# Service difficulty reports: N475UA

A list on [N475UA](https://openairdocs.org/aircraft/N475UA.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 · 125 reports

- [SDR CALA2026092819844](https://openairdocs.org/sdr/CALA2026092819844.md): Oxygen Mask · no discrepancy · Sep 23, 2026 · N475UA · Airbus A320232 · Passenger Compartment Equipment
  > AFT SAFETY DEMO KIT NEED TO BE REPLACED FA REPORT IT HAS A FOUL ODOR. DEMO KIT DEFERRED UNDER NEF 2522JH WITH LOCAL FBO. NO FOUL ODOR NOTED AT THIS TIME. NO BAG SENT. O2 MASK SMELLS FINE ALSO.
- [SDR CALA2026071417776](https://openairdocs.org/sdr/CALA2026071417776.md): Battery · faulty · Jul 14, 2026 · N475UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - EMERGENCY LIGHT ON CIDS BITE TEST FAULT: EPSU BATTERY EMER R R&R BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) IAW AMM 33-51-38 OPS CHECK GOOD PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2026052216451](https://openairdocs.org/sdr/CALA2026052216451.md): Power Supply · faulted · May 20, 2026 · N475UA · Airbus A320232 · Emergency Lighting
  > EPSU COMM FWD L FAULT & EPSU COMM EMER L FAULT DISPLAYED AFTER OPS CHECK OF EPSU FOR OVERWING EXIT SLIDE INSTALL REF AMM 33-51-00-710-001-A. ACCOMPLISHED OPS CHECK OF EPSU UNIT BY BITE CHECK REF AMM 33-51-00-710-001-A, OPS CHECK GOOD, TEST OK
- [SDR CALA2025123012542](https://openairdocs.org/sdr/CALA2025123012542.md): Light · broken · Dec 29, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > FOUND ROW 32 EMERGENCY SEAT LIGHT BROKEN OFF. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & AMM 33-51-19-400-002-A. OPS CHECKED GOOD.
- [SDR CALA2025123012540](https://openairdocs.org/sdr/CALA2025123012540.md): Light · inoperative · Dec 29, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > FOUND SEAT 30ABC EMERGENCY LIGHT INOPERATIVE. R & R ROW 30 EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & AMM 33-51-19-400-002-A. OPS CHECKS GOOD.
- [SDR CALA2025123012538](https://openairdocs.org/sdr/CALA2025123012538.md): Light · inoperative · Dec 29, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > FOUND AFT EMERGENCY LIGHT INOPERATIVE, SEAT 27 ABC. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & 33-51-19-400-002-A. OPS CHECKS GOOD.
- [SDR CALA2025123012536](https://openairdocs.org/sdr/CALA2025123012536.md): Light · broken · Dec 29, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > FOUND FWD EMERGENCY LIGHT INOPERATIVE, SEAT 25 ABC. R & R THE EMERGENCY LIGHT ASSY IAW AMM 33-51-19-000-002-A, & 33-51-19-400-002-A. OPS CHECKED GOOD.
- [SDR CALA2025121612171](https://openairdocs.org/sdr/CALA2025121612171.md): Power Supply · faulted · Dec 13, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > AFT EMERGENCY LIGHTS WOULD RANDOMLY FLICKER ON & OFF. R&E CHANGING BATTERY AND CHARGER AT THIS TIME. ACFT INBOUND CREW REPORTED THAT AFT EMERGECY LIGHT WOULD BLINK OFF & ON, & THEN BACK OFF AT ABOUT THE TIME OF DISARMING THE DOORS DID NOT SEE ANY BLINKING
- [SDR CALA2025071406503](https://openairdocs.org/sdr/CALA2025071406503.md): Wire Splice · damaged · Jul 11, 2025 · N475UA · Airbus A320232 · Light System Wiring
  > PROCEDURE - AFTER DOING CABIN EMERGENCY LIGHTING TEST, FAULT INDICATED EPSU INT LOAD EMER L. EMERGENCY LIGHTS INOP FROM SEAT ROW 26- 28. BITE TEST EMER L PWR SUPPLY, SHOWED SHORT IN LIGHTING SYSTEM. AT ROW 27ABC, FOUND DAMAGED SPLICE AT FLOOR-TO-SEAT CONNECTOR
- [SDR CALA2025061705598](https://openairdocs.org/sdr/CALA2025061705598.md): Light · no discrepancy · Jun 13, 2025 · N475UA · Airbus A320232 · Emergency Lighting
  > REMOVED RH EMERGENCY EXIT PATH TO FOM IN REF TO AMM TASK 52-21-11-000-001-A. FOLLOWED RSC IN REF TO GMM 02-30-25. INSTALLED RH AFT OVERWING HATCH IN REF TO AMM TASK 52-21-11-400-001-A.
