# Service difficulty reports: N490UA

A list on [N490UA](https://openairdocs.org/aircraft/N490UA.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 2 · 88 reports

- [SDR CALA2026072017890](https://openairdocs.org/sdr/CALA2026072017890.md): Warning Message · illuminated · Jul 14, 2026 · N490UA · Airbus A320232 · Hydraulic Indicating System
  > G HYD RSVR LO LVL ECAM COMPLETED AND MANUAL GEAR EXTENSION ACCOMPLISHED.
- [SDR CALA2025121012017](https://openairdocs.org/sdr/CALA2025121012017.md): Warning Message · false activation · Dec 10, 2025 · N490UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > ECAM WARNING, APU EMERGENCY SHUTDOWN. THIS MESSAGE IS GENERATED WHEN THE EMER BUTTON AT THE 108VU (EXT PWR PLUG IN) IS PUSHED OR MALFUNCTIONED. T/S ECAM WARNING APU EMERGENCY SHUTDOWN ON GROUND IAW 49-00-00-810-923-A. RESET C/BS, OPS TESTS PASSED.
- [SDR CALA2025101009893](https://openairdocs.org/sdr/CALA2025101009893.md): Elec Connector · damaged · Oct 9, 2025 · N490UA · Airbus A320232 · Light System Wiring
  > ALL FIRST-CLASS SEAT EMERGENCY LIGHTS INOP FOUND PIN PUSHED BACK IN SIDEWALL CONNECTOR. RE-SEATED INTO LOCKING MECHANISM & PULLED CK WIRE. CONNECTOR & WIRES GOOD EMERGENCY LIGHT NOW OPERATES NORMAL REF. ESPM 20-44-11.
- [SDR CALA2025091708988](https://openairdocs.org/sdr/CALA2025091708988.md): Door · no discrepancy · Sep 15, 2025 · N490UA · Airbus A320232 · Emergency Exits
  > FA REPORTED LOUD SQUEELING SOUND FROM LEFT OVERWING EMERGENCY EX IT ROW 21. PRESSURIZED CABIN TO 4 PSI IAW AMM 05-53-00-780-001-A01. NO SQUEELING COMING FROM EXT ROW ON GROUND.
- [SDR CALA2025082808218](https://openairdocs.org/sdr/CALA2025082808218.md): Gauge · out of position · Aug 26, 2025 · N490UA · Airbus A320232 · Emergency Equipment
  > DOOR 2L SLIDE PRESS GAUGE OSCURED AND HARD 2 READ. UNSURE OF PR ESS DOOR 2L SLIDE PRESS GAUGE CLEARLY VISIBLE AND WITHIN RANGE REF AMM TASK 25-62-00-210-001-A
- [SDR CALA2025081507814](https://openairdocs.org/sdr/CALA2025081507814.md): Wire Harness · broken · Aug 15, 2025 · N490UA · Airbus A320232 · Emergency Lighting
  > PROCEDURE - SEAT 38C EMERGENCY LIGHT IS INOP. FOUND HARNESS, P/N: BR9631-60, UNDER SEAT BROKEN FROM CONNECTOR. HARNESS IS NSU IN SAT, RECONNECT HARNESS. ALL ADJACENT EMERGENCY LIGHTS OPERATE NORMALLY, PLACED ON MEL 3350C.
- [SDR CALA2025080107186](https://openairdocs.org/sdr/CALA2025080107186.md): Bottle · no discrepancy · Jul 29, 2025 · N490UA · Airbus A320232 · Escape Slide
  > 2L SLIDE IN RED HIGH REF 5720017. REF AMM 25-62-00-210-001 FOR NEEDLE READINGS. REF AMM 25-62-00-210-001 GAUGE IS MODEL A AND NEEDLE IS IN AREA B (SLIGHTLY ABOVE GREEN BAND) IS WITHIN LIMITS FOR CONTINUED SERVICE.
