# Service difficulty reports: N449UA

A list on [N449UA](https://openairdocs.org/aircraft/N449UA.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 · 149 reports

- [SDR CALA2026051316218](https://openairdocs.org/sdr/CALA2026051316218.md): Gcu · faulted · May 10, 2026 · N449UA · Airbus A320232 · Rudder Control System
  > CREW REPORTED AT FL 340 UNCOMMANDED RUDDER INPUTS. AUTOPILIT, AUTOTHRUST DISCONNECTED. THE PFD ND FMGC FCU EWD LOWER ECAM BLANKED FLASHED MULTIPLE TIMES. CRC TRUMPETED MULTIPLE TIMES ECAM POPULATED. SOME RETURTNED MULTIPLE TIMES. SOME OF THE ECAMS WERE AUTO F
- [SDR CALA2026042115573](https://openairdocs.org/sdr/CALA2026042115573.md): Fuel Cap · missing · Apr 21, 2026 · N449UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. INSTALLED A NEW REFUEL/DEFUEL CAP IAW AMM 28-25-41-400-005-A.
- [SDR CALA2026041315291](https://openairdocs.org/sdr/CALA2026041315291.md): None · none · Apr 10, 2026 · N449UA · Airbus A320232 · Standard Practices/Structures
  > TSM 05-50-00-810-831-A REQUIRED TO BE PERFORMED DUE TO ODOR IN 1ST CLASS CABIN AREA. DEBREIFED CREW NO SMOKE IN CABIN. ODOR WAS CUSTOMER 3B USE OF A HERBAL REMENDY. OK TO CONTINUE
- [SDR CALA2025120911957](https://openairdocs.org/sdr/CALA2025120911957.md): Profile · cracked · Dec 7, 2025 · N449UA · Airbus A320232 · Emergency Exits
  > LEFT AFT EMERGENCY EXIT HATCH RT LOAD TRANSMITTING PROFILE SUSPECTED CRACK. REMOVED AND REPLACED LT AFT EMERGENCY EXIT HATCH LOAD TRANSMITTING PROFILE SEGMENT IAW SRM 51-42-11/001, AND SRM 51-72-11-911-00 1.
- [SDR CALA2025120911955](https://openairdocs.org/sdr/CALA2025120911955.md): Profile · cracked · Dec 7, 2025 · N449UA · Airbus A320232 · Emergency Exits
  > LEFT FWD EMERGENCY EXIT HATCH LT LOAD TRANSMITTING PROFILE CRACKED. REMOVED AND REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.
- [SDR CALA2025120911953](https://openairdocs.org/sdr/CALA2025120911953.md): Profile · cracked · Dec 7, 2025 · N449UA · Airbus A320232 · Emergency Exits
  > LEFT AFT EMERGENCY EXIT HATCH LT LOAD TRANSMITTING PROFILE SUSPECTED CRACKED. REMOVED & REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.
- [SDR CALA2025120911951](https://openairdocs.org/sdr/CALA2025120911951.md): Profile · cracked · Dec 7, 2025 · N449UA · Airbus A320232 · Emergency Exits
  > RIGHT AFT EMERGENCY EXIT HATCH RT LOAD TRANSMITTING PROFILE SUSPECTED CRACKED. REMOVED AND REPLACED SEGMENT IAW SRM 51-72-11-911-002, AND SRM 51-42-11/001.
