# Service difficulty reports: N852UA

A list on [N852UA](https://openairdocs.org/aircraft/N852UA.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 · 96 reports

- [SDR CALA2026012213146](https://openairdocs.org/sdr/CALA2026012213146.md): Frame Splice · cracked · Jan 17, 2026 · N852UA · Airbus A319131 · Fuselage Main, Frame
  > AFT CARGO FR 61 LEFT FRAME SPLICE SECTION CRACKED BETWEEN STR 34L & 36L. REMOVED AND REPLACED THE LT FRAME SPLICE SECTION.
- [SDR CALA2026012213144](https://openairdocs.org/sdr/CALA2026012213144.md): Panel · cracked · Jan 17, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO, LEFT PROFILE PANEL FROM FR 59 - 63 CRACKED AT STRINGER 35L, IAW AAR LCQ 9296225/36225. REPLACED, AND INSTALLED AFT CARGO BAY PROFILE PANEL IAW SRM 51-42-11-001, SRM 51-44-11-001.
- [SDR CALA2026011212870](https://openairdocs.org/sdr/CALA2026011212870.md): Fitting · cracked · Jan 7, 2026 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT & RIGHT WINDSHIELD CONTINUITY FITTINGS CRACKED. REMOVED & REPLACED LT & RT WINDSHIELD CONTINUITY FITTINGS ON EA 5310-07675 004.
- [SDR CALA2026010712754](https://openairdocs.org/sdr/CALA2026010712754.md): Floor Support · corroded · Jan 6, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT FLOOR SUPPORT Y-512 BETWEEN FR 68-70 WAS CORRODED ON UPPER SURFACE. R & R THE RT FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026010712753](https://openairdocs.org/sdr/CALA2026010712753.md): Floor Support · corroded · Jan 6, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN RT FLOOR SUPPORT, Y-765 BETWEEN FR 66-68 WAS CORRODED ON UPPER SURFACE. R & R THE RT FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026010712752](https://openairdocs.org/sdr/CALA2026010712752.md): Floor Support · corroded · Jan 6, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN LT FLOOR SUPPORT Y512 BETWEEN FR 66-70 WAS CORRODED ON UPPER SURFACE. R & R MAIN CABIN LT FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026010712751](https://openairdocs.org/sdr/CALA2026010712751.md): Floor Support · corroded · Jan 6, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN L/H FLOOR SUPPORT, Y254 BETWEEN FR 68-70 WAS CORRODED ON UPPER SURFACE. R & R MAIN CABIN LT FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026010712750](https://openairdocs.org/sdr/CALA2026010712750.md): Floor Support · corroded · Jan 6, 2026 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR SUPPORT AT Y-765, FR 64-66 WAS CORRODED ON UPPER FLANGE. R & R AFT WET AREA FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026011412960](https://openairdocs.org/sdr/CALA2026011412960.md): Shear Plate · corroded · Jan 1, 2026 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN LT FLOOR SHEAR PLATE BETWEEN FR 69-70 HAS CORROSION SPOT. REMOVED AND REPLACED THE LT SHEAR PLATE IAW SRM 51-42-11/001 PG 16-19 AND 51-72-11-911-001.
- [SDR CALA2026011412958](https://openairdocs.org/sdr/CALA2026011412958.md): Shear Plate · damaged · Jan 1, 2026 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN RT FLOOR SHEAR PLATE BETWEEN FR 69-70 HAS HEAD SHEARED RIVETS. REMOVED AND REPLACED RT SHEAR PLATE IAW SRM 51-42-11/001 PG 16-19 AND 51-72-11-911-001.