- [SDR CALA2025073007088](https://openairdocs.org/sdr/CALA2025073007088.md): Bottle · low pressure · Jul 28, 2025 · N490UA · Airbus A320232 · Escape Slide
  > CREW REPORTS - DOOR L2 SIDE PRESSUE IN RED ZONE. FOUND PRESSURE TO BE LOW PER AMM 25-62-00. REMOVED SLIDE IAW AMM 25-62-44-000-002-A AND EC/RA 2562-01143, INSTALLED SLIDE IAW AMM 25-62-44-400-006-A AND EC/RA 2562-01142. PERFORMED RII INSPECTION OF DOOR 2L E
- [SDR CALA2025070106110](https://openairdocs.org/sdr/CALA2025070106110.md): Slide · no discrepancy · Jun 28, 2025 · N490UA · Airbus A320232 · Escape Slide
  > ACCOMPLISHED THE REMOVAL OF THE R2 ESCAPE SLIDE IN REF WITH AMM TASK 25-62-44-000-802-A. AND RENDER A SAFE CHECK LIST. COMPLETED THE INSTALLATION OF THE R2 ESCAPE SLIDE IN REF WITH AMM 25-62-44-400-802-A. OPS CHECK GOOD. ACCOMPLISHED INSTALLATION INSPECTION OF
- [SDR CALA2025022602487](https://openairdocs.org/sdr/CALA2025022602487.md): Seal · missing · Feb 23, 2025 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LOUD SQUEAL COMINGFROM LEFT OVERWING EXITFOUND SEALANT/SEAL MISSING AT LH WING TO FUSELAGE PANELS 191BT AND 191DT NEAR WHERE NOISE REPORTED. SEE ATTACHED PICTURES. INTERIM REPAIR BELLY FAIRING SEALANT/SEALS FOR PANELS 191BT & 191DT IAW MT 53-004, INSPECT TAPE
- [SDR CALA2025010701836](https://openairdocs.org/sdr/CALA2025010701836.md): Power Supply · no test · Jan 6, 2025 · N490UA · Airbus A320232 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - CHECK OF EMERGENCY LIGHTS FAILS. PRODUCES FAULT- "EPSU BATTERY EMER L" R/R EPSU BATTERY AT EPSU 11WL REF AMM 33-51-38, OPS CHECKS OK. PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2024102100883](https://openairdocs.org/sdr/CALA2024102100883.md): Flt Controls · unknown · Oct 18, 2024 · N490UA · Airbus A320232 · Flight Control System
  > TO MAINTAIN STRAIGHT FLIGHT, PLANE IS IN APPRX3 DEGREE RIGHT BANK BELOK APPROX FL260 VISUALLY CHECKED ALL FLIGHT CONTROL SURFACES, NO ANOMALIES NOTED. PERFORMED BITE TESTS OF ALL FLIGHT CONTROL COMPUTERS AND ELEVATOR AND AILERON DAMPING TESTS PER MCDU. NO DIS
- [SDR CALA2024101702666](https://openairdocs.org/sdr/CALA2024101702666.md): Wire · broken · Oct 14, 2024 · N490UA · Airbus A320232 · Communications System Wiring
  > FOR SDR REPORTING: WIRE CUT AT CONNECTOR NUMBER 200RH12-BSDR #1037418. REF STS NR#0069. REPAIRED WIRE 3321-2190 TO CONNEC TOR 200RH 12-B WITH SPLICE PER AIRBUS ESPM 20-43-11-01-H PROCEED TO PERFORM TEST PER AIRBUS AMM 23-73-46-869-050-A TEST OK.
- [SDR CALA2024062601895](https://openairdocs.org/sdr/CALA2024062601895.md): Solenoid Valve · faulted · Jun 20, 2024 · N490UA · Airbus A320232 · Engine Temperature Indicating System
  > #2 ENGINE EGT EXCEEDANCE ON TAKE OFF. #2 ENGINE EGT EXCEEDANCE ON TAKE OFF, 77-00-00-810-818-B. REPORTING MAX OF 651 FOR 29 SECONDS. WILL CONFIRM REPORT ON A/C. ALSO FAULTING CHA 2.5 BLD ACT/ HC/EEC2. REF TSM 77-00-00-810-818-B PARA 4.F.(6) & AMM REMOVED BO
- [SDR CALA2024062601891](https://openairdocs.org/sdr/CALA2024062601891.md): Sleeve · missing · Jun 20, 2024 · N490UA · Airbus A320232 · Engine Thrust Reverser
  > PDA 2 #2 ENGINE RIGHT REVERSER HALF ACOUSTIC LINER DEPARTED A/C AND WAS FOUND ON THE RUNWAY. REMOVED #2 ENGINE OUTBOARD THRUST REVERSER. REF AMM TASK 78-32-03-000-010-A R&R #2 ENG R/H T/R PER MM 78-32-04-400-010 AND REPLACED #2 ENG R/H SLEEVE PER MM 78-32-76-
