# Service difficulty reports: N495UA

A list on [N495UA](https://openairdocs.org/aircraft/N495UA.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 CALA2026082418862](https://openairdocs.org/sdr/CALA2026082418862.md): Fmc · faulted · Aug 20, 2026 · N495UA · Airbus A320232 · Flight Management Computing Hardware System
  > FMGC 2 KEEPS FAILING FO MAP LOST LOCKING FOR POSITIVE FIX UNLOCKED PERFORMED AFS TEST IAW AMM 22-96-00. TEST OK NO FAULTS NOTED. LAND CAT 3 TEST WAS PERFORMED, IAW AMM 22-97-00, LAND TEST OK, NO FAULTS FOUND. SUSPECT FMGC 2 INSTALLED BAD FROM STOCK CHKD SCE
- [SDR CALA2026081318583](https://openairdocs.org/sdr/CALA2026081318583.md): Pin · corroded · Aug 9, 2026 · N495UA · Airbus A320232 · Emergency Exits
  > FOUND CORRODED ROLLER PIN ON RIGHT FWD EXIT HATCH LOWER AFT ATTACH POINT LOCKING THIS LOG FOR MAINTENANCE FERRY FLIGHT UNLOCKED FOR SIGNOFF LOCKED FOR FERRY UNLOCKED FOR MAINTENANCE ACTION UPDATE REMOVED FWD RH EMERGENCY EXIT HATCH UPTO AND INCLUDING STEP 4. N
- [SDR CALA2026022614113](https://openairdocs.org/sdr/CALA2026022614113.md): Valve · faulted · Feb 19, 2026 · N495UA · Airbus A320232 · Landing Gear Door Retract Section
  > MLG NOT UPLOCKED ECAM PROC DID NOT RESOLVE ISSUE. GEAR REPORTED TO HAVE RETRACTED, BUT DID NOT STAY UPLOCKED TO ALLOW GEAR DOORS TO CLOSE. PERFORMED FIM 32-31-00-810-836-A. MLG DOORS OPENED CORRECTLY BUT GEAR DID NOT PERFORM CORRECTLY. PERFORMED CHECK OF THE
- [SDR CALA2025110310844](https://openairdocs.org/sdr/CALA2025110310844.md): Power Supply · no test · Oct 31, 2025 · N495UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK IAW EA2500-03960 AND EA2500-08031. R & R EPSU BATTERY AT AFT L LOCATION. REF: AMM 33-51-38/401 CONFIG 00. OP CHECK GOOD.
- [SDR CALA2025110310843](https://openairdocs.org/sdr/CALA2025110310843.md): Power Supply · no test · Oct 31, 2025 · N495UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK IAW EA2500-03960 AND EA2500-08031. R & R RT EMERGENCY EXIT EPSU, IAW AMM 33-51-38/401 CONFIG 00. OP CHECK IS GOOD.
- [SDR CALA2025080107204](https://openairdocs.org/sdr/CALA2025080107204.md): Fuel Cap · missing · Jul 31, 2025 · N495UA · Airbus A320232 · Fuel Storage
  > DURING WALK AROUND FOUND FUEL CAP MISSING. INSTALLED NEW FUEL CAP IAW AMM TASK 28-25-41-400-005-A.
