# Service difficulty reports: N426UA

A list on [N426UA](https://openairdocs.org/aircraft/N426UA.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 4 · 166 reports

- [SDR CALA2025063006072](https://openairdocs.org/sdr/CALA2025063006072.md): Connector · disconnected · Jun 28, 2025 · N426UA · Airbus A320232 · Light System Wiring
  > EMERGENCY EXIT ROW LIGHT AT SEAT 38C INOP REF AMM 33-51-18/401 CONFIG 00, REPLACED SEAT 38C EMERGENCY PATH LIGHT MONUMENT, NO HELP. REF WDM 33-51-08 PAGE 278A, FOUND 7260VC CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR AND ACP OPS CHECK REF AMM TASK 33-51-00-7
- [SDR CALA2025022702493](https://openairdocs.org/sdr/CALA2025022702493.md): Lanyard · out of position · Feb 24, 2025 · N426UA · Airbus A320232 · Emergency Equipment
  > DOOR 2L DOES NOT INDICATE ARMED. ARM LIGHT WENT OFF AROUND 20K FT. ARMED HANDLE IS SLIGHTLY OUT FOUND DOOR 2L SLIDE MOORING LINE HANGING BELOW GRIT BAR, RESTOWED MOORING LINE VERIFIED NORMAL, OPS OF DOOR 2L SLIDE ARMED HANDLE AND SLIDE ARMED INDICATION LIGHT
- [SDR CALA2025022000398](https://openairdocs.org/sdr/CALA2025022000398.md): Shear Plate · corroded · Feb 20, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > SUPPORT TASK AFT MAIN CABIN, BETWEEN FR 69 AND FR 70, Y1732 SHEAR PLATE/TRAY, LH SIDE, HAS CORROSION. TRANSCRIBED FROM HAECO GSO NR 9282039 REMOVED AND REPLACED LATERAL SHEAR PLATE BETWEEN LH FR 69 TO FR 70 Y1732 PER AIRBUS DWG 853474180 ISSUE U AND A320-200 S
- [SDR CALA2025022400400](https://openairdocs.org/sdr/CALA2025022400400.md): Shear Web · corroded · Feb 10, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) R2 DOOR CUTOUT SHEAR WEB HAS SURFACE CORROSION JUST AFT OF AFT GIRTH BAR FITTING LOCATION. TRANSCRIBED FROM HAECO GSO NR 9282041 EVALUATED REWORKED AREA ON THE R2 DOOR SILL UPPER SURFACE AT FR68, FOUND AREA TO EXCEED ALLOWABLE LIMITGS PER A320-
- [SDR CALA2025020600308](https://openairdocs.org/sdr/CALA2025020600308.md): Floor Support · corroded · Feb 5, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) R/H LONGITUDINAL EAM HAS 2EA SPOTS OF CORROSION AT -Y1162.5 BETWEEN FR68 AND FR69. REMOVED AND REPLACED LONGITUDINAL BEAM LOCATED BETWEEN FR68 TO FR70 AT -71162.5 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040, ISSUE A,
- [SDR CALA2025021000321](https://openairdocs.org/sdr/CALA2025021000321.md): Beam · damaged · Feb 5, 2025 · N426UA · Airbus A320232 · Fuselage Main, Structure
  > (SUPPORT TASK) R/H LONGITUDINAL BEAM HAS SCREW STRIKE DAMAGE AT FR70 AND -Y464.8 TRANSCRIBED FROM HAECO GSO NR 9282045 REMOVED AND REPLACED LONGITUDINAL BEAM LOCATED BETWEEN FR68 TO FR70 AT -Y464.8 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040, ISSUE A
- [SDR CALA2025021000319](https://openairdocs.org/sdr/CALA2025021000319.md): Beam · corroded · Feb 5, 2025 · N426UA · Airbus A320232 · Fuselage Main, Structure
  > (SUPPORT TASK) AFT MAIN CABIN, BETWEEN FR68 AND FR70, Y160.5, LONGITUDINAL BEAM, HAS CORROSION. REMOVED AND REPLACED LONGITUDINAL BEAM BETWEEN FR68 TO FR70 AT Y160.5 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040 ISSUE A.
