# Service difficulty reports: N817UA

A list on [N817UA](https://openairdocs.org/aircraft/N817UA.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 · 128 reports

- [SDR CALA2026101320358](https://openairdocs.org/sdr/CALA2026101320358.md): Power Supply · faulted · Oct 12, 2026 · N817UA · Airbus A319131 · Emergency Lighting
  > TEST OF THE EMERGENCY LIGHTS FAILS WITH EPSU INT LOAD EMER R, EPSU BATTERY AFT L AND EPSU UNIT EMER L MESSAGES. R&R RIGHT OVER WING EPSU REF AMM 33-51-400-001-A. R&R AFT BATTERY OF EPSU REF AMM 33-51-38-000-002-A. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.
- [SDR CALA2026090719266](https://openairdocs.org/sdr/CALA2026090719266.md): Unknown · odor · Sep 4, 2026 · N817UA · Airbus A319131 · Air Distribution System
  > NOTICED UNUSUAL BURNT PLASTIC/ELEC ODOR AS WE STARTED DESCENT. ALSO NOTICED IN AFT CABIN. PERFORMED ODOR MM 05-50-00.
- [SDR CALA2026082118800](https://openairdocs.org/sdr/CALA2026082118800.md): Power Supply · no test · Aug 21, 2026 · N817UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMERGENCY LIGHT MESSAGE, DURING OPS CHECK. R & R EPSU 11WL. OPS CHKD GOOD IAW AMM 33-51-38.
- [SDR CALA2026062217259](https://openairdocs.org/sdr/CALA2026062217259.md): Idg · faulted · Jun 19, 2026 · N817UA · Airbus A319131 · AC Generator-Alternator
  > ELEC IDG 1 OIL LO PR -AIR RETURN TO IAD PER FLIGHT CREW. VARGAS TOMC CREW PERFORMED ELEC IDG 1 DISCONNECTED, UNCOMFORTABLE CONTINUING TO RDU. VARGAS TOMC LOCKED FOR POSITIVE FIX IMAGES ADDED OF POST FLIGHT REPORT, AND POPPED #1 ENG IDG DPI. UNLOCKED LOG. REF L
- [SDR CALA2026042015540](https://openairdocs.org/sdr/CALA2026042015540.md): Check Valve · faulted · Apr 17, 2026 · N817UA · Airbus A319131 · Aircraft Fuel Distribution System
  > TEST FLIGHT DISCREPANCY, NR 1 ENG FIRE HANDLE DID NOT SHUT DOWN THE ENGINE. REMOVED AND REPLACED NR 1 ENG FUEL RECIRCULATION CHECK VALVE IAW AMM 28-16-42-400-001-A. OPS CHECK GOOD, NO LEAKS NOTED. PERFORMED POST FLIGHT PF-6 ENGINE FIRE SHUTDOWN OPERATION C
- [SDR CALA2025100609618](https://openairdocs.org/sdr/CALA2025100609618.md): Pin · installed · Oct 3, 2025 · N817UA · Airbus A319131 · Standard Practices/Structures
  > INSTALLED SAFTEY PIN IN RH OFF WING SLIDE INFLATION CYLINDER REMOVED AND STOWED RH OFF WING SLIDE INFLATION BOTTLE SAFTEY PIN REF AMM 52-21-11 ACCOMPLISHED RII APPLICABLE STEPS PER GMM 09-25-05.