- [SDR CALA2025052905065](https://openairdocs.org/sdr/CALA2025052905065.md): Unknown · odor · May 26, 2025 · N495UA · Airbus A320232 · Air Distribution System
  > COCKPIT SMELLED LIKE FUMES AND STAYED LIKE THAT FOR A WHILE AFTE R TAKEOFF AND THEN WENTOFF CREW DEBRIEFING: CAPTAIN SAID WHEN THEY START #2 ENGINES, FUEL PRESSURE WAS FLUCTUATING, WHEN ENGINE STARTED THEY SMELL FUMES, AND LINGERS TILL THEY TOOK OFF, ONCE AI
- [SDR CALA2025050704534](https://openairdocs.org/sdr/CALA2025050704534.md): Fmc · faulted · May 5, 2025 · N495UA · Airbus A320232 · Flight Management Computing Hardware System
  > AP1 WAS NOT RELIABLE IN REGARDS TO SPEED OR ALTITUDE. ATTEMPTED TWICE. PERFORMED POST FLIGHT REPORT, NO FAULTS LOGGED. PERFORMED AFS TEST, FMGC 1 FAILED TEST. RESET FMGC1 SYS & PERFORMED AFS TEST A SECOND TIME, ALL TEST PASSED. PERFORMED LAND TEST, TEST FAILED
- [SDR CALA2025012201962](https://openairdocs.org/sdr/CALA2025012201962.md): Door · out of adjust · Jan 22, 2025 · N495UA · Airbus A320232 · Door Warning System
  > INFORMATION ONLY REPORT. CLIMBING THRU 16K WE GOT LEFT AND RIGHT OVERWING EXIT INDICATING OPEN. F/ AS SECURED BOTH COVERS TWO WRITE UPS ON ONE LOG PAGE. CREATED ONE LOG PAGE FOR EACH. REF L/P 3571987 LEFT FWD OVERWING EMERGENCY EXIT DOOR INDICATES OPEN. INT
- [SDR CALA2025012301984](https://openairdocs.org/sdr/CALA2025012301984.md): Battery · faulted · Jan 19, 2025 · N495UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS FOUND ESPU BATTERY FORWARD LEFT (ABOVE DOOR 1L) BAD. REMOVED AND REPLACED L1 ESPU BATTERY REF AMM 33-51-38. SYSTEM TEST PASSED
- [SDR CALA2025012201966](https://openairdocs.org/sdr/CALA2025012201966.md): Handle · detached · Jan 18, 2025 · N495UA · Airbus A320232 · Emergency Exits
  > COVER ON LH FWD OVERWING EXIT HANDLE FELL OFF ADJUSTED AND TIGHTENED GAP ON FASTENER ARMS ON LEFT FWD OVERWING EMERGENCY EXIT HATCH COVER FLAP. REF AMM 52-21-11-400-001-A. OPS CHECK GOOD
- [SDR CALA2025012101951](https://openairdocs.org/sdr/CALA2025012101951.md): Power Supply · faulted · Jan 14, 2025 · N495UA · Airbus A320232 · Emergency Lighting
  > EPSU INT LOAD EMER L/R FAULT PERFORMED EPSU RESET. FAULT STILL STANDS. FOUND RIGHT HAMD EMERGENCY EXIT LIGHT INOP FOUND LIGHT ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED IAW AMM 33-51-00. RESET SYSTEM AGAIN. OPS CHECK GOOD. FAULT STILL STANDS. VOLT CHECKED
- [SDR CALA2025011601916](https://openairdocs.org/sdr/CALA2025011601916.md): Lens · missing · Jan 12, 2025 · N495UA · Airbus A320232 · Escape Slide
  > L SIDE OVERWING EXIT SLI DE ARMED LENS COVER MISSING. REPLACED LEFT SIDE OVERWING SLIDE ARM INDICATOR LENS COVER PER AMM-52-73-21-000-003-A.