- [SDR CALA2024032100811](https://openairdocs.org/sdr/CALA2024032100811.md): Skin · dented · Mar 14, 2024 · N490UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE TOP CROWN AREA RIGHT FR50 TO FR51 STR 5R TO STR 6R HAS BARE METAL WITH DEPRESSION PER HAECO LCQ NR 9292430/324 30 SKIN REPAIRD AREA AT FR50-51 BETWEEN STGR 5R-6R PER PART 2 OF REACHES 110600 TOTAL AIRCRAFT FLIGHT CYCLES OR 221300 TOTAL THE L
- [SDR CALA2024032100809](https://openairdocs.org/sdr/CALA2024032100809.md): Window Post · cracked · Mar 14, 2024 · N490UA · Airbus A320232 · Fuselage Main, Structure
  > WINDSHIELD CENTRAL POST LH UPPER CROSS BOLT CRACK INDICATION AFT OF SPOTFACE AT THE 2:0 CLOCK POS HEAD SIDE OF BOLT (FIG 2 (B) T YPICAL) PER HAECO LCQ NR 9292090/32090 TTL FC. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 4700 TTL FC, THEREAFTER. FO
- [SDR CALA2024032100808](https://openairdocs.org/sdr/CALA2024032100808.md): Window Frame · cracked · Mar 14, 2024 · N490UA · Airbus A320232 · Fuselage Main, Structure
  > ACCOMPLISH MIRROR FITTING REPAIR ON FLIGHT DECK WINDSHIELD FRAME CENTER POST LOWER NODE AREA PER HAECO LCQ NR 9292387/32387 GENE RATED BY V061609 56337 TTL FC. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 4700 TTL FC, THEREAFTER. FOR REPAIR TO THE
- [SDR CALA2024032100807](https://openairdocs.org/sdr/CALA2024032100807.md): Fitting · cracked · Mar 14, 2024 · N490UA · Airbus A320232 · Fuselage Main, Structure
  > WINDSHIELD CENTER LEFT CONTINUITY FITTING CRACKED PER HAECO LCQ NR 9292081/32081 GENERATED BY V062335 56,337 TTL FC. ACCOMPLISH REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 4,700 TTL FC, THEREAFTER. FOR REPAIR TO THE LH & RH FRONT WINDSHIELD FRAME, ACCOMPLISH
- [SDR CALA2024022200499](https://openairdocs.org/sdr/CALA2024022200499.md): Skin · contaminated · Feb 21, 2024 · N490UA · Airbus A320232 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 134 INCHES FROM I/B EDGE, 15 I NCHES FROM TRAILING EDGE, 3 INCHES IN DIAMETER. REPAIRED L/H ELEVATOR UPPER SKIN 134"IN FROM I/B EDGE, 15" IN FR OM T/E 3"IN DIA ZONE 1 IAW A320 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2023101103026](https://openairdocs.org/sdr/CALA2023101103026.md): Fuel Cap · missing · Oct 8, 2023 · N490UA · Airbus A320232 · Fuel Storage
  > FUELER REPORTS MISSING FUEL CAP UPDATED WITH PARTS INFO. NIS @ MSY CDL REQUESTED PLACED ON CDL DISPATCH DESK: 81 NAME: SL DATE: 08-OCT-23- FUEL CAP MISSING.
- [SDR CALA2023051501496](https://openairdocs.org/sdr/CALA2023051501496.md): Battery · no test · May 5, 2023 · N490UA · Airbus A320232 · Emergency Lighting
  > REMOVE & INSTALL EPSU BATTERY (13WL)PART OFF:P/N:AD3214-31, S/N:291942,QTY:1-EA.PART ON:P/N:AD3214-31,S/N:182058,B/N:N463UA 3084,QTY:1-EA.LTPR NR#50012316740010
- [SDR CALA2023051501495](https://openairdocs.org/sdr/CALA2023051501495.md): Battery · no test · May 5, 2023 · N490UA · Airbus A320232 · Emergency Lighting
  > REMOVAL & INSTAL EPSU BATTERY (12WL),PART OFF:P/N:AD3214-31, S/N:283890,QTY:1-EA. PART ON:P/N:AD3214-31,S/N:295192,B/N:N463 UA3086,QTY:1-EA.LTPR NR#50012316740010.
- [SDR CALA2023051501494](https://openairdocs.org/sdr/CALA2023051501494.md): Battery · no test · May 5, 2023 · N490UA · Airbus A320232 · Emergency Lighting
  > REMOVE & INSTALL EPSU BATTERY (11WL),PART OFF:P/N:AD3214-31, S/N:274395,QTY:1-EA.PART ON:P/N:AD3214-31,S/N:293565,B/N:N463UA 3085,QTY:1-EA.LTPR NR#50012316740010.
