# Service difficulty reports: N457UA

A list on [N457UA](https://openairdocs.org/aircraft/N457UA.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 · 138 reports

- [SDR CALA2026021213722](https://openairdocs.org/sdr/CALA2026021213722.md): Elec Connector · disconnected · Feb 11, 2026 · N457UA · Airbus A320232 · Light System Wiring
  > L2 DOOR EMERGENCY LIGHT DID NOT TEST, FOUND CONNECTOR 7245VC DISCONNECTED ENTIRELY IAW AIPC 24-92-04-46M, ITEMS 10, AND 20, AWM 33-51-03 PAGE 8, AND ESPM 20-44-29-01. RECONNECTED & OPS CHECKED PERFORMED IAW AMM 31-51-00-710-007-A. OPS CHKD NORMAL.
- [SDR CALA2026012613283](https://openairdocs.org/sdr/CALA2026012613283.md): Slide · expired · Jan 26, 2026 · N457UA · Airbus A320232 · Escape Slide
  > SCHEDULED REMOVAL. REMOVED AND REPLACED DOOR SLIDE ASSY IAW AMM 25-62-44.
- [SDR CALA2026021813895](https://openairdocs.org/sdr/CALA2026021813895.md): Warning Light · false activation · Jan 18, 2026 · N457UA · Airbus A320232 · Central Warning
  > AFTER TOUCHDOWN, MASTER CAUTION LIGHTS ILLUMINATED WITH NO CHIME OR ECAM DISPLAYED. ACCOMPLISHED AN OPS TEST OF MASTER CAUTION, WARNING LIGHT IAW AMM 31-50-00-710-011-A. NO FAULTS NOTED.
- [SDR CALA2025091508876](https://openairdocs.org/sdr/CALA2025091508876.md): Power Supply · no test · Sep 13, 2025 · N457UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT RT MESSAGE AFTER EMERGENCY LIGHTS TEST NEEDS REPLACED. R & R RT ESPU. REF: AMM TASK 33-51-38-000-002-A & TASK 33-51-38-400-002-A. OP CHECK TEST OKAY, IAW AMM TASK 33-51-00-710-001-A.
- [SDR CALA2025091108756](https://openairdocs.org/sdr/CALA2025091108756.md): None · none · Sep 8, 2025 · N457UA · Airbus A320232 · Standard Practices/Structures
  > RIGHT OVERWING SLIDE INFLATION BOTTLE PINNED FOM, REMOVED PIN, REACTIVATED RH BOTTLE REF AMM 25-62-00-081-001-A. VERIFIED REMOVAL OF THE PIN FROM THE R/H OFF WING SLIDE BOTTLE IN REF TO AMM 25-62-00-061-001-A.
- [SDR CALA2025091008714](https://openairdocs.org/sdr/CALA2025091008714.md): Sensor · out of alignment · Sep 8, 2025 · N457UA · Airbus A320232 · Door Warning System
  > DOOR R FWD EMER EXIT ECAM. DOOR IND OPEN. PRESS NORMAL PERFORMED RENDER SAFE FOR RT FWD OVERWING EXIT HATCH. SLIDE INDICATION OF HATCH IS DEFECTIVE ON LOWER ECAM, HATCH IS IN THE ARM MODE, EMERGENCY EXIT INDICATION IS DEFECTIVE ON LOWER ECAM DU, HATCH IS CO
- [SDR CALA2025040303469](https://openairdocs.org/sdr/CALA2025040303469.md): Target · out of adjust · Mar 30, 2025 · N457UA · Airbus A320232 · Accessory Compartment
  > DOOR L FWD EMER EXIT ECAM IN FLT DURING DESC ENT. FOUND FLAP COVER TARGET ON L FWD EMERGENCY EXIT DOOR OUT OF RANGE, ADJUSTED TARGET ON FLAP COVER REF AMM 52-71-13-400-001-A. ECAM MESSAGE NO LONGER PRESENT AND SYSTEM OPERATES NORMALLY REF TSM 52-21-00-810-80
