# Service difficulty reports: N819UA

A list on [N819UA](https://openairdocs.org/aircraft/N819UA.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 · 131 reports

- [SDR CALA2026092119626](https://openairdocs.org/sdr/CALA2026092119626.md): Frame · corroded · Sep 18, 2026 · N819UA · Airbus A319131 · Fuselage Main, Frame
  > AFT CARGO FR 59 HAD CORROSION AT FASTENER HOLES. PERFORMED PERMANENT A REPAIR AT FR 59 IAW EC/RA 5341-01583.
- [SDR CALA2026081418638](https://openairdocs.org/sdr/CALA2026081418638.md): Cover · faulted · Aug 12, 2026 · N819UA · Airbus A319131 · Escape Slide
  > L1 DOOR SPRING LATCH BROKEN ON TOP ESCAPE SLIDE COVER LATCH PINS BROKEN. COVER REMAINS SECURED OVER THE ESCAPE SLIDE. CONFIRMED SPRING-LOADED BOLT IS IN THE LOCKED POSITION. BOLT CANNOT SLIDE UNLESS ACTUATED WITH A PIN OR EQUIVALENT TOOL. COMPLIED WITH EC/RA
- [SDR CALA2025092209104](https://openairdocs.org/sdr/CALA2025092209104.md): Engine · making metal · Sep 19, 2025 · N819UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > ENG 1 STALL CREW REPORTED TO LOCAL MAINTENANCE THAT THE ENG-1 STALLED 3 TIMES IN CRUISE ENGINE RECOVERED AND FLIGHT CREW KEPT IT AT IDLE ALL THE WAY DOWN. #1 ENG HPC UPPER BLEED VALVE HAS METAL SHARDS IN THE SCREEN AND METAL INSIDE THE VALVE. REF JOB TASK CARD
- [SDR CALA2025081407741](https://openairdocs.org/sdr/CALA2025081407741.md): Skin · punctured · Aug 13, 2025 · N819UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS HOLE ON UPPER SURFACE. REPAIRED LEFT ELEVATOR ON UPPER SURFACE IAW SRM 55-21-11-30 0-004. SANDWICH STRUCTURE AREA NEW STRUCTURAL REPAIR (DAMAGES LESS THAN 1000MNF (1.55IN)) CATEGORY A REPAIR ALL MAINTENANCE REPAIRS RII AND CIR REQUIREMENTS A
- [SDR CALA2025072506916](https://openairdocs.org/sdr/CALA2025072506916.md): Elec Connector · detached · Jul 21, 2025 · N819UA · Airbus A319131 · Light System Wiring
  > CONNECTOR FOR EMERGENCY LIGHTING PATHWAY ILLUMINATION DETACHED. PIC ATTACHED VERIFIED ALL ADJACENT EMERGENCY LIGHT FUNCTION AS NORMAL. CAPPED AND SECURED WIRING POSES NO HAZARD TO PAX. COMPLIED WITH MEL 3350C PIC ATTACHED OK TO APPLY MEL 3350C FOR INOP FLOOR P
- [SDR CALA2025062305783](https://openairdocs.org/sdr/CALA2025062305783.md): Hydraulic Line · leaking · Jun 19, 2025 · N819UA · Airbus A319131 · Hydraulic System, Main
  > GREEN RSVR PRESS LOLOOS OF GREEN SYSTEM. HYDRALIC LEAK FOUND ON HYDRALIC LINE FROM T/R SHUTOFF VALVE TO T UNION IN PYLON IPC 29-11-06-02L ITEM 260 SDR FLAGGED CONFIRMED HYDRALIC LEAK ON HYDRALIC LINE FROM T/R SHUTOFF VALVE TO T UNION IN PYLON IPC 29-11-06-02L