- [SDR CALA2025080707414](https://openairdocs.org/sdr/CALA2025080707414.md): Proximity Sensor · out of adjust · Aug 4, 2025 · N817UA · Airbus A319131 · Door Warning System
  > R FWD DOOR ECAM AFTERT/O TWICE SPORADICALLY.PRESS NORMAL. ADJUSTMENT OF THE FWD PAX/CREW DOOR.AMM TASK 52-71-00-820-002-A: ADJUSTMENT OF THE PROXIMITY SWITCHES LOCKED FOR FIX..WAS A DIVERSION INTO TPA YESTERDAY FOR THE SAME ISSUE. HAS HISTORY.CONTACT TOMC ONC
- [SDR CALA2025080507339](https://openairdocs.org/sdr/CALA2025080507339.md): Door · false indication · Aug 3, 2025 · N817UA · Airbus A319131 · Door Warning System
  > ECAM DOOR RT FWD CABIN ON DEPARTURE. FA REPORTS ORANGE LIGHT FLASHING. ACCOMPLISHED VISUAL INSPECTION OF DOOR, DOOR SEAL, STOP PADS, GUIDE ROLLERS, DOOR CLOSED & OPEN POSITIONS, ARMED AND UNARMED. NO DEFECTS SEEN. MEL 5270AX. CLEANED SENSOR IAW AMM 52-00-0
- [SDR CALA2025080407254](https://openairdocs.org/sdr/CALA2025080407254.md): Elec Connector · dirty · Jul 31, 2025 · N817UA · Airbus A319131 · Light System Wiring
  > EPSU BATTERY EMERGENCY LIGHT RT. CLEANED CONNECTOR AND EMERGENCY LIGHT SYSTEM OP CHECKED GOOD.
- [SDR CALA2025073007084](https://openairdocs.org/sdr/CALA2025073007084.md): Warning Message · false activation · Jul 27, 2025 · N817UA · Airbus A319131 · Door Warning System
  > DURING CLIMBOUT 2 INTERMITTENT ECAM DOOR RT FWD CABIN. CABIN PRESSURE NORMAL. FAULT WAS NOT ACTIVE AND THERE IS NO HISTORY OF THIS FAULT IN 90 DAYS. REF TSM 52-11-00-810-803-A. FWD RIGHT CREW/PASS DOOR INDICATIONS OP CHECK GOOD. OK FOR SERVICE.
- [SDR CALA2024030100615](https://openairdocs.org/sdr/CALA2024030100615.md): Target · distorted · Feb 28, 2024 · N817UA · Airbus A319131 · Door Warning System
  > DOOR R EMER EXIT AT FL320. NO ABN V/S SPOKE WITH CREW, NO PRESSURIZATION PROBLEMS. NO AIR LEAKS NOTED AT EMERGENCY EXIT. PERFORMED VISUAL CHECK OF RT OVERWING EMERGENCY EXIT I.A.W. AMM 52-70-00-040-010-A MEL 5270BK TECH SUPPORT WILL TROUBLESHOOT. T/SING FOUND
- [SDR CALA2023112703475](https://openairdocs.org/sdr/CALA2023112703475.md): Skin · cracked · Nov 22, 2023 · N817UA · Airbus A319131 · Service Doors
  > MAIN CABIN R2 DOOR OUTER SKIN HAS CRACK AT UPPER FWD CORNER PANEL. GEN BY V919150 ON HAECO LCQ NR 9294410/38410 PLATE COVER ASSY (SKIN) REPLACED ON UPPER CORNER R2 DOOR IAW A31 9 SRM 51-72-11-911-001. ACMP BY MECH V945145 INSP BY V921755
- [SDR CALA2023112003442](https://openairdocs.org/sdr/CALA2023112003442.md): Fitting · damaged · Nov 9, 2023 · N817UA · Airbus A319131 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST UPPER ATTACHMENT HAS 3 FASTENER HOLES WITH CRACK INDICATIONS HOLE A FWD OTBD HOLE B FWD INBD HOLE C AFT INBD MARKED WITH DOTS RESPECTIVELY. REPAIRED HOLE A FWD OTBD, HOLE B FWD INBD, HOLE C AFT INBD AT L/ NO CRACKS FOUND. FINAL HOLE SI
- [SDR CALA2023112003440](https://openairdocs.org/sdr/CALA2023112003440.md): Fitting · out of round · Nov 9, 2023 · N817UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LH FR4 SIDE POST UPPER ATTACHMENT CONNECTION FITTING REQUIRES REMOVAL TO FOM SEPERATION OF LAYERS FOR NDT INSPECTION. REINSTALLED LH FR4 SIDE POST UPPER ATTACHMENT CONNECTION FITTING IAW SRM 51-42-11-001 AND 51-72-11-911-001. NO FURTHER ACTION REQUIRED.
