# Service difficulty reports: N491UA

A list on [N491UA](https://openairdocs.org/aircraft/N491UA.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 · 100 reports

- [SDR CALA2025120511782](https://openairdocs.org/sdr/CALA2025120511782.md): Chiller · odor · Dec 3, 2025 · N491UA · Airbus A320232 · Buffet/Galleys
  > FWD CHILLER HAD AN ODOR OF MELTED PLASTIC. FA TURNED OFF. DEFERRED PER MEL, PULLED AND COLLARED CB, INSTALLED INOP STICKER ADJ TO CB. REMOVED AND REPLACED THE FWD GALLEY AIR CHILLER IAW AMM 25-34-51. OPS CHECKED GOOD.
- [SDR CALA2025102410496](https://openairdocs.org/sdr/CALA2025102410496.md): Fuel Cap · missing · Oct 23, 2025 · N491UA · Airbus A320232 · Fuel Storage
  > MISSING FUEL CAP IN REF LOG PAGE 6722035. INSTALLED FUEL CAP REF 28-25-41.
- [SDR CALA2025052104884](https://openairdocs.org/sdr/CALA2025052104884.md): Panel · loose · May 19, 2025 · N491UA · Airbus A320232 · Emergency Exits
  > CLBING THRU 12K ECAM AFT RIGHT EMER EXIT DOOR WARNING AT 2.2PSID PRESS WAS NORMAL AND FND PNL LOOSE. RE-INSTALLED THE PNL AND PFM OPS CHK IAW AMM 52-21-00-710-003-A CHK GOOD.
- [SDR CALA2025030302545](https://openairdocs.org/sdr/CALA2025030302545.md): Slide · faulted · Feb 27, 2025 · N491UA · Airbus A320232 · Emergency Equipment
  > AFT DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0021} - REMOVE AND INSTALL R2 DOOR SLIDE AND RECORD.ROTABLE PARTS DATA REPLACED R2 DOOR ESCAPE SLIDE AS PER AMM 25-62-44-000-802-A, OK FOR SERVICEPARTS USED: 31-2561-9-0015, QTY:1 ROTABLE PARTS CHANGE WA
- [SDR CALA2025010601820](https://openairdocs.org/sdr/CALA2025010601820.md): Battery · no test · Jan 3, 2025 · N491UA · Airbus A320232 · Emergency Lighting
  > RIGHT HAND OFF-WING ESCAPE SLIDE INSTALL {A3NB-25-3-6280} - DURING OPS CHECK OF EMERGENCY LIGHT CIDS DISPLAYED EPSU INT LOAD EMER L MSG. UPDATING ROTABLE PARTS CHANGE WAS INDICATED - TT # 1559479 SN OFF 8303.POWER SUPPLY, P OFF 31-3350-9-9001 8303 ON 31-3350
- [SDR CALA2024061001758](https://openairdocs.org/sdr/CALA2024061001758.md): Fuel Cap · missing · Jun 3, 2024 · N491UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP MISSING ON AIRCRAFT UPON ARRIVAL CONFIRMED WITH CMH STATION THAT FUELER INSTALLED CAP PRIOR TO DEPARTURE. WILL REPORT TO ENGINEERING
- [SDR CALA2024030500636](https://openairdocs.org/sdr/CALA2024030500636.md): Skin · gouged · Mar 4, 2024 · N491UA · Airbus A320232 · Wing, Plate/Skin
  > R/H WING L/E AT #1 SLAT ABOVE #3 TRACK SKIN IS GOUGED APPROX. 1. 5 INCH LONG. REMOVED AND REPLACED SKIN AT RH WING #1 SLAT ABOVE #3 TRACK A320 SRM 51-72-11.
