# Service difficulty reports: N454UA

A list on [N454UA](https://openairdocs.org/aircraft/N454UA.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 · 126 reports

- [SDR CALA2026091419405](https://openairdocs.org/sdr/CALA2026091419405.md): Battery · faulted · Sep 11, 2026 · N454UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - EPSU BAT CAP AFT L FAULT. REMOVED AND REPLACED BATTERY AMM REF 33-51-38-400-002-A. OPS CHECK OK, OK FOR SERVICE.
- [SDR CALA2026080218149](https://openairdocs.org/sdr/CALA2026080218149.md): Spoiler · damaged · Jul 29, 2026 · N454UA · Airbus A320232 · Spoilers
  > LEFT WING NR 2 SPOILER DAMAGED, REMOVED NR 2 LT SPOILER IAW AMM 27-64-42-000-001-A, TRIMMED OUT DAMAGED SKIN SECTION SIZE= 1.0" DIA. CLEANED, INSTALLED COMPOSITE REPAIR, CURED, RESTORED PAINT FINISH AND REINSTALLED PREVIOUSLY REMOVED SEAL AND SEAL RETAINER I
- [SDR CALA2026061717163](https://openairdocs.org/sdr/CALA2026061717163.md): Uplock · faulted · Jun 15, 2026 · N454UA · Airbus A320232 · Landing Gear Position and Warning
  > NOSE LANDING GEAR DOORS DID NOT CLOSE UPON RETRACTING GEAR ON TAKEOFF. CYCLED NO JOY. NLG DOORS DID NOT LOSE UPON RETRACTING GEAR ON TAKEOFF. CYCLED NO JOY. PERFORMED REMOVAL OF THE NLG DOOR-UPLOCK ASSY IAW AMM 32-31-14-000-001. CHECKED MATING SURFACES &
- [SDR CALA2026031014455](https://openairdocs.org/sdr/CALA2026031014455.md): Unknown · odor · Mar 7, 2026 · N454UA · Airbus A320232 · Air Distribution System
  > AIRCRAFT HAD AN ODOR IN BACK, AFTER LIGHTNING STRIKE. C/W TSM TASK 21-00-00-615-802-A, NO SMELL FOUND..NO LIGHTNING STRIKE EVIDENCE FOUND. OK TO CONTINUE
- [SDR CALA2025102010308](https://openairdocs.org/sdr/CALA2025102010308.md): Bottle · low pressure · Oct 20, 2025 · N454UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR 2L PRESSURE IS LOW. PRESSURE IS 1650. DOOR PRESSURE IS SERVICABLE PER AMM 52-13-14-200-001-A.
- [SDR CALA2025093009426](https://openairdocs.org/sdr/CALA2025093009426.md): Tire · bulged · Sep 27, 2025 · N454UA · Airbus A320232 · Tire
  > NR 3 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. RAMP REPORT: NR 3 TIRE HAS A LARGE BULGE AT THE 6 O'OCLOCK POSITION. WILL NEED REPLACEMENT REPLACED #3 MLG TIRE REF. AMM 32-41-11-400-006-A.
- [SDR CALA2025081507803](https://openairdocs.org/sdr/CALA2025081507803.md): Filter · odor · Aug 15, 2025 · N454UA · Airbus A320232 · Air Distribution System
  > SECOND HALF OF FLT NOTICED AN ACCRID OR SMELLY GYM SOCKS WITH PACKS ON. NO SMOKE PRESENT. PER CREW ODOR CONTINOUS WITH APU RUNNING & IN FLIGHT DECK, REF TSM 05-50-810-831-A. APU NEEDS INSPECTION IAW AMM 49-00-00-200-816. NOTED BY MAINT. NO PRIOR HISTORY.