- [SDR CALA2025020600309](https://openairdocs.org/sdr/CALA2025020600309.md): Shear Plate · corroded · Feb 3, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) AFT MAIN CABIN, BETWEEN FR69 AND FR70, -Y1732, SHEAR PLATE/TRAY, RH SIDE, HAS CORROSION. REMOVED AND REPLACED SHEAR PLATE AND SUPPORT AT FR69 TO FR70 AT -Y1732 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53474180, ISSUE U.
- [SDR CALA2025020400279](https://openairdocs.org/sdr/CALA2025020400279.md): Shear Plate · cracked · Feb 3, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) R/H LATERAL SHEAR PLATE CRACKED AT FR68 TO FR69. REMOVED AND REPLACED SHEAR PLATE LOCATED AT FR68 TO FR69, Y1792 PER A320 SRM 51-40-11-1001, AND AIRBUS DWG D53480019 ISSUE RQ
- [SDR CALA2025020200256](https://openairdocs.org/sdr/CALA2025020200256.md): Shear Plate · cracked · Jan 31, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) L/H LATERNAL SHEAR PLATE CRACKED AT FR68 TO FR69 REMOVED AND REPLACED L/H LATERAL SHEAR PLATE AT FR68 TO 69 PER AIRBUS DWG NO. D53480019, ISSUE BQ AND A320-200 SRM 51-21-11
- [SDR CALA2024110601054](https://openairdocs.org/sdr/CALA2024110601054.md): Duct · contaminated · Nov 4, 2024 · N426UA · Airbus A320232 · Air Distribution System
  > BLEED AIR HAS STRONG BURNING PLASIC ODOUR WITH APU OR ENGINE RUN NING PACKS ITEM LOCKED BY TOMC ITEM UNLOCKED BY TOMC. PERFORMED INSP REF AMM 05-50-00-810-831-A. IN CONJUCTION WITH LOGPAGES 9773868 AND 9773874. FOUND SIGNS ON HYD FLUID ON DUCTS AND BOTH SYSTEM
- [SDR CALA2024072500284](https://openairdocs.org/sdr/CALA2024072500284.md): Antenna · inoperative · Jul 24, 2024 · N426UA · Airbus A320232 · Weather Radar System
  > WX RADAR ANT INOP UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE PERFORM BITE TEST OF THE WEATHER RADAR PER AMM 34-41-00-740-002-A MAC METER INITIATED FOR WIT
- [SDR CALA2023112703486](https://openairdocs.org/sdr/CALA2023112703486.md): Fuel Cap · missing · Nov 26, 2023 · N426UA · Airbus A320232 · Fuel Storage
  > PDA 2 AIRCRAFT ARRIVED WITHOUT FUEL CAP REF LP 6395809, CDL CURRENTLY ON THAT LP FOR MISSING FUEL CAP. UNKNOWN IF RETAINED AT PREVIOUS LEGS OR LOST IN FLIGHT. INSTALLED NEW FUEL CAP. PAINT REQUIREMENT ON LP 6417624.
- [SDR CALA2023091102758](https://openairdocs.org/sdr/CALA2023091102758.md): Skin · dented · Sep 10, 2023 · N426UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DENT FOUND. 26" INCHES AFT OF DOOR 312AR 1/4" WIDE 1/8" INCH DEPTH REFERENCE PICTURE HIGHLIGHTED DIMPLE REFERENCE DIMPLE IS 26 INCHES AFT OF ACCESS DOOR 312AR (STR 27R & 28R, REQUEST INTERNAL AND EXTERNAL EDDY CURRENT NDT AND A DEPTH CLEANED UP INSIDE SKIN AND
- [SDR CALA2023041401116](https://openairdocs.org/sdr/CALA2023041401116.md): Stringer · corroded · Apr 12, 2023 · N426UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO STRINGER 43L CORRODED FR 58-59. (A3NB-05-3-6023). GENE RATED BY V892285 AT HAECO LCQ, PER NR 9292470(34470). REMOVED AND REPLACED AFT CARGO STRINGER 43L AT FR 58-59 IAW A320 SRM 51-72-11-911-001. PERFORMED BY N078599 AND INSP BY V061588.