- [SDR CALA2025030302563](https://openairdocs.org/sdr/CALA2025030302563.md): Engine · stalled · Mar 2, 2025 · N457UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > DUE TO EVIDENCE OF ENG #2 STALL, REQUIRED BORESCOPE OF HPC STAGES 3, 4, 5, 6, AND 7 REF TSM 71-00-00-810-809-A STEP 4. D. (2) (A) REMOVED ACCESS PORTS A, B, C AND D FOR BORESCOPE OF HPC REMOVED ENGINE CRANK PAD ACCOMPLISHED BOROSCOPE INSPECTION OF HPC COMPRESS
- [SDR CALA2025021702339](https://openairdocs.org/sdr/CALA2025021702339.md): Fmc · faulted · Feb 17, 2025 · N457UA · Airbus A320232 · Flight Management Computing Hardware System
  > FMGC 1 FAIL REPORTED BY CREW, RESET UNSUCCESSFUL CFDS ATA 22-83-34 FMGC1 SOURCE EFCS 1 PHASE 5, SEE TSM 22-83-00-810-859-A, 3 HITS LAST 10 LEGS LOCKED UNLOCKED FOR CORRECTIVE ACTION FOLLOWED TSM 22-83-00-810-859-A, REMOVED AND REPLACED TERMINAL BLOCKS 1831VT4
- [SDR CALA2024121601536](https://openairdocs.org/sdr/CALA2024121601536.md): Girt Bar · lack of lube · Dec 13, 2024 · N457UA · Airbus A320232 · Emergency Equipment
  > DOOR 2R SLIDE DISARMED SHORTLY AFTER AIRBORNE INDICATED ON COCKP IT DOORS PAGE. CREW STATED THEY LOST WHITE SLIDE INDICATION FOR DOOR ARMED AT DR-2R ON ECAM DOOR/OXY PAGE AS SOON AS THEY TOOK OFF. AFTER TAKEOFF DOOR ARMED HANDLE HAD MOVE SLIGHTLY OUT AND FA C
- [SDR CALA2024121301508](https://openairdocs.org/sdr/CALA2024121301508.md): Proximity Sensor · faulted · Dec 11, 2024 · N457UA · Airbus A320232 · Door Warning System
  > DOOR 2R INDICATING DISARMED AT CRUISE ALT PREV WRITE UP EARLIER TODAY. DEFERRED DOOR 2R SLIDE INDICATION REF MEL 2560T INOP PLACARD INSTALLED VERIFIED DOOR 2R IS CLOSED AND SECURED. DEFERRED DOOR 2R SLIDE INDICATION REF MEL 2560T INOP PLACARD INSTALLED VERIF
- [SDR CALA2024111202836](https://openairdocs.org/sdr/CALA2024111202836.md): Stringer · corroded · Nov 6, 2024 · N457UA · Airbus A320232 · Fuselage Main, Structure
  > MAIN CABIN BELOW FLOOR AT FRAME 65 RT STRINGER 25RT HAS EXFOLIAT ED CORROSION. REMOVED AND REPLACED STRINGER 25RT FR 65-66 IAW A320 SRM 51-72-1 1.
- [SDR CALA2024111102813](https://openairdocs.org/sdr/CALA2024111102813.md): Fitting · cracked · Nov 6, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CRACK INDICATION AROUND FASTENER AS MARKED AT 2 O''CLOCK POSITION BTW FR 40 AND 41 LH SIDE KEEL BEAM SIDE PANEL BEHIND THE VAPOR SEAL. GENERATED BY V947494 ON HAECO LCQ NR 9290461/36461 REMOVED + REPLACED CRACKED KEEL BEAM FITTING AT L/H FR40-41 IAW A320 SRM 5
- [SDR CALA2024110602804](https://openairdocs.org/sdr/CALA2024110602804.md): Door Frame · cracked · Oct 31, 2024 · N457UA · Airbus A320232 · Fuselage Main, Structure
  > RT AFT EMERGENCY EXIT DOOR CRACKED. REMOVED & REPLACED FR SEGMENT @ R/H AFT EMERGENCY HATCH IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2024110402791](https://openairdocs.org/sdr/CALA2024110402791.md): Seat Track · corroded · Oct 29, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > R/H CABIN FLOOR BEAM -Y1292 HAS CORROSION BETWEEN FR.24-36.