- [SDR CALA2025042504219](https://openairdocs.org/sdr/CALA2025042504219.md): Aoa · faulted · Apr 24, 2025 · N454UA · Airbus A320232 · Stall Warning System
  > GRAPHIC DISPLAY OF VLS ON ND IS 5 KNOTS HIGHER THAN FMGC. ND SHO WS VLS SAME AS APP SPEED CREW STATED DISCREPANCY WAS VISIBLE IN BOTH PFDS. FOLLOWED TSM 22-66-00-810-889-A LAST LEG CLASS 3 FAULTS DISPLAYS AOA SENSOR1 ( 3FP1)", ADR1 TEST SHOWS MSG AOA SENSOR
- [SDR CALA2025010601819](https://openairdocs.org/sdr/CALA2025010601819.md): Battery · no test · Jan 3, 2025 · N454UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY EMER L 33-51-38 12WL FAILS BATTERY TEST. LOWER FLOOR PANEL REMOVED ROW 21A REMOVED AND REPLACEDEPSU BATTERY MERL, PER 33-51-11, TEST OK. PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024110801080](https://openairdocs.org/sdr/CALA2024110801080.md): None · none · Nov 5, 2024 · N454UA · Airbus A320232 · Standard Practices/Structures
  > FA EMERGENCY CHECKLIST BEHIND SEAT 3B NEEDS TO BE REPLACED. VERIFIED F/A EMERGENCY CHECKLIST WAS REPLACED IN THE BACK OF SEAT 3B.
- [SDR CALA2024090302367](https://openairdocs.org/sdr/CALA2024090302367.md): Blowout Panel · missing · Aug 29, 2024 · N454UA · Airbus A320232 · Wing Main, Frame Structure
  > TEST FLIGHT, RIGHT WING BLOW OUT PANEL 622AB MISSING.
- [SDR CALA2024083000513](https://openairdocs.org/sdr/CALA2024083000513.md): Blowout Panel · missing · Aug 29, 2024 · N454UA · Airbus A320232 · Wing Main, Frame Structure
  > PDA 2 UPON RETURN OF TEST FLIGHT 3836 IN LCQ. FOUND PANEL # 622AB MISSING FROM RT WING LEADING EDGE REF LOG PAGE 9081839. IAW GMM 02-30-95. UPDATED TO ATTACH IMAGE. RT WING PANEL 622AB FOUND MISSING AFTER TEST FLIGHT.
- [SDR CALA2024082602282](https://openairdocs.org/sdr/CALA2024082602282.md): Hinge Arm · cracked · Aug 20, 2024 · N454UA · Airbus A320232 · Horizontal Stabilizer Structure
  > RIGHT HORIZONTAL STAB NR 3 HINGE ARM CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB NR 3 HINGE ARM IAW SRM 51-42-11/0 01.
- [SDR CALA2024082102248](https://openairdocs.org/sdr/CALA2024082102248.md): Flange · damaged · Aug 17, 2024 · N454UA · Airbus A320232 · Fuselage Main, Structure
  > EA 5310-07639 REQUIRES UPDATED ECRA. CLEARING LP.RII INSPECTION C/W BY HAECO LCQ INSP LC-66 QC RECORDS UPDATE PLANNING TO CONTACT ENGINEERING AFTER 68,165 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 69,165 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE PART 2B INSPECTION R
- [SDR CALA2024081202197](https://openairdocs.org/sdr/CALA2024081202197.md): Threshold · corroded · Aug 10, 2024 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD PIT THRESHOLD FR 27 CORROSION NOTED AT TIE DOWN LOCATION PER HAECO LCQ 9298941/36941.
