# Service difficulty reports: N461UA

A list on [N461UA](https://openairdocs.org/aircraft/N461UA.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 · 121 reports

- [SDR CALA2026090919319](https://openairdocs.org/sdr/CALA2026090919319.md): Bottle · faulted · Sep 8, 2026 · N461UA · Airbus A320232 · Passenger/Crew Doors
  > L1 DOOR ASSIST BOTTLE IN THE DISARMED POSITION. REARMED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00-860-002-A. VERIFIED L1 DOOR ASST BOTTLE IN THE ARMED POSITION AND SAFTIED IAW GMM 09-25-05 REARMED L1 DOOR ASSIST DAMPER IAW AMM 52-10-00-860-002-A. RESET CIRCUIT
- [SDR CALA2026030214141](https://openairdocs.org/sdr/CALA2026030214141.md): Unknown · odor · Feb 28, 2026 · N461UA · Airbus A320232 · Air Distribution System
  > SWEET SMELLING ODOR DETECTED WHEN BOTH PACKS TURNED ON AT GATE ON APU BLEED. TROUBLESHOT IAW TSM 05-50-00/201 DECISION TABLE AND TSM 05-50-00-810-831-A, PER TSM OPERATED IN MULTIPLE CONFIGS WITH E1 & E2, BLEED 1, BLEED 2, APU BLEED, PACKS 1 AND 2 FOR EXTENDED
- [SDR CALA2026030214131](https://openairdocs.org/sdr/CALA2026030214131.md): Unknown · smoke · Feb 26, 2026 · N461UA · Airbus A320232 · Air Distribution System
  > FLIGHT CREW REPORTED VISIBLE SMOKE AND ODOR IN CABIN WHILE AT GATE WITH PACKS RUNNING.
- [SDR CALA2026030214130](https://openairdocs.org/sdr/CALA2026030214130.md): A/C Pack · overheated · Feb 26, 2026 · N461UA · Airbus A320232 · Cabin Cooling System
  > PACK 2 OVERHEAT WHEN INITIALLY SELECTED ON. INSPECTED ACFT FOR SMOKE & ODOR. PACK 2 OVERHEAT MESSAGE CLEARED INITIALLY BUT, RETURNED WHEN RUNNING PACKS. OVERHEAT MESSAGE CLEARED AND PLACED NR 2 PACK ON MEL 2152Z DUE TO REPEAT MESSAGE. PERFORMED LEAK AND O
- [SDR CALA2026022714121](https://openairdocs.org/sdr/CALA2026022714121.md): A/C Pack · contaminated · Feb 26, 2026 · N461UA · Airbus A320232 · Cabin Cooling System
  > SMOKE/FUMES IN CABIN AFTER RESET OF PACK 2. VERIFIED WITH FLIGHT CREW AND OPERATIONS THAT ACFT WAS DE-ICED WITH APU & PACKS ON. RAN PACKS TO CLEAR GLYCOL SMOKE ODOR, PACK 2 OVERHEATED AGAIN. ACCOMPLISHED TSM 05-50-00 AND AMM 05-51-10 AFTER RUNNING PACK 1
- [SDR CALA2026010712787](https://openairdocs.org/sdr/CALA2026010712787.md): Brake Assy · no discrepancy · Jan 5, 2026 · N461UA · Airbus A320232 · Landing Gear Brake System
  > TAKEOFF REJECTED AT 50KTS DUE TO BRAKE SYSTEM 2 FAULT. BRAKE TEMPS ABOUT 300 DEGREES. PERFORM CHECKS OF TIRES AND BRAKES AND ENSURE NO ISSUES NOTED. LOW SPEED REJECTED TAKEOFF BY CREW. BRAKES TEMPS REMAINED IN NORMAL RANGE PERFORMED CHECK OF TIRES AND BRAKES.