- [SDR CALA2024110402792](https://openairdocs.org/sdr/CALA2024110402792.md): Stringer · corroded · Oct 28, 2024 · N457UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT FRAME 58-59 RT STRINGER 41 HAS CORROSION ON VERTIC AL FLANGE AND HORZ. FLANGE. GENERATED BY V052030 ON HAECO LCQ NR 9290433 / 36433
- [SDR CALA2024102802745](https://openairdocs.org/sdr/CALA2024102802745.md): Reinforcement · corroded · Oct 24, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > UNDER AFT CABIN FLOOR CORROSION AROUND WASTE WATER DRAIN MAST HARDWARE AND SKIN REINFORCEMENT PLATE. REMOVED & REPLACED REINFORCEMENT PLATE AT WASTE WATER DRAIN MAST IAW SRM 51-72-11.
- [SDR CALA2024102202702](https://openairdocs.org/sdr/CALA2024102202702.md): Web · cracked · Oct 17, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FLIGHT DECK FLOOR STRUCTURE WEB CRACKED FR 8-11 LBL20. FLIGHT DECK FLOOR STRUCTURE WEB REMOVED AND REPLACED PER A320 SR M 51-72-11-911-002.
- [SDR CALA2024102102694](https://openairdocs.org/sdr/CALA2024102102694.md): Skin · contaminated · Oct 15, 2024 · N457UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT TOP SIDE 20 1/2 INCHES FROM I /B END, 7 INCHES FROM TRAILING EDGE, 1 INCHE DIAMETER, "REPAIR P RIOR TO NEXT FLIGHT" PER HAECO LCQ NR 9290689/36689 REPAIRED R/H ELEVATOR,TOP SIDE, 20.5" FROM I/B END, 7" FROM TRAI LING EDGE IAW
- [SDR CALA2024102102693](https://openairdocs.org/sdr/CALA2024102102693.md): Skin · contaminated · Oct 15, 2024 · N457UA · Airbus A320232 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT TOP SIDE 103 1/2 INCHES FROM I/B END, 21 INCHES FROM TRAILING EDGE, INCHES DIAMETER, "REPAIR PRIOR TO NEXT FLIGHT" PER HAECO LCQ NR 9290690/36690 REPAIRED R/H ELEVATOR, TOP SIDE, 103.5 INCHES FROM I/B END, 21 I NCHES FROM TRA
- [SDR CALA2024101602665](https://openairdocs.org/sdr/CALA2024101602665.md): Floorbeam · corroded · Oct 14, 2024 · N457UA · Airbus A320232 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FLOORBEAM -Y1292 IAW A320 SRM 51-42-11.
- [SDR CALA2024101402636](https://openairdocs.org/sdr/CALA2024101402636.md): Floor Support · corroded · Oct 10, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN R2 DOOR SILL AT FRAME 65 HAS CORROSION AROUND NUT PLATE HO LE. REMOVED AND REPLACED R2 DOOR SILL FR65-68 IAW A320 SRM 51-72-11.
- [SDR CALA2024101402633](https://openairdocs.org/sdr/CALA2024101402633.md): Angle · cracked · Oct 10, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LH INTERNAL FUSELAGE FRAME 68 FLANGE IS CRACKED @ DOORSILL ATTACH. REMOVED AND REPLACED 1EA FLANGE AT FRM68 IAW A320 SRM 51-42-11/0 01 AND 51-72-11-911-001.
- [SDR CALA2024101102626](https://openairdocs.org/sdr/CALA2024101102626.md): Angle · corroded · Oct 8, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L-2 DOOR SILL REPAIR ANGLE CORRODED AT FR68 GENERATED BY V061642 ON HAECO LCQ NR 9290605/36605 PERFORM REPAIR ON L-2 DOOR SILL IAW A320 SRM 53-41-14-300-001.
- [SDR CALA2024100802607](https://openairdocs.org/sdr/CALA2024100802607.md): Shear Web · corroded · Oct 6, 2024 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE FWD OF FR70 LH SHEAR WEB AFT HOLE HAS CORR ISION REMOVED CORRODED SHEAR WEB AT L/H CABIN FWD OF FR70 AND REPLACED IAW A320 SRM 51-42-11/001 AS DIRECTED BY EA 5346-01001 REV.L OP 003.
- [SDR CALA2024100702597](https://openairdocs.org/sdr/CALA2024100702597.md): Seat Track · corroded · Oct 5, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK Y-765 FR 24-35 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK OUT OF LIMITS IAW A320 SRM 51-42-11/001 REV 1 50, REPLACED SEAT TRACK Y-765 FR 24-35 IAW A320 SRM 51-42-11/001 REV 150.