- [SDR CALA2023120603570](https://openairdocs.org/sdr/CALA2023120603570.md): Switch · out of position · Dec 2, 2023 · N491UA · Airbus A320232 · Communications System
  > FA REPORTS THAT OVERHEAD EMERGENCY EXIT SIGNS OVER DOORS 1L AND 1R ARE ILLUMINATED. ACP TEST OF SYSTEM PER AMM 33-51-00. FOUND COCKPIT NO SMOKING SWITCH OUT OF NORMAL POSITION. SECURED SWITCH. GROUND CK GOOD.
- [SDR CALA2022121603392](https://openairdocs.org/sdr/CALA2022121603392.md): Bulb · missing · Dec 13, 2022 · N491UA · Airbus A320232 · Exterior Lighting
  > PDA 2 LH RETRACTABLE LANDING LIGHT BULB IS MISSING, RPLD LH RET LANDING LIGHT ASSY OPS CK NORMAL TASK33-42-11-400-003-A
- [SDR CALA2022042101030](https://openairdocs.org/sdr/CALA2022042101030.md): Plate · corroded · Apr 19, 2022 · N491UA · Airbus A320232 · Fuselage Main, Floor Beam
  > LEFT AFT SHEAR PLATE AT FR 68 HAS CORROSION-A3NB-53-3-6222 GENER ATED BY V061334 AT HAECO LCQ PER NR 9298367 (30367) REMOVED AND REPLACED LEFT AFT SHEAR PLATE AT FR 68 IAW SRM 51-72 -11-911-001 AND 002 PERFORMED BY V052030 INSP BY V061334
- [SDR CALA2022040600880](https://openairdocs.org/sdr/CALA2022040600880.md): None · corroded · Apr 4, 2022 · N491UA · Airbus A320232 · Fuselage Main, Floor Beam
  > R2 DOOR SILL HAS NUMEROUS AREAS OF CORROSION A3NB-53-3-5222 PER HAECO LCQ NON ROUTINE 9298371/30371 GENERATED BY V061334 REMOVED AND REPLACED R2 DOOR SILL PART # D5348004320701 PO#11016 22.9 IAW A320 SRM 53-41-14-80-A AND SRM 51-72-11-911-001 PER MEC H V929087
- [SDR CALA2022040600883](https://openairdocs.org/sdr/CALA2022040600883.md): Stop Fitting · cracked · Apr 4, 2022 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > RH AFT DOOR FR68 STOP FITTING #1 LWR I/B HOLE CRACK AT FRAME LAY ER 6 O''CLOCK POS. AD RELATED TASK EA 5343-01724 001 PER HAECO LC Q NON ROUTINE 9298354/30354 GENERATED BY V061682
- [SDR CALA2022040600882](https://openairdocs.org/sdr/CALA2022040600882.md): Fitting · cracked · Apr 4, 2022 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > LH AFT DOOR FR68 STOP FITTING #1 LWR I/B HOLE CRACK AT FRAME LAY ER 6 O''CLOCK POS. AD RELATED TASK EA 5343-01724 001 PER HAECO LC Q NON ROUTINE 9298355/30355 GENERATED BY V061682
- [SDR CALA2022040600881](https://openairdocs.org/sdr/CALA2022040600881.md): Fitting · corroded · Apr 4, 2022 · N491UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR68 FWD SIDE JUST 2" ABOVE R-2 SILL HAS CORROSION A3NB-53-3- 6222 PER HAECO LCQ NON ROUTINE 9298558/30558 GENERATED BY N07857 0
- [SDR CALA2022040400862](https://openairdocs.org/sdr/CALA2022040400862.md): Fitting · gouged · Apr 1, 2022 · N491UA · Airbus A320232 · Horizontal Stabilizer Structure
  > L/H HORIZONTAL STAB T/E #4 ELEVATOR ATTACHMENT FITTING SUPPORT S TRUCTURE GOUGED. GENERATED AT HAECO LCQ PER NR 9298281 BY V90166 5. (30281) {A3NB-55-3-6005} REMOVED AND REPLACED D5598152200202 HINGE ARM AT #4 ON LH ELEVAT OR, PO # 1111333.1 IAW A320 SRM 51-42