- [SDR CALA2025030502601](https://openairdocs.org/sdr/CALA2025030502601.md): Power Supply · failed · Mar 3, 2025 · N819UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - TEST HAS FAULTS EPSU EMER R, EPSU BATT EMER L, EPSU BATT AFT L, AND EPSU UNIT FWD L. NEEDS PWR. SUPPLY AND 4 FRESH BATTERIES. FWD. L / H POWER SUPPLY. P / N ON 3214-54-10., M & E 31-3350-9-9001
- [SDR CALA2025031900489](https://openairdocs.org/sdr/CALA2025031900489.md): Control Servo · damaged · Feb 27, 2025 · N819UA · Airbus A319131 · Aileron Control System
  > FOUND RH INBOARD AILERON SERVO CONTROL ROD UNABLE TO FULLY RETRACT. INSPECTED ATTACH POINTS, HARDWARE AND VERIFIED NEW SERVO CONTROL SN# 5430 EFFECTIVE FOR AC AND POSITION 33CE2 "RH INBOARD" PER RII 09-25-05 REMOVED RIGHT INBOARD AILERON SERVO CONTROL ACTUATOR
- [SDR CALA2024122601660](https://openairdocs.org/sdr/CALA2024122601660.md): Skin · damaged · Dec 24, 2024 · N819UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > MULTIPLE BIRD STRIKE ON TO. ACCOMPLISHED BIRD STRIKE INSPECTION PER AMM 05-51-14 FOUND 1 STRIKE BELOW RADOME NO DAMAGE, ONE STRIKE TO ENG 1 INLET LIP NO DAMAGE AND ONE STIKE TO ENG 1 SPINNER NO DAMAGE AND NO BIRD REMAINS DOWN CORE OK TO CONTINUE ACCOMPLISHE
- [SDR CALA2024112901356](https://openairdocs.org/sdr/CALA2024112901356.md): Unknown · noise · Nov 27, 2024 · N819UA · Airbus A319131 · Standard Practices/Structures
  > LOUD FLT DECK WHISTLE STARTED ABOUT 3HRSINTO FLT. SOUND NOTPRSNT IN CABIN. INBD CREW STATED NOISE COMING FROM AIR VENTS, 15 MINUTES TOTAL, 3 HOURS INTO FLIGHT AND WENT AWAY 15 MINUTES PRIOR TO DESCENT. RAN PACKS FOR 40 OR MORE MINUTES, RAN 1 PACK AT A TIME AND
- [SDR CALA2024052901624](https://openairdocs.org/sdr/CALA2024052901624.md): Connector · corroded · May 27, 2024 · N819UA · Airbus A319131 · Landing Gear System Wiring
  > LANDING GEAR SYS DISAGREE INFO FROM FLIGHT CREW: STILL FELT RUMBLING FROM GEAR AND GEAR DOORS STAYING OPEN AFTER MOVING GEAR HANDLE TO UP POSITION. FLIGHT CREW ASSUMED GEAR STAYED DOWN. UPDATED SDR REQUIRED. UPDATE MANHOURS... T/S IN REF TO TSM 32-31-00-810-81
- [SDR CALA2023112003441](https://openairdocs.org/sdr/CALA2023112003441.md): Crossbeam · damaged · Nov 16, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH FR 20 CROSSBEAM AREA HOLES H27, H33, H34, H35 HAVE OUT OF ROUND INDICATION. INITIAL INSP OF LH FR20 CROSSBEAM SPLICE HOLES H27, H33, H34, THE ACFT REACHES 120,624 TOTAL FC PER ECRA 5311-03108 PART H35 PER PART 2 OF THE LATEST REV OF ECRA 5311-03108 ON OR BE
