# Service difficulty reports: N433UA

A list on [N433UA](https://openairdocs.org/aircraft/N433UA.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 · 200 reports

- [SDR CALA2026080518296](https://openairdocs.org/sdr/CALA2026080518296.md): Light · split · Aug 4, 2026 · N433UA · Airbus A320232 · Emergency Lighting
  > DURING OPS CHECK OF THE EMERGENCY POWER SUPPLY UNITS PTP DISPLAYS FAULT MESSAGE EPSU EXT LOAD EMR R. FOUND AFT RT OVERWING LIGHT TO BE BURNED OUT. WHEN INSPECTING THE LIGHT FOUND LIGHT HOUSING SPLIT IN HALF. REPLACED OVERWING LIGHT ASSY IAW AMM 33-51-15-400-
- [SDR CALA2026072818065](https://openairdocs.org/sdr/CALA2026072818065.md): Oven · odor · Jul 27, 2026 · N433UA · Airbus A320232 · Buffet/Galleys
  > AFT GALLEY HAS A BURNED ODOR. REF TSM 05-50-00-810-831-A TYPE 10. INSPECTED AFT GALLEY CARTS, DUCTS, AND EQUIPMENT. FOUND LIGHT COFFEE STAINS ON WARMER, REMOVED. REMOVED GALLEY CARTS AND FOUND 2 FULL OF OLD FOOD WITH ODORS. REMOVED FOOD AND CLEANED CART IN
- [SDR CALA2026070617560](https://openairdocs.org/sdr/CALA2026070617560.md): Oven · odor · Jun 22, 2026 · N433UA · Airbus A320232 · Buffet/Galleys
  > FLIGHT ATTENDANTS REPORT NOXIOUS OVEN ODOR REPORTED AFT GALLEY OVEN R42. OPERATED OVEN WITH NO RACKS OR VISIBLE BURNT FOOD. ODOR PERSISTED. PULLED AND COLLARED CB. PLACE ON DEFERRAL.OKAY TO NEF 2522AD ODOR DOES NOT PERSIST UPON DEACTIVATION OF OVEN, PLACED ON
- [SDR CALA2026062217255](https://openairdocs.org/sdr/CALA2026062217255.md): Computer · faulty · Jun 21, 2026 · N433UA · Airbus A320232 · Aileron Control System
  > AILERON SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F- CTL F/CTL AIL SERVO FAULT IN FLIGHT ON CLIMB OUT DURING MOD TURBULENCE. REMOVED AND REPLACED ELAC1 REF AMM TASK 27-93-34-400-001-A, OPS. CHECK SAT, NO FURTHER DEFECTS NOTED.
- [SDR CALA2026042015532](https://openairdocs.org/sdr/CALA2026042015532.md): Fuel Cap · missing · Apr 17, 2026 · N433UA · Airbus A320232 · Fuel Storage
  > RT UNDERWING FUEL CAP MISSING. RT UNDERWING FUEL CAP REPLACED IAW IPC 28-25-41. FUEL CAP SECURE AND OKAY FOR SERVICE.
- [SDR CALA2026022013932](https://openairdocs.org/sdr/CALA2026022013932.md): Fuel Cap · broken · Feb 18, 2026 · N433UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS FUEL CAP BROKEN. VERIFIED NO LEAK FROM COUPLING. FUEL CAP. REMOVED & INSTALLED FUEL CAP IAW AMM 28-25-41. OPS CHKD GOOD.
