# Service difficulty reports: N810UA

A list on [N810UA](https://openairdocs.org/aircraft/N810UA.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 · 146 reports

- [SDR CALA2025092309153](https://openairdocs.org/sdr/CALA2025092309153.md): Handle · no discrepancy · Sep 19, 2025 · N810UA · Airbus A319131 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HANDLE NOT FLUSH WHEN CLOSED. INSPECTED DOOR HANDLE, FOUND HANDLE FLUSH WITH SKIN, DOOR IS CLOSED AND LATCHED. CONFIRMED HOOKS ARE LATCHED AND GREEN, ECAM INDICATION IS NORMAL.
- [SDR CALA2025082108014](https://openairdocs.org/sdr/CALA2025082108014.md): Bottle · discharged · Aug 20, 2025 · N810UA · Airbus A319131 · Escape Slide
  > DURING ACTIVATION OF LT OVERWING EXIT DOOR SLIDE, SLIDE DISCHARGED. R & R THE SLIDE ASSY IAW AMM 25-62-42.
- [SDR CALA2025082107997](https://openairdocs.org/sdr/CALA2025082107997.md): Reservoir · discharged · Aug 19, 2025 · N810UA · Airbus A319131 · Escape Slide
  > OVERWING SLIDE INFLATION RESERVOIR DISCHARGED. REMOVED & REPLACED THE LEFT OVERWING SLIDE INFLATION RESEVOIR IAW AMM 25-62-46 & SRM 51-40-02, NO DEFECTS NOTED. REF FAS W/O FS250137, N/R 00028.
- [SDR CALA2025060505281](https://openairdocs.org/sdr/CALA2025060505281.md): Battery · faulted · Jun 3, 2025 · N810UA · Airbus A319131 · Emergency Lighting
  > EMERGANCY LIGHT BATTERY 10WL FAILED OPS CHECK. R&R BATTERY IRW AMM 33-51-38-400-002-A OPS CHECK GOOD.PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2025050704535](https://openairdocs.org/sdr/CALA2025050704535.md): Warning Message · false indication · May 5, 2025 · N810UA · Airbus A319131 · Central Warning
  > AL FL 190 NAV ADR 2 ECAM. PERFORMED ECAM PROCDS. PERFORMED TEST WITH NO ISSUES REF AMM 34-13-00-740-003-A.
- [SDR CALA2025040103369](https://openairdocs.org/sdr/CALA2025040103369.md): Light · inoperative · Mar 31, 2025 · N810UA · Airbus A319131 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY LIGHT AT ROW 31 IS INOP. REPLACED SEAT MOUNTED LIGHT ASSEMBLY REF MM 33-51-19. OPS CHECK OK.
- [SDR CALA2025032803280](https://openairdocs.org/sdr/CALA2025032803280.md): Power Supply · no test · Mar 27, 2025 · N810UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - "PTP SHOWS FAULTS EPSU BATTERY EMER R", "EPSU BATTERY AFT L" REPLACED FWD EPSU 10WL REF AMM 33-51-38. REPLACED BATTERY PACKS IN UNITS 12WL AND 13WL REF AMM 33-51-38. OPC NORMAL.