- [SDR CALA2022033100851](https://openairdocs.org/sdr/CALA2022033100851.md): Frame · none · Mar 31, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FR35-36 ON R/H PRESS PANEL HOLES CRACKED. ECRA 5331-02868 PART 1.3, PLANNING TO CONTACT EG AFTER 70,336 TTFC, OR 150,519TTLFH, WHICHEVER COMES 1ST, BUT BEFORE 71,336TTFC OR 151,519 TTLFH WHICHEVER COMES 1ST FOR ECRA 5331-02868 INSPECTION REQUIREMENTS. 71,336TT
- [SDR CALA2022033100828](https://openairdocs.org/sdr/CALA2022033100828.md): None · none · Mar 29, 2022 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > RH PRESSURE PANEL FR 35/36 HOLES 3,4,13,14,15,20,22,23,27,28 HAV E CRACK INDICATION. GENERATED BY V061682 ON HAECO LCQ NR 9298423 /30423 AIRS ARE CAT -B- MAJOR REPAIR. START/FINISH DIMENSIONS ARE LISTE NSPECTION PER PART 2 OF THE LATEST ECRA 5331-02868 ON OR B
- [SDR CALA2022033100821](https://openairdocs.org/sdr/CALA2022033100821.md): None · none · Mar 28, 2022 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > AFT WET AREA AT R2 DOOR STRINGER 23RT HAS FOUR EACH HOLES OVER S IZED ON HORZ FLANGE AFT OF FR68, GENERATED AT HAECO LCQ PER NR92 98484 (30484) BY V052030. REMOVED AND REPLACED AFT CABIN STRINGER 23 RT AFT OF FRAME 68 IA W A320 SRM 51-72-11. PERFORMED BY V9252
- [SDR CALA2022033100816](https://openairdocs.org/sdr/CALA2022033100816.md): None · none · Mar 28, 2022 · N491UA · Airbus A320232 · Fuselage Main, Floor Beam
  > RIGHT AFT SHEAR PLATE FLOOR SUPPORT AT FR 68 HAS CORROSION. GENE RATED AT HAECO LCQ PER NR 9298369 (30369) BY V061334. (A3NB-53-3 -6222) RENIVED ABD REOKACED RH AFT SHEAR PLATE FLOOR SUPPORT AT FR STA 68 STRINGE LOCATION 23 RH ALL IAW A320 SRM 51-72-11 AND A32
- [SDR CALA2022033100815](https://openairdocs.org/sdr/CALA2022033100815.md): None · none · Mar 28, 2022 · N491UA · Airbus A320232 · Fuselage Main, Floor Beam
  > RIGHT AFT SHEAR PLATE AT FR 68 HAS CORROSION. GENERATED AT HAECO LCQ PER NR 9298368 (30368) BY V061334. (A3NB-53-3-6222) REMOVE AND REPLAACE RH AFT SHEAR PLATE AT FR STA 68 STR LOCATION 23RH ALL IAW A320 SRM 51-72-11 AND A320 AMM 51-78-00-916-001-A. PERFORMED
- [SDR CALA2022033100813](https://openairdocs.org/sdr/CALA2022033100813.md): Fitting · none · Mar 28, 2022 · N491UA · Airbus A320232 · Fuselage Main, Frame
  > PER NR 9298363/30363 LH VERTICAL FRAME AND FITTING, HOLE #3 HAS A CRACK INDICATION AT APPROX. THE 6 O''CLOCK POSITION IN THE FIT TING.. GENERATED BY V061632 WINDSHIEL LATERAL FR UPPER ATTACHMENT AREA AT REPAIRED HOLE #3 P AC REACHED 35,836 TT FC. PERFORM REP
- [SDR CALA2022032300746](https://openairdocs.org/sdr/CALA2022032300746.md): Intercostal · cracked · Mar 21, 2022 · N491UA · Airbus A320232 · Fuselage Main, Frame