- [SDR CALA2025120511783](https://openairdocs.org/sdr/CALA2025120511783.md): Wire · broken · Dec 1, 2025 · N433UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT AT ROW 35ABC IS INOPERATIVE. RELAMPED NO HELP. VERIFIED THAT NO TWO ADJACENT EMERGENCY LIGHTS ARE INOPERATIVE. VERIFIED THAT ITS THE RED LIGHT THAT WERE INOPERATIVE AND VERIFIED BLUE LIGHTS WORK CORRECLTY. DEFERED UNDER MEL 3350C, COMPLIE
- [SDR CALA2025091508878](https://openairdocs.org/sdr/CALA2025091508878.md): Light · no test · Sep 14, 2025 · N433UA · Airbus A320232 · Emergency Lighting
  > VISUAL INSP FOUND EMERGENCY ROW LIGHTING AT SEAT ROWS 26, 27 AND 28 (ABC) INOPERATIVE. REMOVED AND REPLACED SEAT MOUNTED EMERGENCY LIGHTS FOR ROWS 26,27,28. IAW TASK 33-51-19-000-002-A AND TASK 33-51-19-400-002-A OPS CHECK GOOD.
- [SDR CALA2025080607387](https://openairdocs.org/sdr/CALA2025080607387.md): Battery · no test · Aug 5, 2025 · N433UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EPSU BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED RT EMERGENCY EPSU BATTERY IAW AMM 33-51-38-000-002-A. OPS CHECKED GOOD
- [SDR CALA2025051904762](https://openairdocs.org/sdr/CALA2025051904762.md): Light · damaged · May 16, 2025 · N433UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY FLOOR PROX LIGHT INOP AT SEAT 25C FOUND EMERGENCY FLOOR PROX LIGHT ASSY CRACKED AND WIRE PULLED FROM A/C SIDE CONNECTOR. REMOVED AND REPLACED PROX LIGHT ASSY. REF. AMM 33-51-19. PULLED WIRE STILL NEEDS TO BE CRIMPED INTO CONNECTOR. WIRE CRIMP TOOL FO
- [SDR CALA2024102300906](https://openairdocs.org/sdr/CALA2024102300906.md): Skin · damaged · Oct 3, 2024 · N433UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REF LP 9356893 LIGHTING STRIKE FOUND ON FRAME 54 BETWEEN STR 36L AND STR 37L LENGHT IS.2 BY WIDE 1.7 IAW SRM 53-21-11-283-004 FIG 1,SPEED TAPED DISCREPANT AREA AS PER SRM 51-75-12-911-022. UNLOCKING ACCOMPLISHED GVI OF REMOVED DAMAGED AREA PER SRM 53-21-11-30
- [SDR CALA2024100900798](https://openairdocs.org/sdr/CALA2024100900798.md): Skin · damaged · Oct 3, 2024 · N433UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REF LP 9356893 LIGHTING STRIKE FOUND BETWEEN FRAME 31 AND FRAME 32. BETWEEN STR 39L AND 38L. LENGHT IS.5" BY WIDE.5"... CLOSEST FASTNER IS 28"STRIKE IS 6.8" FROM FR 31. FOUND STRIKE TO BE BURNED THRU SKIN. IAW SRM 53-21-11-283-004 LOCKING LOG PAGE FOR FERRY
- [SDR CALA2023112403460](https://openairdocs.org/sdr/CALA2023112403460.md): Compressor · stalled · Nov 22, 2023 · N433UA · Airbus A320232 · Turbine Engine Compressor Section
  > ENG 1 COMPRESSOR STALL EGT LIMIT EXCEEDED. UE TO REPEAT #1 ENGINE STALLS REPLACE #1 ENGINE PER AMM 71-00-20. INSTALL ESN V10196. TOMC-MEREDITH PARTS UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1047251 SN OFF 0091 UPDATE ENG REMOVAL AND INSTALLATION ROTABL
- [SDR CALA2023112203450](https://openairdocs.org/sdr/CALA2023112203450.md): Bleed Valve · worn · Nov 20, 2023 · N433UA · Airbus A320232 · Compressor Bleed Valve
