# Service difficulty reports: N468UA

A list on [N468UA](https://openairdocs.org/aircraft/N468UA.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 · 112 reports

- [SDR CALA2025112711518](https://openairdocs.org/sdr/CALA2025112711518.md): Fuel Cap · missing · Nov 26, 2025 · N468UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING CONFIRMED FUEL CAP MISSING. INSTALLED REFUEL COUPLING CAP IAW AMM 28-25-41. OPS CHECKED GOOD.
- [SDR CALA2025110210805](https://openairdocs.org/sdr/CALA2025110210805.md): Service Door · missing · Oct 31, 2025 · N468UA · Airbus A320232 · Fluid Service Doors
  > LAVATORY SERVICE DOOR MISSING. REPLACED LAVATORY SERVICE DOOR IAW AMM 52-42-11-400-001-A AND ECRA 52-42-01073. OPS CHECK OF LIMIT SWITCH GOOD.
- [SDR CALA2025110410907](https://openairdocs.org/sdr/CALA2025110410907.md): Door · missing · Oct 17, 2025 · N468UA · Airbus A320232 · Fluid Service Doors
  > LAV SERVICE DOOR MISSING. REPLACED DOOR. OPS CHECK GOOD. REF AMM TASK 52-42-11-400-001-A.
- [SDR CALA2025032403100](https://openairdocs.org/sdr/CALA2025032403100.md): Chiller · faulted · Mar 22, 2025 · N468UA · Airbus A320232 · Buffet/Galleys
  > FA REPORTS BURNING SMELL IN AFT OF AIRCRAFT ADDED PHOTOS OF COMPLETED ODOR FORM. ORIGINAL COPY GIVENT TO SUPERVISOR RONNIE INSPECTED AFT GALLEY FOR OPEN CB. NONE FOUND. INSPECTED G4 AIR CHILLER. NO SMELL ORIGINATING FROM UNIT OR VENTS. INSPECTED G3 AIR CHI
- [SDR CALA2024091800653](https://openairdocs.org/sdr/CALA2024091800653.md): Fuel Cap · misconfigured · Sep 15, 2024 · N468UA · Airbus A320232 · Fuel Storage
  > PDA 2 INSTALLED ACFT FUEL CAP NEEDS TO PAINTTHE MARKINGS IN ACCORDANCE WITH UAL DRAWING 1120DD12514 / ECRA5120-01013 REF AMM 28-25-41-200-001-A STEP 5.A.(4).. PAINTED FUEL CAP ALIGNMENT MARKINGS AS PER UAL DRAWING 1120DD12514 / ECRA5120-01013.
- [SDR CALA2023111003326](https://openairdocs.org/sdr/CALA2023111003326.md): Fuel Cap · missing · Oct 26, 2023 · N468UA · Airbus A320232 · Fuel Storage
  > R/H WING COUPLING, REFUEL CAP MISSING ON ARRIVAL REQUEST CDL, 28A FOR MISSING FUEL CAP. DDP COMPLIED WITH PLACARD DDP. COMPLIED WITH. PLACARD IN FLIGHT DECK OK TO CONTINUE. INSTALLED DISPATCH DESK: 36 NAME: CD DATE: 26-OCT-23- APPROVED REPLACED FUEL CAP.
- [SDR CALA2023063002080](https://openairdocs.org/sdr/CALA2023063002080.md): Frame · cracked · Jun 28, 2023 · N468UA · Airbus A320232 · Fuselage Main, Structure
  > FR 68 LH, DOOR STOP 1, LOWER IB HOLE HAS 2EA CRACK INDICATIONS IN FRAME LAYER @ 12 AND 7 OCLOCK DIRECTION ( AD RELATED SUPPORT T ASK) (AD2022-22-04) GENERATED AT HAECO LCQ PER NR 9296381 (26381) BY MECH V892444 N IAW SRM 53-41-12-300-010. PERFORMED ROTOSCAN,
- [SDR CALA2023062802068](https://openairdocs.org/sdr/CALA2023062802068.md): Door Frame · cracked · Jun 27, 2023 · N468UA · Airbus A320232 · Fuselage Main, Structure
  > FR 68 RH, DOOR STOP 1, LOWER IB HOLE HAS CRACK INDICATION IN FRA ME LAYER @ 6 OCLOCK DIRECTION (AD RELATED SUPPORT TASK)(AD2022-2 2-04) GENERATED AT HAECO LCQ PER NR 9296382 (26382) BY MECH V892 444 N IAW SRM 53-41-12-300-010. PERFORMED ROTOSCAN, NO DEFECTS NO
- [SDR CALA2023062602003](https://openairdocs.org/sdr/CALA2023062602003.md): Fastener · sheared · Jun 23, 2023 · N468UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > RH MLG DOOR ACTUATOR FWD FITTING LOWER OB FASTENER SHEARED "REPAIR BEFORE FURTHER FLIGHT" (AD RELATED TASK) (AD 2015-02-14) GENERATED AT HAECO LCQ PER NR 9296188 (26188) BY MECH V892444.