- [SDR CALA2024020200302](https://openairdocs.org/sdr/CALA2024020200302.md): Seal · damaged · Jan 29, 2024 · N810UA · Airbus A319131 · Landing Gear Doors
  > LOUD AIR HISS HEARD AFTER T.O. IN FLT DECK. ATALT HISS FLX WIT F LX INOUTFL VLV AND CAB VS. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. DEBRIEFED CAPT. AND F/O. CAPT. REPORTS WHISTLING SOUND UNDER FLIGHT DECK WH
- [SDR CALA2024011900139](https://openairdocs.org/sdr/CALA2024011900139.md): Frame · cracked · Jan 14, 2024 · N810UA · Airbus A319131 · Fuselage Main, Frame
  > RH DOUBLE JOGGLE HOLES #6 AND "C" HAVE CRACK INDICATIONS IN THE HOLE #6 INDICATION AT 3:OCLOCK. HOLE "C" AT 9:OCLOCK PER HAECO L CQ NON ROUTINE 9292380/28380 REQUIRES DIP TO ACCOMPLISH INITIAL INSP OF THE RH FR16 UPPER DB CRA 5311-03141 ON OR BEFORE THE ACFT
- [SDR CALA2024011900145](https://openairdocs.org/sdr/CALA2024011900145.md): Track · cracked · Jan 6, 2024 · N810UA · Airbus A319131 · Fuselage Main, Structure
  > AD RELATED SUPPORT TASK (AD 2023-06-08): AFT CARGO TRACK HOLE AT FR58 STR34L HAS CRACK INDICATION AT 6 AND 12 O?CLOCK POSITIONS. REPAIR BEFORE FURTHER FLIGHT. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS PER STEP 12. 5340-01430 ON OR BEFORE THE AC REACHES 71418
- [SDR CALA2023100302929](https://openairdocs.org/sdr/CALA2023100302929.md): Fuel Cap · missing · Sep 30, 2023 · N810UA · Airbus A319131 · Aircraft Fuel Distribution System
  > FUELER REPORTS FUEL CAP MISSING PIC OF ATTACH POINT REQUEST CDL 28A FUEL CAP MISSING MX ACTION COMPLIED WITH. NO LEAKS AT THIS TIME. DISPATCH DESK: 24 NAME: JS DATE: 29-SEP-23- APPROVED CDL FOR FUEL CAP MISSING. CAP REPLACED IN REFERENCE WITH AIRBUS AMM 28-25-
- [SDR CALA2023042801264](https://openairdocs.org/sdr/CALA2023042801264.md): Fitting · leaking · Apr 27, 2023 · N810UA · Airbus A319131 · Landing Gear Doors
  > DURING INSP FOR HYD LEAK & CLEANUP, FOUND RT MLG DOOR FWD HINGE BOLT BEARING VERY LOOSE & WORN. RH MLG DOOR WILL REQUIRE REPLACEMENT OF FWD HINGE ASSY PER IPC 52-81-145-15 ITEM 180. MILL HEAD IS TRAMED IN ZERO AT FULL QUIL EXTENSION BUSHINGS ON MLG DOOR HINDGE
- [SDR CALA2023042601246](https://openairdocs.org/sdr/CALA2023042601246.md): Keelbeam · chafed · Apr 24, 2023 · N810UA · Airbus A319131 · Fuselage Main, Keel
  > RH MLG DOOR KEEL BEAM FITTING REF SRM 53-36-16-A ITM 140-A HAS WORN AREA FROM CHAFING WITH MLG RH DOOR. REMOVED FITTING REF SRM 53-36-16-A ITM 140-A AT RH MLG DOOR FWD ATTACH POINT. REF LOG 4380418 FOR R&R OF FITTING PER REPAIR INSTRUCTIONS R533 07500 F
- [SDR CALA2023031000685](https://openairdocs.org/sdr/CALA2023031000685.md): Compressor · stalled · Mar 10, 2023 · N810UA · Airbus A319131 · Turbine Engine Compressor Section
  > COMPRESSOR STALL NUMBER2 RETRN TO FIELDENGINE WAS NOT SHUT DOW ACCOMPLISH COMPLETE TROUBLESHOOTING OF SURGE OR STALL ON ENGINE 2 PER TSM 71-00-00-810-809-A. MAINTENANCE CONTROL FOR EVALUATION. PERFORMED BOROSCOPE INSPECTION ON NUMBER 2 ENGINE COMPRESSOR SECTIO
- [SDR CALA2022111703170](https://openairdocs.org/sdr/CALA2022111703170.md): Fuel Cap · missing · Nov 17, 2022 · N810UA · Airbus A319131 · Fuel Storage
  > MISSING FUEL CAP RIGHT WING NO VISIBLE OR REPORTED FUEL LEAK. NO LEAKS OR DAMAGE. INSTALLED MISSING FUEL CAP.