- [SDR CALA2023051501493](https://openairdocs.org/sdr/CALA2023051501493.md): Battery · no test · May 5, 2023 · N490UA · Airbus A320232 · Lighting System
  > REMOVAL & INSTALL OF EPSU BATTERY (10WL).PART OFF:P/N:AD3214-31 S/N:287718 QTY:1-EA.PART ON:P/N:AD3214-31,S/N:287688,B/N:N463UA 87,QTY:1-EA.LTPR NR#50012316740010.
- [SDR CALA2022111603147](https://openairdocs.org/sdr/CALA2022111603147.md): None · none · Nov 16, 2022 · N490UA · Airbus A320232 · Standard Practices/Structures
  > INSTALLED LOCKOUT PIN FOR #1 ENGINE TRUST REVERSER HCU. PLZ REMOVE AND RETURN TO TOOLING AFTER INSTALL IS COMPLETE. REMOVED T/R LOCKOUT PIN.
- [SDR CALA2022033100826](https://openairdocs.org/sdr/CALA2022033100826.md): Fitting · none · Mar 29, 2022 · N490UA · Airbus A320232 · Landing Gear System
  > RT MLG W/W DOOR ATTACH FITTING HAS CHAFE ON FWD HINGE FITTING AF T LOBE GEN BY V892429 PER NR9290026/42026 RMVD AND RPLD RT MLG W/W ATTACH FITTING IAW SRM 51-72-11 BY MECH V914162 IMSP BY LC-40
- [SDR CALA2021120602262](https://openairdocs.org/sdr/CALA2021120602262.md): Panel · damaged · Dec 6, 2021 · N490UA · Airbus A320232 · Fuselage Structure (General)
  > EMERGENCY EXIT HATCH FRAME ( EXIT AT SEAT 21A) HAS DAMAGED FILLER PANEL AT FRAME FR41 (LH). DAMAGE IS APROX.5 SQ IN IN HATCH SEAL CONTACT AREA WITH PROBABLE PRESSURIZATION LEAK OF MATING SEAL / FILLER PANEL. FILLER PANEL MUST BE RESTORED PER AMM: 53-31-00-440
- [SDR CALA2021042800564](https://openairdocs.org/sdr/CALA2021042800564.md): Door Sill · corroded · Apr 28, 2021 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R- 2 DOOR LOWER SILL PLATE CORR @ AFT END FR68 MKD DOT 60-076 REF. AAR N/R:9478800 GENERATED BY: V891378 REMOVED R2 DOOR LOWER SILL PLATE AND INSTALLED NEW R2 DOOR LOWER SILL PLATE IAW A320 SRM 51-42-11 AND 53-41-14-80A, AND RECONECTED DRAIN HOSES L
- [SDR CALA2021042800555](https://openairdocs.org/sdr/CALA2021042800555.md): Door Sill · corroded · Apr 26, 2021 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN R- 2 DOOR LOWER SILL PLATE CORR @ AFT END FR68 MKD DOT 60-076 REF. AAR N/R:9478800 GENERATED BY: V891378 REMOVED R2 DOOR LOWER SILL PLATE AND INSTALLED NEW R2 DOOR LOWER SILL PLATE IAW A320 SRM 51-42-11 AND 53-41-14-80A, AND RECONECTED DRAIN HOSES L
- [SDR CALA2021041900491](https://openairdocs.org/sdr/CALA2021041900491.md): Stop Fitting · cracked · Apr 17, 2021 · N490UA · Airbus A320232 · Fuselage Main, Structure
  > DOOR STOP FITTING NO1 FR16L LOWER INBOARD FASTENER HOLE EXHIBITS CRACK BETWEEN THE INTERCOSTAL AND FRAME. (REF AAR NON-ROUTINE 9479245) REF N/R AAR- 9479245 REWORKED DOOR STOP #1 AT FR16L LOWER I/B FASTENER HOLE AS PER EC/RA 5311-02546. PART-1 INTERIM REPAIR
- [SDR CALA2019040100506](https://openairdocs.org/sdr/CALA2019040100506.md): Screw · missing · Mar 31, 2019 · N490UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > PDA 3 ON RIGHT HYD ACCESSPANEL ABOVE FLAP ONFUSELAGE/ ONE SCREWMISSING AND ONE LOOSE, SEE LOGPAGE 9277638 INSTALLED NEW FASTNER AND SECURED LOOSE FASTNER ON RH OFF WING SLIDE PACK, REF AMM SUBTASK 25-62-42-420-052-A, PDA CLASS 3 ITEM