- [SDR CALA2025103010754](https://openairdocs.org/sdr/CALA2025103010754.md): Cover · unsecure · Oct 28, 2025 · N852UA · Airbus A319131 · Emergency Exits
  > DOOR L EMER EXIT ECAM IN FLIGHT ECAM WAS FOR LEFT WING EMERGENCY EXIT DOOR HATCH. LEFT OVER WING EMERGENCY DOOR FLAP COVER THAT COVERS EMERGENCY RELEASE HANDLE CAME OFF CAUSING DOOR WARNING AND SLIDE ARMED LIGHT AT HATCH IN CABIN TO COME ON. RESECURED FLAP C
- [SDR CALA2025080407251](https://openairdocs.org/sdr/CALA2025080407251.md): Actuator · faulted · Aug 1, 2025 · N852UA · Airbus A319131 · Compressor Bleed Control
  > ENG 1 COMPRESSOR VANE. CHA/CHB VSV ACT/HC/EEC1 FOUND WITH FAULT ACRONYM OF SVATK, REF TSM'S 75-30-00-810-843-A AND 75-30-00-810-845, PERFORMED TSM 75-30-00-810-805B FOUND ENGINE 1 VSV BOTH CHANNELS DEFECTED. REMOVED AND REPLACED ENGINE 1 VSV REF AMM 75-32-
- [SDR CALA2025061705594](https://openairdocs.org/sdr/CALA2025061705594.md): Power Supply · faulted · Jun 17, 2025 · N852UA · Airbus A319131 · Emergency Lighting
  > FA/S REPORT EMER EXIT LIGHTS COMING ON/OFF DURING FLIGHT PERFORMED BITE CHECK OF THE EMERGENCY POWER SUPPLY UNITS REF AMM 33-51-00-710-001-A. FOUND FAULT EPSU UNIT FWD L PRESENT. PERFORMED TEST ON EPSU ABOVE DOOR AT 1L, UNIT FAULT LED ILLUMINATES. REMOVED AND
- [SDR CALA2025032002997](https://openairdocs.org/sdr/CALA2025032002997.md): Skin · contaminated · Mar 19, 2025 · N852UA · Airbus A319131 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS AT 31.5 IN FROM INBOARD END, 18. 5 IN TRAILING EDGE, 2 IN DIAMITER. REPAIRED L/H ELEVATOR 31.5 IN FROM INBOARD AND 18.5 IN TRAILING EDGE. CATEGORY A REPAIR IAW A319 SRM 55-21-11-300-005. ACMP BY ECH V061767 INSP BY V061626. COM
- [SDR CALA2025032002996](https://openairdocs.org/sdr/CALA2025032002996.md): Skin · contaminated · Mar 19, 2025 · N852UA · Airbus A319131 · Elevator, Plate/Skin
  > R/H ELEVATOR HAS LIQUID INGRESS AT TOP 16.5 IN FROM INBOARD END, 6.5 IN FROM TRAILING EDGE, 2.5 IN DIAMETER, BOTTOM SIDE 17 IN F ROM INBOARD, 5 IN FROM TRAILING EDGE, 1 IN DIAMETER. GEN BY V061 632 ON HAECO LCQ NR 9296165 / 22165 ESFR ENTERED REPAIRED R/H ELEV
- [SDR CALA2024121801570](https://openairdocs.org/sdr/CALA2024121801570.md): Battery Pack · no test · Dec 17, 2024 · N852UA · Airbus A319131 · Emergency Lighting
  > FWD L CABIN EMERGENCY LIGHTING BATTERY FAILED CAPACITY OPERATIONAL CHECK REMOVED AND REPLACED FWD L CABIN EMERGENCY LIGHTING BATTERY. IAW AMM 33-51-38. OPS CHECK GOOD. NO FAULTS FOUND. PARTS USED: 18-3351-3-0001, QTY:1
- [SDR CALA2024121801569](https://openairdocs.org/sdr/CALA2024121801569.md): Battery Pack · no test · Dec 17, 2024 · N852UA · Airbus A319131 · Emergency Lighting
  > AFT L ESPU CABIN EMERGENCY LIGHTING BATTERY FAILED CAPACITY OPERATIONAL CHECK REMOVED AND REPLACED AFT L EPSU IAW AMM 33-51-38 OPS CHECK GOOD NO FAULTS FOUND.
- [SDR CALA2023090602731](https://openairdocs.org/sdr/CALA2023090602731.md): Spoiler · warning message · Sep 2, 2023 · N852UA · Airbus A319131 · Drag Control System
  > GND SPLR 5 ECAM ON TAKEOFF. CREW RESET SEC SWITCHES PER QRH AND FAULT CLEARED. ABORT WAS APROX 30 KNOTS.