- [SDR CALA2025091608955](https://openairdocs.org/sdr/CALA2025091608955.md): Battery · no test · Sep 16, 2025 · N461UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY FWD L FAULT DURING EMERGENCY LIGHT TEST. R & R FWD LT EPSU BATTERY REF AMM 33-51-38. OPS CHECK PASSED. PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2025091508899](https://openairdocs.org/sdr/CALA2025091508899.md): Unknown · odor · Sep 11, 2025 · N461UA · Airbus A320232 · Air Distribution System
  > FA HEARD BANG ON APPROACH & LOUD NOISE FROM R2 DOOR, SMELLED SMOKE IN AFT GALLEY, AFT FLT ATTENDENTS STATED THEY HEARD BANGING COMING FROM AFT RT DOOR THROUGHOUT FLT. AFT PORTION OF ACFT SMELLED LIKE SMOKE. PILOT STATED ODOR CAME AFTER LANDING, IN AFT CABIN
- [SDR CALA2025091008710](https://openairdocs.org/sdr/CALA2025091008710.md): Lamp · inoperative · Sep 7, 2025 · N461UA · Airbus A320232 · Passenger Compartment Lighting
  > DOOR 1R ENTRY LT INOP. REQUESTING MEL 3320A MEL 3320A APPROVED STICKER APPLIED. RELAMPED OPS CHECK GOOD.
- [SDR CALA2025082608136](https://openairdocs.org/sdr/CALA2025082608136.md): Flange · cracked · Aug 16, 2025 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 68 AT S22R FLANGE HAS CRACK INDICATION IN RADIUS JUST ABOVE LWR INBD STOP BOLT. INTERIM REPAIR HAS BEEN ACCOMPLISHED IAW PART 1 OF ECRA 5341-01503 WITHOUT DEVIATIONS. REPAIR PART HORIZONTAL FLANGE AND INNER CAP FILLET RADIUS PER PART 2A OF THE LATEST R
- [SDR CALA2025082608137](https://openairdocs.org/sdr/CALA2025082608137.md): Frame · cracked · Aug 15, 2025 · N461UA · Airbus A320232 · Fuselage Main, Frame
  > FRAME 35, S30R HOLE #1, #3, #9 DAMAGED.ACCOMPLISHED INTERIM REPAIR PER ECRA 5311-02126 REV C. WITH NO DEVIATIONS. ACCOMPLISH INSPECTION REQUIREMENTS AT RH FR35 STGR30RH ANGLE FITTING AND LH/RH FR35 STGR30 HOLES #1, #3-#9 PER PART 2B OF THE LATEST REVISION OF E
- [SDR CALA2025081207628](https://openairdocs.org/sdr/CALA2025081207628.md): Shear Tie · damaged · Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FORWARD CARGO AT FR 32 SHEAR-TIE BETWEEN STR 39L-40L HAS ELONGAT ED FASTENER HOLES REQUIRES REPLACEMENT. REMOVED AND REPLACED SHEAR TIE AT FWD CARGO FR32 BTW STR 39L-40L IAW A320 SRM 51-42-11 AND 51-72-11.
- [SDR CALA2025081207627](https://openairdocs.org/sdr/CALA2025081207627.md): Shear Tie · damaged · Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > HAS ELONGATED FASTENER HOLES REQUIRES REPLACEMENT. REMOVED AND REPLACED CLEAT AT FWD CARGO FR32 BTW STR 40L-41L IAW A320 SRM 51-42-11 51-72-11.
- [SDR CALA2025081207626](https://openairdocs.org/sdr/CALA2025081207626.md): Shear Tie · damaged · Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FORWARD CARGO COMPARTMENT AT FR 32 SHEAR TIE BETWEEN STR 41L-42L HAS ELONGATED FASTENER HOLES REQUIRES REPLACEMENT. GENERATED BY V077960 PER HAECO LCQ NR 9296915/30915. ESFR COMPLETED REMOVED AND REPLACED SHEAR TIE AT FWD CARGO FR 32 BTW STR 41L-ST R42L IAW A3
- [SDR CALA2025080507327](https://openairdocs.org/sdr/CALA2025080507327.md): Skin · corroded · Aug 3, 2025 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO COMP CORRODED FASTENERS FWD OF FR 32 BETWEEN STR 40L A ND SRT 42L. ACCOMPLISED REPAIR INSTRUCTIONS PER HAECO REO L25555 WITH NO DEV IATIONS AT FWD CARGO COMP FR32 BETWEEN 39L-42L STRG IAW SRM 53-2 1-11-300-063 AND ECRA 5321-02165
- [SDR CALA2025081207625](https://openairdocs.org/sdr/CALA2025081207625.md): Stringer · damaged · Aug 2, 2025 · N461UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 39R BETWEEN FR 47 & 48 DAMAGED FROM CHAFING W ITH HYDRAULIC LINE. REPAIRED STRINGER IN AFT CARGO BETWEEN FR47-49 STGR 39R IAW A320 SRM 53-41-13-300-010 INSPECTION THRESHOLD FROM TIME OF ADL/REPA IR EMBODIMENT IS 60000FC/120000FH WHICHEVER O
- [SDR CALA2025081207624](https://openairdocs.org/sdr/CALA2025081207624.md): Cover · corroded · Aug 2, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR BOTTOM CUTOUT HAS CORROSION SPOTS ON TORSION BOX UPPER SURFACE. REMOVED AND REPLACED AFT CARGO TORSION BOX UPPER COVER IAW A320 DWG D53475500 AND SRM 51-42-11/001.