- [SDR CALA2024072602114](https://openairdocs.org/sdr/CALA2024072602114.md): Floor Support · cracked · Jul 26, 2024 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLIGHT DECK HAS 1 EA CRACKED FLOOR WEBS 1 ON CAPT. SIDE. GENERAT ED BY PER HAECO LCQ NR9298360/36360 REMOVED AND REPLACED WEB IN FLIGHT DECK L/H FR 8-11 IAW A320 SRM 51-72-11. ACCOMPLISHED BY INSPECTED BY
- [SDR CALA2024072602113](https://openairdocs.org/sdr/CALA2024072602113.md): Floor Support · cracked · Jul 26, 2024 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RH FLIGHT DECK CRACKED FLOORBEAM AT FR8-11. GENERATED BY ON HAECO LCQ NR 9298874/36874 REMOVED AND REPLACED WEB IN FLIGHT DECK R/H FR 8-11 IAW A320 SRM 51-72-11. PERFORMED BY INSPECTED BY
- [SDR CALA2024072902118](https://openairdocs.org/sdr/CALA2024072902118.md): Torque Box · corroded · Jul 24, 2024 · N454UA · Airbus A320232 · Fuselage Structure (General)
  > AFT PIT TORSION BOX COVER CORRODED. REMOVED AND REPLACED TORSION BOX COVER AT AFT PIT IAW A320 SRM 5 1-42-11-001
- [SDR CALA2024071902065](https://openairdocs.org/sdr/CALA2024071902065.md): Skin · abnormal · Jul 14, 2024 · N454UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR TOP SIDE HAS LIQUID INGRESS AT 91 INCHES FROM I/B 5 1/2 INCHES FROM TRAILING EDGE 2 INCHES IN DIAMETER. DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SURFACE 91 IN FROM VB 5.5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006 A PAR 4 A(6)
- [SDR CALA2024071502036](https://openairdocs.org/sdr/CALA2024071502036.md): Profile · gouged · Jul 11, 2024 · N454UA · Airbus A320232 · Emergency Exits
  > EMERGENCY EXIT INTERNAL STRUCTURE R/H FWD HATCH GOUGES ON AFT LO AD TRANSMITTING PROFILE. REMOVED AND REPLACED AFT FRAME SEGMENT ON FWD O/W HATCH RH IAW A 320 SRM 51-72-11-911-001
- [SDR CALA2024071502035](https://openairdocs.org/sdr/CALA2024071502035.md): Profile · gouged · Jul 11, 2024 · N454UA · Airbus A320232 · Emergency Exits
  > EMERGENCY EXIT INTERNAL STRUCTURE R/H FWD GOUGES ON FWD LOAD TRA NSMITTING PROFILE. REMOVED AND REPLACED FWD FRAME SEGMENT ON FWD O/W HATCH IAW A320 SRM 51-72-11-911-001
- [SDR CALA2024052201558](https://openairdocs.org/sdr/CALA2024052201558.md): Battery · discharged · May 22, 2024 · N454UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSI BATTERY EMER R AND EPSU BATTERY AFT L MSGS PRESENT R&R EMER R AND AFT L EPSU BATTERY PACKS REF AMM 33-51-38. OPS CK GOOD OF BOTH PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024040901008](https://openairdocs.org/sdr/CALA2024040901008.md): Computer · intermittent · Mar 28, 2024 · N454UA · Airbus A320232 · Leading Edge Slat Control System
  > SLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL FOLLOW TSM 27-51-00-810-806-A C/W 27-51-00-810-06A NO FAULTS FOUND. LOOK IN LAST LEG REPORT FOR SLAT FOUND DE POWER INTERRUPT WITH NO T/S DATA REF TSM 27-81-00-810-811A. CLEARS DEFECT. DUE TO HISTORY W
- [SDR CALA2024010200005](https://openairdocs.org/sdr/CALA2024010200005.md): Fuel Cap · missing · Dec 29, 2023 · N454UA · Airbus A320232 · Fuel Storage
  > DURING WALK AROUND FOUND REFUELING CAP COUPLING MISSING CAP COUPLING NIS AT SFO, REQ DEFERRAL INSTALLED NEW REFUEL COUPLING CAP PER AMM 28-25-41-400-005-A. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1555928 SN OFF 2814 CAP, COUPLING R OFF 31-2825-9-0001 281
- [SDR CALA2022121903423](https://openairdocs.org/sdr/CALA2022121903423.md): Fitting · cracked · Dec 17, 2022 · N454UA · Airbus A320232 · Fuselage Main, Structure