- [SDR CALA2025041804022](https://openairdocs.org/sdr/CALA2025041804022.md): Slide · no discrepancy · Apr 18, 2025 · N475UA · Airbus A320232 · Escape Slide
  > RQST INSPECTION OF DOOR 2L SLIDE PX INSPECTED DOOR 2L SLIDE PRESSURE GUAGE, PRESSURE IN LIMITS. REF AMM 25-62-00/601
- [SDR CALA2024032600866](https://openairdocs.org/sdr/CALA2024032600866.md): Fuel Cap · missing · Mar 21, 2024 · N475UA · Airbus A320232 · Fuel Storage
  > PDA 2 CHS REPORTED MISSING FUEL CAP POST FLIGHT 1573. FUEL CAP CDL''D. NOTIFIED BUY STATION OPS FUEL CAP MISSING. DEFERRED PER CDL, VERIFIED NO LEAKS, INSTALLED INOP STICKER ADJ TO REG NUMBER IN COCKPIT. REPLACED REFUEL/DEFUEL COUPLING CAP PER A320 AMM 28-25
- [SDR CALA2024031900784](https://openairdocs.org/sdr/CALA2024031900784.md): Skin · damaged · Mar 18, 2024 · N475UA · Airbus A320232 · Leading Edge Devices
  > UPON OKAY TO CLOSE, FOUND RIGHT WING SLAT NO.3, HAS DAMAGE TO THE I/B TRAILING EDGE. REPAIRED RIGHT WING SLAT NO.3 I/B TRAILING EDGE AS PER REF A320 SRM 57-44-21-300-001 FIG 2 PG8. INSPECTED PER SRM 57-44-21 SEE AMES NON ROUTINE FOR WORK ACCOMPLISHED.
- [SDR CALA2024031800761](https://openairdocs.org/sdr/CALA2024031800761.md): Power Supply · failed · Mar 15, 2024 · N475UA · Airbus A320232 · Emergency Lighting
  > DURING OPS TEST OF CABIN EMERGENCY LIGHTS EPSU ARME/ON EMER R&L FAILS ON PTP PANEL.REF TO PEMCO R 15100.0020 REMOVED AND REPLACED EPSU11WR AND 12WL. OPS CHECK GOOD IAW A320 AMM33-51-38. REMOVED AND REPLACED EPSU 11WL (BAD FROM STOCK) AN 12WL. OPS CHE CK GOOD.
- [SDR CALA2023082802640](https://openairdocs.org/sdr/CALA2023082802640.md): Unknown · missing · Aug 21, 2023 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > PDA 2 SCREW MISSING FROM LEFT WING RUB STRIP SCREW WAS CLASS 2PDA
- [SDR CALA2023073102391](https://openairdocs.org/sdr/CALA2023073102391.md): Engine · slow · Jul 28, 2023 · N475UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > ON T/O ROLL..THR LEVERS SET TO FLX SETTING..ENG1 WENT TO PROPER EPR 1.46..ENG 2 WENT TO..CONT.. PERFORMED TEST 11 HIGH POWER ASSURANCE TEST ON #2 ENG. ALL ENGINE PARAMETERS WITHIN LIMITS REF AMM 71-00-00-710-013C. A/C OKAY FOR SERVICE. ADD EMP:U246551
- [SDR CALA2023020600348](https://openairdocs.org/sdr/CALA2023020600348.md): Battery Pack · no test · Feb 6, 2023 · N475UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - MOST AFT EPSU BAT FAILED TEST REMOVED AND REPLACED EPSU BAT, OPS TST GOOD.