- [SDR CALA2025073107136](https://openairdocs.org/sdr/CALA2025073107136.md): Door Sill · corroded · Jul 29, 2025 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO DOOR BOTTOM CUTOUT HAS CORROSION SPOTS ON DOOR SILL UP PER SURFACE. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW A320 DWN E534705000 08 AND SRM 51-72-11-911.
- [SDR CALA2025071606620](https://openairdocs.org/sdr/CALA2025071606620.md): Floor Support · corroded · Jul 15, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT, BETWEEN FRS 48-52A STRINGER 38R, FLOOR SUPPORT PROFILE HAS CORROSION AND ELONGATED FASTENER HOLES. REMOVED FLOOR SUPPORT PROFILE IAW SRM 51-44-11/001 REPLACED FLOOR PANEL IAW SRM 51-42-11/001.
- [SDR CALA2025071606612](https://openairdocs.org/sdr/CALA2025071606612.md): Intercostal · corroded · Jul 9, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF PROFILE PANEL AFT CARGO, FRS 58-59 FOUND CORROSION ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL PLATE IN AFT CARGO FR 58-FR59 STR 38R IAW A320 SRM 51-42-11/001 51-44-11/001.
- [SDR CALA2025071006425](https://openairdocs.org/sdr/CALA2025071006425.md): Floor Support · corroded · Jul 9, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR FR 58-FR 59 STR38 PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED CORNER SECTION IN AFT CARGO FR 58-FR59 STR 38R IAW 51-42-11/001 51-44-11/001 51-42-11/001
- [SDR CALA2025071606611](https://openairdocs.org/sdr/CALA2025071606611.md): Web · cracked · Jul 7, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SHEAR WEB @ FR 11 ON F/O SIDE UNDER FLOOR CRACKED. REMOVED AND REPLACED SHEAR WEB, FR 11, F/O SIDE UNDER FLOOR IAW SRM 51-42-11 AND SURFACE PROTECTION IAW SRM 51-23-11 AND 51-21-00.
- [SDR CALA2025071406494](https://openairdocs.org/sdr/CALA2025071406494.md): Skin · contaminated · Jul 3, 2025 · N461UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR, UPPER SURFACE HAS INDICATION OF WATER INGRESS AT 54 INCHES FROM IB EDGE, 12 INCHES FROM TRAILING EDGE, 2 INCHES IN D IAMETER. EVALUATED AND REPAIRED LH ELEVATOR,UPPER SURFACE @ 54 INCHES FRO M IB EDGE.12 INCHES FROM TRAILING.2 INCHES IN DIAMETER
- [SDR CALA2025070306193](https://openairdocs.org/sdr/CALA2025070306193.md): Door Sill · corroded · Jul 2, 2025 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CABIN R2 ENTRANCE FLOOR HAS CORROSION AT FR 68. REPAIRED DOOR SILL BEAM AT AFT CABIN R2 DOOR BETWEEN FR67-68 IAW A320 SRM 53-41-14-283-002.
- [SDR CALA2025063006063](https://openairdocs.org/sdr/CALA2025063006063.md): Intercostal · cracked · Jun 27, 2025 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT FWD EMERGENCY EXIT DOOR INTERCOSTAL CRACKED. R & R WITH NEW INTERCOSTAL D522790620451, ON RT FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11/001 AND 51- 72-11-911-001.
- [SDR CALA2025050604489](https://openairdocs.org/sdr/CALA2025050604489.md): Cover · detached · May 5, 2025 · N461UA · Airbus A320232 · Emergency Exits
  > ECAM LEFT AFT OVER WING EXIT OPEN NOTED MESSAGE ON DOOR PAGE ECAM DISPLAY. FOUND COVER FOR OVER WING EXIT LYING ON FLOOR IN FRONT OF DOOR. UNABLE TO DETERMINE WHY THIS PANEL FELL OFF OR WAS REMOVED. REPLACED PANEL AND DETERMINED THAT IT IS SECURELY INSTALLED.