- [SDR CALA2023111703407](https://openairdocs.org/sdr/CALA2023111703407.md): Crossbeam · cracked · Nov 14, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > RH FR20 CROSSBEAM AREA HOLE H26 HAS CRACK INDICATION IN BOTH SKIN LAYER, HOLES H27, H28, H30, H34 AND H35 HAVE OUT OF ROUND INDICATION AT CROSSBEAM LAYER. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5311-03109 ALL SUBSEQUENT ARE CAPTURED ON LP 6303821. INSPECTION REQ
- [SDR CALA2023111503385](https://openairdocs.org/sdr/CALA2023111503385.md): Stringer · corroded · Nov 14, 2023 · N819UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, UNDERFLOOR COMPARTMENT, FR65-66 R/H STR 26, UPPER FWD CORNER OF OUTFLOW VALVE, EXFOLIATION CORROSION PER NR9296331/40 331. REMOVED STR26 FR64 TO FR67 RH IAW SRM 51-42-11/001. INSTALLED ST EC/RA 5341-01419 CATEGORY A REPAIR IAW SRM 51-42-11/001 AND
- [SDR CALA2023111503371](https://openairdocs.org/sdr/CALA2023111503371.md): Floor Panel · corroded · Nov 13, 2023 · N819UA · Airbus A319131 · Fuselage Floor Panel
  > CABIN UNDERFLOOR, FLOOR PANEL 242HF, FR, 41-42 O/B Y-1292 FASTENER HEAD WITH PITTING AROUND IT IN PRESSURE FLOOR PER HAECO LCQ N ON ROUTINE 9296338/40338. ACCOMPLISHED REPAIR AT CABIN UNDER FLOOR PANEL 242 HF FH 41-42 O/B OF Y1292 PRESSURE FLOOR IAW REO-L2469
- [SDR CALA2023111503382](https://openairdocs.org/sdr/CALA2023111503382.md): Stringer Splice · corroded · Nov 12, 2023 · N819UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > STRING SPLICE AT FR66, STR26R, HAS CORROSION A3NB-53-3-6185 PER HAECO LCQ NON ROUTINE 9296784/40784. FOUND STRINGER SPLICE TO BE OUT OF LIMITS IAW SRM 51-71-11 MAX L AND SRM 51-72-11-911-001 AT FR66 STR26R. RESTORED SURFACE PROTEC OSS.086" REMAINING.010" MA
- [SDR CALA2023111503354](https://openairdocs.org/sdr/CALA2023111503354.md): Doubler · gouged · Nov 10, 2023 · N819UA · Airbus A319131 · Aerodynamic Fairings
  > UPON REMOVAL OF BELLY FAIRING AT FR 34, PREVIOUS REPAIR DOUBLER IS GOUGED FROM PANEL. GENERATED BY N078625 PER HAECO LCQ NR 9296 775/40775 REMOVED AND REPLACED REPAIR DOUBLER AT FR 34 IAW A319 EC/RA# 533 1-02275 REV IR. ACMP BY V925324 INSP BY V892285
- [SDR CALA2023111503367](https://openairdocs.org/sdr/CALA2023111503367.md): Stringer · corroded · Nov 9, 2023 · N819UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPARTMENT STRINGER 42R HAS CORROSION FR30-34 PER HAECO LCQ NON ROUTINE 9296845/40845. FC/120,000 FH IAW SRM 53-21-13-205-019 TAB 1 PERFORMED REPAIR AT FWD CARGO COMP STR 42R FROM FR 27-34 IAW SRM 53-21-13-300-18.