- [SDR CALA2024122601653](https://openairdocs.org/sdr/CALA2024122601653.md): Cover · detached · Dec 23, 2024 · N495UA · Airbus A320232 · Emergency Exits
  > ECAM MSG DOOR FWD EMER EXIT AFTER LANDING CREW REPORT EMERGENCY EXIT COVER FLAP FOR FWD RIGHT OVERWING EXIT FELL OFF, RE ATTATCHED COVER FLAP, OPS CHECK GOOD, DOOR INDICATIONS NORMAL REF AMM 52-21-11 ADD EMP: U115923
- [SDR CALA2024122001600](https://openairdocs.org/sdr/CALA2024122001600.md): Sensor · faulted · Dec 18, 2024 · N495UA · Airbus A320232 · Door Warning System
  > DOOR R AFT EMER EXIT CABIN PRESSURE NORMAL ECAM OCCURED CLIMB OU T 7000FT CREW REPORTS R FWD OPEN ECAM INTERMITTENT ALSO THEN THEY GO OUT WHEN AIRCRAFT IS FULLY PRESSURIZED APPLIED MEL 5270AZ. MEL 5270AZ ACCOMPLISHED REPAIR TROUBLESHOT SENSOR MONITORING FAULT
- [SDR CALA2024122001597](https://openairdocs.org/sdr/CALA2024122001597.md): Cover · detached · Dec 18, 2024 · N495UA · Airbus A320232 · Emergency Exits
  > DOOR L EMER EXIT ECAM UPON ENTERING AIRCRAFT NOTICED EMER EXIT HANDLE COVER WAS OFF AND SITTING ON GROUND INCORRECTLY LABELED AS TRIM (LOGPAGE# 3241711). REINSTALLED FWD DOOR L EMER EXIT HANDLE COVER AND OPS CHECKED EMER DOOR PROX SWITCH REF AMM 52-22-00. FAUL
- [SDR CALA2024122001592](https://openairdocs.org/sdr/CALA2024122001592.md): Warning Light · intermittent · Dec 18, 2024 · N495UA · Airbus A320232 · Door Warning System
  > DOOR R AFT EMER EXIT CREW STATED MOMENTARY RH FWD AND AFT EMERGENCY EXIT LITE ON WITH NO NOISE, VIBRATION OR PREASSURIZATION PROBLEM. INSPECTED DOOR AND FOUND PROPERLY CLOSED PER AMM 52-22-00-410 AND INDICATIONS ARE NORMAL. NO HISTORY OK TO CONTINUE
- [SDR CALA2024060701737](https://openairdocs.org/sdr/CALA2024060701737.md): Frame · cracked · Jun 2, 2024 · N495UA · Airbus A320232 · Fuselage Main, Frame
  > FR16RH DOUBLE JOGGLE HOLE #5 HAS A CRACK INDICATION IN THE OUTER FRAME LAYER ONLY 5311-0320 DEVIATION TO EA 5311-02442 OPS 002 TO USE AIRBUS DWG LAYER POST REAMING PER NTM 51-10-01 & 51-10-18 WITH NO DEFECT SIZE 7.142 (.2811), INSP THRESHOLD FROM TIME OF EMBOD
- [SDR CALA2023052601647](https://openairdocs.org/sdr/CALA2023052601647.md): Battery · no test · May 25, 2023 · N495UA · Airbus A320232 · Emergency Lighting
  > PER PRODUCTION REQUEST, ESPU BATTERY "L" FAILED OPS TEST. REMOVED AND REPLACED IIWL EPSU BATTERY PER A320 AMM 33-51-39-000 -007-C2 / 33-51-39-400-007-C2. PERFORMED OP CHECKS PER A320 AMM 33-51-00-710-001-A / 3351-00-710-002-62. SYSTEM CHECKS GOOD.
- [SDR CALA2023020100308](https://openairdocs.org/sdr/CALA2023020100308.md): None · none · Feb 1, 2023 · N495UA · Airbus A320232 · Lighting System
  > FWD EMERGENCY BATTERY FAILED CAPACITY TEST. R+R FWD EMERGENCY LIGHT BATTERY REF 33-51-38. OPS CHECK GOOD.
- [SDR CALA2023020100307](https://openairdocs.org/sdr/CALA2023020100307.md): Light · failed · Feb 1, 2023 · N495UA · Airbus A320232 · Lighting System
  > RH OVERWING EMERGENCY BATTERY FAILED CAPACITY TEST. R+R RH OVERWING EMERGENCY LIGHT REF 33-51-38. OPS CHECK GOOD. SUPPOSED TO READ EMERGENCY LIGHT BATTERY.
- [SDR CALA2022121903440](https://openairdocs.org/sdr/CALA2022121903440.md): Pump · low pressure · Dec 19, 2022 · N495UA · Airbus A320232 · Aircraft Fuel Filter/Strainer
  > CTR TK PUMP 1 LO PR DISPLAYED ON UPPER ECAM SCREEN. - FUEL SHORTLY AFTER DEPARTURE CENTER TANK FUEL PUMP 1 WAS REPLACED.