- [SDR CALA2022082402170](https://openairdocs.org/sdr/CALA2022082402170.md): Servicing Valve · leaking · Aug 22, 2022 · N810UA · Airbus A319131 · Waste Disposal System
  > FUSELAGE BELLY DRAIN LEAKING BLUE WATER JUST UNDER AFT CARGO COMPARTMENT UNDER CARGO DOOR ENTRANCE 2011-01000 LAVATORY SPILL, SECTION 2B FROM WASTE TANK TO AFT CARGO DOOR, WITH-IN 7 DAYS. FOUND TANK BLUE WATER SEVICING LINE LEAKING, SECURED LINE BNUT, NO MORE
- [SDR CALA2022041400980](https://openairdocs.org/sdr/CALA2022041400980.md): Fitting · cracked · Apr 13, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTE D ON AFT LOWER HOLE. INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5321-02067 REF VT MAE NR0024388. EXTERNAL ANGLE FITTING BEFORE AC4010 REACHES 61391TFC / 132942TF ECRA 5321-02067 H WHICHEVER OCCURS
- [SDR CALA2022041400976](https://openairdocs.org/sdr/CALA2022041400976.md): Bulkhead · cracked · Apr 12, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > (SDR) RH FR16: DURING ROTO INSP OF RH FR16 DOUBLE JOGGLE, CRACK INDICATION WAS NOTED IN HOLES #B, #C, AND #D. V934344. ACCOMPLISH INITIAL INSPECTION OF FR16 LHS HOLES #C AND BEFORE THE AIRCRAFT REACHES 37,691 TOTAL AIRCRAFT FLIGHT 4,700 FLIGHT CYCLES THEREAFTE
- [SDR CALA2022041100945](https://openairdocs.org/sdr/CALA2022041100945.md): Fitting · damaged · Apr 9, 2022 · N810UA · Airbus A319131 · Fuselage Main, Structure
  > REF LP 8282032 PLANNING TO CONTACT ENGINEERING BEFORE AC4010 REA CHES 60391TFC / 130942TFH WHICHEVER OCCURS FIRST PER STEP 37 OF ECRA 5321-02067 LATEST REV OF ECRA 5321-02067 INTERIM REPAIR ACCOMPLISHED PER ECRA 5321-02067 PART 1. PLANNING TO CONTACT ENGINEERI
- [SDR CALA2022040800919](https://openairdocs.org/sdr/CALA2022040800919.md): Frame · corroded · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Main, Frame
  > (A3NB-53-3-6299) FRAME 68 INBD FLANGE HAS CORROSION JUST ABOVE F LOOR LEVEL. (DOT 74-26 MARKED) () OF THE LATEST REV OF ECRA 5341-01305 ON OR BEFORE ACFT REACHES THERAFTER 47291TFC. PERFORM REPEAT INSP AT INTERVALS NOT TO EXCEED 16400FC ACCOMPLISHED INTERIM RE
- [SDR CALA2022040800918](https://openairdocs.org/sdr/CALA2022040800918.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR16 HOLES H1, H3, H8. HOLES H1 AND H3-H16 AT FR 16 LHS ON OR BEFORE A/C 4010 REACHES REVISION OF EC 5310-07992. 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.
- [SDR CALA2022040800917](https://openairdocs.org/sdr/CALA2022040800917.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR16 HOLE H2. H2 AT FR 16 LHS ON OR BEFORE A/C 4010 REACHES 79,391 TOTAL ECRA 5310-07992. AIRCRAFT FLIGHT CYCLES PER PART 2.5 OF THE LATEST REVISION OF PERFORMED
- [SDR CALA2022040800916](https://openairdocs.org/sdr/CALA2022040800916.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR20: H17, H18, H19, H26. HOLES H 17-H36 AT FR 20 LHS ON OR BEFORE A/C 4010 REACHES REVISION OF ECRA 5310-07992. 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.