- [SDR CALA2023041001061](https://openairdocs.org/sdr/CALA2023041001061.md): Fitting · cracked · Apr 6, 2023 · N426UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR 68 STGR 22 HAS A CRACK IN THE RADIUS OF WEB AND FLANGE GE N BY MECH V061632 ON HAECO LCQ NR #9292027(34027) 341-01385. WORK ACCOMPLISHED BY LCQ EMP V061673. ACCOMPLISH INIT ATEST REVISION OF EC/RA 5341-01385 ON OR BEFORE 55,060 TOTAL AIR NOT TO EXCEED 1
- [SDR CALA2023040601056](https://openairdocs.org/sdr/CALA2023040601056.md): Web · cracked · Apr 6, 2023 · N426UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR 68 STGR 22 HAS A CRACK IN THE RADIUS OF WEB AND FLANGE GE N BY MECH V061632 ON HAECO LCQ NR #9292027(34027) 341-01385. WORK ACCOMPLISHED BY LCQ EMP V061673. ACCOMPLISH INIT ATEST REVISION OF EC/RA 5341-01385 ON OR BEFORE 55,060 TOTAL AIR NOT TO EXCEED 1
- [SDR CALA2023040601047](https://openairdocs.org/sdr/CALA2023040601047.md): Plate · corroded · Apr 5, 2023 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO SHEAR PLATE AT STR38L BETWEEN FR62-FR63 HAS CORROSION ON UPPER FLANGE. GEN AT HAECO LCQ BY V061609 PER NR 9292592 (345 92) REMOVED REPLACED AND REPROTECTED SHEAR PLATE AT STR 38L BETWEEN FR 62-63 IAW A320 SRM 51-72-11-911-002. ACMP BY MECH V061609 IN
- [SDR CALA2023032900912](https://openairdocs.org/sdr/CALA2023032900912.md): Channel · cracked · Mar 28, 2023 · N426UA · Airbus A320232 · Doors
  > RH AFT EMERGENCY DOOR FWD INTERNAL PLATE ATTACHMENT CRACKED A3NB -4-6031 PER NR9292433/34433 GEN BY V798788 RMVD AND RPLD FWD FRAME SEGMENT ON RH AFT EMERGENCY DOOR IAW SRM 51-72-11-911-001 BY MECH V061673 INSP BY V892442
- [SDR CALA2023032900911](https://openairdocs.org/sdr/CALA2023032900911.md): Channel · cracked · Mar 28, 2023 · N426UA · Airbus A320232 · Doors
  > LH FWD EMERGENCY DOOR FWD INTERNAL PLATE ATTACHMENT CRACKED A3NB -52-4-6031 PER NR9292460/34460 RMVD AND RPLD FWD FRAME SEGMENT ON LH FWD EMERGENCY DOOR IAW SRM 51-72-11-911-001 BY MECH V061673 INSP BY V892442
- [SDR CALA2023032900910](https://openairdocs.org/sdr/CALA2023032900910.md): Channel · cracked · Mar 28, 2023 · N426UA · Airbus A320232 · Doors
  > LH FWD EMERGENCY DOOR AFT INTERNAL PLATE ATTACHMENT CRACKED A3NB -52-4-6031 PER NR9292432/34432 RMVD AND RPLD AFT FRAME SEGMENT ON LH FWD EMERGENCY DOOR IAW SRM 51-72-11-911-001 BY MECH V061673 INSP BY V892442.