- [SDR CALA2018041601166](https://openairdocs.org/sdr/CALA2018041601166.md): Connector · disconnected · Apr 16, 2018 · N490UA · Airbus A320232 · Light System Wiring
  > SEAT EMERGENCY LIGHTS INOPERATIVE AT ROWS 12 - 22, FOUND THE CONNECTOR DISCONNECTED UNDER SEAT 21A, CONNECTED THE CONNECTOR AND PREFORMED AN OPS CHECK OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-001A, AND 33-51-00-710-009A. OPS CHECKED GOOD, NO FAULTS NOTE
- [SDR CALA2018021600666](https://openairdocs.org/sdr/CALA2018021600666.md): Handle · loose · Feb 16, 2018 · N490UA · Airbus A320232 · Passenger/Crew Doors
  > L2 DOOR ARMING LEVER FEELS LOOSE, FOUND THE FLAT HANDLE PIECE AT END OF HANDLE WHERE YOU GRAB IT SLIGHTLY LOOSE.TIGHTENED HANDLE END PIECE.NO ADJUSTMENTS WHERE MADE T O SYSYTEM.VERIFIED WITH INSPECTION THAT THIS WAS NOT AN INSPECT ION ITEM. IAW TASK 52-10-0
- [SDR CALA2018020900509](https://openairdocs.org/sdr/CALA2018020900509.md): Fan · failed · Feb 9, 2018 · N490UA · Airbus A320232 · Air Distribution Fan
  > BLOWER FAULT DISPLAYED ON UPPER ECAM SCREEN. VENT FAULT ASSOCIATED WITH A GRINDING NOISE AND ELECTRICAL ODOR. REPLACED THE BLOWER FAN IAW MM 21-26-51. LEAK AND OPS CHECKED GOOD.
- [SDR CALA2017100903550](https://openairdocs.org/sdr/CALA2017100903550.md): Stringer · corroded · Oct 9, 2017 · N490UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > BULK CARGO BAY, FRAMES 65 - 66, STRINGER 31R HAS CORROSION. REMOVED AND REPLACED THE STRINGER IAW SRM 51-72-11-911-001.
- [SDR CALA2017091803251](https://openairdocs.org/sdr/CALA2017091803251.md): Power Supply · no test · Sep 18, 2017 · N490UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED, FWD LT, DURING 2 SVC. REPLACED THE EPSU IAW MM 33-51-38, OPS CHECKED NORMAL.
- [SDR CALA2017090903113](https://openairdocs.org/sdr/CALA2017090903113.md): Lens · damaged · Sep 9, 2017 · N490UA · Airbus A320232 · Emergency Equipment
  > RIGHT FORWARD SLIDE INDICATION INOP. FROSTED AND EXTREMELY HARD TO READ. REPLACED DAMAGED LENS IAW EC/RA 2523-01203 PART 3 PERMANENT REPAIR.
- [SDR CALA2017010900056](https://openairdocs.org/sdr/CALA2017010900056.md): Battery · discharged · Jan 9, 2017 · N490UA · Airbus A320232 · Emergency Lighting
  > EMER LIGHTS IN CABIN FLICKERING ON/OFF DURING TAXI OUT. CEASED PRIOR TO TAKEOFF FOUND CIDS MESSAGE EPSU UNIT FWD L. REPLACED EPSU BATTERY PER AM M 33-51-38. OPS CHECK OK AND MESSAGE CLEARED.
- [SDR CALA2014092292255](https://openairdocs.org/sdr/CALA2014092292255.md): Switch · faulty · Sep 21, 2014 · N490UA · Airbus A320232 · Emergency Lighting
  > ALL EMER LIGHTS IN THE CABIN CAME ON FOR ABOUT 10 SECONDS IN FLIGHT. REPLACED SWITCH 4WL IAW TSM 33-51-00-810-881-A. OPERATIONS CHECKED OK IAW AMM 33-51-00710-004-A.