- [SDR CALA2025021802361](https://openairdocs.org/sdr/CALA2025021802361.md): Door · contaminated · Feb 15, 2025 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > APU OIL SMELL IN CABINPACKS RUNNING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INVESTIGATE AND CONTACT AIRCRAFT MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003129638 AND PRTR ACCOMPLISHED ENGINE RUN AT GATE WITH FLIGHT CREW AND WI
- [SDR CALA2025012902104](https://openairdocs.org/sdr/CALA2025012902104.md): Rod · out of alignment · Jan 28, 2025 · N449UA · Airbus A320232 · Landing Gear Door Retract Section
  > L/G DOORS NOT CLOSED ECAM WITH FAULT MSGS N LG DOOR UPLOCK(2534GM)/(2531GM) /IDLGCIU 2 AND N LG DOOR UPLOCK(2534GM)/(2531GM) /IDLGCIU 1. LOCKING LOG FOR POSITIVE FIX. ADDING SDR CREW REPORTS. UPON TAKE OFF, CREW PULLED GEAR HANDLE TO UP POSITION. GOT ECAM MES
- [SDR CALA2025012802093](https://openairdocs.org/sdr/CALA2025012802093.md): Uplock · faulted · Jan 26, 2025 · N449UA · Airbus A320232 · Landing Gear Position and Warning
  > L/G DOORS NOT CLOSED ECAM, N LG DOOR UPLOCK (2534GM/2531GM CFDS) - FIELD RETURN LOCKED PRINTED PFR REPORT AND LAST LEG ECAM REPORT. SPOKE TO FLIGHT CREW UPON ARRIVAL. CREW CYCLED THE GEAR SEVERAL TIMES IN FLIGHT AND MESSAGE REMAINED. NO ABNORMAL SOUND BUT NLG
- [SDR CALA2025012301973](https://openairdocs.org/sdr/CALA2025012301973.md): Warning Message · illuminated · Jan 21, 2025 · N449UA · Airbus A320232 · Landing Gear Door Retract Section
  > L/G DOORS NOT CLOSEDECAM ON DEPARTURE. NOSEGEAR DOORS INDICATING NOT CLOSED. GROUND TIME AND LABOR HOURS INFORMATION UPDATE ONLY. INSPECTED NLG DOORS, HINGES, ACTUATING CYLINDER AND UPLOCKS, NO DEFECTS NOTED. ACCOMPLISHED BITE CHECK OF BOTH LGCIUS WITH NO DEFE
- [SDR CALA2025012100161](https://openairdocs.org/sdr/CALA2025012100161.md): Stringer Clip · corroded · Jan 17, 2025 · N449UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > AFT CARGO COMPARTMENT AREA AROUND PRESSURIZATION OUTFLOW VALVE L OWER STRINGER AT FR65 CORRODED. REMOVED AND REPLACED DISCREPANT STRINGER CLIP AND FRAME ST RAP BTW FR 64-67 AT STGR 31 IAW A320 SRM 51-72-11 51-42-11 51-44 -11.
- [SDR CALA2025012100160](https://openairdocs.org/sdr/CALA2025012100160.md): Skin · dented · Jan 17, 2025 · N449UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UPPER R/H SIDE ABOVE HORZ BESIDE RUDDER BETWEEN FR 79-80 STR3-4 R/H HAS PUNCTURE. ACOMPLISHED CAT-A PERMANANT REPAIR ON FUSELAGE SKIN BETWEEN STR3 -4 R/H AT FR79-80 IAW A320 SRM 53-51-11-300-002
- [SDR CALA2023082302610](https://openairdocs.org/sdr/CALA2023082302610.md): Cap · missing · Aug 21, 2023 · N449UA · Airbus A320232 · Aircraft Fuel Distribution System
  > REPORTED ACFT ARRIVER WITHOUT FUELING CAP CAP NON STCK LAX COMPLIED WITH CDL DISPATCH DESK: 12 NAME:TA DATE: 20-AUG-23- OK TO DEFER FUEL CAP PER CDL 28A.CAP, COUPLING R OFF 0000 ON 31-2825-9-0001 2301 INSTALLED MISSING FUEL CAP. PARTS USED: 31-2825-9-0001,QT
- [SDR CALA2023081102478](https://openairdocs.org/sdr/CALA2023081102478.md): Fuel Cap · missing · Aug 6, 2023 · N449UA · Airbus A320232 · Fuel Storage
  > PDA 2 REF LOGPAGE 5378717 FUEL CAP MISSING. VARGAS TOMC DOCUMENTED PDA2 EVENT INTO AIRCRAFT LOGBOOK IAW GMM 02-30-95. VARGAS TOMC. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR
- [SDR CALA2023022700566](https://openairdocs.org/sdr/CALA2023022700566.md): Packing · leaking · Feb 27, 2023 · N449UA · Airbus A320232 · Hydraulic Power System
  > FLIGHT CREW REPORTS VIA DISPATCH ARINC HYD B RSVR LO LVL, HYD B SYS LO PR ECAM. VARGAS TOMC PERFORMED HYDRAULIC LEAK CHECK OF THE BLUE SYSTEM IN REFERENCE T PROTRUDING. REMOVED AND REPLACED PACKING IN REFERENCE TO AMM 29 O AMM 29-00-99-200-001-C1. INSPECTED BL
- [SDR CALA2023021300413](https://openairdocs.org/sdr/CALA2023021300413.md): Unknown · cracked · Feb 11, 2023 · N449UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > FUSELAGE FR68 (RH) CRACKED BETWEEN FRAME WEB AND FRAME STIFFENER (STR 22RH) AND CORROSION DAMAGE NOTED IN THE FRAME FWD FACE & INNER CAP AREA BETWEEN STR23R-24R. REF HAECO LCQ NR 9296525 AND NR 9296374. BETWEEN STR23R-24R PER HAECO REO-L242211 REV IR AND ECRA
- [SDR CALA2023021300411](https://openairdocs.org/sdr/CALA2023021300411.md): Unknown · corroded · Feb 11, 2023 · N449UA · Airbus A320232 · Fuselage Main, Frame
  > FRAME 68 R/H FWD FACE HAS CORROSION AROUND ANCHOR NUT AND ALONG FLOOR LINE. GENERATED AT HAECO LCQ PER NR 9296525 (40525) BY V07 7960 {A3NB-53-3-6222} IR AND ECRA 5341-01367. WORK ACCOMPLISHED BY LCQ EMP V080280. LATEST REVISION OF EC/RA 5341-01367 ON OR BEFOR
- [SDR CALA2023021300410](https://openairdocs.org/sdr/CALA2023021300410.md): Door · corroded · Feb 11, 2023 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > R1 DOOR FR 20 STGR 22R- STGR 23R PER HAECO LCQ N/R 9296513/40513 GEN BY V061629 ACCOMPLISHED BY LCQ EMP V080280. ACCOMPLISH INITIAL INSPECTIONS LEVEL PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02946 ON OR ON THE REPAIR AT THE RH FR20 LOWER FWD WEB FACE AT
- [SDR CALA2023021000403](https://openairdocs.org/sdr/CALA2023021000403.md): Frame · corroded · Feb 9, 2023 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > R1 DOOR FR16 STGR 22R-STGR 23R CORRODED PER HAECO LCQ N/R 929651 4/40514 GEN BY V061629 "ACCOMPLISH A PERMANENT REPAIR ON THE FRAME AT RH FR16 AFT OF ECRA 5310-08111 ON OR BEFORE JANUARY 27, 2024" WEB FACE AT Z-520 FLOOR LEVEL PER PART 3 OF THE LATEST REVISION
- [SDR CALA2023020300312](https://openairdocs.org/sdr/CALA2023020300312.md): Not Entered · corroded · Feb 1, 2023 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > R2 DOOR SILL HAVE CORROSION AT FR66 AND FR68 CORNERS PER HAECO L CQ N/R 9296323/40323 GEN BY V061682 REMOVED AND REPLACED R2 DOOR SILL BETWEEN FR66 AND FR68 ALONG WI TH CORNER FITTINGS FWD AND AFT IAW A320 SRM 51-72-11/001 51-42-1 1/001 51-75-12/001 BY MECH V0
- [SDR CALA2023020100280](https://openairdocs.org/sdr/CALA2023020100280.md): None · none · Jan 30, 2023 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT DOOR SILL HAS MULTIPLE SPOTS OF CORROSION FR52A-56. GENERATED AT HAECO LCQ PER NR 9296630 (40630) BY V077 960 {A3NB-53-4-6179} REMOVED AND REPLACED AFT CARGO COMPT DOOR SILL WITH PN D53475575 25800 PO 11257852. RESTORED STRUCTURE PAINT I
- [SDR CALA2023013000239](https://openairdocs.org/sdr/CALA2023013000239.md): Torsion Box · corroded · Jan 27, 2023 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT DOOR TORSION BOX COVER HAS MULTIPLE SPOTS OF CORROSION FR52A-56. REMOVED AND REPLACED TORSION BOX COVER WITH PN D5347556521200 P. O # 1108282.3 IAW A320 SRM 51-42-11/01. APPLIED PRIMER TOPCOAT T O FASTENERS IAW A320 SRM 51-23-00/001.