- [SDR CALA2023111503376](https://openairdocs.org/sdr/CALA2023111503376.md): Skin · cracked · Nov 8, 2023 · N819UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > L/H FR35 STR30 HOLE #2 CRACKED IN AFT SKIN LAYER AT THE 5 O''CLOC K POSITION A3NB-53-3-6315 PER HAECO LCQ NON ROUTINE 9296122/4012 2 GENERATED BY V061632 INTERIM REPAIR WAS COMPLETED IAW ECRA 5330-07105 PART 1. INSPECTION REQUIREMENTS OF ECRA 5330-07105 PART 2
- [SDR CALA2023111503369](https://openairdocs.org/sdr/CALA2023111503369.md): Stringer · cracked · Nov 8, 2023 · N819UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > R/H FRAME 68 STR.22 HAS A CRACK ABOUT 1 INCH IN LENGTH PER HAECO LCQ NON ROUTINE 9296154/40154. ACCOMPLISH A PERMANENT REPAIR AT FR68 STGR22RH FRAME INNER 5341-01418 ON OR BEFORE 03MAY24. WEB/STIFFENER PER PART 3 OF THE LASTEST REVISOIN OF ECRA PERFROMED REP
- [SDR CALA2023111703421](https://openairdocs.org/sdr/CALA2023111703421.md): Crossbeam · cracked · Nov 6, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > RH FR 16 CROSSBEAM AREA, HOLE H8 HAS CRACK INDICATION IN CROSSBE AM LAYER. AD 2018-14-09 PER HAECO LCQ NON ROUTINE 9296495/40495 ACCOMPLISHED INTERIM REPAIR IAW ECRA 5311-03106 PART 1. INSPECTION REQUIREMENTS OF ECRA 5311-03106 ARE CAPTURED ON LP 6304222. NOT
- [SDR CALA2023111503356](https://openairdocs.org/sdr/CALA2023111503356.md): Crossbeam · cracked · Nov 6, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH FR 16 CROSSBEAM AREA, HOLE H1 AND H3 HAS CRACK INDICATION IN CROSSBEAM LAYER. AD 2018-14-09 PER HAECO LCQ NON ROUTINE 9296492 /40492 GENERATED BY V892444 PART 2 OF THE LATEST REVISION OF ECRA 5311-03105 ON OR BEFORE AIRCRAFT REACHES 120624 TOTAL AIRCRAFT FL
- [SDR CALA2023110803316](https://openairdocs.org/sdr/CALA2023110803316.md): Doubler · corroded · Nov 4, 2023 · N819UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FWD CARGO FR 30-34 STR 43-43 CORROSION ON DOUBLER AROUND FASTENER HEADS (A3NB-53-3-6105) GENERATED AT HAECO LCQ PER NR 9296612 ( 40612) REMOVED AND REPLACED DOUBLER FWD CARGO FR30-34 STR 43R-44 IAW A 319 SRM 51-42-11 RESTORED SURFACE PROTECTION IAW A319 SRM
- [SDR CALA2023110803311](https://openairdocs.org/sdr/CALA2023110803311.md): Crossbeam · damaged · Nov 4, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH FR 16 CROSSBEAM AREA, HOLE H10, H11 AND H16 HAS OUT OF ROUND IN CROSSBEAM LAYER. "REPAIR BEFORE NEXT FLIGHT" (AD RELATED SUPP ORT TASK) (AD 2018-14-09) GENERATED AT HAECO LCQ PER NR 9296493 (40493
- [SDR CALA2023110603289](https://openairdocs.org/sdr/CALA2023110603289.md): Beam · cracked · Nov 4, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH FR 16 CROSSBEAM AREA, HOLE H1 AND H3 HAS CRACK INDICATION IN CROSSBEAM LAYER. (AD RELATED, SUPPORT TASK) (AD 2018-14-09) GENE RATED AT HAECO LCQ PER NR 9296492 REAMED HOLE H1 TO FINAL DIAMETER OF 0.2170" AND HOLE H3 TO A FIN LOGPAGE TO READ AS FOLLOWS, ACCO
- [SDR CALA2023103103253](https://openairdocs.org/sdr/CALA2023103103253.md): Door Frame · cracked · Oct 30, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH OW EMERGENCY HATCH AFT FRAME SEGMENT IS CRACKED PER NR9296310 /40310 REMOVED AND REPLACED L/H O/W EMERGENCY HATCH AFT FRAME SEGMENT IAW A319 SRM 51-72-11.