- [SDR CALA2023081802549](https://openairdocs.org/sdr/CALA2023081802549.md): Fuel Cap · missing · Aug 16, 2023 · N852UA · Airbus A319131 · Fuel Storage
  > REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NOTED. CREW APPLIED STICKER DISPATCH DESK: 10 NAME: MB DATE: 16-AUG-23- DEFERRED DIRECTLY BY TOMC SECURED FUEL COUPLING CAP REF. AMM 28-25-41 REMOVED PLACED.
- [SDR CALA2023062101970](https://openairdocs.org/sdr/CALA2023062101970.md): Skin · bent · Jun 19, 2023 · N852UA · Airbus A319131 · Spoilers
  > LH WING T/E SEAL PLATE OF SPOILER#3 BENTED. LTPR NR#50012411630010. 660MM/25.98INCHES; CHORDWISE 110MM/4.33INCHES. WEIGHT, C/RA 5721-01478 ON OR BEFORE THE AIRCRAFT REACHES 47,298 TOTAL A 651.5G/1.43LBS. IRCRAFT FLIGHT CYCLES OR 96,175 TOTAL AIRCRAFT FLIGHT HO
- [SDR CALA2023061901930](https://openairdocs.org/sdr/CALA2023061901930.md): Battery · no test · Jun 14, 2023 · N852UA · Airbus A319131 · Lighting System
  > EPSU BATTERY (13WL) FAILED ON EMERGEMCY LIGHTING. LTPR NR#50012411240010
- [SDR CALA2023061901929](https://openairdocs.org/sdr/CALA2023061901929.md): Battery · no test · Jun 14, 2023 · N852UA · Airbus A319131 · Lighting System
  > EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTING. LTPR NR#50012411240010.
- [SDR CALA2023061901928](https://openairdocs.org/sdr/CALA2023061901928.md): Battery · no test · Jun 14, 2023 · N852UA · Airbus A319131 · Lighting System
  > EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTING. LTPR NR#50012411240010
- [SDR CALA2023061901927](https://openairdocs.org/sdr/CALA2023061901927.md): Battery · no test · Jun 14, 2023 · N852UA · Airbus A319131 · Lighting System
  > EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTING. LTPR NR#50012411240010.
- [SDR CALA2023020800370](https://openairdocs.org/sdr/CALA2023020800370.md): Pump · not reported · Feb 8, 2023 · N852UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y RSVR OVRHT. GROUND TEST OF ELECTRI C PUMP IS NORMAL, NO RESERVOIR OVERHEAT OR ABNORMAL OPERATION. DEBRIEFED CREW, #2 EDP WHEN TURNED OFF, OVERHEAT CONDITION GOES AWAY. SUSPECT BAD HYD EDP. MULTIPLE PARTS ON ORDER. REMOVED AND REPLACED #2 ENG. HYD.ENGIN
- [SDR CALA2022041400983](https://openairdocs.org/sdr/CALA2022041400983.md): Sensor · failed · Apr 14, 2022 · N852UA · Airbus A319131 · Outside Air Temperature Indicator/Sensor
  > ADR 1 FAULT ON CLIMBOUT REPLACED #1 ADR REF AMM 34-12-34-400-001, GROUND CHECKS OK. ADD EMP:U303859 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1133095 SN OFF 9498 IPC REFERENCE # 34-34-12 UNIT, AIR DATA OFF 31-3411-9-0002 6775 ON 31-3411-9-0002 0669
- [SDR CALA2021053100750](https://openairdocs.org/sdr/CALA2021053100750.md): Battery Pack · discharged · May 29, 2021 · N852UA · Airbus A319131 · Emergency Lighting
  > L/H OVERWING EXIT EMERGENCY LIGHTS EPSU BATTERYL PACK FAILS THE CAPACITY TEST (11WL). (A3NB-33-3-0004). GENERATED BY V061627 AT HAECO LCQ PER NR 9296033 (42033). REMOVED AND REPLACED L/H OVERWING EXIT EMERGENCY BATTERY 11WL AN D OP CHECKS GOOD IAW A319/AMM 33-