- [SDR CALA2025011001853](https://openairdocs.org/sdr/CALA2025011001853.md): Fuel Cap · broken · Jan 8, 2025 · N461UA · Airbus A320232 · Fuel Storage
  > HANDLE TO FUEL CP FOUND MISSING UPON ARRIVAL. REPORTS FUEL CAP BROKE FOUND FUEL CAP HANDLE MISSING. CREATED PDA, REMOVED AND REPLACED FUEL CAP REF 28-25-41-02B.
- [SDR CALA2024031100690](https://openairdocs.org/sdr/CALA2024031100690.md): Pressure Switch · faulty · Mar 8, 2024 · N461UA · Airbus A320232 · Hydraulic System, Main
  > YELLOW SYSTEM RESERVOIR LO LEVEL ECAM. CREW FOLLOWED QRH,, YELLOW EDP OFF, PTU OFF. CREW REPORTS YELLOW RESERVOIR LEVEL AT BOTTOM OF SERVICING BAND ON ECAM. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK YELL
- [SDR CALA2023080702433](https://openairdocs.org/sdr/CALA2023080702433.md): Frame · cracked · Aug 4, 2023 · N461UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR16 UPPER DOUBLE JOGGE AREA HOLE 7, A AND C HAVE CRACK INDICATIONS IN FRAME LAYER. "REPAIR BEFORE NEXT FLIGHT" GEN BY V89244 4 ON HAECO LCQ NR 9294380/34380 TO ACMP INITIAL INSP OF RH FR16 UPPER DBL JOGGLE HOLES 7,8,A,&B 36,316 TOTAL FC. REPEAT INSP AT INT
- [SDR CALA2023072802349](https://openairdocs.org/sdr/CALA2023072802349.md): Skin · corroded · Jul 27, 2023 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > SKIN AROUND AFT LAV EXHAUST HAS CORROSION ON OUTTER SURFACE (SUP PORT TASK) GENERATED AT HAECO LCQ PER NR 9294338 (34338) BY MECH V079881 SKIN AROUND AFT LAV EXHOUST VENT DUCT REPAIRED IAW A320 SRM 53-4 1-11-300-004 PAR.2 ACMP BY MECH V905639 AND INSP BY V0798
- [SDR CALA2023072402312](https://openairdocs.org/sdr/CALA2023072402312.md): Fitting · worn · Jul 22, 2023 · N461UA · Airbus A320232 · Landing Gear System
  > LT MLG DOOR RETRACK ACTUATOR FITTING HAS INDICATION OF WEAR UNDE R BOLT HEAD (SUPPORT TASK) GENERATED AT HAECO LCQ PER NR 9294100 (34100) BY MECH V079881 REMOVED AND REPLACED L/H AFT ACTUATOR FITTING 6 IAW REPAIR DRAW ING R53370501E ACMP BY MECH V929087 AND I
- [SDR CALA2023020100302](https://openairdocs.org/sdr/CALA2023020100302.md): Battery · none · Feb 1, 2023 · N461UA · Airbus A320232 · Emergency Lighting
  > WHILE 101S WERE PREFORMING EMERGENCY LIGHT TEST ASSOCIATED WITH SLIDE CHANGE THEY GOT MSG EPSU INT LOAD EMER L. ALL LIGHTS ARE OPERATIONAL BUT DUE TO FAULT NEED NEW BATTERY R&R BATTERY FOR EMERGENCY LIGHTS PER AMM TASK 33-51-38 AND TEST PASSED
- [SDR CALA2022110203027](https://openairdocs.org/sdr/CALA2022110203027.md): Fastener · missing · Nov 2, 2022 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > PDA 3 REF LP''S 9871420, 9871495, 9871527, 9871538, 9871545, 9871558 FOR MISSING FASTENERS, CREATING PDA CAT 3 REF GMM 02-30-95 PDA CREATED REF GMM 02-30-95. LP 9871420: INSTALLED MISSING FASTENER ON 197AB PANEL IAW AMM 53-35-03-40E. LP 9871495: INSTALLED MIS
- [SDR CALA2022030100545](https://openairdocs.org/sdr/CALA2022030100545.md): Lanyard · missing · Mar 1, 2022 · N461UA · Airbus A320232 · Aircraft Fuel System
  > PDA 3 OPS REPORTS FUEL CAP LANYARD IS MISSING LUSK, GREG (V901923) DEFERRED PER CDL, APPLIED INOP STICKER ADJ THE REG #. DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V901923 PLEASE CONTACT TOM