  > DUE TO ENGINE 1 STALL SFOEP REPORTING NACELLE TEMPERATURE WAS EXTREMELY HI AND LOSS OF 30 DEGREES OF EGT MARGIN. CREW DEBRIEF: #1 ENGINE, MULTIPLE STALLS WHILE IN CLIMB. DID NOT SHUTDOWN ENGINE INFLIGHT. ENGINE SHUTDOWN NORMALLY AT GATE. DURING THE STALL EVENT
- [SDR CALA2023060901794](https://openairdocs.org/sdr/CALA2023060901794.md): Gps · inoperative · Jun 7, 2023 · N433UA · Airbus A320232 · Navigation System
  > GPS PRIMARY LOST ALIGN LIGHTS FLASHING.SWITCHED DATABASE ANDREAL IGN PER MX. OPS NML T/S REF TSM 34-12-00-810-801-A. ALIGNED ADIRS. OPS CHECK GOOD AT THIS TIME. ADD EMP:U399271
- [SDR CALA2023041701147](https://openairdocs.org/sdr/CALA2023041701147.md): Frame · punctured · Apr 16, 2023 · N433UA · Airbus A320232 · Fuselage Main, Frame
  > FR 24A FWD CARGO PUNCTURE FOUND ON INBOUND WALK. EA79-2023-061 PERFORMED DT THICKNESS CHECK OF GOUGE IAW NTM 51-1 REPAIR TO BE EMBODIED BY 33,799 TFC, FH NOT RELEVANT 0-04. FABRICATED REPAIR ANGLE IAW EA 79-2023-061 INSTALLED REPAI R ANGLE IAW EA 79-2023-061 R
- [SDR CALA2023041201100](https://openairdocs.org/sdr/CALA2023041201100.md): Lamp · inoperative · Apr 12, 2023 · N433UA · Airbus A320232 · Emergency Lighting
  > INOP EMERGENCY EXIT LAMP AT SR 36C. NEW BULB DID NOT CHANGE ISSU E. NO POWER DETECTED AT CONNECTOR. COORECTED WIRE ISSUE AT SR 36 LH IAW ESPM 20-43-11-01-H. OPC EME RGENCY LIGHTING SYSTEM IAW AMM 33-51-00-710-805-A TEST OK.
- [SDR CALA2022112503227](https://openairdocs.org/sdr/CALA2022112503227.md): Drain Line · damaged · Nov 25, 2022 · N433UA · Airbus A320232 · Engine Drains
  > PDA 3 ENGINE #1 ZONE F DRAIN TUBE, APPROXIMATELY 8 INCHES, MISSING FROM AIRCRAFT. INSTALLED LH ZONE F DRAIN TUBE. REF AMM 54-51-29.
- [SDR CALA2022102702977](https://openairdocs.org/sdr/CALA2022102702977.md): Light · inoperative · Oct 27, 2022 · N433UA · Airbus A320232 · Flight Compartment Lighting
  > READING LIGHT INOP AT 30B 30C RELAMPED READING LIGHTS AT SEAT 30 B AND 30 C, NO HELP. APPLIED NEF. APPROVED. READING LIGHT PANEL ASSY M&E 31-2373-3-0003 FOUND READING LIGHT 30C OP CHK OK BUT 30 B STILL INOP AFTER RELAMP NO HELP, WILL REQUIRE READING LIGTH PANE
- [SDR CALA2022032500779](https://openairdocs.org/sdr/CALA2022032500779.md): Keelbeam · not reported · Mar 24, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE RH KEEL BEAM MLG ATTACHMENT STRUCTURE. ER ECRA 5330-06914. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24
- [SDR CALA2022032500778](https://openairdocs.org/sdr/CALA2022032500778.md): Not Reported · not reported · Mar 24, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE LH KEEL BEAM MLG ATTACHMENT STRUCTURE. ECRA 5330-06914. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24-FE
- [SDR CALA2022032500777](https://openairdocs.org/sdr/CALA2022032500777.md): Not Reported · punctured · Mar 24, 2022 · N433UA · Airbus A320232 · Elevator Control System