  > FR 16 RH DOOR STOP #7 IB UPPER HOLE HAS CRACK INDICATION IN INTE RCOSTAL LAYER @ 6 OCLOCK DIRECTION PER HAECO LCQ NON ROUTINE 929 8352/30352 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT INTERCOSTAL AT R/H FR16 STOP #7 IAW R531-13118 AND A320 SRM 57-42-
- [SDR CALA2022032300745](https://openairdocs.org/sdr/CALA2022032300745.md): Intercostal · cracked · Mar 21, 2022 · N491UA · Airbus A320232 · Fuselage Main, Frame
  > FR 16 LH DOOR STOP #7, IB UPPER HOLE HAS CRACK INDICATION IN INT ERCOSTAL LAYER @ 6 OCLOCK DIRECTION PER HAECO LCQ NON ROUTINE 92 98347/30347 GENERATED BY V892444 REMOVED AND REPLACED DISCREPANT INTERCOSTAL AT L/H FR16 STOP #7 IAW R531-13118 AND A320 SRM 51-42
- [SDR CALA2022032100704](https://openairdocs.org/sdr/CALA2022032100704.md): Stringer · corroded · Mar 17, 2022 · N491UA · Airbus A320232 · Standard Practices/Structures
  > AFT CARGO COMPARTMENT STR 43L HAS CORROSION BETWEEN FR 60 AND FR 61 PER HAECO LCQ NON ROUTINE 9298272/30272 GENERATED BY V061771 REMOVED AND REPLACED STRINGER AT 43L AND FR 60-64 IAW A320 SRM T ASK 51-72-11-911-001 PERFORMED BY V936070 INSPECTED BY V061334
- [SDR CALA2022031400656](https://openairdocs.org/sdr/CALA2022031400656.md): None · corroded · Mar 12, 2022 · N491UA · Airbus A320232 · Standard Practices/Structures
  > FWD PIT CORR SPLICE STR 41R BETWEEN FR 30 & 31 A3NB-05-3-6013 GENERATED BY:V061334 AT HAECO LCQ PER NR#9298265 (30265) REMOVED AND REPLACED FISHPLATE SPLICE AT STR 42R BETWEEN FR30-31 IAW A320 SRM TASK 51-72-11-911-001. PERFORMED BY V936070 INSP B Y V061334.
- [SDR CALA2022031400655](https://openairdocs.org/sdr/CALA2022031400655.md): None · corroded · Mar 12, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO CLEAT AT FR30 STR41RT TO STR42RT HAS CORROSION GENERAT ED BY N078592 NON ROUTINE 9298360/30360. REMOVED AND REPLACED CLEAT AT FWD CARGO AT FR30 BETWEEN STRG 41R AND STRG 42R IAW A320 SRM 51-72-11-911-002 AND SRM 51-42-11-001 (RII MAJOR REPAIR) PERFOR
- [SDR CALA2022031400644](https://openairdocs.org/sdr/CALA2022031400644.md): None · corroded · Mar 11, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FWD PIT CORR CLEAT 42R FR32 (A3NB-05-3-6013). GENERATED BY V0613 34 AT HAECO LCQ PER NR 9298266 (30266) REMOVED AND REPLACED CLEAT AT FWD CARGO COMPARTMENT BETWEEN FR31 -FR32, STRG:41R-42R IAW A320 SRM 51-72-11-911-002 AND SRM 51-42- 11-001. PERFORMED BY V9172
- [SDR CALA2022031400641](https://openairdocs.org/sdr/CALA2022031400641.md): None · corroded · Mar 11, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FWD CARGO CLEAT AT FR32 SRT 41RT TO STR 40RT HAS CORROSION (A3NB-05-03-6013). GENERATED BY N078592 AT HAECO LCQ PER NR 9298 361 (30361). REMOVED AND REPLACED CLEAT AT FWD CARGO COMPARTMENT BETWEEN STRG 40R-41R AT FR 32 IAW A320 SRM 51-72-11-911-002 AND SRM 51-
