdocs.org/sdr/CALA2025012100147.md): Fitting · corroded · Jan 15, 2025 · N455UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT PYON SPIGOT BEARING RECEPTACIE FITTING AND SLEEVE HAVE CORROSION. REMOVED & REPLACED #2 PYLON SPIGOT FITTING IAW A320 SRM 54-51-12 -300-002. REPLACED SPIGOT SLEEVE IAW AMM 57-26-12-400-002-A.
- [SDR CALA2025011600131](https://openairdocs.org/sdr/CALA2025011600131.md): Web · cracked · Jan 15, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH FLOOR STRUCTURE B/W FR10 AND 11 WEB IS CRACKED. REMOVED & REPLACED 1 EACH WEB IN THE COCKPIT FLOOR STRUCTURE BTW N FRM 10-11 ICW A320 SRM 51-92-11/001 & 51-72-11-911-001.
- [SDR CALA2025011400117](https://openairdocs.org/sdr/CALA2025011400117.md): Floor Support · corroded · Jan 10, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR STRUCTURE CORROSION AT RH FLOOR BEAM Y-81 AT FR 14 AT I/B FWD MONUMENT MOUNT. GENERATED BY ON HAECO LCQ NR 9292880 / 36880 REMOVED AND REPLACED FLOOR BEAM -Y81 FR 12-14 IAW A320 SRM 51-42 -11 P18-21
- [SDR CALA2025011500128](https://openairdocs.org/sdr/CALA2025011500128.md): Floorbeam · corroded · Jan 9, 2025 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR STRUCTURE CORROSION AT L/H Y 1732 FR 68.
- [SDR CALA2025011400115](https://openairdocs.org/sdr/CALA2025011400115.md): Floor Support · corroded · Jan 9, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR BEAM Y1292 HAS CORROSION BETWEEN 67 AND 68.
- [SDR CALA2025011300093](https://openairdocs.org/sdr/CALA2025011300093.md): Seat Track · corroded · Jan 9, 2025 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK +Y765 CORROSION OUT OF LIMITS FR 35-36. REMOVED & REPLACED 1 EACH SEAT TRACK BETWEEN FRM 35-36 IAW A320 SRM 51-42-11/001 51-49-00/001.
- [SDR CALA2025011300091](https://openairdocs.org/sdr/CALA2025011300091.md): Seat Track · corroded · Jan 9, 2025 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN FLOOR STRUCTURE CORROSION AT SEAT TRACK Y-1292 AT MOUNT RECEPTACLE AT FR 66. REMOVED AND REPALCED DISCREPANT FLOOR BEAM AT Y1292 FR 66-68 IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025011300088](https://openairdocs.org/sdr/CALA2025011300088.md): Seat Track · corroded · Jan 9, 2025 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK Y765 FR 24-35 CORROSION OUT OF LIMITS. REMOVED AND REPLACED +Y765 FR24-35 SEAT TRACK IAW A320 SRM 57-72 -12-911-001.
- [SDR CALA2025011300097](https://openairdocs.org/sdr/CALA2025011300097.md): Floor Support · corroded · Jan 8, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR STRUCTURE CORROSION AND BROKEN FASTENERS AT RH P ROFILE FWD OF R-1 DOOR FR 13 TO FR 16. REMOVED AND REPLACED FWD CABIN FLOOR ANGLE ASSY AT RH PROFILE FW D OF R-1 DOOR FR13 TO FR16 IAW SRM 57-42-11/001 PARA D.
- [SDR CALA2025011300089](https://openairdocs.org/sdr/CALA2025011300089.md): Floorbeam · corroded · Jan 8, 2025 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR BEAM Y512.5 HAS CORROSION. REMOVED AND REPLACED AFT CABIN FLOOR BEAM Y512.5 IAW A320 SRM 51 -72-11-911-001.
- [SDR CALA2025011300087](https://openairdocs.org/sdr/CALA2025011300087.md): Web · corroded · Jan 8, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN CORROSION AT R/H WEB Y-1732 AT FR20 O/B OF R/H FLOOR BEAM Y-1584 I/B OF R-1 DOOR FRAME. REMOVED AND REPLACED RH WEB Y-1732 AR FR20 IAW A320 SRM 51-42-11 PAGE 18-21.