- [SDR CALA2021060700799](https://openairdocs.org/sdr/CALA2021060700799.md): Skin · scratched · Jun 6, 2021 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-53-4-6229 DURING INSPECTION OF LOWER FUSE EXTERNAL SURFACE FR47-FR70 FOUND SCRATCH FUSE SKIN FR53-54 STGR29L-30L. EVALUATE IAW THE CURRENT SRM STANDARDS. SEQ 461 ZONE 100. 2 SCRATCHES FOUND ON FUSELAGE SKIN BTW FR53-54 STR29-30 LH. SCRATCHES BLENDED IAW S
- [SDR CALA2020111601277](https://openairdocs.org/sdr/CALA2020111601277.md): Controller · defective · Nov 13, 2020 · N461UA · Airbus A320232 · Cabin Pressure Controller
  > AFTER TAKEOFF CREW REPORTED TO DISPATCH DUAL CABIN PRESSURE SYSTEM FAILURES. ALSO DD STATED CREW REPORTED MANUAL OPERATION INOPERABLE LOCKING ITEM FOR CONFIRMATION UNLOCKED FOR DISPOSITION. REF L/P 5475842 FOR NR 1 AND NR 2 CPC REPLACEMENT AND OUTFLOW VALVE
- [SDR CALA2019042200628](https://openairdocs.org/sdr/CALA2019042200628.md): Battery · inoperative · Apr 21, 2019 · N461UA · Airbus A320232 · Emergency Lighting
  > EPSU 13WL SHOWS FAULT DURING EMERGENCY LIGHT S BITE TEST, REMOVED AND REPLACED EPSU AND BATTERY IAW AMM 33-51-38-000- 00 AND 33-51-38-400-001, 33-51-38-000-002 AND 33-51-38-400-002 O PS TEST GOOD.
- [SDR CALA2019042200626](https://openairdocs.org/sdr/CALA2019042200626.md): Skin · cracked · Apr 21, 2019 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > ROTO PROBE INSEPCTION SHOWS CRACK INDICATION AT FUSELAGE SKIN, FR35, STR30, LH SIDE, LOWER AFT HOLE INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02126. DTA DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 10 OCT 1 9. PLANNING TO CONTACT ENGINEER
- [SDR CALA2019041900615](https://openairdocs.org/sdr/CALA2019041900615.md): Door Frame · cracked · Apr 18, 2019 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > ROTO PROBE INSPECTION OF DOUBLE JOGGLE SHOW S CRACK INDICATION AT DOOR STOP #7 LOCATION (UPPER LOCATIONS) RH SIDE, 3RD FASTENER OF AFT COLUMN INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02125.
- [SDR CALA2019041900614](https://openairdocs.org/sdr/CALA2019041900614.md): Skin · cracked · Apr 18, 2019 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > ROTO PROBE INSPECTION SHOWS CRACK INDICATIO N AT FUSELAGE SKIN FR35, STR 30, RH SIDE, LOWER AFT HOLE INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02126. DTA DIP INITIATED TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE 10 OCT 1 9. PLANNING TO CONTACT ENGINEE
- [SDR CALA2019041900612](https://openairdocs.org/sdr/CALA2019041900612.md): Door Frame · cracked · Apr 18, 2019 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > ROTO PROBE INSPECTION OF DOUBLE JOGGLE SHOW S CRACK INDICATION AT DOOR STOP #7 LOCATION (UPPER LOCATION) LH SIDE, 4TH FASTENER OF AFT COLUMN INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-02127. *DIP CREATED* THEREAFTER INTERIM REPAIR PERFORMED PER PART 1 OF
- [SDR CALA2019041200557](https://openairdocs.org/sdr/CALA2019041200557.md): Stringer · corroded · Apr 8, 2019 · N461UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > SUPPORT TASK ( NO DOT L-5) EA 5100-02750 REV A OP 003 CORROSION ON STRINGER 30R BETWEEN FR65 AND FR66 REMOVED STR 30R FR64-67 IAW A320 SRM 51-42-11-001. CORROSION LIM ITED TO STR30R ONLY NO CORROSION ON INTERNAL SKIN MATING SURFACE. REMOVED CLEAT AT STR30R FR