- [SDR CALA2022031400640](https://openairdocs.org/sdr/CALA2022031400640.md): None · corroded · Mar 11, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FWD PIT CORR CLEAT STR 41R FR 31(A3NB-05-3-6013). GENERATED BY V 061334 AT HAECO LCQ PER NR 9298267 (30267). REMOVED AND REPLACED CLEAT AT FWD CARGO COMPARTMENT BETWEEN STRG: 41R-42R AT FR31 IAW A320 SRM 51-72-11-911-002 AND SRM 51-42-11 -001. PERFORMED BY V9
- [SDR CALA2022031400642](https://openairdocs.org/sdr/CALA2022031400642.md): None · corroded · Mar 11, 2022 · N491UA · Airbus A320232 · Fuselage Structure (General)
  > FWD PIT CORR CLEAT STR 40R FR 30 (A3NB-05-3-6013). GENERATED BY V061334 AT HAECO LCQ PER NR 9298264 (30264). REMOVED AND REPLACED CLEAT AT FWD CARGO COMPARTMENT BETWEEN FR29 -FR30 STRG:40R-41R IAW A320 SRM 51-72-11-911-002 AND SRM 51-42-1 1-001. PERFORMED BY V
- [SDR CALA2022031000627](https://openairdocs.org/sdr/CALA2022031000627.md): None · none · Mar 9, 2022 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO PIT STRINGER 42 LEFT BETWEEN FRAME 63-64 HAS CORROSION A3NB-53-4-6179 PER HAECO LCQ NON ROUTINE 9298197/30197 GENERATED BY V052030 REMOVED & INSTALLED STRINGER @ FRAMES 60-64, 42L STR. IAW A320 T ASK 51-72-11-11-001, TASK 53-41-13-283-002 & TASK 51-7
- [SDR CALA2019120302125](https://openairdocs.org/sdr/CALA2019120302125.md): Stringer · corroded · Nov 30, 2019 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FR56-57 STR43L PREVIOUS REPAIR CORRODED, A3NB-33-3-601 0, PER HAECO LCE NR 9290441, ACCOMPLISHED SPLICE REPAIR ON STRG 43L AT FR 56-59 IAW SRM 53-00 -13-300-001 FIG 001.THIS IS A CAT B REPAIR WITH INSPECTION AT 60,000 FC/120,000 FH FROM REPAIR EMBO
- [SDR CALA2019120302124](https://openairdocs.org/sdr/CALA2019120302124.md): Stringer · corroded · Nov 30, 2019 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FR56-FR57 STR 41L STRINGER CORRODED, A3NB-33-3-6010, PER NR 9290443, STRINGER SPLICE REPAIR INSTALLED IAW SRM 53-00-13-300-001 ON STR 41 AT BETWEEN FR55-56. THIS IS A CAT B REPAIR REQUIRING REINSPEC TIONS PER SRI 53-00-13-205-001 BEGINNING AT 60,000
- [SDR CALA2019120302123](https://openairdocs.org/sdr/CALA2019120302123.md): Stringer · corroded · Nov 30, 2019 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FR58-FR59 STR 42L CORRODED, A3NB-33-3-6010, PER HAECO LCQ NR 9290445, ACCOMPLISHED SPLICE REPAIR ON STRG 42L AT FR 54-59 IAW SRM 53-00 -13-300-001.REPAIR CAT B REQUIRES INSPECTION FROM REPAIR EMBODIM ENT AT 60,000 FC/120,000 FH IAW SRI 53-00-13-205-
- [SDR CALA2019120302122](https://openairdocs.org/sdr/CALA2019120302122.md): Stringer · corroded · Nov 30, 2019 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO FR65 STR31R CORRODED AT OUTFLOW VALVE, SUPPORT TASK, P ER NR 9290448, REMOVED AND REPLACED STRINGER 31R, FR64R-68R, R/H SIDE IAW A320 SRM 51-42-11-801, PARAGRAPH 6, 2E, 2F.