- [SDR CALA2023103103251](https://openairdocs.org/sdr/CALA2023103103251.md): Door Frame · cracked · Oct 30, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > LH OW EMERGENCY HATCH FWD FRAME SEGMENT ARE CRACKED PER NR 92962 39/40239 REMOVED AND REPLACED L/H O/W EMERGENCY HATCH FWD FRAME SEGMENT I AW A319 SRM 51-72-11.
- [SDR CALA2023103103249](https://openairdocs.org/sdr/CALA2023103103249.md): Door Frame · cracked · Oct 30, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > RH OW EMERGENCY HATCH AFT FRAME SEGMENT IS CRACKED PER NR9296311 / 40311 GEN BY N078625 REMOVED AND REPLACED R/H O/W EMERGENCY HATCH AFT FRAME SEGMENT I AW A319 SRM 51-72-11. PERFORMED BY V039746 AND INSP BY V077960
- [SDR CALA2023103103247](https://openairdocs.org/sdr/CALA2023103103247.md): Door Frame · cracked · Oct 30, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > RH OW EMERGENCY HATCH FWD FRAME SEGMENT ARE CRACKED PER NR 92962 40 / 40240 GEN BY N078625 REMOVED AND REPLACED R/H O/W EMERGENCY HATCH FWD FRAME SEGMENT I AW A319 SRM 51-72-11. PERFORMED BY V039746 AND INSP BY V077960
- [SDR CALA2023103003224](https://openairdocs.org/sdr/CALA2023103003224.md): Threshold · corroded · Oct 29, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT DOOR THRESHOLD UPPER SURFACE AND FASTENERS HAS CORROSION GEN BY V061771 ON HAECO LCQ NR9296629/40629 BLENDED CORROSION FOUND TO EXCEED MAX ALLOWED LENGTH IAW A319 SR SRM 51-23-11/001 ON AFT CARGO COMPARTMENT M 53-41-49-283-003 OUT OF LIMI
- [SDR CALA2023110303263](https://openairdocs.org/sdr/CALA2023110303263.md): Cleat · corroded · Oct 28, 2023 · N819UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD PIT CLEAT CORRODED AT FR28 STR 44L-44R. REMOVED AND REPLACED FWD PIT CLEAT AT FR28 STR 43R TO 43L IAW A3 19 SRM 51-72-11 REMOVED DOT NP16 PER MECH V943896 INSP V061704
- [SDR CALA2023102703206](https://openairdocs.org/sdr/CALA2023102703206.md): Stringer · corroded · Oct 26, 2023 · N819UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT PIT FRAME 59 RT STRINGER 38RT HAS CORROSION. GENERATED BY V052030 PER NR 9296733 (40733) AT HAECO LCQ. REMOVED AND REPLACED AFT PIT FR59 STR 38RH IAW A319 SRM 51-72-11 PAR. 2. ACMP BY V925324 INSP BY V061704
- [SDR CALA2023102503184](https://openairdocs.org/sdr/CALA2023102503184.md): Hinge · cracked · Oct 24, 2023 · N819UA · Airbus A319131 · Fuselage, Door Hinge
  > LMLG DOOR FWD HINGE PRODUCED A CRACK INDICATION DURING THE HFEC INSPECTION. INDICATION FOUND AT AFT FACE OF LMLG DOOR FWD HINGE PER NR 9296211 / 40211 RMVD AND RPLD LMLG DOOR FWD HINGE IAW SRM 51-72-11
- [SDR CALA2023102503186](https://openairdocs.org/sdr/CALA2023102503186.md): Fitting · corroded · Oct 20, 2023 · N819UA · Airbus A319131 · Fuselage Main, Structure
  > L2 DOOR FRAME AFT CORNER FITTING HAS CORROSION. RMVD AND RPLD AFT CORNER FITTING FR68 LH L2 DOOR IAW SRM 51-42-1 1, 53-41-79-02-A, 51-44-11/001 AND 51-72-11-911-001
- [SDR CALA2023102503180](https://openairdocs.org/sdr/CALA2023102503180.md): Door Sill · corroded · Oct 20, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L-2 DOOR SILL AT FR68 HAS CORROSION. GEN BY N078625 ON HAECO LCQ NR 9296218/40218 RMVD AND RPLD L2 DOOR SILL BETWEEN FR66-68 IAW SRM 51-72-11-911- 001, 51-42-11/001, 51-75-12/001
- [SDR CALA2023102303165](https://openairdocs.org/sdr/CALA2023102303165.md): Web · cracked · Oct 20, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SHEAR WEB AT FR68-69 IS CRACKED. REMOVED AND REPLACED AFT CABIN RH SHEAR WEB AT FR68-69 IAW A319 SRM 51-72-11 PAR 2.