- [SDR CALA2022050601164](https://openairdocs.org/sdr/CALA2022050601164.md): Unknown · odor · May 6, 2022 · N468UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > ON T/O BURNING/COMBUSTION SMELL IN CLIMB WENT AWAY CRUISE THEN RE TURNED POWER REDUCTION TO LAND UPDATED MAA CODE FIX USING VENDOR MAA SCREEN REF AMM 05-51-10-200-801-C1 SMOKE OR FUMES IN CABIN INSPECTION AND AMM 05-50-00-810-831-A PLEASE CONTACT TOMC BEFORE C
- [SDR CALA2021051000624](https://openairdocs.org/sdr/CALA2021051000624.md): Door Frame · cracked · May 7, 2021 · N468UA · Airbus A320232 · Fuselage Main, Structure
  > L1 DOOR FRAME 16 STOP FITTING NO7 LWR INBRD HOLE IS CRACKED IN TH E INTERCOSTAL FITTING AND UPPER INBRD HOLE IS CRACKED IN THE WEB AND INTERCOSTAL. REPAIR B EFORE NEXT FLT CONTACT ENG APPROVED R ERPAIR INSTRCTIONS PER NR 9292142 / 22142 GEN BY V061633 ACCOMPLI
- [SDR CALA2021051000625](https://openairdocs.org/sdr/CALA2021051000625.md): Intercostal · cracked · May 7, 2021 · N468UA · Airbus A320232 · Fuselage Structure (General)
  > R1 DOOR FRAME 16 STOP FITTING #1 LWR INBRD HOLE IS CRACKED IN TH E INTERCOSTAL FITTING REPAIR BEFORE NEXT FLIGHT CONTACT ENGINEER ING FOR APPROVED INSTRUCTIONS PER NR 9292144 / 22144 AD 2019-20- 10 GEN BY V061633. ACCOMPLISHED INTERIM REPAIR AT R 1 DOOR FRAME
- [SDR CALA2021051000623](https://openairdocs.org/sdr/CALA2021051000623.md): Intercostal · cracked · May 7, 2021 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L1 DOOR FRAME 16 STOP FITTING NO 1 LWR INBRD HOLE IS CRACKED IN TH E INTERCOSTAL FITTING. REPAIR BEFORE NEXT FLT CONTACT ENG FOR AP PROVED REPAIR INSTRUCTIONS AD 2019-20-10 PER NR 9292141 / 22141 GEN BY V061633 REPAIRED L1 DOOR FRAME 16 STOP FITTING NO 1 IAW U
- [SDR CALA2021050600617](https://openairdocs.org/sdr/CALA2021050600617.md): Door Frame · cracked · May 6, 2021 · N468UA · Airbus A320232 · Fuselage Main, Structure
  > R1 DDOR FRAME 16 STOP FITTING #7 LWR IN BOARD HOLE IS CRACKED IN THE INTERCOSTAL FITTING AND UPPER INBRD HOLE IS CRACKED IN THE WEB AND INTERCOSTAL REPAIR BEFORE NEXT FLIT CONTACT ENG. FOR APP ROVED INSTRUCTIONS PER NR 9292145/22145 AD 2019-20-10. REPAIRED R1
- [SDR CALA2019100541687](https://openairdocs.org/sdr/CALA2019100541687.md): Intercostal · corroded · Oct 1, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FR56-57 INTERCOSTAL ST38R HAS CORROSION PER HAECO LCQ NR LP 9299062 GENERATED BY N078625 REMOVED AND REPLACED INTERCOSTAL IN AFT CARGO COMPARTMENT BTWN F RAME 56 AND 57 AT STGR 38R IAW A320 SRM 51-42-11-801/TO80673599/ 005/2019 #A ECRA5341-01189.