- [SDR CALA2021052400719](https://openairdocs.org/sdr/CALA2021052400719.md): Intercostal · cracked · May 23, 2021 · N852UA · Airbus A319131 · Service Doors
  > R1 DOOR FR16 #7 DOOR STOP BOTH INBD FASTENER HOLES PRODUCED CRAC K INDICATIONS DURING ABHEC INSPECTION. UPPER HOLE CRACK IS AT TH E 7:00 POSITION AND LOWER HOLE CRACK IS AT THE 8:00 - AD 2019-20 -10 - NR 9296250 (42250) GENERATED BY V061690 AT HAECO LCQ. REMOV
- [SDR CALA2021052400718](https://openairdocs.org/sdr/CALA2021052400718.md): Stop Fitting · cracked · May 23, 2021 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > L1 DOOR FR16 #7 DOOR STOP BOTH INBD FASTENER HOLES PRODUCED CRAC K INDICATIONS DURING ABHEC INSPECTION. UPPER HOLE CRACK IS AT TH E 4:00 POSITION AND LOWER HOLE CRACK IS AT THE 3:00 POSITION - A D 2019-20-10 - NR 9296249 (42249) GENERATED BY V061690 AT HAECO L
- [SDR CALA2021052400717](https://openairdocs.org/sdr/CALA2021052400717.md): Intercostal · cracked · May 23, 2021 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > L1 DOOR FR 20 #7 DOOR STOP BOTH UPPER FASTENER HOLEDS PRODUCED C RACK INDICATIONS DURING ABHEC INSPECTION. INBD HOLE CRACK IS AT THE 4:00 POSITION AND OTBD CRACK IS AT THE 2:00 POSITION - AD 20 19-20-10 - NR 9296248 (42248) GENERATED BY V061690 AT HAECO LCQ. R
- [SDR CALA2021051900688](https://openairdocs.org/sdr/CALA2021051900688.md): Stringer · corroded · May 18, 2021 · N852UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL FOUND CORROSION ON STRINGER 38RT BETWEEN FR59RT-FR6 0RT - A3NB-53-4-6179 - NR 9296571 (42571) GENERATED BY V052030 A T HAECO LCQ. REMOVED AND REPLACED CORRODED SECTION OF STR 38R FROM FR59-FR61 IAW A319 SRM 51-72-11. ACCOMPLISHED BY V052030, INSP
- [SDR CALA2021051200639](https://openairdocs.org/sdr/CALA2021051200639.md): Floor Support · corroded · May 11, 2021 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR, AFT WET AREA, FR 66-68, R-2 DOOR SILL FRAME, H AS 2EA. AREAS OF CORROSION - A3NB-53-3-6222 - NR 9296328 (42328) GENERATED BY V917055 AT HAECO LCQ. REMOVED & REPLACED MAIN CABIN, AFT WET AREA DOOR SILL FROM R/H F R66-FR68 IAW A319 SRM 51-72-11
- [SDR CALA2021051200638](https://openairdocs.org/sdr/CALA2021051200638.md): Fitting · corroded · May 11, 2021 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN FLOOR, AFT WET AREA, FR68, R-2 DOOR CUT OUT, LOWER CO RNER FITTING, HAS CORROSION - A3NB-53-3-6222 - NR 9296327 (42327) GENERATED BY V917055 AT HAECO LCQ. REMOVED & REPLACED MAIN CABIN AT FR 68 R/H, AFT CORNER FITTING I AW A319 SRM 51-72-11-911-001
- [SDR CALA2020022900557](https://openairdocs.org/sdr/CALA2020022900557.md): Circuit Breaker · tripped · Feb 28, 2020 · N852UA · Airbus A319131 · Airfoil Anti/De-ice System