- [SDR CALA2022030300553](https://openairdocs.org/sdr/CALA2022030300553.md): Intercostal · cracked · Mar 3, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2019-20-10) FR 16 LH DOOR STOP #7 FITTING FRAME HOLES UPPER AND LOWER I/B HOLES HAVE CRACK INDICATIONS. HOLES CIRCLED IN RED. REPAIR BEFORE NEXT FLIGHT PER EA 5311-02164. () TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED
- [SDR CALA2022030300550](https://openairdocs.org/sdr/CALA2022030300550.md): Frame · cracked · Mar 2, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2016-14-03) DURING ROTO PROBE OF FRAME 35 STRG 30 FOUND DAMAG E INDICATION IN HOLE #2 AND #1 PERFORM AN INSPECTION PER PART 2 OF LATEST REVISION OF ECRA 5310 -07982"REF VT MAE NRC 0020638 FOR WORK PERFORMED. REPAIRED DAMAGE HOLES AT FR35 STRG 30 ASS PER ECR
- [SDR CALA2022030300549](https://openairdocs.org/sdr/CALA2022030300549.md): Frame · cracked · Mar 2, 2022 · N475UA · Airbus A320232 · Fuselage Main, Structure
  > (AD2016-14-03) (WORK TRANSFERRED FROM NR''S 0020546, 0020547, 002 0547) DURING ROTO PROBE INSPECTION OF LH FR35 STRG 30. CRACK IND ICATIONS NOTED IN IN HOLES #1, #2 & #3. () ERROR IN DISCREPANCY GENERATED NEW ELB 8082931 FOR REPAIR
- [SDR CALA2022030300548](https://openairdocs.org/sdr/CALA2022030300548.md): Intercostal · cracked · Mar 2, 2022 · N475UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2019-20-10) FR16 RH DOOR STOP FITTING FRAME HOLES, FITTING # 7 UPPER AND LOWER I/B HOLES HAVE CRACK INDICATIONS. HOLES CIRCLE D IN RED. REPAIR BEFORE NEXT FLIGHT PER EA 5311-02164.() TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED
- [SDR CALA2022030300547](https://openairdocs.org/sdr/CALA2022030300547.md): Intercostal · cracked · Mar 2, 2022 · N475UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2019-20-10) FR 16 RH DOOR STOP FITTING FRAME HOLES. FITTING #1, LOWER I/B HOLE HAS CRACK INDICATIONS. HOLE CIRCLED IN RED. R EPAIR BEFORE NEXT FLIGHT PER EA 5311-02164. () TRANSFERRED TO ELB 809638, REF THIS LOG FOR WORK ACCOMPLISHED
- [SDR CALA2022030300546](https://openairdocs.org/sdr/CALA2022030300546.md): Plate · corroded · Mar 2, 2022 · N475UA · Airbus A320232 · Aircraft Fuel System
  > (SUPPORT TASK) FOUND CORROSION ON TOP OF LH OUTBOARD MAIN TANK ( BETWEEN LH LONGERON Y1292 AND LH BULKHEAD) FORWARD OF FRAME 42 N EXT TO APU FUEL PUMP. () ACCOMPLISHED REPAIR OF LH O/B MAIN TANK PER FINAL EA 320-5711-13 -A2789 AND UAL EC/RA 5711-01168. ACCOMPL
- [SDR CALA2022030100535](https://openairdocs.org/sdr/CALA2022030100535.md): Frame · cracked · Mar 1, 2022 · N475UA · Airbus A320232 · Fuselage Main, Structure
  > (AD2020-20-05) WORK TRANSFERRED FROM 0020428, 0020429) DURING RO TO PROBE OF RH FR16 DOUBLE JOGGLE CRACK INDICATION NOTED IN HBOL ES #7 & #A. DAMAGE INDICATIONS ALSO NOTED IN HOLES #4 & #19. ALL 4 INDICATIONS NOTED ON 1ST & 2ND LAYER LOOKING O/B. REPAIRED RH F
- [SDR CALA2022030100534](https://openairdocs.org/sdr/CALA2022030100534.md): Frame · cracked · Mar 1, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-06-04) R/H SIDE PRESSURE PANEL BTWN FR35-FR36 HAS 1 HOL E OUTSIDE THE ALLOWABLE CUT-OUT AREA THAT HAS A CRACK INDICATION DOT 07-183" CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPA IR BEFORE NEXT FLIGHT. TRANFERED ALL MX ACTIONS TO LP8088915