- [SDR CALA2019040800547](https://openairdocs.org/sdr/CALA2019040800547.md): Stringer · corroded · Apr 6, 2019 · N461UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AAR N/R S/N 9817876.(A3NB-05-3-6022,A27-080) AFT CARGO BAY STR 4 1R CORRODED AT FR 63-64 REMOVED DAMAGED SECTION OF STR41 FR63 TO 64 IAW A320 SRM 53-00-1 3-300-001 AND SRM 51-42-11-001. CORROSION LIMITED TO STRINGER ON LY, NO CORROSION ON INTERNAL SKIN MATING
- [SDR CALA2019040800546](https://openairdocs.org/sdr/CALA2019040800546.md): Skin · corroded · Apr 6, 2019 · N461UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > R2 DOOR CUTOUT A HAS CORROSION ON THE OUTSIDE SKIN OF THE FUSELAGE BETWEEN FR66 AND FR68 REPAIRED R2 DOOR CUTOUT EXT SKIN BELOW THE DOOR BETWEEN FR66 AND FR68 IAW ECRA 5341-01159 PART 1, ACCOMPLISH THE INITIAL INSPECTION REQUIREMENTS AT THE FUSELAGE SKIN AT FR
- [SDR CALA2019040100509](https://openairdocs.org/sdr/CALA2019040100509.md): Threshold · corroded · Apr 1, 2019 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6186. A-10-028. CABIN FLOOR BEAM INSP. AFT WET AREA FR 66 L/H SIDE +Y1732 SPLICE TO L2 DOOR THRESHOLD CORRODED. REMOVED DAMAGED ON L2 DOOR SILL FR66 AT +Y1732 SPLICE, MAX MATER IAL LOSS.043. MAX ALLOWED.039 AND IS OUT OF LIMITS IAW A320 SR M 53-41-
- [SDR CALA2019040100508](https://openairdocs.org/sdr/CALA2019040100508.md): Door Sill · corroded · Apr 1, 2019 · N461UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6299 A-36-016 R2 DOOR SILL HAS AREAS OF CORROSION AFT CORNER REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW A320 SRM 51-75-12 ADD EMP:V918901
- [SDR CALA2019040100495](https://openairdocs.org/sdr/CALA2019040100495.md): Door Frame · cracked · Mar 29, 2019 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > EMERGENCY EXIT LT AFT 834. IB FWD VERTICAL FRAME CRACKED AT FAST ENER HOLES. AAR NONROUTINE 9817724 REMOVED AND REPLACED FWD VERTICAL FRAME (BEAM AND SEGMENT) ON L/ H AFT EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. AAR NON ROUTINE 9817724 INSPECTION COM
- [SDR CALA2019040100493](https://openairdocs.org/sdr/CALA2019040100493.md): Beam · cracked · Mar 29, 2019 · N461UA · Airbus A320232 · Fuselage Main, Structure
  > EMERGENCY EXIT LT AFT 834. IB AFT VERTICAL FRAME CRACKED AT FAST ENER HOLES. AAR NONROUTINE 9817723 REMOVED AND REPLACED EMERGENCY EXIT LT AFT 834 IB AFT VERTICAL F RAME IAW A320 SRM 51-72-11-911-001. AAR NONROUTINE 9817723 INSPECTION COMPLIED WITH
- [SDR CALA2019032200435](https://openairdocs.org/sdr/CALA2019032200435.md): Door Frame · cracked · Mar 18, 2019 · N461UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK. A34-17) EMERGENCY EXIT RT AFT 844 IB FWD VERTICAL FRAME CRACKED AT FASTENER HOLES. NONROUTINE 9817689 REMOVED AND REPLACED FWD VERTICAL FRAME (SEGMENT AND BEAM) ON RT AFT EMERGENCY EXIT DOOR IAW SRM 51-72-11-911-001. NON ROUTINE 9817689.
- [SDR CALA2019031800428](https://openairdocs.org/sdr/CALA2019031800428.md): Door Frame · cracked · Mar 16, 2019 · N461UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK A34-19) EMERGENCY EXIT RT FWD 843AZ. IB AFT VERTICAL FRAME CRACKED AT FASTENER HOLES. NONROUTINE 9817699 REMOVED AND REPLACED EMERGENCY EXIT RT FWD 843AZ I/B AFT SEGMEN T AND BEAM IAW SRM 51-72-11-911-001. NONROUTINE 9817699 REMOVED AND REPLACED

Next page: https://openairdocs.org/aircraft/N461UA/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 = 'N461UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N461UA/reports

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