- [SDR CALA2019100541682](https://openairdocs.org/sdr/CALA2019100541682.md): Stringer · corroded · Sep 30, 2019 · N468UA · Airbus A320232 · Fuselage Structure (General)
  > UPON REMOVAL OF FASTENERS FOUND CORROSION IN FWD CARGO PIT ST43L BTWN FR31-32(A3NB-53-3-61105) REF HAECO LCQ NR 9299072 AND GEN B Y N078625 REMOVED CORROSION ON STR 43L BETWEEN FR 31-32 L=3" W=.75" ORIGIN AL MATERIAL.087",MATERIAL LOSS.025,MATERIAL REMAINING
- [SDR CALA2019100541681](https://openairdocs.org/sdr/CALA2019100541681.md): Shear Tie · corroded · Sep 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT,BILGE AREA,SHEAR TIE ON FR 28, BTWN STRG 4 2R-43R,HAS CORROSION FR 28,STR 42R-STR 43R. REMOVED AND REPLACED 1EA CORRODED SHEAR TIE IN THE FWD CARGO COM PARTMENT BILGE AREA FR28 STR42R-43R IAW AIRBUS A320 SRM 51-72-11 -911-001 BY MECH V914
- [SDR CALA2019100541680](https://openairdocs.org/sdr/CALA2019100541680.md): Shear Tie · corroded · Sep 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT BILGE AREA SHEAR TIE ON FR30 BTWN STRG 43L -44 HAS CORROSION FR30 STR43L-44 A3NB-53-3-6105 PER HAECO LCQ NO N ROUTINE 9298304 GENERATED BY V917055 REMOVED AND REPLACED 1EA CORRODED SHEAR TIE IN THE FWD CARGO COM P BILGE AREA ON FR30 BETWE
- [SDR CALA2019100541679](https://openairdocs.org/sdr/CALA2019100541679.md): Skin · dented · Sep 30, 2019 · N468UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REMOVE UNAPPROVED REPAIR, MAP OUT DAMAGE OF SKIN PNL AND CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE FURTHER FLIGHT. FR34 ST43L{AD 2016-18-09} {EA5300-02120-001} REF HAECO LCQ NR 929913 2 AND GENERATED BY N078625 REMOVED AND REPLACED REPAIR DOUBLER ON F
- [SDR CALA2019093001669](https://openairdocs.org/sdr/CALA2019093001669.md): Panel · corroded · Sep 29, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT,BILGE AREA POTABLE WATER FWD DUMP BOX AND ADJACENT SKIN STR 43L BETWEEN FR 28-29 HAS CORROSION. REMOVED AND REPLACED FWD CARGO COMPARTMENT BILGE AREA POTABLE WA TER FWD DUMP BOX AT STR 43L BETWEEN FR 28-29 IAW SRM 51-72-11-91 1-001,BLENDE
- [SDR CALA2019093001664](https://openairdocs.org/sdr/CALA2019093001664.md): Stringer · corroded · Sep 28, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO PIT STR41R CORROSION FR33-34 A3NB-53-3-6105 PER HAECO LCQ NR 9299130 GENERATED FOUND STR 41R IN FWD CARGO PIT FR 33-34 TO BE OUT OF LIMITS,ORIG INAL MATERIAL.087,MATERIAL LOSS.033, REMAINING MATERIAL.054 ALLOWABLE LOSS.024 IAW SRM 53-21-13-283-0
- [SDR CALA2019093001662](https://openairdocs.org/sdr/CALA2019093001662.md): Stringer · corroded · Sep 28, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO PIT STR42L HAS CORROSION FR33-34 (A3NB-53-3-6105) REF HAECO LCQ NR 9299131 AND GEN ACCOMPLISHED REPAIR ON STR 42L AT FR 33-34 IAW SRM 53-21-13-300- 004.THIS IS A CATEGORY B REPAIR. REQUIRES INSPECTION AT 60,000 F C/120,000 FH WHICHEVER OCCURES FIRST
- [SDR CALA2019093001661](https://openairdocs.org/sdr/CALA2019093001661.md): Stringer · corroded · Sep 28, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > 171/172 EVIDENCE OF CORROSION STR. 31R AT FR 65 TO 66 (A3NB-05-3 -6029) REF HAECO LCQ NR 9298469 AND GENERATED REMOVED AND REPLACED AFT CARGO COMPARTMENT STRINGER 31R BETWEEN FRAME 65-66 IAW A320 SRM 51-72-11-911-002 PARA 2 REO L22288 OASS IER REFERENCE 806787
- [SDR CALA2019093001659](https://openairdocs.org/sdr/CALA2019093001659.md): Stringer Splice · corroded · Sep 28, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT, BILGE AREA, STGR 41L SPLICE, BTWN FR30-31 HAS CORROSION FR 30 - FR 31 STR 41L (A3NB-53-3-6105) REF HAECO LCQ NR 9298314 AND GEN FOUND FWD CARGO COMPARTMENT BILGE AREA STR 41L SPLICE BTWN FR30- 31 TO BE OUT OF LMITS IAW A320 SRM 51-43-00-