  > WING ANTI ICE WOULD NOT TURN ON IN FLIGHT FOUND C-2 CB ANTI ICE WING CTL OUT,RESET CB AND ACP OPS TEST AMM 30-11-00-710-001-A,TESTED GOOD RAN BOTH ENGINES AT GATE,ACP OPS TEST AMM 30-11-00-710-001-A 3 TIMES TESTED GOOD
- [SDR CALA2020021200405](https://openairdocs.org/sdr/CALA2020021200405.md): Clamp · failed · Feb 10, 2020 · N852UA · Airbus A319131 · Cabin Pressure Control System
  > UNABLE TO PRESSURIZE AIRCRAFT IN CLIMB. OUTFLOW VALVE CONFIRMED CLOSED AND ECAM CAB PR EXCESS CAB ALT DISPLAYED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN OPEN PACK 2 BAY LOOK FOR LEAKS MAC RELATED WORK ORDER 000000002351443 AND PRTR FOUND TUBE GOING TO ACM
- [SDR CALA2020020200293](https://openairdocs.org/sdr/CALA2020020200293.md): Plate · corroded · Jan 27, 2020 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > COLLECTING PLATE FOR AFT PIT TORSION BOX COVER AND THRESHOLD HAS CORROSION FROM FR55 TO FR59 - SUPPORT TASK - GENERATED BY MECH V061644 ON N/R 9292385 AT HAECO LCQ REMOVED AND REPLACED CONNECTING PLATE FOR THE AFT PIT TORSION BO X COVER AND THRESHOLD IAW A319
- [SDR CALA2020020200292](https://openairdocs.org/sdr/CALA2020020200292.md): Threshold · corroded · Jan 27, 2020 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT THRESHOLD HAS CORROSION THROUGHOUT. REMOVED AND REPLACED AFT PIT THRESHOLD IAW A319 SRM 51-72-11. OP S CHECKED GOOD ON ALL DISTURBED SYSTEMS. PERFORMED BY MECH V0616 44 AND INSP BY V077960.
- [SDR CALA2019052400831](https://openairdocs.org/sdr/CALA2019052400831.md): Fuel Cap · missing · May 24, 2019 · N852UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING, INBOUND TO MEX. SEE LOG PAGE 3295327 FOR ACTION TAKEN. CONTACTED IAH, NO FUEL CAPS FOUND ON INVESTIGATION. MISSING CAP TO BE REPLACED ON LOG PAGE 3295327 REF GMM 02-30-95.
- [SDR CALA2019020800232](https://openairdocs.org/sdr/CALA2019020800232.md): Proximity Sensor · out of tolerance · Feb 8, 2019 · N852UA · Airbus A319131 · Landing Gear Position and Warning
  > L/G SHOCK ABSORBER FAULT AT GEAR RETRACTION.GEAR DID NOT RETRACT ACP JACKING OF A/C NLG PER MM7-11-010-581-003-A AND THAN ACP NLG SWING PER MM32-31-00-720-003-A FOUND TARGET SENSOR INTERMITTENL Y OUT OF TARGET RANGE DUE HISTORY OF SAME WRITE UPS FOUND TARGET A
- [SDR CALA2018121402580](https://openairdocs.org/sdr/CALA2018121402580.md): Bottle · empty · Dec 13, 2018 · N852UA · Airbus A319131 · Escape Slide
  > FOUND DOOR 1 LEFT SLIDE PARTIALY DEPLOYED AND DOOR ASSIST BOTTLE EMPTY. REPLACED DOOR 1LEFT ESCAPE SLIDE PACK REF AMM 25-62-44-400-006-A THRU STEP 4A PG 9. CONTINUE AT STEP 4B PG 9. ADD EMP:U348944,U349201,U109226 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1207
- [SDR CALA2017082102820](https://openairdocs.org/sdr/CALA2017082102820.md): Oven · smoke · Aug 21, 2017 · N852UA · Airbus A319131 · Buffet/Galleys
  > AFT OVEN 405-131 SMOKING, SET OFF BOTH AFT LAVATORY SMOKE DETECTORS. PERFORMED OPS CHECK OF OVEN. NO FAULTS FOUND AT THIS TIME. OK FOR SERVICE.