  > F.O LOWER WINDHISELD CONTINUITY FITTING AT LOWER CENTER POST PRODUCED A CRACK INDICATION DURING THE HFEC INSPECTION. GENERATED A T HAECO LCQ PER NR 9298244 (32244) BY V061690 EA 5310-07675 AD 2 020-17-03. THE FRONT WINDSHIELD FRAME RH CONTINUITY FITTING, ACCOM
- [SDR CALA2022112503216](https://openairdocs.org/sdr/CALA2022112503216.md): Frame · cracked · Nov 23, 2022 · N454UA · Airbus A320232 · Fuselage Main, Frame
  > FR 68 RH AT STR 22 HAS CRACK INDICATION IN RADIUS ABOVE LOWER IB BOLT. (EA RELATED). GENERATED BY V892444 AT HAECO LCQ PER NR 92 98138(32138). INITIAL INSP AT RH FR68 STR22 RPR PART HORZ FLANGE & INNER CAP N OR BEFORE 49,080 TOTAL ACFT FC. ACMP REPEAT INSP NOT
- [SDR CALA2022111703156](https://openairdocs.org/sdr/CALA2022111703156.md): Floor Support · corroded · Nov 16, 2022 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN, R-2 DOOR ENTRYWAY SILL PLATE CORRODED. GEN BY V913126 ON HAECO LCQ NR 9298338/32338 REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001 AND A320 SRM 51-42-11-001. ACMP BY MECH V077956 INSP BY N078570
- [SDR CALA2022110203009](https://openairdocs.org/sdr/CALA2022110203009.md): Skin · contaminated · Oct 31, 2022 · N454UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECTION. INDICATION LOCATION IS 16.25IN FR OM INBD EDGE AND 8.75IN FWD OF THE T/E. 1.25 INCH WIDTH BY 1.5IN LENGTH. GENERATED AT HAECO LCQ PER NR 9298181 (32181) BY V06169 0
- [SDR CALA2022110203008](https://openairdocs.org/sdr/CALA2022110203008.md): Skin · contaminated · Oct 31, 2022 · N454UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECTION. INDICATION LOCATION IS 15.5 IN FR OM INBD EDGE AND 24.5IN FWD OF THE T/E. 1 IN WIDTH BY 1.5 IN LEN GTH. GENERATED AT HAECO LCQ PER NR 9298182 (32182) BY V061690. {E
- [SDR CALA2022110203007](https://openairdocs.org/sdr/CALA2022110203007.md): Skin · contaminated · Oct 31, 2022 · N454UA · Airbus A320232 · Elevator Control System
  > R/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECION. INDICATION LOCATION IS 13.5 IN FRO M INBD EDGE AND 9 IN FWD OF THE T/E. 1 INCH WIDTH BY 1.5 INCH LE NGTH. GENERATED AT HAECO LCQ PER NR 9298180 (32180) BY V061690. {
- [SDR CALA2022050601161](https://openairdocs.org/sdr/CALA2022050601161.md): Accumulator · overserviced · May 6, 2022 · N454UA · Airbus A320232 · Hydraulic Filter, Main
  > LOWSPEED ABORT DUE TO BLUE HYD LO AIR PR ECAM VERBAL FROM CAPTAIN: THERE WAS NOT "HYD B RSVR LO AIR PR" MSG. T/S PER TSM 29-12-00-810-801A FOUND BLUE SYS OVERSERVICED AND ACCUMLATOR PRESS LOW. SERVICED ACCUMLATOR AND DRAINED RES IAW AMM 29-10-00-680-003A AND
- [SDR CALA2019052700839](https://openairdocs.org/sdr/CALA2019052700839.md): Battery · failed · May 24, 2019 · N454UA · Airbus A320232 · Lighting System
  > (SUPPORT TASK) L-58 NO DOT. THE RT EPSU (12WL) FAILS IT'S BATTERY WHEN TESTED FROM THE PTP. NONROUTINE 9619154 REMOVED AND REPLACED RT EPSU BATTERY IAW AMM 33-51-38-000- 002-A AND 33-51-38-400-002A. PERFORMED TEST OF EPSU BATTERY IAW AMM 33-51-38-000-002-A SUB
- [SDR CALA2018081731790](https://openairdocs.org/sdr/CALA2018081731790.md): Relay · inoperative · Aug 13, 2018 · N454UA · Airbus A320232 · Door Warning System
  > DOOR WARNING FAILED STEP 8, CLOSED CIRCUIT BREAKER P11 AND OPEN CIRCUIT BREAKER P10 OF THE DOOR WARNING CARD. REMOVED AND REPLACED THE RELAY 12WN IAW ESPM 20-46-50, FOUND FAULTY WHEN TROUBLESHOT IAW TSM 52-11-00. AFFIRMED THE OPS TEST OF THE DOOR WARNING I
- [SDR CALA2018081701801](https://openairdocs.org/sdr/CALA2018081701801.md): Fitting · cracked · Aug 12, 2018 · N454UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT WINDSHIELD SIDE POST AT FRAME 4, UPPER ATTACHMENT FITTING HAD A CRACK INDICATION. REPAIRED THE WINDSHIELD POST IAW ECRA 5311-01984, PART 3.