- [SDR CALA2022030100533](https://openairdocs.org/sdr/CALA2022030100533.md): Frame · cracked · Mar 1, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-06-04) LH SIDE 4 FASTENERS HOLES ON THE PRESSURE PANEL OUTSIDE THE ALLOWABLE CUTOUT AREA HAVE CRACK INDICATIONS AND THE MIDDLE HOLE ON THE O/B BRACKET UNDER THE PRESSURE PANEL IS DAMAG ED DOTS 07-182 "CONTACT. TRANFERED ALL MX ACTIONS TO LP8088915
- [SDR CALA2022022800511](https://openairdocs.org/sdr/CALA2022022800511.md): None · cracked · Feb 26, 2022 · N475UA · Airbus A320232 · Standard Practices/Structures
  > (SUPPORT TASK) LH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER H OLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK, NEEDS TOBE REPAIRED BEFORE NEXT FLIGHT. () NOTED IAW NTM 51-10-01, INSTALLED FREEZE PLUG. REINSTALLED #1 FROM TIME OF ADL/REPAIR EMBODIMENT 3
- [SDR CALA2022022400498](https://openairdocs.org/sdr/CALA2022022400498.md): Tank · corroded · Feb 24, 2022 · N475UA · Airbus A320232 · Aircraft Fuel System
  > (SUPPORT TASK) FOUND CORROSION ON TOP OF LH OUTBOARD MAIN TANK ( BETWEEN LH LONGERON Y1292 AND LH BULKHEAD) FORWARD OF FRAME 42 N EXT TO APU FUEL PUMP. () ACCOMPLISHED REPAIR OF LH O/B MAIN TANK PER FINAL EA 320-5711-13 -A2789 AND UAL EC/RA 5711-01168. ACCOMPL
- [SDR CALA2022022200479](https://openairdocs.org/sdr/CALA2022022200479.md): Stringer · corroded · Feb 21, 2022 · N475UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > A3NB-53-3-6186 AFT CARGO BILGE AREA FR54 TO FR55 S42L HAVE CORRO SION DOT 42-036 () FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 001 SHT 53-00-13-300-001 FIG 001 SHEET 02. REQUIRES INSPECTIONS PER SRI EMBODIMENT, SUBSEQUENT INSPECTION AND METHOD TBD.
- [SDR CALA2022021600401](https://openairdocs.org/sdr/CALA2022021600401.md): Intercostal · damaged · Feb 15, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-53-4-0033) DURING ROTO INSPECTION OF RH FR66 STGR12 GUSSET PLATE. REJECTABLE DAMAGE WAS NOTED IN BOTTOM HOLE DUE TO MECHAN ICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN RED.() DURING ROTO INSPECTION OF RH FR66 STGR 12 GUSET PLATE REJECTABLE MOBI
- [SDR CALA2022021600398](https://openairdocs.org/sdr/CALA2022021600398.md): Fitting · cracked · Feb 14, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 LH SIDE CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR BEFO RE NEXT FLIGHT.
- [SDR CALA2022021600397](https://openairdocs.org/sdr/CALA2022021600397.md): Crossbeam · cracked · Feb 14, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IA
- [SDR CALA2022021400383](https://openairdocs.org/sdr/CALA2022021400383.md): Crossbeam · cracked · Feb 14, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-14-09) LH FR20 CROSSBEAM HAS CRACK INDICATIONS ON H17, H18,H23, H25 AND H26 FASTENER HOLES, REPAIR LH FR20 CROSSBEAM BE FORE NEXT FLIGHT PER STEP 8. CIRCLED IN RED. () REPAIRED LBH FR20 CROSSBEAM HOLES H17, H18, H25 & H26 BY OVER SI ZED COLDWORKING IA
- [SDR CALA2022021400372](https://openairdocs.org/sdr/CALA2022021400372.md): Stringer · corroded · Feb 13, 2022 · N475UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > A3NB-53-3-6186 AFT CARGO BILGE AREA STRINGER FR56 TO FR57 S43L H AVE CORROSION DOT 42-037 () REMOVED AND INSTALLED NEW COUPLING AND STRINGER IAW SRM 51-42-11 -00. ACCOMPLISHED BY EMP#V934344 AT BFM ST AEROSPACE MOBILE. NR #0020417.