  > SUPPORT TASK: HAIL DAMAGE, RH ELEVATOR HAS A PUNCTURW UPPER SURF ACE 28 INCHES FROM INBOARD END 25 INCHES FROM TE() REPAIRED R/H ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11-300-00 7. EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM
- [SDR CALA2022032500776](https://openairdocs.org/sdr/CALA2022032500776.md): Skin · corroded · Mar 24, 2022 · N433UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > (SDR) AFT CARGO LOWER BILGE, C54-55 SKIN BETWEEN STR42R-43R HAS CORROSION NEAR DOME NUTS PERFORMED BY VTMAE BFM EMPLOYEE V934344. ON OR BEFORE REVISION OF ECRA 5341-01032 SEP. 10, 2022 PERFORM AN INSPECTION AS PER PART 2 OF THE LATEST PERFORMED INTERIM REPAIR
- [SDR CALA2022032500775](https://openairdocs.org/sdr/CALA2022032500775.md): Not Reported · cracked · Mar 23, 2022 · N433UA · Airbus A320232 · Standard Practices/Structures
  > (AD2020-20-05) DURING ROTO INSPECTION OF THE RH FR16 DOUBLE JOGG LE HOLE #19. REJECTABLE DAMAGE INDICATION WAS NOTED DUE TO MECHA NICAL DAMAGE IN THE I/B LAYER (FRAME). REPAIR BEFORE NEXT FLIGHT REF VT MAE NR#0023205, REPAIRD RH FR16 DOUBLE JOGGLE HOLE #19 IAW
- [SDR CALA2022032300770](https://openairdocs.org/sdr/CALA2022032300770.md): Frame · cracked · Mar 23, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2020-20-05) DURING ROTO INSPECTION OF THE RH FR16 DOUBLE JOGG LE HOLE #19. REJECTABLE DAMAGE INDICATION WAS NOTED DUE TO MECHA NICAL DAMAGE IN THE I/B LAYER (FRAME). REPAIR BEFORE NEXT FLIGHT REF VT MAE NR#0023205, REPAIRD RH FR16 DOUBLE JOGGLE HOLE #19 IAW
- [SDR CALA2022032300771](https://openairdocs.org/sdr/CALA2022032300771.md): Elevator · punctured · Mar 23, 2022 · N433UA · Airbus A320232 · Elevator Control System
  > SUPPORT TASK: HAIL DAMAGE, RH ELEVATOR HAS A PUNCTURW UPPER SURF ACE 28 INCHES FROM INBOARD END 25 INCHES FROM TE() REPAIRED R/H ELEVATOR UPPER SURFACE IAW A320 SRM 55-21-11-300-00 7. EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM
- [SDR CALA2022032100738](https://openairdocs.org/sdr/CALA2022032100738.md): None · corroded · Mar 21, 2022 · N433UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (SDR) AFT CARGO LOWER BILGE, C54-55 SKIN BETWEEN STR42R-43R HAS CORROSION NEAR DOME NUTS PERFORMED BY VTMAE BFM EMPLOYEE V934344. ON OR BEFORE REVISION OF ECRA 5341-01032 SEP. 10, 2022 PERFORM AN INSPECTION AS PER PART 2 OF THE LATEST PERFORMED INTERIM REPAIR
- [SDR CALA2022032100737](https://openairdocs.org/sdr/CALA2022032100737.md): Stringer · corroded · Mar 21, 2022 · N433UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (SDR) AFT CARGO LOWER BILGE. C54-55 STRINGER 44 HAS CORROSION BFM EMPLOYEE V934344. ON OR BEFORE SEP. 10, 2022 PERFORM AN 5341-01032 INSPECTION AS PER PART 2 OF THE LATEST REVISION OF ECRA PERFORMED INTERIM REPAIR OF AFT CARGO LOWER BILGE. C54-55 STRINGER 44 A
- [SDR CALA2022032100734](https://openairdocs.org/sdr/CALA2022032100734.md): None · cracked · Mar 21, 2022 · N433UA · Airbus A320232 · Standard Practices/Structures