- [SDR CALA2023011600126](https://openairdocs.org/sdr/CALA2023011600126.md): Fitting · cracked · Jan 15, 2023 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > FLIGHT DECK WINDSHIELD CTR POST RH CONTINUITY FITTING HAS CRACK IN UPPER FLANGE PER HAECO LCQ N/R 9296409/40409 GEN BY V892444 RMVD AND RPLD L/H AND R/H CONTINUITY FITTINGS IAW A320 AIRBUS RE PAIR DWG R53112919 AND DWG R53113426 EC/RA 5310-08103 REPAIR CAT A I
- [SDR CALA2023011000079](https://openairdocs.org/sdr/CALA2023011000079.md): Stringer · corroded · Jan 10, 2023 · N449UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STR41L HAS CORROSION 3" FWD FR58 (A3NB-53- 4-6179) GEN AT HAECO LCQ BY V077960 PER NR 9296638 (40638) ORIG MTL.079", REM''D MTL.013", REM''ING.066" FOUND TO BE OUT STR41L IAW SRM 53-00-13-300-001 FIG 001, INSP THRES FROM TIME INSPECT M
- [SDR CALA2023011000078](https://openairdocs.org/sdr/CALA2023011000078.md): Frame · corroded · Jan 10, 2023 · N449UA · Airbus A320232 · Fuselage Main, Frame
  > FRAME 66 R/H AFT FACE HAS CORROSION AROUND ACHOR NUT AND ALONG F LOOR LINE. PER HAECO LCQ NON-ROUTINE 9296532/40532 GENERATED BY V077960. SPEC: A3NB-53-3-6222. REM''D=.050, MAX REM''L ALLOWED=.020,.107 MTL REM''ING, BRACKET TO FACILITATE ACCESS IAW SRM 51-42
- [SDR CALA2023010900055](https://openairdocs.org/sdr/CALA2023010900055.md): Intercostal · corroded · Jan 6, 2023 · N449UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT PIT STR38L AFT FR 58 INTERCOSTAL WEB HAS CORROSION. REMOVED AND REPLACED (1)EACH INTERCOSTAL WEB, AFT CARGO FR58 - F R59 STRG 38L, IAW SRM 53-41-89-02-A ITEM 095-A PG 72, SRM 51-42-11/001 PARA F PG 15, AND 51-23-11/001 PARA B,2,3, PG9.
- [SDR CALA2022122803507](https://openairdocs.org/sdr/CALA2022122803507.md): Shear Plate · corroded · Dec 27, 2022 · N449UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA RH SHEAR PLATE HAVE CORROSION BETWEEN FR69 AND FR70. RMVD AND RPLD NEW RH SHEAR PLATE DUE TO CORROSION IAW SRM 51-72- 001. PRIME AND PAINTED NEW PART IAW SRM 51-23-11-001 CIC PART 11. RECEIVED AND VERIFIED NEW PORT IAW SRM 53-41-17 AND CERT BEA A
- [SDR CALA2022122803505](https://openairdocs.org/sdr/CALA2022122803505.md): Support · corroded · Dec 27, 2022 · N449UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA WEB SUPPORT HAVE CORROSION TOP AND UNDER BETWEEN FR 69 AND FR70 RST23 PER NR9296332/40332. RMVD AND RPLD NEW RH WEB SUPPORT DUE TO OUT OF LIMIT MATERIAL LOSS IAW SRM 51-72-41. VERIFIED NEW PART RECEIVED IAW SRM 53-41-17. LOCATED AND DRILLED NEW
- [SDR CALA2022122603491](https://openairdocs.org/sdr/CALA2022122603491.md): Fitting · corroded · Dec 24, 2022 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > L2 DOOR LOWER CUT OUT AFT CORNER FITTINGS HAVE CORROSION. REMOVED CORROSION ON L2 AFT CORNER FITTING FOUND TO BE OUT OF LI MITS REMOVED AND REPLACED IAW A320 SRM 51-42-11.
- [SDR CALA2022122303464](https://openairdocs.org/sdr/CALA2022122303464.md): Door Sill · corroded · Dec 21, 2022 · N449UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION IN SEVERAL AREAS. REMOVED AND REPLACED L2 DOOR SILL. IAW A320 SRM 51- 42-11. RESTORED SURFACE PROTECTION IAW SRM 51-75-12-911-001.
- [SDR CALA2022122103454](https://openairdocs.org/sdr/CALA2022122103454.md): Door Sill · corroded · Dec 20, 2022 · N449UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAVE CORROSION FWR AND AFT ENDS PER HA ECO LCQ N/R 9296328/40328. FWD SIDE WAS FOUND TO BE WITHIN LIMITS, AFT WAS OUT OF LIMITS, PERFORMED REPAIR PRINCIPLE 5 IAW SRM 53-41-14-300-001. RESTORED SURFACE PROTECTION IAW SRM 51-21-11.