- [SDR CALA2023032900909](https://openairdocs.org/sdr/CALA2023032900909.md): Channel · cracked · Mar 28, 2023 · N426UA · Airbus A320232 · Doors
  > RH AFT EMERGENCY DOOR AFT INTERNAL PLATE ATTACHMENT CRACKED A3NB -52-4-6031 PER NR9292459/34459 GEN BY V798788 RMVD AND RPLD AFT FRAME SEGMENT ON RH AFT EMERGENCY DOOR IAW SRM 51-72-11-911-001 BY MECH V061673 INSP BY V892442
- [SDR CALA2022101802858](https://openairdocs.org/sdr/CALA2022101802858.md): Fuel Cap · missing · Oct 18, 2022 · N426UA · Airbus A320232 · Fuel Storage
  > FUEL CAP FOUND MISSING ON ARRIVAL FROM DEN FLT 2662-15. REPLACED ON RIGHT LOWER WING FUEL CAP ASSY.
- [SDR CALA2022071101688](https://openairdocs.org/sdr/CALA2022071101688.md): Accumulator · leaking · Jul 11, 2022 · N426UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > *EMERGENCY DECLARED* HYDRAULIC QUANTITY LOW RIGHT OR YELLOW SYSTEM YELLOW HYD QUANTITY 0 IS THE AREA OF CONCERN. UPON ARRIVAL, CHECKED YELLOW SYSTEM QUANTITY AND SOME FLUID REMOVED YELLOW SYTEM ACUMALATER REF MM29-13-42-000-001-A. PTU YELLOW ACCUMULATOR WAS L
- [SDR CALA2022020700337](https://openairdocs.org/sdr/CALA2022020700337.md): Hydraulic Line · leaking · Feb 7, 2022 · N426UA · Airbus A320232 · Hydraulic System, Main
  > G RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD GRN RSVSR LOW LEVELECAM IN FLIGHT HYDRAULIC LEAK COMING FROM NUMBER 1 ENGINE. ENGINE CASE DRAIN FILTER NO METAL FOUND, INSTALLED CASE DRAIN FILTER PER MM 29-11-43-400-010-A. C/B R-35 PULLED FOR GREEN HYD PUMP
- [SDR CALA2022012400211](https://openairdocs.org/sdr/CALA2022012400211.md): Seal · cracked · Jan 23, 2022 · N426UA · Airbus A320232 · Nacelle/Pylon Structure
  > PDA 2 #1 ENG INBD SIDE T-R TO PYLON FLEX SEAL PIECES MISSING AND CRACKED...REF FIG 3 ITEMS 90 AND 110 OF ECRA 5450-02357...SEE PHOTO ABD APPLIED SPEED TAPE. ISSUE DIP TO DO VISUAL INSP ONCE PER DAY 50 FLIGHT HOURS. PER PART 2A, AND ACCOMPLISH PERMANENT REPAIR
- [SDR CALA2021091001539](https://openairdocs.org/sdr/CALA2021091001539.md): Shield · damaged · Sep 8, 2021 · N426UA · Airbus A320232 · Emergency Equipment
  > CAPTAIN''S OXYGEN FACE SHIELD IS DAMAGED. CAPT MASK ISFOGGY NIS ORD CURRENTLY M&E IS 31-3515-9-9001 CAPTAINS OXYGEN MASK HAS BEEN REPLACED SEE LOG PAGE 6965234 FOR SIGN OFF
- [SDR CALA2021091001537](https://openairdocs.org/sdr/CALA2021091001537.md): Oxygen Mask · faulted · Sep 8, 2021 · N426UA · Airbus A320232 · Crew Oxygen System
  > FO''S OXYGEN FACE SHIELD IS DAMAGED. FO MASK DOES NOTSEAL WELLHAD TO HOLD ONFACE NIS ORD M&E REQUIRED 31-3515-9-9001 FO''S MASK HAS BEEN REPLACED SEE LOG PAGE 6965235 FOR SIGN OFF
- [SDR CALA2021090101483](https://openairdocs.org/sdr/CALA2021090101483.md): Cabin Pressure · pressure loss · Sep 1, 2021 · N426UA · Airbus A320232 · Cabin Pressure Control System
  > EMERGENCY LANDING- CABIN PRESSURIZATION RUNAWAY. ON DECENT FROM FL390...AROUND FL360 CREW NOTICED CABIN PRESSUIZATION FLUCTION 3000-5000. CABIN PRESSURIZATION SWITCH WAS IN AUTO THE ENTIRE TIME THEY WERE DECENDING, QRH DID NOT SAY SWITCH TO MANUAL SO THEY DI
- [SDR CALA2021090101473](https://openairdocs.org/sdr/CALA2021090101473.md): Lanyard · obstructed · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > DURING EMERGENCY EVENT, REF LP 6960737, AFTER OXYGEN MASKS WERE DEPLOYED AND ACTIVATED AT ROW 23ABC, FOUND MASK LANYARD PIN STUCK UNDER O2 GENERATOR FIRING PIN. SEE PHOTO.