- [SDR CALA2023112003428](https://openairdocs.org/sdr/CALA2023112003428.md): Skin · sheared · Nov 8, 2023 · N817UA · Airbus A319131 · Landing Gear Doors
  > AD 2015-02-14 RMLG DOOR ACTUATOR FITTING FWD LUG FWD OTBD FASTENER COMMON TO LOWER EXTERNAL SKIN IS SHEARED (BROEKN HEAD) (EA533 0-04821) GENERATED AT HAECO LCQ PER NR 9294537 LATEST REVISION OF ECRA 5330-07150 ON OR BEFORE 02-NOV-24. P REVISION OF ECRA 5330-
- [SDR CALA2023112003426](https://openairdocs.org/sdr/CALA2023112003426.md): Frame · cracked · Nov 8, 2023 · N817UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 35 STR 30 RH HOLE #2 HAS CRACK INDICATION IN FRAME LAYER 7 O''CLOCK POSITION 30% SCREEN HEIGHT. REPAIRED HOLE #2 AT RH FR35 STR30 IAW ECRA 5331-03064. CREATED CORRECT TO READ: PERFORMED INTERIM REPAIR RH FR35 STR30 HOLE #2 DIP FOR PERMANENT REPAIR TO B
- [SDR CALA2023111503384](https://openairdocs.org/sdr/CALA2023111503384.md): Crossbeam · cracked · Nov 8, 2023 · N817UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 16 LH CROSSBEAM HOLES H1, H2 AND H8 HAVE CRACK INDICATIONS IN LAYER (AD RELATED SUPPORT TASK) (AD 2018-14-09) GENERATED AT HAECO LCQ PER NR 9294461. ON OR BEFORE THE AIRCRAFT REACHES 81,622 TOTAL AIRCRAFT FLIGHT CYCLES ACCOMPLISH INITIAL INSPECTION OF L
- [SDR CALA2023110803305](https://openairdocs.org/sdr/CALA2023110803305.md): Stringer · corroded · Nov 4, 2023 · N817UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, UNDERFLOOR COMPARTMENT, AFT FR.65 R/H STR. 25, EXFOLIATION CORROSION. PER HAECO LCQ NR 9294659/38659 REMOVED AND REPLACED STR 25R AT FR 64-67 IAW A319 SRM 53-41-13-3 00-004.
- [SDR CALA2023102503182](https://openairdocs.org/sdr/CALA2023102503182.md): Angle · cracked · Oct 24, 2023 · N817UA · Airbus A319131 · Wing Miscellaneous Structure
  > L/H WING RIB 15 L/E WEB SUPPORT ANGLE CRACKED. PER HAECO LCQ NR 9294242/38242 REMOVED AND REPLACED WEB SUPPORT ANGLE ON LH WING RIB 15 L/E IAW A319 SRM 51-42-11
- [SDR CALA2023102303152](https://openairdocs.org/sdr/CALA2023102303152.md): Floor Support · corroded · Oct 22, 2023 · N817UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN R/H FR20, Y-254 FLOOR SUPPORT BEAM HAS CORROSION ON U PPER SUFACE A3NB-53-3-6038 PER HAECO LCQ NON ROUTINE 9294357/383 57 GENERATED BY V919150
- [SDR CALA2023102503177](https://openairdocs.org/sdr/CALA2023102503177.md): Seat Track · chafed · Oct 20, 2023 · N817UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK Y-1292 HAS CHAFE MARKS IN TRACK @ FR 54,59 GEN BY V926223 ON HAECO LCQ NR 9294371/38371 REMOVED AND REPLACED -Y 1292 FR 47/51-66 SEAT TRACK IAW SRM 51-7 2-11-911-001.
- [SDR CALA2023102303162](https://openairdocs.org/sdr/CALA2023102303162.md): Door Sill · corroded · Oct 20, 2023 · N817UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > MAIN CABIN L/H DOOR SILL FR 68 IAW A319 SRM 53-41-14-300-001. REPAIRED MAIN CABIN LH DOOR SILL AT FR68 IAW A319 SRM 53-41-14-3 00-001.
- [SDR CALA2023102303159](https://openairdocs.org/sdr/CALA2023102303159.md): Floor Support · worn · Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FLOOR BEAM -Y254 FRAME 68-70 HAS OUT OF ROUND HOLES AT SPLICE AREA. PER HAECO LCQ NR 9294677/38677 REPLACED BEAM AT -Y 254 FR 68-70 I.A.W. A319 SRM 51-72-11-911-0 01.