- [SDR CALA2022121903432](https://openairdocs.org/sdr/CALA2022121903432.md): Intercostal · corroded · Dec 18, 2022 · N449UA · Airbus A320232 · Fuselage Structure (General)
  > SUPPORT TASK AFT WET AREA LH WEB SUPPORT BETWEEN FR69 AND FR70 HAVE CORROSION PER HAECO LCQ N/R9296334/40334 GENERATED BY V06168 2 STEP 1 REMOVED LH WEB SUPPORT @ FR 69-70 DUE TO CORROSION IAW A3 PART AT LH FRAME AREA 69-70 IAW SRM SOR A320-200-51-42-11-001 AP
- [SDR CALA2021011800047](https://openairdocs.org/sdr/CALA2021011800047.md): Beam · corroded · Jan 15, 2021 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > LT EMERGENCY EXIT DOOR INT STRUT CORROSION ON LOWER EDGE BEAM INTERNAL SURFACE A3NB-52-4-6031, GEN BY V061754 PER NR 9294348 HAECO OPS 36348. REMOVED AND REPLACED LOWER EDGE BEAM ON LT FWD EMERGENCY EXIT DOOR, IAW A320 SRM 51-72-11.
- [SDR CALA2021011300039](https://openairdocs.org/sdr/CALA2021011300039.md): Intercostal · cracked · Jan 11, 2021 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > L1 DOOR FR 16 NR 7 STOP, UPPER INBOARD HOLE HAS CRACK INDICATION IN INTERCOSTAL LAYER IN INBOARD DIRECTION. REPAIR BEFORE NEXT FLIGHT CONTACT ENGEERING FOR APPROVED REPAIR INSTRUCTIONS, PER NR 9294106 HAECO OPERATIONS 36106 GEN BY V89244. REPAIRED L1 DOOR FR
- [SDR CALA2021011300038](https://openairdocs.org/sdr/CALA2021011300038.md): Intercostal · cracked · Jan 11, 2021 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > R1 DOOR FR 16 NR 7 STOP, UPPER INBOARD HOLE HAS CRACK INDICATION IN INTERCOSTAL LAYER IN INBOARD DIRECTION. REPAIR BEFORE NEXT FLIGHT "CONTACE ENGINEERING FOR APPROVED REPAIR INSTRUCTIONS", PER NR 9294 109 HAECO OPERATIONS 36109 GEN BY V892444. REPAIRED R1 D
- [SDR CALA2021011100033](https://openairdocs.org/sdr/CALA2021011100033.md): Fitting · cracked · Jan 9, 2021 · N449UA · Airbus A320232 · Fuselage, Landing Gear Attach Fittings
  > LEFT MLG ACTUATOR FITTING AFT LUG HAS CRACK INDICATION AT 12 O`CLOCK POSITION. REPAIRED BEFORE FURTHER FLIGHT REPLACE FITTING, IAW AIRBUS REPAIR DRAWING D53370501 PER NR 9294092 HAECO OP 36092. REMOVED AND REPLACED LT MLG AFT ACTUATOR FITTING, IAW AIRBUS REP
- [SDR CALA2021010400004](https://openairdocs.org/sdr/CALA2021010400004.md): Skin · corroded · Jan 2, 2021 · N449UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > RT EXT FUSELAGE HAS CORROSION AT LAV VENT, REPAIRED RH EXT FUSELAGE AT LAV EXHAUST VENT, IAW A320 SRM 53-41-11-300-004.