- [SDR CALA2021101801918](https://openairdocs.org/sdr/CALA2021101801918.md): Stringer · corroded · Oct 17, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > CORROSION ON AFT CARGO COMPT BILGE AREA, FR56, STRINGER 41L SPLICE AT FR52. RECEIVED NEW STRINGER D5347042020800, BATCH INITIAL INSPECTION TO OCCUR 60,000 FC OR 120,000 FH FROM REPAIR # 0003843117, AND REPAIR COUPLING R5307111220800, BATCH EMBODIMENT AND SUBSE
- [SDR CALA2021101801910](https://openairdocs.org/sdr/CALA2021101801910.md): None · corroded · Oct 17, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > CORROSION ON AFT CARGO COMPT BILGE AREA, FR56, STRINGER 41L. CORRECTED ON DUPLICATE ELB LOGPAGE 7247641
- [SDR CALA2021101801905](https://openairdocs.org/sdr/CALA2021101801905.md): None · corroded · Oct 16, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > CORROSION ON BULK CARGO COMPT. BILGE AREA, STGR41R, FWD AND AFT OF FR59. REMOVED CORROSION FROM S41R FR59 AT BULK CARGO IAW SRM 51-74-00 L=12" D=0.03" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13-283-602 FIG 001 SHEET 01. REMOVED AND REPLACED S41R FROM FR58 TO F
- [SDR CALA2021101801898](https://openairdocs.org/sdr/CALA2021101801898.md): None · corroded · Oct 15, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > CORROSION ON STRINGER AT AFT FUSELAGE OUTFLOW VALVE CUT-OUT AREA, FR65 STRINGER 31R. REMOVED AND INSTALLED OUTFLOW VALVE IAW AMM 21-31-51 OPS TEST GO OD IAW AMM 21-31-00-710. BLENDED AREA ON S31R FR65 IAW SRM 51-74 -00 L=4.110" W=0.940" ORIGINAL THICKNESS 0.1
- [SDR CALA2021101801887](https://openairdocs.org/sdr/CALA2021101801887.md): None · corroded · Oct 14, 2021 · N495UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION ON BULK CARGO COMPT STGR 42R BETWEEN FR63 AND FR64 (A3 NB-53-3-6185) REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS L=18" D=.050", OUT OF LIMITS IAW A320 SRM 53-41-13-283-002, REMOVED AND REPLA CED STRINGER 42R, BETWEEN FR60 TO FR64 P/N D5347041
- [SDR CALA2021101401881](https://openairdocs.org/sdr/CALA2021101401881.md): None · none · Oct 14, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > DURING ROTO PROBE INSPECTION OF THE LH DOOR STOP FITTING #7 AT F R16, CRACK INDICATION WAS NOTED IN LOWER I/B HOLE FWD LAST TWO L AYERS, REPAIR BEFORE NEXT FLIGHT. (AD2019-20-10) REPLACED L/H DOOR STOP #7 FITTING INTERCOSTAL BY C/W EC/RA 5311- 02649, REPLACEME
- [SDR CALA2021101401880](https://openairdocs.org/sdr/CALA2021101401880.md): Stringer · none · Oct 14, 2021 · N495UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64. REPLACED STRINGER 41L BETWEEN FR60 TO FR64. P/N: D5347041821600 BTCH: 0003849002 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11. SFR# 1026673. MAINTENANCE ACCOMPLISHED BY V934700 ON WC 0014944 AT S
- [SDR CALA2021101401879](https://openairdocs.org/sdr/CALA2021101401879.md): Stringer · none · Oct 14, 2021 · N495UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64 REPLACED STRINGER 42L, BETWEEN FR60 TO FR64, P/N: D5347041821800 BATCH: 0003848975 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-1 1. SFR# 1026673 MAINTENANCE ACCOMPLISHED BY V934585 ON WC 001494 3 A
- [SDR CALA2021101101845](https://openairdocs.org/sdr/CALA2021101101845.md): None · corroded · Oct 10, 2021 · N495UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64.