- [SDR CALA2023102303147](https://openairdocs.org/sdr/CALA2023102303147.md): Beam · corroded · Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN BEAM -Y 254 HAS CORROSION AT FR 66. PER HAECO LCQ NR 9294349/38349 REPLACED BEAMS AND SPLICES AT -Y254 & FR 64 - 68 I.A.W. A319 SRM 51-72-11-911-001.
- [SDR CALA2023102303143](https://openairdocs.org/sdr/CALA2023102303143.md): Seat Track · corroded · Oct 19, 2023 · N817UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN R/H FR20, Y-1292 FLOOR SEAT TRACK BEAM HAS CORROSION ON UPPER SURFACE. PER HAECO LCQ NR 9294356/38356 TRACK BEAM DAMAGE WAS REMOVED, NEW TRACK BEAM WAS INSTALLED IAW A319 SRM TASK 51-72-11-911-001
- [SDR CALA2023080402430](https://openairdocs.org/sdr/CALA2023080402430.md): Door · warning message · Aug 2, 2023 · N817UA · Airbus A319131 · Door Warning System
  > R FRD DOOR OPEN ECAMON T/O VISUALLY CHECKED DOOR THAT IT IS CLOSED AND LOCK.. VERIFY WHITE DOOR IS CLOSED AND LOCKED AND SLIDE ARMED. SLIDE ARMED LIGHT ON INSTALLED INOPERATIVE STICKER ADJACENT TO LOWER ECAM DISPLAY "SLIDE ARMED" LIGHT(S) ON THE DOOR DOES NOT
- [SDR CALA2022081602090](https://openairdocs.org/sdr/CALA2022081602090.md): Skin · damaged · Aug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGED AT FR26 BETWEEN STR 38-39 LEFT. GENERATED BY V913126 ON HAECO LCQ NR 9298041/28041 X=.900 AND Y=.200. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 703 FR24 THRU FR35 ZONE A THE INSPECTION THRESHOLD FROM TIME OF INSPECTION UNTIL 60,000 FC
- [SDR CALA2022081602089](https://openairdocs.org/sdr/CALA2022081602089.md): Skin · dented · Aug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT FR26 JUST BELOW STR 29 LEFT. GENERATED B Y V913126 ON HAECO LCQ NR 9298042/28042 X=.900, AND Y=.900. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-21- 073 FR24 THRU FR35 ZONE A INSPECTION THRESHOLD FROM TIME OF ADL/ UNTIL 60,000FC/120,000FH
- [SDR CALA2022081602088](https://openairdocs.org/sdr/CALA2022081602088.md): Skin · dented · Aug 12, 2022 · N817UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT FR 19 RH BETWEEN STR 37-38R. GENERATED B Y V913126 ON HAECO LCQ NR 9298043/28043 =.150, Y=.800. ACCOMPLISHED A DOUBLER REPAIR IAW SRM 53-11-11- FR1 THRU FR24 ZONE F INSPECTION THRESHOLD FROM TIME OF REPAIR 60,000 FC/ 120,000 FH AT INTER
- [SDR CALA2021101401884](https://openairdocs.org/sdr/CALA2021101401884.md): Wheel · damaged · Oct 14, 2021 · N817UA · Airbus A319131 · Landing Gear System
  > REJECTED TAKEOFF AT APPROX 80 KNOTS DO TO HAIL. ACCOMPLISHED REJECTED TAKEOFF / EMERGENCY BRAKE APPLICATION REF. AMM 05-51-16-200-001-A. REMOVED AND REPLACED BOTH #1 & #2 MAIN TIRE ASSY''S
- [SDR CALA2021072101152](https://openairdocs.org/sdr/CALA2021072101152.md): Fuel Cap · missing · Jul 20, 2021 · N817UA · Airbus A319131 · Fuel Storage
  > PDA 3 FUEL CAP REPORTED MISSING REF LOG 6689310 FOR FUEL CAP REPLACEMENT
- [SDR CALA2021032200362](https://openairdocs.org/sdr/CALA2021032200362.md): Brake · overheated · Mar 22, 2021 · N817UA · Airbus A319131 · Landing Gear Brake System
  > HOT L/INBD BRAKE AFTERT/O..DROPPED GEAR TO COOL..COULD NOT RETRA CT #2 MLG BRAKE READING APROX. 430 DEG. COMPAIRED TO THE OTHER 3 BRAKES READING APROX. 220 WHEN ARRIVED AT GATE. REPLACED WHEEL ASSEMBLY PER AMM 32-41-11. CHECKS GOOD. ROTABLE PARTS CHANGE WAS IN
- [SDR CALA2020100701155](https://openairdocs.org/sdr/CALA2020100701155.md): Battery · no test · Sep 30, 2020 · N817UA · Airbus A319131 · Emergency Lighting
  > 13WL FAILS BATTERY CAPACITY CHECK - SUPPORT TASK. REMOVED AND INSTALLED SERVICEABLE EPSU BATTERY (13WL) IAW A319 A MM 33-51-38-000-002-A / 400-002-A. OPERATIONAL BITE CHECK GOOD I AW A319 AMM 33-51-00-710-001-A.