- [SDR CALA2019092801646](https://openairdocs.org/sdr/CALA2019092801646.md): Stringer Splice · corroded · Sep 25, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT, BILGE AREA, STGR 43L SPLICE, BTWN FR 30-3 1, HAS CORROSION FR 30 - FR 31, STR 43L (A3NB-53-3-6105) REF HAE CO LCQ NR 9298315 AND GENERATED BY V917055. FOUND FWD CARGO COMPARTMENT BILGE AREA STR 43L SPLICE BTWN FR 30 -31 CORODED OUT OF LI
- [SDR CALA2019092701638](https://openairdocs.org/sdr/CALA2019092701638.md): Stringer · corroded · Sep 24, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO PIT STR41L HAS CORROSION FR33-34 (A3NB-53-3-6105) REF HAECO LCQ NR 9299127 AND GEN REMOVED CORROSION ON STRINGER 41L BETWEEN FR33-34 IAW A320 SRM 5 1-74-00 FOUND TO BE OUT OF LIMITS IAW A320 SRM 51-72-11 PERFORME D BY V079529 INSP BY COMPLETED AT HAE
- [SDR CALA2019092701634](https://openairdocs.org/sdr/CALA2019092701634.md): Stringer · corroded · Sep 23, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STR 41R HAS CORROSION BETWEEN FR 30-31 (SUPPORT TASK) AT HAECO LCQ REF. NO. 9299083, GENERATED. REPAIRED CORRODED STRINGER IN FWD CARGO AT STR 41R BETWEEN FR 30 -31 IAW A320 SRM 53-21-13-300-003. THIS REPAIR REQUIRES A SRI I NSPECTION AT 60000 FC/12
- [SDR CALA2019092301621](https://openairdocs.org/sdr/CALA2019092301621.md): Shear Tie · corroded · Sep 20, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO PIT SHEAR TIE AT FR 34 STR 42R-43R HAS CORROSION (A3NB -53-3-6105) REF NR 9299142. EVALUATED CORROSION ON FWD CARGO PIT SHEAR TIE AT FR14 STR 42R-4 3R ORIGINAL THICKNESS.055IN MATERIAL LOSS.005IN REMAINING MATERIAL.050IN ALLOWABLE LOSS.004IN FOUN
- [SDR CALA2019092301618](https://openairdocs.org/sdr/CALA2019092301618.md): Shear Tie · corroded · Sep 20, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT, BILGE AREA, SHEAR TIE ON FR 33 BTWN STR 42R-43R HAS CORROSION FR 33 STR 42R-STR 43R (A3NB-53-3-6105) REF NR 9298293. EVALUATED CORROSION ON FWD CARGO COMPT BILGE AREA SHEAR TIE FR33 STR 42R-43R ORIGINAL THICKNESS.055IN MATERIAL LOSS.00
- [SDR CALA2019092301617](https://openairdocs.org/sdr/CALA2019092301617.md): Stringer · corroded · Sep 19, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF FASTENERS FOUND CORROSION IN FWD CARGO PIT ST42R BETWEEN FR31-32 A3NB-53-3-6105 PER NON ROUTINE 9299070. REMOVED AND REPLACED FWD CARGO STRINGER LOCATED AT FR30.5-FR34 AND AT STRINGER 42R IAW SRM 51-42-11 PG 9,18, AND 19.
- [SDR CALA2019092301616](https://openairdocs.org/sdr/CALA2019092301616.md): Stringer · corroded · Sep 19, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF FASTENERS FOUND CORROSION IN FWD CARGO PIT ST43R BETWEEN FR 31-32 (A3NB-53-3-61105) REF NR 9299069. REMOVED AND REPLACED STR 43R IN FWD CARGO IAW SRM 51-42-11- 801 AND SRM 51-72-11-911-001 EVALUATED STR 43R FOUND STR TO HAVE 50 PERCENT MATERAIL
- [SDR CALA2019092301615](https://openairdocs.org/sdr/CALA2019092301615.md): Shear Tie · corroded · Sep 19, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO PIT SHEAR TIE AT FR 32 STR 42R-43R HAS CORROSION (A3NB -53-3-6105) REF NR 9299141. EVALUATED CORROSION ON SHEAR TIE ORIG THICKNESS.055IN MATERIAL LOSS.006IN MATERIAL REMAINING.049IN MAX ALLOWABLE LOSS.004IN OUT OF LIMITS IAW DWG D53230398 AND GEN
- [SDR CALA2019092301614](https://openairdocs.org/sdr/CALA2019092301614.md): Door Sill · corroded · Sep 19, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT, SILL PLATE, FR 52A-56, HAS CORROSION (A3NB -52-3-6042) AT REF NR 9298402. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SILL PLATE IAW SRM 51-72-11-911-001. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SILL PLATE IAW SRM 51-72-11-911-01.