- [SDR CALA2021101101844](https://openairdocs.org/sdr/CALA2021101101844.md): None · corroded · Oct 10, 2021 · N495UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64
- [SDR CALA2021101101846](https://openairdocs.org/sdr/CALA2021101101846.md): Intercostal · none · Oct 10, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)
  > DURING ROTO PROBE INSPECTION OF THE LH DOOR STOP FITTING #7 AT F R16, CRACK INDICATION WAS NOTED IN LOWER I/B HOLE FWD LAST TWO L AYERS, REPAIR BEFORE NEXT FLIGHT. (AD2019-20-10)
- [SDR CALA2021100401766](https://openairdocs.org/sdr/CALA2021100401766.md): Beam · corroded · Oct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y512.5 AT FR68. (A3NB-53-3-622 2) CORROSION ON FLOOR BEAM Y512.5 FR68 BLENDED OUT IAW SRM 51-74-00 SFR# 1026596. MAINTENANCE ACCOMPLISHED BY V933868 ON WC 0014619, BLENDED AREA MEASURES LENGTH 1.5" WIDTH 0.15" ORIGINAL THICKN
- [SDR CALA2021100401765](https://openairdocs.org/sdr/CALA2021100401765.md): Beam · corroded · Oct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSIN ON AFT CABIN FLOOR BEAM Y-1292 AT FR66. (A3NB-53-3-6222) BLENDED OUT CORROSION ON AFT CABIN BEAM Y-1292 AT FR66 IAW SRM 5 ING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-0 0-15-283-002 L=4.0" W=2.0" D=.046". REMOVED AND REPLACE
- [SDR CALA2021100401764](https://openairdocs.org/sdr/CALA2021100401764.md): Beam · corroded · Oct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 AND FR68 (A 3NB-53-3-6222) BLEND OUT CORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 A E ACCOMPLISHED BY V933486 ON WC 0014617 AT ST ENGINEERING BFM ND FR68IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW S
- [SDR CALA2021100401763](https://openairdocs.org/sdr/CALA2021100401763.md): Beam · corroded · Oct 1, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 AT FR68. (A3NB-53-3-6 222) BLENDED OUT CORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 IAW SRM 5 ENGINEERING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT LIMITS IAW SRM 53-00-1 5-283-002 L=0.80" W=0.5" D=0.150". REMOVED A
- [SDR CALA2021092901726](https://openairdocs.org/sdr/CALA2021092901726.md): Flap Track · corroded · Sep 28, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y 160.5 BETWEEN FR68 AND FR70. (SDR REQUIRED) A3NB-53-3-6222 EVALUATED FLOOR BEAM IAW A320 SRM 53-00-15-283-002 AND FOUND OUT OF LIMITS, RECEIVED NEW FLOOR BEAM. REPLACED IAW A320 SRM 51-42 -11. SFR# 1026536. MAINTENANCE ACCOM
- [SDR CALA2021092901725](https://openairdocs.org/sdr/CALA2021092901725.md): Fitting · corroded · Sep 28, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON R2 DOOR CUTOUT LOWER AFT CORNER FITTING AT FR68. (S DR REQUIRED) A3NB-53-3-6299 NO ESTABLISHED LIMITS FOUND IN SRM. REPLACED FR68R DOOR CUTOUT C ORNER FITTING WITH NEW PART IAW SRM 53-41-69-02-A, ITEM 200-A. L OCATED AND DRILLED IAW SRM 51-44-11.