- [SDR CALA2024100702598](https://openairdocs.org/sdr/CALA2024100702598.md): Seat Track · corroded · Oct 4, 2024 · N457UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN SEAT TRACK Y-1292 FR 36-42 CORRODED OUT OF LIMITS.
- [SDR CALA2024032000800](https://openairdocs.org/sdr/CALA2024032000800.md): Indication Sys · false indication · Mar 18, 2024 · N457UA · Airbus A320232 · Hydraulic Indicating System
  > GREEN HYD RESEVOIR SEEMS TO BE LOSING FLUID LOCKED ALL HYD SYSTEM WAS AT NORMAL ON GROUND WITH NO INDICATION OF TOMC RECOMMENDS ENGINE RUN TO CK EDP AND LEAKS DUE TO HYD SEE AMM TASK 29-11-00-710-001-A OPERATIONAL TEST OF THE GREEN LEAKS. POWERED ALL 3 SYSTEMS
- [SDR CALA2024021200383](https://openairdocs.org/sdr/CALA2024021200383.md): Fuel Cap · missing · Feb 9, 2024 · N457UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP NOT INSTALLED ON AIRCRAFT. NO LEAKS NOTED AT COUPLING. INOP STICKER APPLIED BY CREW. OK TO DEFER PER CDL 28A. INSTALLED NEW FUEL CAP.
- [SDR CALA2023050301344](https://openairdocs.org/sdr/CALA2023050301344.md): Fuel Cap · missing · May 3, 2023 · N457UA · Airbus A320232 · Fuel Storage
  > PDA 2 FOUND FUEL CAP MISSING ON ARRIVAL TO DCA FROM ORD SUSPECT FUEL CAP DEPARTED AIRCRAFT DURING FLIGHT. INSPECTED AIRCRAFT FOR DAMAGE REF GMM-02-30-95. NO DAMAGE FOUND. REPLACED MISSING FUEL CAP AS REQ.
- [SDR CALA2022111703161](https://openairdocs.org/sdr/CALA2022111703161.md): Pipe · leaking · Nov 17, 2022 · N457UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD HYD YELLOW SYSTEM LO MASSIVE LEAK SOMEHERE ON TOP OF THE #2 ENG UNDERNEATH THE PYLON. FOUND HYD PIPE CUT AND LEAKING HYD FLUID AT DOWNSTREAM OF T/R CHECK OF THE YELLOW HYD SYSTEM PER AMM 29-13-00-710-002-
- [SDR CALA2022110703051](https://openairdocs.org/sdr/CALA2022110703051.md): Web · cracked · Nov 4, 2022 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FR 68 STR22R INNER CAP AND WEB FLANGE HAS A 1.068 IN CRACK. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF LATEST REVISION OF ECRA 5341-01351 ON OR BEFORE APPROVED DIP TO ACCOMPLISH A PERMANENT REPAIR AT THE RH FR 68, STR 22R
- [SDR CALA2022082402162](https://openairdocs.org/sdr/CALA2022082402162.md): Spring · missing · Aug 24, 2022 · N457UA · Airbus A320232 · Steering Unit
  > PDA 3 NOSE GEAR BYPASS LEVER ONE SPRING CLIP MISSING OUT OF TWO...SEE PHOTO PHOTO ADDED INSTALLED NEW SPRING CLIP AT NLG BYPASS LEVER...REF IPC 32-51-12-01E.
- [SDR CALA2022072701885](https://openairdocs.org/sdr/CALA2022072701885.md): Radar · inoperative · Jul 27, 2022 · N457UA · Airbus A320232 · Doppler System
  > WEATHER RADAR SYSTEM INOP - NAV RED WR ANT DISPLAYED AND ECAM PRED WS INOP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V933475 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. RESET THE MAC RELATED WORK ORDER 0000000
- [SDR CALA2022051301226](https://openairdocs.org/sdr/CALA2022051301226.md): None · none · May 13, 2022 · N457UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > HYD G RSVR LO LVL ECAM DISPLAYED. CREW CONFIRMS FOLLOWED QRH 130.19 AND TURNED OFF GREEN ENG 1 PUMP AS SOON AS ECAM MSG DISPLAYED. TOMC MX CNTL HILL. SVC GREEN HYD TO FULL PERFORMED LEAK CHECK AFTER LEAK CORRECTED.