- [SDR CALA2020091801124](https://openairdocs.org/sdr/CALA2020091801124.md): Feeder Cable · loose · Sep 17, 2020 · N817UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHTS AT SEAT ROWS 23L; 24L ARE INOP. A3NB-33-3-6015 PER HAECO LCQ NON ROUTINE 9294339 GENERATED BY V061674.
- [SDR CALA2019042900671](https://openairdocs.org/sdr/CALA2019042900671.md): Cap · missing · Apr 29, 2019 · N817UA · Airbus A319131 · Fuel Storage
  > FUEL CAP FOUND MISSING ON LOG PAGE 3093282 ADDING SDR FOR PDA 2 PDA COMPLIED WITH PER GMM 023095
- [SDR CALA2018120202458](https://openairdocs.org/sdr/CALA2018120202458.md): Strut · lack of lube · Nov 29, 2018 · N817UA · Airbus A319131 · Nose/Tail Landing Gear Strut/Axle
  > GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G ON TAKEOFF GEAR WOULD NOT RETRACT SHOCK ABSORBER FAULT. ACP FULL NLG STRUT SVC AND LUBE OF ALL NLG ZERK FITTINGS JACKED AIRCRAFT AND CKED DIMENSIONS OF NLG STRUT EXTEND SWITCHES 24 & 25 GA ACP A FULL GEAR
- [SDR CALA2018102702183](https://openairdocs.org/sdr/CALA2018102702183.md): Fitting · corroded · Oct 23, 2018 · N817UA · Airbus A319131 · Wing, Landing Gear Attach Fittings
  > RT MLG SIDESTAY ATTACHMENT LUGS TO REAR SPAR HAVE CORROSION IN BORES. BOTH LUGS HAD CORROSION REMOVED AND WERE OVERSIZED PER SRM 57-26-13-300-023. FINISHING CUTS WERE MADE AND OVERSIZED BUSHINGS INSTALLED PER EA 5700-03259 OP 2 PER SRM 57-26-13-300-023 PARA 1D
- [SDR CALA2018101302086](https://openairdocs.org/sdr/CALA2018101302086.md): Power Supply · defective · Oct 9, 2018 · N817UA · Airbus A319131 · Emergency Lighting
  > EPSU 11WL DEFECTIVE, MULTIPLE SEAT ROWS WILL NOT LIGHT. REMOVED EPSU 11WL IAW AMM 33-51-38-000-001-A, REMOVED BATTERY FORM EPSU 11WL IAW AMM 33-51-000-002-A, INSTALLED BATTERY ON REPLACEMENT ESPU 11WL IAW AMM 33-51-38-400-002-A AMD INSTALLED EPSU 11WL IAW AMM
- [SDR CALA2017050101223](https://openairdocs.org/sdr/CALA2017050101223.md): Lamp · inoperative · May 1, 2017 · N817UA · Airbus A319131 · Emergency Lighting
  > MESSAGE EPSU EMERGENCY LOAD RT APPEARED. REPLACED TWO LAMPS. OP CHECKED GOOD IAW AMM 33-51-15. AND AMM 33-51-00.