- [SDR CALA2014092292274](https://openairdocs.org/sdr/CALA2014092292274.md): Battery · faulted · Sep 18, 2014 · N490UA · Airbus A320232 · Emergency Lighting
  > OVERHEAD EMER LIGHTS INOPERATIVE. OVERWING EMER EXIT LIGHTS CAME ON SOMETIME AFTER TAKEOFF RECYCLED SWITCH. ACCOMPLISHED TEST OF THE EMER LIGHTS IAW MM 33-51-00 HAD 2 FAULTS EPSU BATTERY RT & EPSU BATTERY AFT LT. REPLACED BATTERY IN POWER SUPPLY UNITS RT &
- [SDR CALA2014091292106](https://openairdocs.org/sdr/CALA2014091292106.md): Battery · discharged · Sep 9, 2014 · N490UA · Airbus A320232 · Emergency Lighting
  > EPSU BATTERY EMER LIGHT MSG ON PTP PANEL AFTER EMER LIGHT OPERATIONAL TEST. REPLACED BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED OK.
- [SDR CALA2014063091368](https://openairdocs.org/sdr/CALA2014063091368.md): Structure · cracked · Jun 28, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LEFT MLG WW LT SIDE TORSION BOX LOWER SIDE SHELL HORIZONTAL FLANGE CRACKED AT FASTENER HOLE COMMON TO FRAME 43. REPAIR WAS ACCOMPLISHED IAW ECRA 5330-04864 REV A. THIS ECRA ACCOMPLISHED SBA 320-53-1251 TO BOTH THE LT & RT SIDES.
- [SDR CALA2014062791345](https://openairdocs.org/sdr/CALA2014062791345.md): Light · broken · Jun 27, 2014 · N490UA · Airbus A320232 · Door Warning System
  > R2 DOOR SLIDE LIGHT BROKEN. R & R BULB IAW MM 52-73-21-400-002. OPERATIONS CHECKED GOOD IAW MM 52-73-00-710-001-A. IDT TASK.
- [SDR CALA2014062091316](https://openairdocs.org/sdr/CALA2014062091316.md): Door Sill · corroded · Jun 20, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL IS CORRODED AT 7 LOCATIONS AT FWD & AFT ENDS. AFTER BLENDING CORROSION AT 7 LOCATIONS MATERIAL LOSS WAS.065 OUT OF LIMITS IAW SRM 53-41-14 FIG 101. ORIGINAL MATERIAL T=.177 & REMAINING T=.112. R & R L2 DOOR SILL IAW SRM 53-41-14 FIG 101.
- [SDR CALA2014062091315](https://openairdocs.org/sdr/CALA2014062091315.md): Stringer · corroded · Jun 19, 2014 · N490UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 42R IS CORRODED BETWEEN FRAME 63 & 64 IN AFT CARGO COMPARTMENT. CORROSION WAS OUT OF LIMITS FOR BLENDING. CUT OUT STRINGER BETWEEN FRAME 62 & 63 & REMOVED FACTORY INSTALLED SPLICE. INSTALLED NEW STRINGER & SPLICE. THIS REPAIR REQUIRES RE-INSPECTI
- [SDR CALA2014062091314](https://openairdocs.org/sdr/CALA2014062091314.md): Door Sill · corroded · Jun 19, 2014 · N490UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL IS CORRODED ALONG ENTIRE LENGTH. FOUND CORROSION TO BE OUT OF LIMITS FOR BLENDING. R & R R2 DOOR SILL & SPLICE BETWEEN FRAME 66 - 68. RESTORED THE AREA, HIS IS A MAJOR REPAIR.
- [SDR CALA2014062091313](https://openairdocs.org/sdr/CALA2014062091313.md): Spar · chafed · Jun 17, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACCOMPLISHED REPAIR IAW SRM54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.
- [SDR CALA2014062091312](https://openairdocs.org/sdr/CALA2014062091312.md): Spar · chafed · Jun 17, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon, Frame/Spar/Rib
  > NUMBER 1 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. ACP REPAIR IAW SRM 54-51-12 FIG 202. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS.
- [SDR CALA2014061691293](https://openairdocs.org/sdr/CALA2014061691293.md): Rub Strip · chafed · Jun 15, 2014 · N490UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 2 PYLON LOWER RUB STRIP FOUND CHAFFED AT RIBS 5 & 10. REPAIRED LOWER SPAR PLATE CNA ANTI- CHAFE IAW SRM54-51-12 P 207 REPAIR 5 BA REQUIRES INSPECTION IAW SRI 54-51-12-2-001-00. INITIAL INSPECTION THRESHOLD TO BEGIN AT 102297 PTT 66543PTC.

Next page: https://openairdocs.org/aircraft/N490UA/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 = 'N490UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N490UA/reports

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