- [SDR CALA2022040800915](https://openairdocs.org/sdr/CALA2022040800915.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR20 HOLES H17, H18, H19, H26. INSPECT HOLES H17-H36 AT FR 20 RHS ON OR BEFORE A/C 4010 REVISION OF ECRA 5310-07992. REACHES 118,591 TOTAL AIRCRAFT FLIGHT PER PA
- [SDR CALA2022040800913](https://openairdocs.org/sdr/CALA2022040800913.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR16 HOLES H1, H2, H3. HOLES H1-H7 AND H9-H16 AT FR 16 RHS ON OR BEFORE A/C 4010 REACHES 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.4 OF THE REACHES 118,591
- [SDR CALA2022040800912](https://openairdocs.org/sdr/CALA2022040800912.md): Beam · misrepaired · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR16 HOLE H8. H8 AT FR 16 RHS ON OR BEFORE A/C 4010 REACHES 79,391 TOTAL ECRA 5310-07992. AIRCRAFT FLIGHT CYCLES PER PART 2.3 OF THE LATEST REVISION OF PERFORMED
- [SDR CALA2022040600904](https://openairdocs.org/sdr/CALA2022040600904.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR16 HOLES H1, H2, H3. HOLES H1-H7 AND H9-H16 AT FR 16 RHS ON OR BEFORE A/C 4010 REACHES 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.4 OF THE REACHES 118,591
- [SDR CALA2022040600903](https://openairdocs.org/sdr/CALA2022040600903.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR16 HOLE H2. H2 AT FR 16 LHS ON OR BEFORE A/C 4010 REACHES 79,391 TOTAL ECRA 5310-07992. AIRCRAFT FLIGHT CYCLES PER PART 2.5 OF THE LATEST REVISION OF PERFORMED
- [SDR CALA2022040600902](https://openairdocs.org/sdr/CALA2022040600902.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR16 HOLE H8. H8 AT FR 16 RHS ON OR BEFORE A/C 4010 REACHES 79,391 TOTAL ECRA 5310-07992. AIRCRAFT FLIGHT CYCLES PER PART 2.3 OF THE LATEST REVISION OF PERFORMED
- [SDR CALA2022040600901](https://openairdocs.org/sdr/CALA2022040600901.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR20: H17, H18, H19, H26. HOLES H 17-H36 AT FR 20 LHS ON OR BEFORE A/C 4010 REACHES REVISION OF ECRA 5310-07992. 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.
- [SDR CALA2022040600900](https://openairdocs.org/sdr/CALA2022040600900.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON RHS FR20 HOLES H17, H18, H19, H26. INSPECT HOLES H17-H36 AT FR 20 RHS ON OR BEFORE A/C 4010 REVISION OF ECRA 5310-07992. REACHES 118,591 TOTAL AIRCRAFT FLIGHT PER PA
- [SDR CALA2022040600899](https://openairdocs.org/sdr/CALA2022040600899.md): None · none · Apr 6, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING HMV-4 CHECK AT VT MAE, PRODUCTION REPORTED EXISTING REPAIR WITH NO RECORD OF REPAIRS ON LHS FR16 HOLES H1, H3, H8. HOLES H1 AND H3-H16 AT FR 16 LHS ON OR BEFORE A/C 4010 REACHES REVISION OF EC 5310-07992. 118,591 TOTAL AIRCRAFT FLIGHT CYCLES PER PART 2.