- [SDR CALA2017031700645](https://openairdocs.org/sdr/CALA2017031700645.md): Circuit Breaker · malfunctioned · Mar 17, 2017 · N817UA · Airbus A319131 · Escape Slide
  > SLIDE ARMED LIGHT STAYS ILLUMINATED WITH SLIDE IN THE DISARM POSITION. CYCLED THE CIRCUIT BREAKER 121-P10, TESTED OK IAW MM 52-73-00-710-001-A
- [SDR CALA2017031300598](https://openairdocs.org/sdr/CALA2017031300598.md): Warning System · false activation · Mar 13, 2017 · N817UA · Airbus A319131 · Door Warning System
  > DOOR 2R SLIDE ARMED LIGHT ILLUMINATED IN FLIGHT. CYCLED DOOR. DOOR ARMED AND DISARMED. NO DEFECTS FOUND WHILE ARMED. OPS CHECK GOOD REF AMM 52-13-00.
- [SDR CALA2017081402644](https://openairdocs.org/sdr/CALA2017081402644.md): Shear Tie · corroded · Feb 20, 2017 · N817UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > FWD CARGO UNDER FLOOR AREA SHEAR TIE, FRAME 30, STRINGERS 43 - 44R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11.
- [SDR CALA2017081402643](https://openairdocs.org/sdr/CALA2017081402643.md): Plate · chafed · Feb 18, 2017 · N817UA · Airbus A319131 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 ENGINE LOWER PLATE IS CHAFED. INSTALLED NEW PLATE IAW SRM 54-51-12 FIG 202.
- [SDR CALA2017022000429](https://openairdocs.org/sdr/CALA2017022000429.md): Plate · chafed · Feb 18, 2017 · N817UA · Airbus A319131 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 NACELLE LOWER CHAFE PLATE HAS A CHAFE. REMOVED AND REPLACED THE CHAFE PLATE IAW SRM 54-51-12, F 202, PAR 5B.
- [SDR CALA2017022000428](https://openairdocs.org/sdr/CALA2017022000428.md): Stringer · corroded · Feb 18, 2017 · N817UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FWD CARGO STRINGER 43L HAS SURFACE CORROSION FRAMES 30 - 31. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-11, PARA 7.
- [SDR CALA2017021700405](https://openairdocs.org/sdr/CALA2017021700405.md): Tee Fitting · corroded · Feb 16, 2017 · N817UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LEFT EMERGENCY EXIT DOOR LOWER CUTOUT AFT AND FWD SKIN CORRODED ON INNER SKIN AT ATTACH POINTS. REMOVED AND REPLACED THE TEE FITTINGS IAW SRM 51-42-11.
- [SDR CALA2017021700404](https://openairdocs.org/sdr/CALA2017021700404.md): Cleat · corroded · Feb 16, 2017 · N817UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO UNDER FLOOR AREA CLEAT ON FR29 STR43R HAS SURFACE CORROSION. REMOVED AND REPLACED THE CLEAT IAW SRM 51-42-11, PAR 7.
- [SDR CALA2017081402641](https://openairdocs.org/sdr/CALA2017081402641.md): Doubler · corroded · Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FWD CARGO UNDER FLOOR AREA INNER SKIN HAS SURFACE CORROSION ON DOUBLER FWD OF FRAME 31 AND STRINGERS 43 - 44R. REMOVED AND REPLACED THE DOUBLER.
- [SDR CALA2017081402640](https://openairdocs.org/sdr/CALA2017081402640.md): Shear Tie · corroded · Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Structure (General)
  > C2, FWD CARGO UNDER FLOOR AREA SHEAR TIE ON FRAME 28, STRINGERS 42R - 43R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 5 1-92-11.
- [SDR CALA2017081402639](https://openairdocs.org/sdr/CALA2017081402639.md): Shear Tie · corroded · Feb 13, 2017 · N817UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > C2, FWD CARGO UNDER FLOOR AREA SHEAR TIE ON FRAME 29 AND STRINGER 43L HAS SURFACE CORROSION. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-42-11, FIG 8.

Next page: https://openairdocs.org/aircraft/N817UA/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 = 'N817UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N817UA/reports

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