- [SDR CALA2023102303163](https://openairdocs.org/sdr/CALA2023102303163.md): Shear Plate · corroded · Oct 20, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SHEAR PLATE SUPPORT AT FR69 TO 70 HAS EVIDENCE OF L IGHT SURFACE OXIDATION ON BOTTOM SURFACE. AFT CABIN RH SHEAR PLATE SUPPORT REMOVED AND REPLACED AT FR69-70 IAW A319 SRM 51-42-11 PAR 2.
- [SDR CALA2023102303158](https://openairdocs.org/sdr/CALA2023102303158.md): Fitting · corroded · Oct 20, 2023 · N819UA · Airbus A319131 · Service Doors
  > R2 DOOR SILL AFT CORNER FITTING HAS CORROSION. REMOVED AND REPLACED R2 DOOR SILL AFT CORNER FITTIN IAW A319 SRM 51-72-11-911/001 51-75-12-911-002 AND RESTORED SURFACE PROTECTION. 5
- [SDR CALA2023102303156](https://openairdocs.org/sdr/CALA2023102303156.md): Door Sill · corroded · Oct 20, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS MULTIPLE AREAS OF CORROSION AT FR68. REMOVED AND REPLACED R2 DOOR SILL BETWEEN FR66-68 IAW A319 SRM 5 1-72-11-911-001- 51-42-11/001 51-75-12/001 AND RESTORED SURFACE PROTECTION.
- [SDR CALA2023102303161](https://openairdocs.org/sdr/CALA2023102303161.md): Skin · contaminated · Oct 18, 2023 · N819UA · Airbus A319131 · Rudder, Plate/Skin
  > RUDDER LH LOWER HOIST POINT #1 HAS POSSIBLE WATER INTRUSION ON LOWER AFT AREA. REPAIRED RUDDER LH SKIN LOWER FWD HOIST POINT #2 LOWER AFT AREA 2.5 IN BY 2IN ZONE O IAW A319 SRM 55-41-13-300-030 CATEGORY ARE PAIR.
- [SDR CALA2023101703102](https://openairdocs.org/sdr/CALA2023101703102.md): Shear Tie · corroded · Oct 16, 2023 · N819UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > FWD CARGO, FR 34 RH STR. 41-42 FRAME SHEAR TIE, CORROSION PER HA ECO LCQ NR 9296616 (40616) REMOVED AND REPLACED CLEAT FROM FR 34 BTW STRINGERS 41-42 RH IAW A319 SRM 51-42-11.
- [SDR CALA2023101703097](https://openairdocs.org/sdr/CALA2023101703097.md): Shear Plate · corroded · Oct 16, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SHEAR PLATE @ FR69-FR70 HAS CORROSION PER HAECO LCQ NR 9296228 (40228) REMOVED AND REPLACED AFT CABIN RH SHEAR PLATE AT FR69-FR70 IAW A 319 SRM 51-72-11 PAR 2.