- [SDR CALA2020021600426](https://openairdocs.org/sdr/CALA2020021600426.md): Skin · cracked · Feb 13, 2020 · N449UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF RIGHT HAND FRAME 35-36 EA5330-05216 FOUND MULTIPLE HOLES WITH DEFECTS/CRACKS ACCOMPLISHED INTERIM REPAIR IN REF TO ECRA 5331-02607 PART 1, ACCOMPLISH PERMANENT REPAIR IN REF TO PER PART 3 OF ECRA 5331-02607 ON OR BEFORE 76,475CYCLES OR 166
- [SDR CALA2019042900673](https://openairdocs.org/sdr/CALA2019042900673.md): Oxygen Gen · unwanted deploy · Apr 29, 2019 · N449UA · Airbus A320232 · Passenger Oxygen System
  > OXYGEN MASKS DPOPPED AT ROW 37 D-E-F, REPACK MASKS AND CARRY PER AMM 35-21-43 OXYGEN CYL FIRED MUST BE REPLACED DEF PER MEL - SEATS 37 DEF INO P DO NOT USE PER MEL 3521A MAC RELATED WORK ORDER 000000001885672 AND PRTR MAC METER INITIATED FOR WITH VENDOR ID V9
- [SDR CALA2018111202362](https://openairdocs.org/sdr/CALA2018111202362.md): Bulb · inoperative · Nov 12, 2018 · N449UA · Airbus A320232 · Emergency Lighting
  > RH OVERWING FWD EXTERIOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. UPDATE RELAMPED BULB AT RH OVERWING FWD EXTERIOR EMERGENCY EXIT LIGHT. OPS CHECKED GOOD REF AMM33-51-00-710-001. INSPECTED LIGHT OPERATION, RH OVERWING EXTERIOR EMERGENCY EXIT LIGHT.
- [SDR CALA2018060531361](https://openairdocs.org/sdr/CALA2018060531361.md): Skin · dented · May 25, 2018 · N449UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A DENT WAS FOUND ON THE SKIN BETWEEN FRAMES 68-69 AND STR 41L-35L. REPAIRED IAW SRM 53-41-11-300-018.
- [SDR CALA2018060531338](https://openairdocs.org/sdr/CALA2018060531338.md): Window Post · cracked · May 21, 2018 · N449UA · Airbus A320232 · Fuselage Main, Structure
  > LEFT WINDSHIELD SIDE POST LOWER ATTACHMENT, FRAME 4 AFT LOWER WEB WAS CRACKED. REPAIRED THE WINDSHIELD POST LOWER WEB IAW ECRA 5311-01939.
- [SDR CALA2018060531327](https://openairdocs.org/sdr/CALA2018060531327.md): Cover · cracked · May 20, 2018 · N449UA · Airbus A320232 · Escape Slide
  > THE LT OVERWING SLIDE COVER WAS CRACKED.
- [SDR CALA2018060531326](https://openairdocs.org/sdr/CALA2018060531326.md): Cover · cracked · May 20, 2018 · N449UA · Airbus A320232 · Escape Slide
  > THE RT OVERWING ESCAPE SLIDE COVER WAS CRACKED AND SEPERATING. REMOVED & REPLACED THE OVERWING ESCAPE SLIDE IAW AMM 25-62-42-400-001-A.
- [SDR CALA2018051501255](https://openairdocs.org/sdr/CALA2018051501255.md): Control Rod · damaged · May 11, 2018 · N449UA · Airbus A320232 · Trailing Edge Flaps
  > LEFT INBD FLAP TRACK NR. 2. CANOE CONTROL ROD UPPER ATTACHMENT FITTING HOLES ELONGATED. REMOVED AND REPLACED THE CONTROL ROD UPPER ATTACHMENT FITTING IAW CMM 57-5 2-21-410-009-A01.
- [SDR CALA2017041000951](https://openairdocs.org/sdr/CALA2017041000951.md): Director · malfunctioned · Apr 10, 2017 · N449UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COME ON. RESET CIDS 2 DIRECTOR EMERGENCY LIGHTS. OPS CHECK GOOD REF MM 33-51-00.
- [SDR CALA2016123001201](https://openairdocs.org/sdr/CALA2016123001201.md): Battery Pack · no test · Dec 30, 2016 · N449UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY AT 3L FAILED CAPACITY CHECK. REPLACED BATTERY IAW MM 33-51-38-400-002-A
- [SDR CALA2016123001200](https://openairdocs.org/sdr/CALA2016123001200.md): Battery Pack · no test · Dec 30, 2016 · N449UA · Airbus A320232 · Emergency Lighting
  > BATTERY PACK AT EMERGENCY EXIT RIGHT FAILED CAPACITY TEST. REPLACED THE BATTERY PACK IAW MM 33-51-38-400-002-A
- [SDR CALA2016090195709](https://openairdocs.org/sdr/CALA2016090195709.md): Shear Tie · corroded · Aug 31, 2016 · N449UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO AT FRAME 33 BETWEEN STRINGERS 40 & 41R SHEAR TIE HAS CORROSION. REMOVED & REPLACED THE SHEAR TIE IAW SRM51-42-11.

Next page: https://openairdocs.org/aircraft/N449UA/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 = 'N449UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N449UA/reports

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