- [SDR CALA2022040400859](https://openairdocs.org/sdr/CALA2022040400859.md): None · cracked · Apr 4, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > (SDR) RH FR16: DURING ROTO INSP OF RH FR16 DOUBLE JOGGLE, CRACK INDICATION WAS NOTED IN HOLES #B, #C, AND #D. V934344. ACCOMPLISH INITIAL INSPECTION OF FR16 LHS HOLES #C AND BEFORE THE AIRCRAFT REACHES 37,691 TOTAL AIRCRAFT FLIGHT 4,700 FLIGHT CYCLES THEREAFTE
- [SDR CALA2022033100858](https://openairdocs.org/sdr/CALA2022033100858.md): Floorbeam · corroded · Mar 31, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON LH SIDE FLOOR SUPPORT BEAM Y-765 BETWEEN FR67-FR68 REMOVED CORROSION ON BEAM Y765 FR67-68 IN CABIN FLOOR IAW SRM 51 STA: ST ENG BFM SFR# 1028160 -74-00 BLENDED AREA MEASURES L=2.5" W=1" DEPTH=0.080" FOUND OUT OF LIMITS IAW SRM 53-00-14-283-002 FIG
- [SDR CALA2022033100857](https://openairdocs.org/sdr/CALA2022033100857.md): Floorbeam · corroded · Mar 31, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-1292 BETWEEN FR65-FR66 CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-1292 BTWN FR65-66 REMO LOCATED AND DRILLED IAW SRM 51-44-11 INSTALLED RH SIDE SUPPORT B VED IAW SRM 51-74-00, FOUND OUT OF LIMITS IAW SRM 53-00-14-283-0
- [SDR CALA2022033100856](https://openairdocs.org/sdr/CALA2022033100856.md): Fitting · corroded · Mar 31, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON R2 DOOR CUTOUT LOWER FWD CORNER FITTING AFT OF FR66 RECEIVED NEW CORNER FITTING AFT FR60 PN D5348004220501 (OUT OF S EQUENCE ENTRY) REMOVED DAMAGE FITTING IAW SRM 51-42-11. INSTALLE D NEW CORNER FITTING IAW SRM 51-42-11. EMP: V934718 WC: 0024194 S
- [SDR CALA2022033100855](https://openairdocs.org/sdr/CALA2022033100855.md): Floorbeam · corroded · Mar 31, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-765 HAS CORROSION BETW EEN FR67-FR68 REMOVED CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-765 BTW FR67-6 (CALIPER T91558, DEPTH GAUGE T93985) REMOVED AND REPLACED FLOOR 8 IAW SRM 51-74-00. BLEND OUT FOUND OUT OF LIMITS IA
- [SDR CALA2022033100850](https://openairdocs.org/sdr/CALA2022033100850.md): None · damaged · Mar 31, 2022 · N810UA · Airbus A319131 · Long-Range Navigation (LORAN) System
  > (A3NB-53-4-6134) ADF 1 COVER PLATE HAS 2 EA SCREWS NEED REMOVED (REPAIR AS REQUIRED). 2EA SCREWS DAMAGED ON ADF1 COVER PLATE WERE REMOVED AND AFTER IN VESTIGATION STRINGER CORROSION WAS FOUND, THIS WAS REMOVED AND R EPLACED IAW SRM 51-42-11/001, 51-72-11-911-0
- [SDR CALA2022033100849](https://openairdocs.org/sdr/CALA2022033100849.md): None · none · Mar 30, 2022 · N810UA · Airbus A319131 · Doors
  > (SFR) FOUND CRACK ON RH EMERGENCY EXIT DOOR INTERIOR FRAME P/N: D5227902620200 REMOVED FRAME (SEGMENT ANGLE) THE EMERGENCY EXIT DOOR AND INSTAL LED NEW SEGMENT ANGLE IAW SRM 51-72-11. EMP: V933870 WC: 0024111 STA: ST ENG BFM
- [SDR CALA2022033100848](https://openairdocs.org/sdr/CALA2022033100848.md): None · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6299) FRAME 68 INBD FLANGE HAS CORROSION JUST ABOVE F LOOR LEVEL. (DOT 74-26 MARKED) () OF THE LATEST REV OF ECRA 5341-01305 ON OR BEFORE ACFT REACHES THERAFTER 47291TFC. PERFORM REPEAT INSP AT INTERVALS NOT TO EXCEED 16400FC ACCOMPLISHED INTERIM RE