- [SDR CALA2023101603081](https://openairdocs.org/sdr/CALA2023101603081.md): Plate · cracked · Oct 14, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN FRAME 68 LEFT SECTION CONNECTION PLATE IS CRACKED. REMOVED AND REPLACED CONNECTING PLATE AT FR68 LEFT SECTION IAW A 319 SRM 51-72-1 PAR2.
- [SDR CALA2023101603088](https://openairdocs.org/sdr/CALA2023101603088.md): Shear Web · corroded · Oct 13, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN LH SHEAR WEB SUPPORT @ FR69-70 HAS CORROSION ON BOTTOM SIDE. REMOVED AND REPLACED AFT CABIN FLOOR FRAME SUPPORT LH IAW A319 S RM 51-42-11.
- [SDR CALA2023101603085](https://openairdocs.org/sdr/CALA2023101603085.md): Shear Tie · corroded · Oct 13, 2023 · N819UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > FWD CARGO, FR.28 R/H STR. 41-42 FRAME SHEAR TIE, CORROSION. REMOVED AND REPLACED SHEAR TIE AT FR28 BTW 41-42 RH IAW A319 SRM 51-73-11 PAR 2.
- [SDR CALA2023101603083](https://openairdocs.org/sdr/CALA2023101603083.md): Shear Plate · corroded · Oct 13, 2023 · N819UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN LH SHEAR PLATE AT FR 69-70 HAS CORROSION. REMOVED AND REPLACED AFT CABIN LH SHEAR PLATE FROM FR69-70 IAW A 319 SRM 51-42-11 AND SRM 51-72-11-911-001.
- [SDR CALA2023101603082](https://openairdocs.org/sdr/CALA2023101603082.md): Skin · contaminated · Oct 12, 2023 · N819UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR SHOWS LIQUID INGRESS AT 19 1/2IN FROM I/B END, 10IN FROM T/E, 1IN IN DIAMETER."REPAIR BEFORE NEXT FLIGHT" SUPPORT TA SK ON HAECO LCQ NR 9296565/40565 DRILLED WITNESS HOLES IN RH ELEVATOR UPPER SKIN 19.5IN FROM VB E ND. 10IN FORM T/E ZONE 1 IAW A31
- [SDR CALA2023101603080](https://openairdocs.org/sdr/CALA2023101603080.md): Skin · contaminated · Oct 12, 2023 · N819UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR SHOWS LIQUID INGRESS AT 21IN FROM I/B ENF, 10IN FROM T/E, 3/4IN IN DIAMETER."REPAIR BEFORE NEXT FLIGHT" SUPPORT TASK ON HAECO LCQ NR 9296566/40566 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 21IN FROM VB END 10IN FROM T/E ZONE 1 IAW A319 AMM 55
- [SDR CALA2023101603076](https://openairdocs.org/sdr/CALA2023101603076.md): Skin · contaminated · Oct 12, 2023 · N819UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 16FT 8IN FROM I/B END, 4 1/2IN FROM T/E, 2IN IN DIAMETER "REPAIR BEFORE NEXT FLIGHT" SUPPORT T ASK ON HAECO LCQ NR9296564/40564 REPAIRED LH ELEVATOR 200IN FROM VB END 4.5IN FROM T/E 2IN DIA ZO NE 3 IAW A319 SRM 55-21-11-300-0
- [SDR CALA2023101603072](https://openairdocs.org/sdr/CALA2023101603072.md): Skin · contaminated · Oct 12, 2023 · N819UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS A LIQUID INGRESS INDICATION AT 20.35" FROM T/E 1 3"FROM I/B, 1" DIA.REPAIR BEFORE NEXT FLIGHT. GEN BY V061671 ON HAECO LCQ NR 9296779/40779 DRILLED WITNESS HOLES IN RH ELEVATOR UPPER SKIN 20.5IN FROM T/E 13IN FROM I/B END IAW A319 AMM 55-20-00-

Next page: https://openairdocs.org/aircraft/N819UA/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 = 'N819UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N819UA/reports

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