- [SDR CALA2025011700133](https://openairdocs.org/sdr/CALA2025011700133.md): Skin · dented · Jan 7, 2025 · N455UA · Airbus A320232 · Passenger/Crew Doors
  > R-2 DOOR EXTERNAL MID LOWER SURFACE HAS DENT (A3NB-52-4-6024) PE R HAECO LCQ NON ROUTINE 9292021/36021 ACCOMPLISHED DOUBLER & FILLER INSP AT 60,000 FC FROM RPR EMBODIMENT IAW SRI RPR IAW SRM 52-10-00-300-005. THIS IS A CAT B RPR & REQUIRES 52-10-00-205-011.WO
- [SDR CALA2025011300096](https://openairdocs.org/sdr/CALA2025011300096.md): Floor Support · cracked · Jan 7, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH FR 4 FLOOR SUPPORT ANGLE CRACKED. REMOVED AND REPLACED DISCREPANT FR4 L/H FLOOR SUPPORT ANGLE IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025010800059](https://openairdocs.org/sdr/CALA2025010800059.md): Skin · contaminated · Jan 7, 2025 · N455UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT 29 IN FROM INBOARD, 14 IN FRO M TRAILING EDGE, 1 1/2 IN DIAMITER.
- [SDR CALA2025010800058](https://openairdocs.org/sdr/CALA2025010800058.md): Skin · contaminated · Jan 7, 2025 · N455UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT 141 A/2 IN FROM INBOARD, 16 I N FROM TRAILING EDGE, A 1/2 IN DIAMITER.
- [SDR CALA2025010700055](https://openairdocs.org/sdr/CALA2025010700055.md): Floorbeam · gouged · Jan 6, 2025 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOOR BEAM -Y106.5 FRAME 70 HAS GOUGE ON HARD POINT.
- [SDR CALA2025010700054](https://openairdocs.org/sdr/CALA2025010700054.md): Door Sill · corroded · Jan 6, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R-2 DOOR SHAPE SILL UPPER SURFACE HAS CORROSION (3EA) SPOTS.
- [SDR CALA2025010700056](https://openairdocs.org/sdr/CALA2025010700056.md): Floorbeam · corroded · Jan 4, 2025 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FWD CABIN FLOOR STRUCTURE CORROSION AT L/H FLOOR BEAM Y 503.2 AT FR 16 ABOVE RUDDER AND THSA CABLES. RMVD+RPLCD DISPLACED Y503.2 FLOOR SUPPORT FR12-20 IAW A320 SRM 5 1-42-11-001 + 51-72-11-911-001.
- [SDR CALA2025010600031](https://openairdocs.org/sdr/CALA2025010600031.md): Floor Support · gouged · Jan 3, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT -Y254 HAS GOUGE. REMOVED AND REPLACED -Y254 FLOOR SUPPORT IAW A320 SRM 51-72-11-911- 001.
- [SDR CALA2025010600027](https://openairdocs.org/sdr/CALA2025010600027.md): Panel · cracked · Jan 2, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO FR 56-58 RSTR 38 PROFILE PANEL IS CRACKED. REMOVED & REPLACED AT AFT CARGO FR56-FR58 STR 38 PROFILE PNL IAW A320 SRM 51-42-11/001 - SRM 51-72-11-911-001.
- [SDR CALA2025010600030](https://openairdocs.org/sdr/CALA2025010600030.md): Floor Support · corroded · Jan 2, 2025 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CABIN FLOOR SUPPORT Y765 HAS CORRISOION.
- [SDR CALA2025010600037](https://openairdocs.org/sdr/CALA2025010600037.md): Shear Web · corroded · Dec 31, 2024 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN SHEAR WEB ON LH SIDE HAS CORRISION. REMOVED AND REPLACED L/H SHEAR WEB @ AFT CABIN IAW A320 SRM 51-4 2-11/001.