- [SDR CALA2021090101472](https://openairdocs.org/sdr/CALA2021090101472.md): Oxygen Mask · misinstalled · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > DURING EMERGENCY EVENT, REF LP 6960737, 2 OF 4 OXYGEN MASKS AT ROW 37ABC WERE FOUND NOT CONNECTED TO O2 GENERATOR. SEE PHOTO.
- [SDR CALA2021090101471](https://openairdocs.org/sdr/CALA2021090101471.md): Oxygen Mask · misinstalled · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > DURING EMERGENCY EVENT, REF LP 6960737, 2 OF 4 OXYGEN MASKS AT ROW 34DEF WERE FOUND NOT CONNECTED TO O2 GENERATOR PROPERLY. SEE PHOTO.
- [SDR CALA2021090101470](https://openairdocs.org/sdr/CALA2021090101470.md): Lanyard · failed · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > PASSENGER OXYGEN AUTO CONTROL SYSTEM INOP - OXYGEN MASKS IN ROW 32FAILED TO AUTODEPLOY SEAT ROW 32DEF MASK DEPLOYED,LANYARD FAILED BEFORE FIRING PIN WA S ACTIVATED
- [SDR CALA2021090101469](https://openairdocs.org/sdr/CALA2021090101469.md): Ring · obstructed · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > DURING EMERGENCY EVENT, REF LP 6960737, AFTER MASKS WERE DEPLOYED AND ACTIVATED AT ROW 30DEF, FOUND MASK LANYARD RING STUCK UNDER O2 GENERATOR FIRING PIN. SEE PHOTO.
- [SDR CALA2021090101468](https://openairdocs.org/sdr/CALA2021090101468.md): O2 Generator · failed · Aug 31, 2021 · N426UA · Airbus A320232 · Passenger Oxygen System
  > O2 GENERATOR FAILED TO OPERATE FIRE REMOVED PSU FOR QUARANTINE SEE ATTACHED PHOTO SDR INSP DUE PSU WAS 24 RIGHT
- [SDR CALA2020053101003](https://openairdocs.org/sdr/CALA2020053101003.md): Unknown · malfunctioned · May 30, 2020 · N426UA · Airbus A320232 · Hydraulic System, Main
  > ECAM CAUTION MESSAGE. Y ENG PUMP LO PR MESSAGE INOP. HYD TOMC UPDATE FLAGGING AS SDR ITEM CREW STATES THE Y-ENG PUMP FAILED AND PTU TOOK OVER, YELLOW SYS WAS NORMAL WITH PTU. REF TSM 29-13-00-810-804-A FOR TROUBLESHOOTING IAW TSM 29-13-00-810-804-A. ACCOMP
- [SDR CALA2020051700964](https://openairdocs.org/sdr/CALA2020051700964.md): Pressure Panel · damaged · May 5, 2020 · N426UA · Airbus A320232 · Fuselage Main, Structure
  > RH FRAME 35-36 PRESSURE PANEL HOLE #''S 4, 5, 7, 9, 11, 19, 22, 25, 26, 28 & 60 REPAIRED IAW EC/RA 5331-02674. PLACE ON DIP TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5331-02674 ON OR BEFORE NOVEMBER 4, 2020. PLANNING TO CONTACT ENGINEERING AFTER OC