- [SDR CALA2018081761796](https://openairdocs.org/sdr/CALA2018081761796.md): Skin · cracked · Aug 10, 2018 · N454UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > INTERNAL FUSELAGE SKIN, FRAME 35, STRINGER 30L, AFT LOWER FASTNER HOLE HAD A CRACK INDICATION. REPAIRED IAW PART 3 OF ECRA 5311-01981.
- [SDR CALA2018080601760](https://openairdocs.org/sdr/CALA2018080601760.md): Floorbeam · corroded · Aug 4, 2018 · N454UA · Airbus A320232 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOORBEAM AFT SIDE OF FRAME 64, BETWEEN STRINGERS 44R TO 43R WAS CORRODED. REPAIRED IAW EC/RA 5341-01125.
- [SDR CALA2018080601751](https://openairdocs.org/sdr/CALA2018080601751.md): Rib · cracked · Aug 2, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > CRACKS WERE FOUND ALONG THE RIVET HEADS AT THE AFT INNER VERTIVAL RIB IN THE RT AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRM 51-42-11-001, AND SRM 51-72-11-911-001.
- [SDR CALA2018080601750](https://openairdocs.org/sdr/CALA2018080601750.md): Rib · cracked · Aug 2, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > CRACKS WERE FOUND ALONG THE RIVET HEADS AT THE FWD INNER VERTICAL RIB IN THE LT FWD EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRMS 51-42-1 1-001, AND 51-72-11-911-001.
- [SDR CALA2018080601749](https://openairdocs.org/sdr/CALA2018080601749.md): Rib · cracked · Aug 2, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > CRACKS FOUND ALONG THE RIVET HEADS AT LOWER AFT INNER VERTICAL RIB IN THE RT FWD EMERGENCY EXIT HATCH., REMOVED AND REPLACED THE RIB IAW SRM 51-42-11-001, AND 51-7 2-11-911-001.
- [SDR CALA2018080601748](https://openairdocs.org/sdr/CALA2018080601748.md): Rib · cracked · Aug 2, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > CRACKS FOUND ALONG THE RIVET HEADS AT THE FWD INNER VERTICAL RIB ON THE RT AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE VERTICAL RIB IAW SRM 51-42-11-001, AND 51-72-11-911-001.
- [SDR CALA2018080601747](https://openairdocs.org/sdr/CALA2018080601747.md): Rib · cracked · Aug 2, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > FOUND CRACKS ALONG RIVET HEAD AT UPPER AFT INNER VERITCAL RIB ON THE LT FWD EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRMS 51-42-11-001, AND 51-72-1 1-911-001.
- [SDR CALA2018073001731](https://openairdocs.org/sdr/CALA2018073001731.md): Wire Harness · damaged · Jul 28, 2018 · N454UA · Airbus A320232 · Light System Wiring
  > DURING REMOVAL OF THE EEP HARNESSES, IT WAS NOTED THAT ROWS 7-8 HAVE A BROKEN WIRE. REMOVED AND REPLACED EEPL HARNESSES AT SEAT ROWS 7-8 WITH NEW ONES IAW AMM 33-51-22-400-802CL. OPS CHECK TO BE PERFORMED ON WORK CARD.