- [SDR CALA2019120302121](https://openairdocs.org/sdr/CALA2019120302121.md): Torsion Box · corroded · Nov 30, 2019 · N491UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO TORSION BOX UPPER SURFACE HAS LIGHT SURFACE CORROSION MULTIPLE AREAS, A3NB-33-3-6010, PER LCQ NR 9290450, REMOVED AND REPALCED AFT CARGO TORSION BOX WRB R/H SIDE FR52-56 IAW A320 SRM 51-42-11-801 PARAGRAPH 6 2E,2F.
- [SDR CALA2019120302120](https://openairdocs.org/sdr/CALA2019120302120.md): Angle · cracked · Nov 29, 2019 · N491UA · Airbus A320232 · Fuselage Main, Keel
  > R/H AFT KEEL BEAM SIDE PANEL. LOWER FORWARD ANGLE HAS CRACK AT L OWER FASTENER. DOT E940. AD RELATED TASK "REPAIR PER EA 5331-017 18 OP 08 BEFORE NEXT FLIGHT" (SUPPORT TASK) PER HAECO LCQ NR# 92 90253 REPAIRED CRACK AND REPLACED TI-ANGLE AT RH AFT KEEL BEAM SI
- [SDR CALA2017080802520](https://openairdocs.org/sdr/CALA2017080802520.md): Reservoir · warning light · Aug 8, 2017 · N491UA · Airbus A320232 · Hydraulic Indicating System
  > HYD RESERVOIR OVERHEAT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. REPLACED LOW PRESSURE FILTER MODULE, REPLACED HIGH PRESS FILTER MODULE. REPLACED THE GREEN SYS CHECK VALVE. REPLACED LANDING GEAR DOOR SELECTOR VALVE IAW AMM32-31-34, AMM 29-11-44,
- [SDR CALA2017020300266](https://openairdocs.org/sdr/CALA2017020300266.md): Wire · broken · Feb 3, 2017 · N491UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 29, 30, 31. FOUND A BROKEN WIRE AT SIDEWALL CONNECTOR AT ROW29. REPAIRED BROKEN WIRE AND REPLACED CONN BACKSHELL AT SIDEWALL ROW 29, LIGHTS CHECKED GOOD.
- [SDR CALA2016091995746](https://openairdocs.org/sdr/CALA2016091995746.md): Battery Pack · inoperative · Sep 16, 2016 · N491UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAULTED. REPLACED EPSU BATTERY, OPS TESTED GOOD.
- [SDR CALA2014071591465](https://openairdocs.org/sdr/CALA2014071591465.md): Skin · damaged · Jul 12, 2014 · N491UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DOUBLER REPAIR ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN JUST AFT OF FRAME 1 & AT Y-330 RT. ORIGINAL SKIN THICKNESS 0.055INCHES. REPAIR ACCOMPLISHED IAW SRM 53-00-11 TBL 203 PARA 4 W FIG 239. REPAIR REQUIRES INSPECTION IAW SRI 53-00-11-2-017-00 PARA 3 L TBL 22
- [SDR CALA2014071591463](https://openairdocs.org/sdr/CALA2014071591463.md): Stringer · corroded · Jul 11, 2014 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER FOUND CORRODED BETWEEN FRAME 58 & 60. STRINGER SECTION REPLACED FROM FRAME 58 TO 64.
- [SDR CALA2014071591462](https://openairdocs.org/sdr/CALA2014071591462.md): Stringer Splice · corroded · Jul 11, 2014 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 41R SPLICE PLATE CORRODED AT FRAME 58. R & R STRINGER SPLICE PLATES.