- [SDR CALA2020050900932](https://openairdocs.org/sdr/CALA2020050900932.md): Pressure Panel · damaged · May 5, 2020 · N426UA · Airbus A320232 · Fuselage Main, Structure
  > LHS FRAME 35-36 PRESSURE PANEL HOLE #''S 4-11, 22, 27, 28, 35, 45 AND HOLE AT LONGITUDINAL BEAM AT Y+765 REPAIRED IAW EC/RA 5331-02673. PLACED ON DIP TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5331-02673 ON OR BEFORE NOVEMBER 4, 2020. PLANNING TO CO
- [SDR CALA2019012800166](https://openairdocs.org/sdr/CALA2019012800166.md): Stringer · corroded · Jan 25, 2019 · N426UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > (A3NB-53-4-6179 A-41 DOT 150) AFT CARGO STGR 39R BETWEEN FR56 A N FR58 IS CORRODED. NONROUTINE 9020983 REMOVED FASTNERS AT STR 39R FR56-58 IAW SRM 51-42-11-006 CLEANED STRINGER IAW SRM 51-75-00 AT STR39 FR56-58 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-13-3
- [SDR CALA2019012500150](https://openairdocs.org/sdr/CALA2019012500150.md): Frame · cracked · Jan 23, 2019 · N426UA · Airbus A320232 · Fuselage Main, Frame
  > DURING HMV-4 WHILE ACCOMPLISHING INSP. OF THE LT SIDE POST FR4 UPPER ATTACHMENT, FOUND CRACK INDICATION ON HOLE LABELE D #3. ACCOMPLISHED INTERIM REPAIR AS PER ECRA 5311-02068 PART 1. CREATED DIP TO ACCOMPLISH PERMANENT REPAIR AS PER PART 3 OF ECRA 5311-02068
- [SDR CALA2019012500149](https://openairdocs.org/sdr/CALA2019012500149.md): Stop Fitting · cracked · Jan 23, 2019 · N426UA · Airbus A320232 · Fuselage Main, Structure
  > DURING HMV-4 CHECK AT AAR-ASD WHILE ACCOMPLISHING ALI INSP. 53-11-03, A CRACK WAS FOUND AT LWR INBD HOLE OF THE RT FR20 DOOR STOP FITTING #1 (HOLE #3 AS PER REPAIR DRAWING R531-13118, ISSUE D). ACOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5311-02064. DIP CREA
- [SDR CALA2019012100131](https://openairdocs.org/sdr/CALA2019012100131.md): Door Sill · corroded · Jan 19, 2019 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6105 (A33-015) FWD CARGO BAY ENTRY SILL IS CORRODED. NONROUTINE 9021032 COMPLIED WITH ECRA 5341-01150. REPAIR CONSIDERED PERMENANT. NO F URTHER ACTION REQUIRED FWD CARGO BAY ENTRY SILL.
- [SDR CALA2019011800106](https://openairdocs.org/sdr/CALA2019011800106.md): Door Frame · cracked · Jan 14, 2019 · N426UA · Airbus A320232 · Emergency Exits
  > REMOVED AND REPLACED LT FWD OVER WING EXIT DOOR FWD VERTICAL FR AME AND BEAM DUE TO CRACK IAW SRM 51-72-11-911-001. NON ROUTINE 9021460. LT FWD O/W EXIT DOOR FWD VERTICAL FRAME HAS CRACKS.