  > (AD2020-20-05) L/H FR 16 DOUBLE JOGGLE HOLES 7,AB, AND D HAVE CR ACK INDICATIONS IN MIDDLE AND AFT LAYERS OF THE HOLES.() REPAIR BEFORE NEXT FLIGHT COMPLIED WITH EC/RA 5311-02775. REPAIRED FR16 L/H AND R/H DOUBLE JOGGLE FASTENER HOLES. NO DEVIATIONS NOTED. EMP
- [SDR CALA2022032100733](https://openairdocs.org/sdr/CALA2022032100733.md): Keelbeam · none · Mar 21, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE LH KEEL BEAM MLG ATTACHMENT STRUCTURE. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24-FEB-2023. PERFORMED
- [SDR CALA2022032100715](https://openairdocs.org/sdr/CALA2022032100715.md): Stringer · corroded · Mar 19, 2022 · N433UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (SDR) AFT CARGO FR62-63 STRINGER 32R HAS CORROSION COMPLIED W/ EC/RA 5311-02784 NO DEVIATIONS NOTED.ACCOMPLISHED BY EMP#V934344 AT ST BFM AEROSPACE MOBILE. NR#0023443
- [SDR CALA2022031700695](https://openairdocs.org/sdr/CALA2022031700695.md): None · damaged · Mar 17, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > FR16 LH DOUBLE JOGGLE FASTENER HOLES #7, #A, #B, #D, & #E DAMAGE INSPECTION REQUIREMENTS ON LHS HOLES #7, #8, #A AND #B PER BEFORE THE AIRCRAFT REACHES 37,605 TOTAL FLIGHT CYCLES. 4,700 FLIGHT CYCLES THEREAFTER. PART 2A OF THE LATEST REVISION OF EC/RA 5311-027
- [SDR CALA2022031700683](https://openairdocs.org/sdr/CALA2022031700683.md): Skin · cracked · Mar 16, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING EA 5310-07772 REV. ORIG, OP. 001 AND 004; PRODUCTION REPORTED DAMAGE INDICATIONS AT HOLE #1 AND CRACK INDICATIONS AT HOLES #2 AND #3 IN THE RIGHT HAND FR35 AT STGR30. 135,400 FH OR 67,700 FC, WHICHEVER OCCURS FIRST, PERFORM 5310-07989. INSP
- [SDR CALA2022031700682](https://openairdocs.org/sdr/CALA2022031700682.md): Skin · cracked · Mar 16, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2020-20-05) DURING ROTO INSPECTION OF RH FR20 DOUBLE JOGGLE HOLES. CRACK INDICATION WAS NOTED IN HOLE A. REPAIR BEFORE NEXT F LIGHT.() REPAIRED R/H FR20 DOUBLE JOGGLE HOLE #A BY OVERSIZING IAW EC/RA 5311-02774. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERI
- [SDR CALA2022031700681](https://openairdocs.org/sdr/CALA2022031700681.md): Skin · cracked · Mar 16, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2020-20-05) L/H FR 16 DOUBLE JOGGLE HOLES 7,AB, AND D HAVE CR ACK INDICATIONS IN MIDDLE AND AFT LAYERS OF THE HOLES.() REPAIR BEFORE NEXT FLIGHT
- [SDR CALA2022031700680](https://openairdocs.org/sdr/CALA2022031700680.md): Fitting · damaged · Mar 16, 2022 · N433UA · Airbus A320232 · Nacelle/Pylon Structure
  > LH PYLON, TYPE B HOLES 1A (LHS O/B HOLE) AND 1B (LHS I/B HOLE) DAMAGE INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF TOTAL FC OR 133,744 TOTAL FH, WHICHEVER OCCURS FIRST. THERE EC/RA 5451-01386 EVERY 27,400 FC OR 54,800FH, WHICHEVER EC/RA 5451-01
- [SDR CALA2022031700678](https://openairdocs.org/sdr/CALA2022031700678.md): Fitting · damaged · Mar 16, 2022 · N433UA · Airbus A320232 · Nacelle/Pylon Structure