- [SDR CALA2025010600036](https://openairdocs.org/sdr/CALA2025010600036.md): Shear Web · corroded · Dec 31, 2024 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN SHEAR WEB ON RH SIDE HAS CORRISION. REMOVED AND REPLACED R/H SHEAR WEB @ AFT CABIN IAW A320 SRM 51-4 2-11/001.
- [SDR CALA2025010300018](https://openairdocs.org/sdr/CALA2025010300018.md): Seat Track · corroded · Dec 31, 2024 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CABIN FLOOR STRUCTURE CORROSION AT L/H SEAT TRACK Y Y 765 AT MOUNT RECEPTACLE AT FR 66. REMOVED AND REPLACED LH SEAT TRACK AT FR66 IAW A320 SRM 51-42-11 P 18-21.
- [SDR CALA2025010300017](https://openairdocs.org/sdr/CALA2025010300017.md): Seat Track · corroded · Dec 31, 2024 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK -1292 FRAME 20 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK -Y1292 FN 12-24 IAW A320 SRM 51- 42-11/001.
- [SDR CALA2025010300015](https://openairdocs.org/sdr/CALA2025010300015.md): Plate · corroded · Dec 31, 2024 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT BULK CARGO FR 59-63 LSTR 38 PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED PROFILE PNL AT AFT CARGO FR 59-63 STR 38 IA W SRM 51-42-11/001.
- [SDR CALA2024123103199](https://openairdocs.org/sdr/CALA2024123103199.md): Floorbeam · corroded · Dec 29, 2024 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR BEAM -Y1292 HAS CORROSION BETWEEN FR68-69 GEN BY V918855 ON HAECO LCQ NR 9292769/36769 REMOVED AND REPLACED FLOOR BEAM -Y1292 FR 68-69 IAW A320 SRM 51- 42-11 P 18-21.
- [SDR CALA2024123103198](https://openairdocs.org/sdr/CALA2024123103198.md): Floorbeam · corroded · Dec 28, 2024 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > FWD CABIN CORROSION AT L/H SEAT TRACK Y1292 AT FR24. REMOVED AND REPLACED FWD CABIN LH SEAT TRACK +Y1292 FR12-24 IAW A320 SRM 51-42-11 P18-21.
- [SDR CALA2024123003179](https://openairdocs.org/sdr/CALA2024123003179.md): Floorbeam · corroded · Dec 27, 2024 · N455UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CABIN FLOOR BEAM Y160.5 HAS CORROSION. REMOVED AND REPLACED Y160.5 FLOORBEAM IN AFT CABIN AT FR68 AND 7 0 IAW A320 SRM 53-41-14-283-809 51-42-11 51-44-11/001 51-75-12-9 11-003 AND AMM 51-78-00-916-001.
- [SDR CALA2024123003178](https://openairdocs.org/sdr/CALA2024123003178.md): Floor Support · corroded · Dec 27, 2024 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR BEAM - Y1292 HAS CORROSION BETWEEN FRAMES 67 AND 68. REMOVED AND REPLACED FLOOR BEAM -Y1292 FR67-68 IAW A320 SRM 51-4 2-11 P 18-21.
- [SDR CALA2024122603162](https://openairdocs.org/sdr/CALA2024122603162.md): Seat Track · corroded · Dec 24, 2024 · N455UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK -765 FRAME 20 HAS CORROSION. REMOVED AND REPLACED CABIN SEAT TRACK -Y765 FRM 12-24 IAW A320 S RM 51-42-11 P18-21.
- [SDR CALA2024122303142](https://openairdocs.org/sdr/CALA2024122303142.md): Floor Support · corroded · Dec 20, 2024 · N455UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR STRUCTURE GOUGE/CORROSION AT R/H SEAT TRK Y-765 AT FR 66. REMOVED AND REPLACED FLOOR BEAM Y-765 FROM FR64 TO FR66 AFT CABI N IAW A320 SRM 51-42-11.

Next page: https://openairdocs.org/aircraft/N455UA/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 = 'N455UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N455UA/reports

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