- [SDR CALA2019011400092](https://openairdocs.org/sdr/CALA2019011400092.md): Rib · damaged · Jan 13, 2019 · N426UA · Airbus A320232 · Wing, Rib/Bulkhead
  > (A3NB-57-3-6303)A-30-002 RT WING TRACK 5 INBOARD RIB IS DAMAGED AAR NONROUTINE 9021414 REPAIRED RT WING TRACK 5 INBOARD RIB IAW ECRA 5741-01373 REPAIR IS CONSIDERED PERMANENT WITH NO FURTHER ACTION REQUIRED NONROUTINE 9021414.
- [SDR CALA2019011400091](https://openairdocs.org/sdr/CALA2019011400091.md): Threshold · corroded · Jan 13, 2019 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-4-6179 A43-033) AFT CARGO BETWEEN FR52-56, DOOR THRESH OLD PLATE UPPER SURFACE ATTACHED TO TORSION BOX HAS MULTIPLE ARE AS OF CORROSION (M) NONROUTINE 9020987 REMOVED CORROSION, BLENDED AND SMOOTHED IAW SRM 51-75-00-00 1. UT THICKNESS OF BLEND AREAS
- [SDR CALA2019011400099](https://openairdocs.org/sdr/CALA2019011400099.md): Rib · damaged · Jan 13, 2019 · N426UA · Airbus A320232 · Wing, Rib/Bulkhead
  > (A3NB-57-3-6303)A-30-002 RT WING TRACK 5 INBOARD RIB IS DAMAGED NONROUTINE 9021414 REPAIRED RT WING TRACK 5 INBOARD RIB IAW ECRA 5741-01373 REPAIR IS CONSIDERED PERMANENT WITH NO FURTHER ACTION REQUIRED NONROUTINE 9021414.
- [SDR CALA2019011400098](https://openairdocs.org/sdr/CALA2019011400098.md): Threshold · corroded · Jan 13, 2019 · N426UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > (A3NB-53-4-6179 A43-033) AFT CARGO BETWEEN FR52-56, DOOR THRESH OLD PLATE UPPER SURFACE ATTACHED TO TORSION BOX HAS MULTIPLE ARE AS OF CORROSION (M) NONROUTINE 9020987 REMOVED CORROSION, BLENDED AND SMOOTHED IAW SRM 51-75-00-00 1. UT THICKNESS OF BLEND AREAS
- [SDR CALA2019011200063](https://openairdocs.org/sdr/CALA2019011200063.md): Fitting · damaged · Jan 10, 2019 · N426UA · Airbus A320232 · Fuselage Main, Keel
  > SUPPORT TASK (NO DOT L-5) KEELBEAM, LT FWD ACTUATOR FITTING HOLE L10 IS DAMAGED. NONROUTINE 9021034 REMOVED AND REPLACED LT FWD ACTUATOR FITTING ON KEELBEAM IAW SRM 51-72-11-911-001. NONROUTINE 9021034.
- [SDR CALA2019011200062](https://openairdocs.org/sdr/CALA2019011200062.md): Fitting · damaged · Jan 10, 2019 · N426UA · Airbus A320232 · Fuselage Main, Keel
  > (SUPPORT TASK) KEELBEAM, RT AFT REINFORCEMENT FITTING IS DAMAGED. REFER TO N/R: 9021106. LOCATED AND DRILLED NEW RT AFT REINFORCEMENT FITTING IAW SRM 51-72-11-911-001. FITTING INSTALLED ON ROUTINE CARD 4250290, 18-0553-8-0008 SEQ. NO. 1944.
- [SDR CALA2019011200061](https://openairdocs.org/sdr/CALA2019011200061.md): Door Frame · cracked · Jan 9, 2019 · N426UA · Airbus A320232 · Emergency Exits
  > SUPPORT TASK A14-072, LT FWD O/W EXIT DOOR AFT VERTICAL FRAME HAS CRACKS. NONROUTINE 9021462 REMOVED AND REPLACED AFT VERTICAL FRAME AND HORIZONTAL BEAM IN LT FWD EMERGENCY EXIT DOOR IAW SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW SRM 51-75-12 INSPEC

Next page: https://openairdocs.org/aircraft/N426UA/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 = 'N426UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N426UA/reports

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