- [SDR CALA2018073001730](https://openairdocs.org/sdr/CALA2018073001730.md): Seal · blown · Jul 27, 2018 · N454UA · Airbus A320232 · Passenger/Crew Doors
  > L2 DOOR FLEXABLE CONTROL CABLE HAS BLOWN SEAL. REMOVED AND REPLACED L2 DOOR FLEXABLE CABLE IAW AMM-52-13-2 2-400-001-A SUBTASK 52-13-22-420-052-C. LUBRICATED CABLE IAW SUBTASK 52-13-22-640-051-A. RIGGING PERFORMED ON ROUTINE CARD.
- [SDR CALA2018073001726](https://openairdocs.org/sdr/CALA2018073001726.md): Roller · seized · Jul 27, 2018 · N454UA · Airbus A320232 · Emergency Exits
  > SIDE ROLLER SEIZED ON LT AFT EMERGENCY EXIT. HATCH REMOVED AND REPLACED SIDE ROLLER (FWD) ON LT AFT EMERGENCY EXIT HATCH IAW CMM-52-21-11 SUBTASK 52-21-11-400-004-A01.
- [SDR CALA2018073001725](https://openairdocs.org/sdr/CALA2018073001725.md): Hinge Fitting · worn · Jul 27, 2018 · N454UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR UPPER HINGE ARM BEARING MIGRATING OUT OF HOUSING. REMOVED AND REPLACED L1 DOOR UPPER HINGE ARM FITTING ASSEMBLY IAW 52-11-31-400-002-A SUBTASK 52-11-31-420-054-A.
- [SDR CALA2018073001724](https://openairdocs.org/sdr/CALA2018073001724.md): Wire Harness · damaged · Jul 27, 2018 · N454UA · Airbus A320232 · Light System Wiring
  > (DURING REMOVAL OF THE EEPL HARNESS ES, IT WAS NOTED THAT ROWS 32-35 HAVE A DAMAGED WIRE NEAR THE SWD CONNECTOR. REMOVED AND REPLACED EEPL HARNESSES AT SEAT ROWS 32-35 WITH NEW HARNESSES IAW AMM 33-51-22-400-802C1. OPS CHECK PERFORMED ON WORK CARD.
- [SDR CALA2018071901659](https://openairdocs.org/sdr/CALA2018071901659.md): Plate · corroded · Jul 17, 2018 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > REMOVED, MATCH DRILLED & REPLACED CORRODED FISH PLATE AT FR 32 STR 43-44 LT, RESTORED SURFACE PROTECTION IAW SRM 51-72-11 -911-001 IAW ER5100R01017 REV E. FWD CARGO COMPARTMENT FROM FR32 FROM STRG 43-44 ON LT SIDE FISH PLATE & RIVETS HAVE CORROSION. INSP COMPL
- [SDR CALA2018071901658](https://openairdocs.org/sdr/CALA2018071901658.md): Plate · corroded · Jul 17, 2018 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FROM FR 30 FROM STR 43-44 ON LT SIDE. FISH PLATE & RIVETS HAVE CORROSION. REMOVED, MATCH DRILLED & INSTALLED FISH PLATE AT FR 30 STR 43L TO 43R DUE TO CORROSION, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911-001, ER 5100R01017 REV E. I
- [SDR CALA2018071901657](https://openairdocs.org/sdr/CALA2018071901657.md): Plate · corroded · Jul 17, 2018 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FROM FR 26 FROM STG 43-44 ON RT SIDE FISHPLATE & RIVETS HAVE CORROSION. REMOVED, MATCHDRILLED & REPLACED CORRODED FISH PLATE AT FR 26 STG 43-44 RT, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-9 11-001 IAW ER 5100R01017 REV E. INSP COMPLI
- [SDR CALA2018071901656](https://openairdocs.org/sdr/CALA2018071901656.md): Plate · corroded · Jul 17, 2018 · N454UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT FROM FR 30 FROM STR 40-41 ON LT SIDE. FISH PLATE & RIVETS HAVE CORROSION. REMOVED, MATCHDRILLED & REPLACED CORRODED FISHPLATE AT FR 30 STR 40-41 LT RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911- 001, ER5100R01017 REV E. INSP COMPLIED W

Next page: https://openairdocs.org/aircraft/N454UA/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 = 'N454UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N454UA/reports

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