- [SDR CALA2022033100847](https://openairdocs.org/sdr/CALA2022033100847.md): Frame · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTE D ON AFT LOWER HOLE. INTERIM REPAIR WAS ACCOMPLISHED PER ECRA 5321-02067 REF VT MAE NR0024388. EXTERNAL ANGLE FITTING BEFORE AC4010 REACHES 61391TFC / 132942TF ECRA 5321-02067 H WHICHEVER OCCURS
- [SDR CALA2022033100846](https://openairdocs.org/sdr/CALA2022033100846.md): Frame · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING ROTO INSP OF "RH" FR35 STGR30 A CRACK INDICATION WAS NOTED ON AFT LOWER HOLE #2RH FR35 STGR30 DIP CREATED PER STEP 36 OF ECRA 5321-02067 REF VT MAE NR0024389 132942TFH WHICHEVER OCCURS FIRST PER PART 2.1 OF THE LATEST RE OF ECRA 5321-02067 INTERIM REPAI
- [SDR CALA2022033100845](https://openairdocs.org/sdr/CALA2022033100845.md): Frame · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > DURING ROTO INSP OF "LH" FR35 STGR30 A CRACK INDICATION WAS NOTED ON HOLE #2LHS FR35 STGR30 "AFT SKIN". DIP CREATED PER STEP 41 OF ECRA 5321-02067 REACHES 44091TFC / 98342TFH WHICHEVER OCCURS FIRST PER PART 2.4 IN INTERVALS OF 8800FC / 17200FH WHICHEVER OCCURS
- [SDR CALA2022033100830](https://openairdocs.org/sdr/CALA2022033100830.md): Beam · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-765 HAS CORROSION BETW EEN FR67-FR68
- [SDR CALA2022033100831](https://openairdocs.org/sdr/CALA2022033100831.md): Beam · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON LH SIDE FLOOR SUPPORT BEAM Y-765 BETWEEN FR67-FR68
- [SDR CALA2022033100829](https://openairdocs.org/sdr/CALA2022033100829.md): Fitting · none · Mar 30, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON R2 DOOR CUTOUT LOWER FWD CORNER FITTING AFT OF FR66
- [SDR CALA2022033100827](https://openairdocs.org/sdr/CALA2022033100827.md): Beam · none · Mar 29, 2022 · N810UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON RH SIDE FLOOR SUPPORT BEAM Y-1292 BETWEEN FR65-FR66
- [SDR CALA2022032800799](https://openairdocs.org/sdr/CALA2022032800799.md): Cover · not reported · Mar 26, 2022 · N810UA · Airbus A319131 · Fuselage Structure (General)
  > (A3NB-53-4-6134) ADF 1 COVER PLATE HAS 2 EA SCREWS NEED REMOVED (REPAIR AS REQUIRED).
- [SDR CALA2022032800798](https://openairdocs.org/sdr/CALA2022032800798.md): Door Frame · cracked · Mar 26, 2022 · N810UA · Airbus A319131 · Doors
  > (SFR) FOUND 2 CRACKS ON RH EMERGENCY EXIT DOOR INTERIOR FRAME P/ N: D5227902620300
- [SDR CALA2022032800795](https://openairdocs.org/sdr/CALA2022032800795.md): Door Frame · cracked · Mar 25, 2022 · N810UA · Airbus A319131 · Fuselage Main, Structure
  > (SFR) FOUND CRACK ON RH EMERGENCY EXIT DOOR INTERIOR FRAME P/N: D5227902620200

Next page: https://openairdocs.org/aircraft/N810UA/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 = 'N810UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N810UA/reports

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