- [SDR CALA2017060501729](https://openairdocs.org/sdr/CALA2017060501729.md): Power Supply · inoperative · Jun 5, 2017 · N852UA · Airbus A319131 · Emergency Lighting
  > RIGHT OVERWING EMERGENCY EPSU INOPERATIVE. REMOVED AND REPLACED EPSU AND BATTERY IAW AMM 33-51-000-001-A, 3 3-51-38-400-001-A, 33-51-38-000-002-A, AND 33-51-38-400-002-A. OPS T ESTED GOOD IAW AMM 33-51-00-710-001-A.
- [SDR CALA2015040793509](https://openairdocs.org/sdr/CALA2015040793509.md): Engine · fire · Apr 4, 2015 · N852UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > NUMBER 2 ENG FIRE AT START. APPROACHED EGT LIMIT & APPEARED FUEL VLV DIDN'T CLOSE. BORECOPE INSPECTION OF HP TURBINE BLADE & COMBUSTION CHAMBER WITH NO LIMITING DEFECTS FOUND. PNEUMATIC HEALTH CHECKS COMPLETE. R & R PCMIA CARD & REVIEW.
- [SDR CALA2014082192005](https://openairdocs.org/sdr/CALA2014082192005.md): Epsu · inoperative · Aug 20, 2014 · N852UA · Airbus A319131 · Emergency Lighting
  > NUMEROUS EMER ESCAPE PATH LIGHTS INOPERATIVE THROUGHOUT CABIN DURING HMV TEST. R & R EPSU 10WL IAW AMM 33-5 1-38-000-001-A & 33-51-38-400-001-A. R & R BATTERY PACK 13WL IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A, EEPL LIGHTS OPERATIONS CHECKED GOOD IAW
- [SDR CALA2014081891995](https://openairdocs.org/sdr/CALA2014081891995.md): Stringer · corroded · Aug 15, 2014 · N852UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 42R AT FRAME 60 IN AFT PIT. UPON FURTHER EVALUATION FOUND STRINGER 42R CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF STRINGER & SPLICED IN NEW SECTION OF STRINGER BETWEEN FRAME 59.5 & 60.5 IAW SRM 53-00-13 FIG 201.
- [SDR CALA2014081391982](https://openairdocs.org/sdr/CALA2014081391982.md): Door Sill · corroded · Aug 11, 2014 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FWD & AFT HAS CORROSION FRAME 68 - 68, STRINGER 22L - 23L. FABRICATED & INSTALLED REPAIR IAW SRM 53-41-14 REPAIR PRINCIPLE 5 FIG 201 SHEET 3 AREA K.
- [SDR CALA2014081391976](https://openairdocs.org/sdr/CALA2014081391976.md): Door Sill · corroded · Aug 10, 2014 · N852UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL WAS FOUND CORRODED. SILL REPLACED IAW SRM 51-42-11.
- [SDR CALA2014081391975](https://openairdocs.org/sdr/CALA2014081391975.md): Stringer · corroded · Aug 9, 2014 · N852UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER 31R CORRODED BETWEEN FRAME 65 & 66. STRINGER SECTION WAS REPLACED FROM FRAME 65 - 69 IAW SRM 53-00-13.
- [SDR CALA2014081191949](https://openairdocs.org/sdr/CALA2014081191949.md): Door Frame · corroded · Aug 7, 2014 · N852UA · Airbus A319131 · Fuselage Main, Structure
  > DETAILED INSPECTION, ROTO OF AFT PAX CREW DOOR CUT OUT. DOOR STOP FITTINGS HOLES, AT FRAME 68 WEB, LT & RT IAW AMM 53-41-00-220-813. CORROSION DMG NOTED AT R2 POS 1, 2, 3 & 6. L2 NR 2. CLEANED & RESCANNED, NO INDICATIONS.
- [SDR CALA2014061791298](https://openairdocs.org/sdr/CALA2014061791298.md): Warning System · faulty · Jun 17, 2014 · N852UA · Airbus A319131 · Door Warning System
  > RIGHT WING OVERWING EXIT NOT SHOWING ARMED. PLACED ON MEL, DDP COMPLIED WITH.

Next page: https://openairdocs.org/aircraft/N852UA/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 = 'N852UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N852UA/reports

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