- [SDR CALA2019092301613](https://openairdocs.org/sdr/CALA2019092301613.md): Plate · corroded · Sep 19, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT LT SIDE TORSION BOX TOP PLATE FR 52.5-56 HAS CORROSION A3NB-05-3-6022 PER NON ROUTINE 9298448. REMOVED AND REPLACED AFT CARGO COMPT RT SIDE TORSION BOX TOP PLA TE IAW SRM 51-72-11-91-001.
- [SDR CALA2019091701552](https://openairdocs.org/sdr/CALA2019091701552.md): Shear Tie · corroded · Sep 15, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR26 BTWN STR 42R-43R HAS CORROSION FR26 STR 42R-43R PER NR LP 9298313. REMOVED AND REPLACED 1EA CORRODED SHEAR TIE IN THE FWD CARGO COM PT BILGE AREA FR26 BTWN STR 42R-43R IAW SRM 51-72-11-911-001.
- [SDR CALA2019091401540](https://openairdocs.org/sdr/CALA2019091401540.md): Light · inoperative · Sep 12, 2019 · N468UA · Airbus A320232 · Escape Slide
  > N/R FOR SDR REPORTING REQUIREMENTS ONLY. DURING INTENTIONAL DEPLOYMENT OPS CHECK OF RT O/W SIDE IT WAS FOUND THAT THE SLIDE PATH WAY LIGHTS DID NOT ILLUMINATE ON REF 9298162 SPEC A3NB -25-3-6275.
- [SDR CALA2019091401539](https://openairdocs.org/sdr/CALA2019091401539.md): Shear Tie · corroded · Sep 12, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR32 BTWN STRG 43L-44 HAS CORROSION FR32 STR 43L-44. PER NR LP 9298299 REMOVED AND REPLACED 1EA CORRODED SHEAR TIE IN THE FWD CARGO COMPT BILGE AREA FR 32 STR 43L-44 IAW SRM 51-72-11-911-001.
- [SDR CALA2019091401538](https://openairdocs.org/sdr/CALA2019091401538.md): Shear Tie · corroded · Sep 12, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR29 BTWN 42L-43L HAS CORROSION FR29 STR 42L-43L PER NR LP 9298308 REMOVED AND REPLACED 1EA CORRODED SHEAR TIE IN THE FWD CARGO COM PT BILGE AREA FR29 BTWN STR 42L-43L IAW SRM 51-72-11 -911-001.
- [SDR CALA2019091401532](https://openairdocs.org/sdr/CALA2019091401532.md): Stringer · corroded · Sep 10, 2019 · N468UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT PIT INTERNAL LOWER LOBE FR 63-64 STR 41 STR CORRODED. (A3NB -53-4-6179) REF NR 9298950 AND EVALUATED CORROSION ON AFT PIT INTERNAL LOWER LOBE FR63-64 STR 41R FOUND NO ALLOWABLE DAMAGE LIMITS REMOVED AND REPLACED STR 41R FR 58-64 IAW SR, 51-72-11-911-001 UP
- [SDR CALA2019091301530](https://openairdocs.org/sdr/CALA2019091301530.md): Fitting · corroded · Sep 9, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD CARGO FWD INBD CORNER FITTING HAS CORROSION A3NB-53-3-6222. PER NR 9298906 REMOVED AND REPLACED FWD CARGO INBD CORNER FITTING IAW SRM 5 1-42-11-801/51-72-11-911-002 PARA 2.