- [SDR CALA2022021100357](https://openairdocs.org/sdr/CALA2022021100357.md): Floor Support · corroded · Feb 10, 2022 · N475UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) AFT CABIN SUPPORT FRAME BETWEEN FR69-FR70 STGR23R IS CORRODED. () REMOVED AFT CABIN SUPPORT IAW SRM 51-42-11 LOCATED AND DRILLED N EW PART IAW SRM 51-44-11 INSTALLED NEW PART IAW SRM 51-42-11 RES TORED SURFACE PROTECTION IAW SRM 51-23-11. ACCOMP
- [SDR CALA2022021100358](https://openairdocs.org/sdr/CALA2022021100358.md): Hinge Fitting · cracked · Feb 10, 2022 · N475UA · Airbus A320232 · Horizontal Stabilizer Structure
  > (A3NB-55-3-6005) RH HORIZONTAL #4 HINGE FITTING UPPER BONDING PL ATE CRACKED () REMOVED DAMAGE BONDING STRAP IAW SRM 51-42-11 FABRICATED NEW BON W 20-28-00. ACCOMPLISHED BY EMP#V934718 AT BFM ST AEROSPACE MOBI. DING STRAP MATERIAL P/N 2024T3050 BATCH#00038321
- [SDR CALA2022020700326](https://openairdocs.org/sdr/CALA2022020700326.md): Frame · cracked · Feb 4, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > L/H AFT FR 68 DOORSTOP FITTING #3 O/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE. IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM
- [SDR CALA2022020700325](https://openairdocs.org/sdr/CALA2022020700325.md): Frame · cracked · Feb 4, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > L/H AFT FR 68 DOORSTOP FITTING #1 I/B LOWER (D1) HAS CRACK INDIC ATION NOTED IN HOLE IAW NTM 51-10-01 PT6. INSTALLED FREEZE PLUG AND WASHERS. REINSTA SHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 24500 FC (FH NOT RELEVA ETHOD NTM 51-10-08 AND ROTO TEST REF TO AMM 5
- [SDR CALA2022020400313](https://openairdocs.org/sdr/CALA2022020400313.md): Stop Fitting · cracked · Feb 3, 2022 · N475UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > LH AFT DOOR FR68 DOOR STOP FITTING #3 O/B TOP HOLE HAS A CRACK I NDICATION HOLE IS CIRCLED IN BLACK. NEEDS TO BE REPAIRED. L/H AFT DOOR FITTING FR68 LOWER I/B HOLE REAMED TO 0.391 NO CRAC OVED FOR ACCESS) IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V934344 A K INDIC
- [SDR CALA2022020400312](https://openairdocs.org/sdr/CALA2022020400312.md): Stop Fitting · cracked · Feb 3, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > RH AFT DOOR FR68 DOOR STOP FITTING #1 I/B LOWER HOLE HAS A CRACK INDICATION, HOLE IS CIRCLED IN BLACK. NEEDS TO BE REPAIRED BEFOR E FURTHER FLIGHT () L/H AFT DOOR STOP FITTING FR68 LOWER I/B HOLE REAMED TO 0.391 NO #1 (REMOVED FOR ACCESS) IAW SRM 51-42-11. ACC
- [SDR CALA2022020200296](https://openairdocs.org/sdr/CALA2022020200296.md): Bonding Plate · cracked · Feb 1, 2022 · N475UA · Airbus A320232 · Horizontal Stabilizer Structure
  > (A3NB-55-3-6005) RH HORIZONTAL #4 HINGE FITTING UPPER BONDING PL ATE CRACKED () REMOVED DAMAGE BONDING STRAP IAW SRM 51-42-11 FABRICATED NEW BON W 20-28-00. ACCOMPLISHED BY EMP#V934718 AT BFM ST AEROSPACE MOBI. DING STRAP MATERIAL P/N 2024T3050 BATCH#00038321
- [SDR CALA2022013100266](https://openairdocs.org/sdr/CALA2022013100266.md): Gusset · damaged · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-53-4-0033) DURING ROTO INSPECTION OF GUSSET PLATE RH FR68 STGR14 REJECTABLE DAMGE NOTED IN LWR TWO HOLES & STGR16 UPER AND LAST TWO LWR HOLES DUE TO MECHANICAL DAMAGE IN ALL LAYERS WITH OVER 75% SH. CIRCLED IN. DURING ROTO INSPECTION OF GUSSET PLATE RH F