- [SDR CALA2021092701693](https://openairdocs.org/sdr/CALA2021092701693.md): Beam · corroded · Sep 27, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR BEAM Y-765 AT FR20 (A3NB-53-3-6038) EVALUATED FLOOR BEAM AND FOUND OUT OF LIMITS IAW A320 SRM 53-11- 14-283-007, REMOVED AND REPLACED BEAM P/N D5311278220207, BATCH 00037288690 Y-765 IAW A320 SRM 51-42-11. MAINTENANCE ACCOMPLISHE D BY
- [SDR CALA2021092701692](https://openairdocs.org/sdr/CALA2021092701692.md): Beam · corroded · Sep 27, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR BEAM Y-1292 AT FR20. (A3NB-53-3-6038) CORROSION ON CABIN FLOOR BEAM Y-1292 FOUND OUT OF LIMITS IAW SRM 53-11-14-283-007. REMOVED AND REPLACED FLOOR BEAM Y-1292 FROM F R12 TO FR20 IAW SRM 51-42-11. MAINTENANCE ACCOMPLISHED BY V93386 6 O
- [SDR CALA2021092701691](https://openairdocs.org/sdr/CALA2021092701691.md): Beam · corroded · Sep 27, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y1162.5 AT FR68. (A3NB-53-3-62 22) FLOOR BEAM EVALUATED AND FOUND OUT OF LIMITS IAW A320 SRM 53-41- 15-283-002 AND REPLACED FOR NEW FLOOR BEAM PN: D5347218820400 BA TCH: 0002716527 IAW SRM 51-52-11/001. MAINTENANCE ACCOMPLISHE
- [SDR CALA2021092701679](https://openairdocs.org/sdr/CALA2021092701679.md): Door Frame · cracked · Sep 24, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > DURING ROTO PROBE OF RH FR16 #7 DOOR STOP FITTING FASTENER HOLES A CRACK WAS NOTED IN THE BOTTOM I/B HOLE. THE CRACK IS IN THE I NTERCOSTAL AT 9 O''CLOCK. REMOVED INTERCOSTAL FITTING P/N: D531-12307-201-00 AND REPLACED INTERCOSTAL FITTING P/N: D53114236-201-91
- [SDR CALA2021092401665](https://openairdocs.org/sdr/CALA2021092401665.md): Beam · corroded · Sep 23, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR BEAM Y-765 AT FR20 (A3NB-53-3-6038)
- [SDR CALA2021092401664](https://openairdocs.org/sdr/CALA2021092401664.md): Beam · corroded · Sep 23, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM Y1162.5 AT FR68. (A3NB-53-3-62 22)
- [SDR CALA2021092401666](https://openairdocs.org/sdr/CALA2021092401666.md): Seat Track · corroded · Sep 23, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR BEAM Y-1292 AT FR20. (A3NB-53-3-6038)
- [SDR CALA2021092401660](https://openairdocs.org/sdr/CALA2021092401660.md): Beam · corroded · Sep 22, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE (LOWER SURFACE) AT Y-1162.5 FR68 (A3NB-53-3-6222) (SDR) AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE WAS AVALUATED IAW S RM 53-00-15 AND FOUND OUT OF LIMITS, L=0.620" W=0.400" D=0.110", RECEIVED, LOCATE
- [SDR CALA2021092401658](https://openairdocs.org/sdr/CALA2021092401658.md): Beam · corroded · Sep 22, 2021 · N495UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR DUMMY RAIL AT APPRX Y-150 BETWEEN FR20 AND FR23. (A3NB-53-3-6038) REPLACED RAIL BETWEEN FR20 TO FR23 Y-150 IAW A320 SRM 51-72-11- 911-001 AND SRM 51-42-11. P/N: D5311141420200 BTCH: 0003838983. SFR# 1026487. MAINTENANCE ACCOMPLISHED B
- [SDR CALA2021092001606](https://openairdocs.org/sdr/CALA2021092001606.md): Shear Plate · corroded · Sep 19, 2021 · N495UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R/H SIDE FLOOR STRUCTURE LATERAL SHEAR PLATE CRACKED A PPRX 5" AFT FR69. INSTALLED NEW SHEAR PLATE AFT FR69 AND ANGLE IAW SRM 51-75-11 AN D SRM 51-42-11. SFR# 1026424. MAINTENANCE ACCOMPLISHED BY V93387 0 ON WC 0014622 AT ST ENGINEERING BFM
- [SDR CALA2021091701599](https://openairdocs.org/sdr/CALA2021091701599.md): Floor Support · corroded · Sep 17, 2021 · N495UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > CORROSION ON CABIN FLOOR SUPPORT AT APPRX Y-1673 AT FR20 REMOVED CORROSION ON CABIN FLOOR SUPPORT AT Y-1673 FR20 IAW SRM 51-74-00 FOUND OUT LIMITS IAW SRM 53-11-14-07 ORIGINAL THICKNESS 0.080" REMAINING THICKNESS 0.030" D=0.050". REMOVED AND REPLACE D FLOOR S

Next page: https://openairdocs.org/aircraft/N495UA/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 = 'N495UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N495UA/reports

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