- [SDR CALA2019091301529](https://openairdocs.org/sdr/CALA2019091301529.md): Shear Tie · corroded · Sep 9, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPARTMENT, BILGE AREA, SHEAR TIE ON FR 32, BTWN STR 40R-41R, HAS CORROSION FR 32, STR 40R - STR 41R. (A3NB-53-3-610 5) REF NR 9298297 AND EVALUATED FWD CARGO COMPT BILGE AREA SHEAR TIE AT FR32 STR 40R-41R ORIGINAL THICKNESS.033IN MATERIAL LOSS.00
- [SDR CALA2019090901507](https://openairdocs.org/sdr/CALA2019090901507.md): Hinge Fitting · worn · Sep 7, 2019 · N468UA · Airbus A320232 · Fuselage, Door Hinge
  > LT MLG DOOR FWD HINGE FITTING TO KEEL BEAM FWD LUG FWD FACE HAS W EAR AROUND THE BUSHING HOLE PER NR LP 9298529. REMOVED AND REPLACED LT MLG DOOR FWD HINGE FITTING IAW SRM 51-72-11.
- [SDR CALA2019090201477](https://openairdocs.org/sdr/CALA2019090201477.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR28 BTWN STR 42L-43L HA S CORROSION FR28 STR 42L-43L PER NR LP 9298312. FOUND FWD CARGO COMPT BILGE AREA SHEAR TIE ORIG THKNESS.055IN M AT LOSS.006IN REMAINING MAT.048IN ALLOWABLE LOSS.003IN IAW S ASMA3042 REMOVED A
- [SDR CALA2019090201473](https://openairdocs.org/sdr/CALA2019090201473.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR31 BTWN STR 41R-42R HAS CORROSION FR31 STR 41R-42R PER NR LP 9298301. FOUND FWD CARGO BILGE AREA SHEAR TIE FR31 STR 41R-42R TO BE OUT OF LIMITS ORIG THICKNESS.055IN MAT LOSS.017IN MAT REMAINING.038IN ALLOWABLE LOSS
- [SDR CALA2019090201472](https://openairdocs.org/sdr/CALA2019090201472.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR33 BTWN STR 42L-43L HA S CORROSION FR33 STR 42L-43L PER NR LP 9298296. REMOVED AND REPLACED FWD CARGO COMPT BILGE AREA SHEAR TIE BTWN S TR 42L-43L AT FR33 IAW SRM 51-72-11 ORIG THICKNESS.055IN MAT LOSS.004IN REMAININ
- [SDR CALA2019090201476](https://openairdocs.org/sdr/CALA2019090201476.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE O FR28 BTWN STR 43R-44 HAS CORROSION FR28 STR 43R-44 PER NR LP 9298311 FOUND FWD CARGO BILGE AREA SHEAR TIE FR28 STR 41R-44 OUT OF LIMITS ORIG THICKNESS.055IN MAT LOSS.031IN REMAINING MAT.024IN AL LOWABLE LOSS.003IN IAW
- [SDR CALA2019090201475](https://openairdocs.org/sdr/CALA2019090201475.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR33 BTWN STR 40R-41R HAS CORROSION FR33 STR 40R-41R PER NR LP 9298292 REMOVED CORROSION FROM SHEAR TIE AT FWD CARGO FR33 STR 40R-41R IAW SRM 51-74-00-801 PG 6 ORIG THCK.055IN MAT LOSS.005IN REMAIN ING MAT.050IN ALLOW
- [SDR CALA2019090201474](https://openairdocs.org/sdr/CALA2019090201474.md): Shear Tie · corroded · Aug 30, 2019 · N468UA · Airbus A320232 · Fuselage Internal Mounting Structure
  > FWD CARGO COMPT BILGE AREA SHEAR TIE ON FR31 BTWN STR 40R-41R HA S CORROSION FR31 STR 40R-41R PER NR LP 9298300 FOUND FWD CARGO BILGE AREA SHEAR TIE OUT OF LIMITS ORIG THICKNES S.055IN MAT LOSS.011IN REMAINING MAT.044IN ALLOWABLE LOSS.003IN IAW SM ASNA3042
- [SDR CALA2019083001446](https://openairdocs.org/sdr/CALA2019083001446.md): Door Sill · corroded · Aug 26, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FR66 UNDERNEATH CORNER FITTING CORROSION.
- [SDR CALA2019082301423](https://openairdocs.org/sdr/CALA2019082301423.md): Shear Plate · cracked · Aug 22, 2019 · N468UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN FR69 STR23 L/H SHEAR PLATE CRACKED. REMOVED AND REPLACED AFT CABIN SHEAR PLATE FR69 STR 23L/H IAW A3 20 SRM 51-72-11-911-001.

Next page: https://openairdocs.org/aircraft/N468UA/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 = 'N468UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N468UA/reports

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