  > RH PYLON, TYPE B HOLES 1A (RHS O/B HOLE) AND 1B (RHS I/B HOLE) DAMAGE INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION OF TOTAL FC OR 133,744 TOTAL FH, WHICHEVER OCCURS FIRST. THERE EC/RA 5451-01386 EVERY 27,400 FC OR 54,800FH, WHICHEVER EC/RA 5451-01
- [SDR CALA2022031400664](https://openairdocs.org/sdr/CALA2022031400664.md): None · cracked · Mar 14, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING EA 5310-07772 REV. ORIG, OP. 001 AND 004; PRODUCTION REPORTED DAMAGE INDICATIONS AT HOLE #1 AND CRACK INDICATIONS AT HOLES #2 AND #3 IN THE RIGHT HAND FR35 AT STGR30. 135,400 FH OR 67,700 FC, WHICHEVER OCCURS FIRST, PERFORM 5310-07989. INSP
- [SDR CALA2022031400663](https://openairdocs.org/sdr/CALA2022031400663.md): Keelbeam · damaged · Mar 14, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > WHILE ACCOMPLISHING INSPECTIONS PER FCD 5330-05575D, PRODUCTION REPORTED MULTIPLE DISCREPANT/OVERSIZED HOLES IN THE RH KEEL BEAM MLG ATTACHMENT STRUCTURE. ECRA 5330-06914. ACCOMPLISH A PERMANENT REPAIR PER LATEST REVISION OF EC/RA 5330-06914 ON OR BEFORE 24-FE
- [SDR CALA2022031400650](https://openairdocs.org/sdr/CALA2022031400650.md): None · cracked · Mar 12, 2022 · N433UA · Airbus A320232 · Passenger/Crew Doors
  > A3NB-05-3-6159 LH FWD EMERGENCY EXIT DOOR FWD INNER FRAME HAS CR ACKS FWD OF WINDOW. DOT 102-06() REMOVED AND REPLACED SEGMENT ANGLE ON L/H FWD EMERGENCY EXIT DOO R IAW SRM 51-42-11. EMP# V934342 WORK ACCOMPLISHED AT ST ENGINEE RING AEROSPACE OF MOBILE AT BFM
- [SDR CALA2022031400649](https://openairdocs.org/sdr/CALA2022031400649.md): None · cracked · Mar 12, 2022 · N433UA · Airbus A320232 · Passenger/Crew Doors
  > A3NB-05-3-6159 LH AFT EMERGENCY EXIT HATCH STRUCTURE AFT OF WIND OW HAS CRACK AT RIVET. DOT 102-50() REMOVED AND REPLACED SEGMENT ANGLE ON L/H AFT EMERGENCY EXIT DOO R IAW SRM 51-42-11. EMP# V934342 WORK ACCOMPLISHED AEROSPACE OF MOBILE AT BFM ON NR# 0023065
- [SDR CALA2022031400648](https://openairdocs.org/sdr/CALA2022031400648.md): None · cracked · Mar 12, 2022 · N433UA · Airbus A320232 · Passenger/Crew Doors
  > A3NB-05-3-6159 RH FWD EMERGENCY EXIT DOOR AFT INNER FRAME HAS PO SSIBLE CRACK COMING FROM FASTENER HOLE MARKED.() REMOVED AND REPLACED SEGMENT ANGLE ON R/H FWD EMERGENCY EXIT DOO R IAW SRM 51-42-11. EMP# V934342 WORK ACCOMPLISHED AT ST ENGINEE RING AEROSPACE O
- [SDR CALA2022031400647](https://openairdocs.org/sdr/CALA2022031400647.md): None · cracked · Mar 12, 2022 · N433UA · Airbus A320232 · Passenger/Crew Doors
  > A3NB-05-3-6159 RH AFT EMERGENCY EXIT AFT INNER FRAME HAS CRACKS. DOT 102-09() REMOVED AND REPLACED SEGMENT ANGLE ON R/H AFT EMERGENCY EXIT IAW SRM 51-42-11. EMP# V934342 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 0022699
- [SDR CALA2022031000636](https://openairdocs.org/sdr/CALA2022031000636.md): Skin · cracked · Mar 10, 2022 · N433UA · Airbus A320232 · Standard Practices/Structures