- [SDR CALA2022021600406](https://openairdocs.org/sdr/CALA2022021600406.md): Reservoir · low · Feb 16, 2022 · N457UA · Airbus A320232 · Hydraulic Pressure Indicator
  > *EMERGENCY* Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD ECAM HYD Y RSVR LO LVL CREW REPORTS NO ALTERNATE EXTEND REPLACED YELLOW SYSTEM LOW LEVEL SWITCH PER AMM 29-13-41. ECAM MESSAGE CLEARED NO FURTHER ISSUES ADD EMP:U377618 ROTABLE PARTS CHANGE WAS IN
- [SDR CALA2021111502103](https://openairdocs.org/sdr/CALA2021111502103.md): Landing Gear · faulty · Nov 14, 2021 · N457UA · Airbus A320232 · Nose/Tail Landing Gear Strut/Axle
  > L/G DOORS NOT CLOSEDECAM NLG DOORS BYPASS IS IN THE OPEN POSITION. PHOTO IS FROM PILOTS PHONE. REMOVED AND REPLACED NLG DOOR ACTUATOR WITH NEW SERVICEABLE ONE, REF AMM 32-31-16-400-001-A, OPS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1936428 SN OF
- [SDR CALA2020111101259](https://openairdocs.org/sdr/CALA2020111101259.md): Pressure Panel · cracked · Nov 11, 2020 · N457UA · Airbus A320232 · Fuselage Main, Structure
  > CRACK INDICATION FOUND AT OUTBOARD FASTENER HOLE OUTSIDE OF REPAIR AREA FR 35 LT PRESSURE PANEL, REF EA-5330-05216 REV "B", REF AAR N/R: 9469368 GENERATED BY: V903469. ACCOMPLISHED INTERIM REPAIR PART 1, AS PER ECRA 5330-06774 AND EA 5330-05216 REV B ON OR BE
- [SDR CALA2020110401241](https://openairdocs.org/sdr/CALA2020110401241.md): Pressure Blkhd · cracked · Nov 3, 2020 · N457UA · Airbus A320232 · Fuselage Main, Bulkhead
  > CRACK FOUND AT RT SIDE FASTENER HOLE ''B'' ON THE PRESSURE PANEL BETWEEN FR 35 & FR 36, REF EA 5330-05216 REV. "B". CRACK LOCATION 6 O'CLOCK, REF AAR N/R: 9469143 GENERATED BY: V909151. INSTALLED REPAIR AT RT SIDE PRESSURE PANEL BETWEEN FR 35-FR 36, AS PER U
- [SDR CALA2018111602389](https://openairdocs.org/sdr/CALA2018111602389.md): Actuator · leaking · Nov 16, 2018 · N457UA · Airbus A320232 · Passenger/Crew Doors
  > REMOVE AND REPLACE L1 PAX DOOR POST ACTUATOR DUE TO LEAKAGE. SN OFF 1934 IPC REFERENCE ACTUATOR, PAX DOOR OFF 31-5210-9-9001 1934 ON 31-5210-9-9001 0031.