- [SDR CALA2014071191447](https://openairdocs.org/sdr/CALA2014071191447.md): Stringer · corroded · Jul 7, 2014 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA FRAME 60 - 64 RT HAS CORROSION. AFT CARGO STRINGER 42R CORRODED BEYOND LIMITS. FRAME 60 - 64 REPAIRED BY SPLICING IN NEW STRINGER SECTION SRM 53-00-13 FIG 202. THIS SRM REFERS TO SRI 53-00-13 TBL 205 PG 205. RE-INSP AT 6000
- [SDR CALA2014071191424](https://openairdocs.org/sdr/CALA2014071191424.md): Stringer · corroded · Jul 6, 2014 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STRINGER 39 RT CORROSION ON OUTER FLANGE BETWEEN FRAME 62 - 63 & STRINGER 39. REMOVED CORROSION STRINGER 39 AFT CARGO FRAME 62 - 63 IAW SRM 53-00-13 FIG 202. HFEC ACCOMPLISHED NO CRACKS NOTED IAW NTM 51-10-04. INSTALLED REPAIR IAW SRM53-00-13 FIG
- [SDR CALA2014071191423](https://openairdocs.org/sdr/CALA2014071191423.md): Stringer · corroded · Jul 6, 2014 · N491UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT BILGE AREA STRINGER FRAME 61 - 64 STRINGER 40 RT HAS CORROSION. OUT OF LIMITS REPAIR EXTENDS PASSED 2 BAYS IAW SRM 53 -41-13 & 53-00-13 FIG 202 SHEET 2. REMOVED DAMAGED STRINGER 40 FRAME 61 - 64 APPROX 51.25 INCHES SRM53-00-13 FIG 202.
- [SDR CALA2014071191422](https://openairdocs.org/sdr/CALA2014071191422.md): Access Panel · gouged · Jul 6, 2014 · N491UA · Airbus A320232 · Wing, Plate/Skin
  > LEFT WING FUEL PANEL 540MB HAS TWO EACH GOUGED FASTENER S HOLES. REAMED TWO EACH HOLES ON PANEL 540MB, COLD WORKED HOLES & REAMED. FABRICATED TWO BUSHINGS & INSTALLED ON PANEL. BRIDGE PLATE INSTALLED WET IAW SRM 57-21-11 PARA 5 B FIG 202. PANEL REQUIRES RE
- [SDR CALA2014071191421](https://openairdocs.org/sdr/CALA2014071191421.md): Door Sill · corroded · Jul 5, 2014 · N491UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION FRAME 66 & STRINGER 23R. BLENDED CORROSION ON R2 DOOR SILL BEAM OUT OF LIMITS IAW SRM51-41-14 FIG 101. R & R BEAM IAW SRM 51-42-11 PAGES 6 - 7.
- [SDR CALA2014071191420](https://openairdocs.org/sdr/CALA2014071191420.md): Fitting · cracked · Jul 5, 2014 · N491UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FRAME 43 WING BAY CORD, TORSION BOX & MLG FREE FALL BRACKET AFT HOLE HAS A CRACK RT SIDE. R & R LT & RT REINFORCEMENT FITTINGS TORSION BOX LOWER SIDE SHELL.
- [SDR CALA2014070191395](https://openairdocs.org/sdr/CALA2014070191395.md): Door Sill · corroded · Jul 1, 2014 · N491UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS CORROSION AT FRAME 66 STRINGER L23 BOTTOM SURFACE. CORROSION FOUND OUT OF LIMITS IAW SRM 53-41-14 PB 102 FIG 101. 0.035 LOSS REPAIRED SILL IAW SRM53-41-14 PB202 P5-A FIG 101 PRP 1 SHEET 2 CAT A REPAIR NO FURTHER ACTION.

Next page: https://openairdocs.org/aircraft/N491UA/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 = 'N491UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N491UA/reports

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