  > (AD2020-20-05) DURING ROTO INSPECTION OF RH FR20 DOUBLE JOGGLE H OLES. CRACK INDICATION WAS NOTED IN HOLE A. REPAIR BEFORE NEXT F LIGHT.() REPAIRED R/H FR20 DOUBLE JOGGLE HOLE #A BY OVERSIZING IAW EC/RA 5311-02774. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEER
- [SDR CALA2022030900616](https://openairdocs.org/sdr/CALA2022030900616.md): None · damaged · Mar 8, 2022 · N433UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (SUPPORT TASK) AD2018-03-12 WORK TRANSFERRED FROM NR 0023193,002 3192,0023191 FR66 DOOR STOP FITTING HAVE DAMAGE INDICATIONS AT S TOP #''S, HOLE #''S LHS #3, H4 #1, H3 AND RHS #6, H3() (GOUGES) AS PER ECRA 5341-01300. WORK ACCOMPLISHED BY VT MAE PART 2 OF THE
- [SDR CALA2022030900615](https://openairdocs.org/sdr/CALA2022030900615.md): Floor Support · cracked · Mar 8, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2018-14-09) DURING ROTO INSP OF LH FR20 CROSSBEAM CRACK INDIC ATION AT HOLES H17 AT 6 O''CLOCK, H20 AT 12 O''CLOCK, H21 AT 12 O'' CLCOK IN BOTH LAYERS WITH SH OVER 125% CIRCLED IN RED, REPAIR BE FORE NEXT FLIGHT PER STEP 8. () ACCOMPLISHED BY VT MAE EMPLOYE
- [SDR CALA2022030700600](https://openairdocs.org/sdr/CALA2022030700600.md): Fitting · damaged · Mar 7, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > DAMAGE INDICATION IN THE RIGHT HAND DOORSTOP FITTING 6 HOLE #3 (SCRATCHES) ACCOMPLISHED BY VT MAE EMPLOYEE ACCOMPLISH OF EC/RA 5341-01300 BEFORE THE AIRCRAFT REACHES 56,600 TOTAL INSPECTION REQUIREMENTS PER PART 2 OF THE LATEST REVISION FLIGHT CYCLES PERFORMED
- [SDR CALA2022030700598](https://openairdocs.org/sdr/CALA2022030700598.md): Crossbeam · cracked · Mar 7, 2022 · N433UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2018-14-09) DURING ROTO INSP OF LH FR20 CROSSBEAM CRACK INDIC ATION AT HOLES H17 AT 6 O''CLOCK, H20 AT 12 O''CLOCK, H21 AT 12 O'' CLCOK IN BOTH LAYERS WITH SH OVER 125% CIRCLED IN RED, REPAIR BE FORE NEXT FLIGHT PER STEP 8. () ACCOMPLISHED BY VT MAE EMPLOYE
- [SDR CALA2022030700597](https://openairdocs.org/sdr/CALA2022030700597.md): Fitting · damaged · Mar 7, 2022 · N433UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (SUPPORT TASK) AD2018-03-12 WORK TRANSFERRED FROM NR 0023193,002 3192,0023191 FR66 DOOR STOP FITTING HAVE DAMAGE INDICATIONS AT S TOP #''S, HOLE #''S LHS #3, H4 #1, H3 AND RHS #6, H3() (GOUGES) AS PER ECRA 5341-01300. WORK ACCOMPLISHED BY VT MAE PART 2 OF THE
- [SDR CALA2022030700584](https://openairdocs.org/sdr/CALA2022030700584.md): None · corroded · Mar 5, 2022 · N433UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > A3NB-53-4-6179 AFT CARGO C56-57 STRINGER 43R HAS CORROSION ALONG I/B SIDE. DOT 102-401.() REMOVED AND REPLACED STRINGER 43R FR56-60 IAW SRM 51-42-11. RECE IVED NEW PN# D5347042620260. RESTORED PROTECTIVE FINISH (INTERNA L) IAW SRM 51-75-12. FORM 44-0008 ATTACH

Next page: https://openairdocs.org/aircraft/N433UA/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 = 'N433UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N433UA/reports

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