- [SDR CALA2018111202351](https://openairdocs.org/sdr/CALA2018111202351.md): Bulkhead · cracked · Nov 10, 2018 · N457UA · Airbus A320232 · Fuselage Main, Bulkhead
  > REF TO AAR NON ROUTINE-9813264, CRACK IN VERTICAL WEB R/H SIDE BELOW F/O SLIDING WINDOW RAIL. REPAIRED VERTICAL WEB R/H SIDE BELOW F/O SLIDING WINDOW AT FR4 IAW ECRA 5311-02040, ACCOMPLISH THE INITIAL INSPECTION REQUIRMEN TS PER PART 2 OF ECRA 5311-02040 AT TH
- [SDR CALA2018110902340](https://openairdocs.org/sdr/CALA2018110902340.md): Door Frame · cracked · Nov 9, 2018 · N457UA · Airbus A320232 · Fuselage Main, Structure
  > A3NB-05-3-6159 A-34-023 RH AFT EMERGENCY EXIT. RH AFT IB LOWER V ERTICAL FRAME CRACKED. REMOVED AND REPLACED RH AFT EMERGENCY EXIT RH AFT IB LOWER VERTI CAL FRAME IAW A320 SRM 51-42-11, SRM 51-44-11, SRM 51-75-12 ADD EMP:V925284 INSP C/W
- [SDR CALA2018110502279](https://openairdocs.org/sdr/CALA2018110502279.md): Frame · cracked · Nov 2, 2018 · N457UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK) (A-38 NO DOT) L/H FWD EMERGENCY EXIT 833 R/H VER TICAL FRAME CRACKED AAR NONROUTINE 9813987 REMOVED AND REPLACED L/H FWD EMERGENCY EXIT 833 R/H VERTICAL FRA ME IAW A320 SRM 51-42-11-001 PARA 2.E. AAR NONROUTINE 9813987 ADD EMP:V919097
- [SDR CALA2018110502278](https://openairdocs.org/sdr/CALA2018110502278.md): Frame · cracked · Nov 2, 2018 · N457UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK) (A-38) NO DOT) R/H FWD EMERGENCY EXIT 843 R/H VER ICAL FRAME CRACKED AAR NONROUTINE 9813988 REMOVED AND REPLACED CRACKED FRAME AT R/H FWD EMERGENCY EXIT, IA W A320 SRM 51-42-11. AAR NONROUTINE 9813988 ADD EMP:V925284
- [SDR CALA2018110502277](https://openairdocs.org/sdr/CALA2018110502277.md): Frame · cracked · Nov 2, 2018 · N457UA · Airbus A320232 · Emergency Exits
  > A3NB-05-3-6159 A34-26 RH FWD EMERGENCY EXIT 843 LH VERTICAL F RAME CRACKED. AAR NONROUTINE 9813613 REMOVED AND REPLACED CRACKED FRAME AT L/H VERTICAL OF DOOR, R/H FWD EMERGENCY EXIT IAW A320 SRM 51-42-11 AAR NONROUTINE 98136 13 ADD EMP:V925284
- [SDR CALA2018110502276](https://openairdocs.org/sdr/CALA2018110502276.md): Frame · cracked · Nov 2, 2018 · N457UA · Airbus A320232 · Emergency Exits
  > A3NB-05-3-6159 A34-24 LH AFT EMERGENCY EXIT 834 AFT VERTICAL FRAMES CRACKED 2PL AAR NONROUTINE 9813595 REMOVED AND REPLACED LH AFT EMERGENCY EXIT AFT VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-24-00-001, 51-23-11-001, 51-23 -12-001 AAR NONROU
- [SDR CALA2018110502275](https://openairdocs.org/sdr/CALA2018110502275.md): Frame · cracked · Nov 2, 2018 · N457UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK) A-38 NO-DOT) L/H AFT EMERGENCY EXIT 834 FWD VERTI CAL FRAME CRACKED AAR NONROUTINE 9813986 REMOVED AND REPLACED LH AFT EMERGENCY EXIT FWD VERTICAL FRAME IA W A320 SRM 51-42-11, 51-72-11, 51-23-12-001, 51-24-00-001. AAR NONROUTINE 9813986 ADD
- [SDR CALA2018110302268](https://openairdocs.org/sdr/CALA2018110302268.md): Plate · damaged · Nov 2, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING REPAIR ON +Y1292 AT FR24 DAMAGE WAS FOUND ON CROSSBEAM AFT VERTICAL FACE AROUND 5 HI LOKS. REMOVED & REPLACED FR24 UPPER FISHPLATE, P/N D5323252020000 AND LOWERFISH PLATE, P/N D5323074920000 IAW SRM 51-42-11-001, AND SRM 51-72-11.
- [SDR CALA2018110202232](https://openairdocs.org/sdr/CALA2018110202232.md): Door Sill · corroded · Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP COMPLIED WITH.
- [SDR CALA2018102902227](https://openairdocs.org/sdr/CALA2018102902227.md): Door Sill · corroded · Oct 29, 2018 · N457UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (CUSTOMER REQUEST) AFT CARGO PIT DOOR THRESHOLD HAS CORROSION AROUND THE FWD NR 2 TIEDOWN FITTING AND ALONG THE OUTER EDGE FR 53-56. N/R 9813949. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-11-0 01. INSP. COMPLIED WITH.

Next page: https://openairdocs.org/aircraft/N457UA/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 = 'N457UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N457UA/reports

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