- [SDR CALA2022013100264](https://openairdocs.org/sdr/CALA2022013100264.md): Shear Tie · corroded · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > (A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR31 STR 40R-42R ARE CORRODED (REPLACE SHEAR TIES/CLEATS.) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR 31 STRG 40R TO 42R I AW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AERO SPACE MOBILE. NR#0020646
- [SDR CALA2022013100263](https://openairdocs.org/sdr/CALA2022013100263.md): Shear Tie · corroded · Jan 29, 2022 · N475UA · Airbus A320232 · Aerodynamic Fairings
  > (A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR33 STR40R-42R ARE COR RODED (REPLACE SHEARTIES/CLEATS.) REMOVED AND REPLACED (2E) SHEARTIES ON FR33 STGR 40R TO 42R IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROSPA CE MOBILE. NR#0020645
- [SDR CALA2022013100262](https://openairdocs.org/sdr/CALA2022013100262.md): Shear Tie · corroded · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > (A3NB-5321-1-2706) 2EA SHEAR TIES/CLEATS FR30 STR40R-42R ARE COR RODED (REPLACE SHEAR TIES/CLEATS) REMOVED AND REPLACED (2EA) SHEAR TIES ON FR30 STGR 40R TO 42R IA W A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V928493 AT BFM ST AEROS PACE MOBILE NR#0020647
- [SDR CALA2022013100261](https://openairdocs.org/sdr/CALA2022013100261.md): Frame · cracked · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (AD2020-18-06) DURING ROTO INSPECTION OF THE FRAME FOOT AT FR43 RH SIDE. CRACK INDICATION WAS NOTED AT FASTENER HOLE. REPAIR NEF ORE NEXT FLIGHT. () REPAIRED RH FR43 RH IAW UAL EA 5330-06692 OPT 1 & R DWG R5337023 3. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROS
- [SDR CALA2022013100260](https://openairdocs.org/sdr/CALA2022013100260.md): Frame · cracked · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > A3NB-53-3-6132 RH FWD EMREGENCY EXIT DOOR RH I/B BEAM FRAME CRAC KED DOT 42-055. () PERFORMED HFEC SURFACE INSPECTION ON DOOR WITH SERIAL NO VH4011 BY EMP#V936054 AT BFM AEROSPACE MOBILE NR#0020651. IAW NTM 51-10-08. CRACK INDICATIONS NOTED AROUND FASTENERS RE
- [SDR CALA2022013100259](https://openairdocs.org/sdr/CALA2022013100259.md): Bracket · corroded · Jan 29, 2022 · N475UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-05-3-6013) FWD CARGO COMPT: FR33 BETWEEN STR42 LH AND STR4 2 RH HAS CORROSION EVIDENCE. DOT 61-081. REMOVED SHEAR TIE FR33 BETWEEN STR43CL AND REPLACED BY SHEAR TIE 3. FABRICATED ON VTMAE TRAVELER#T21/1592356, INSTALLED NEW SHEAR TI E P/N UAD532303992000
- [SDR CALA2022013100258](https://openairdocs.org/sdr/CALA2022013100258.md): Floor Support · corroded · Jan 28, 2022 · N475UA · Airbus A320232 · Fuselage Main, Floor Beam
  > A3NB-53-3-6279 AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 HAVE CORROSION DOT 42-019 EVALUATED AFT GALLEY FLOOR SUPPORT BEAM Y765 AT FR70 WITH CORROS ION OUT OF LIMITS DIM L=1.782, W=1.516, REMAIN THICKNESS 0.3, RE MOVED AND REPLACED FOR NEW BEAM IAW SRM 51-42-
- [SDR CALA2022013100257](https://openairdocs.org/sdr/CALA2022013100257.md): Seat Track · corroded · Jan 28, 2022 · N475UA · Airbus A320232 · Fuselage Main, Structure
  > (A3NB-53-3-6038) FLOOR MAIN CABIN SEAT TRACK OUTBOARD RH BETWEEN FR 19 AND FR 20 HAS CORROSION. DOT 61-071 () EVALUATED SEAT TRACK Y-1292 OUTBOARD RH BETWEEN FR19 AND FR20 WI 936040 AT BFM ST AEROSPACE MOBILE. NR#0020359. TH CORROSION ON HARD POINT AREA AND W

Next page: https://openairdocs.org/aircraft/N475UA/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 = 'N475UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N475UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.