# Service difficulty reports: N814UA

A list on [N814UA](https://openairdocs.org/aircraft/N814UA.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 · 134 reports

- [SDR CALA2026092819854](https://openairdocs.org/sdr/CALA2026092819854.md): Oil System · low · Sep 24, 2026 · N814UA · Airbus A319131 · Turbine Engine Oil System
  > ENG 1 LOW OIL, AFTER ROTATIONIND 4.5 QT AFTER LEVEL OFF 6-8 QT ENGINE 1 FAN COWLS AND THRUST REVERSERS OPENED TO PERFORM VISUAL INSP OF ENGINE. NO LEAKS NOTED. SERVICED ENGINE WITH 9 QUARTS OF OIL AND PERFORMED DRY MOTOR OF ENGINE 1 IAW AMM TASK 71-00-00-710-0
- [SDR CALA2026082718946](https://openairdocs.org/sdr/CALA2026082718946.md): Frame · cracked · Jul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 16 RT DOUBLE JOGGLE HOLES NR 1, 6, & C HAD CRACK INDICATIONS DURING ACCOMPLISHMENT OF TC 17-5311-1-2837. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5311-02463, PART 1, ITEM 1. IAW ECRA PART 1 ITEM 2.
- [SDR CALA2026082718944](https://openairdocs.org/sdr/CALA2026082718944.md): Frame · cracked · Jul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, Frame
  > EA 5341-01231 004, RT SIDE FRAME 68 AT STR 22 INNER CAP & WEB FLANGE IS CRACKED 6.50 INCH LONG. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01578 WITHOUT DEVIATIONS. ORIGINAL DISCREPANCY UNDER LCQ NR 9292250 AND ECRA 5341-01231. CARRIED TO ACCOMPLISH
- [SDR CALA2026081218525](https://openairdocs.org/sdr/CALA2026081218525.md): Door Frame · damaged · Jul 25, 2026 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT FR 16 DOOR STOP FITTING NR 1, HOLE NR 3, ELONGATED AND PREVIOUS REPAIR AT CROSSBEAM. INTERIM REPAIR ACCOMPLISHED IAW 5311-03459 WITHOUT DEVIATION. ORIGINAL DISCREPANCY UNDER LCQ NR 9292380 AND LP 9532232.
- [SDR CALA2026072618004](https://openairdocs.org/sdr/CALA2026072618004.md): Door Frame · cracked · Jul 23, 2026 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > R2 DOOR FR 68, NR 7 DOOR STOP LOWER INBD HOLE WAS CRACKED, REAMED HOLE IAW SRM 52-41-12, FG 202. NDT INSP IAW 51-10-01 AND NO CRACK NOTED. FABRICATED FREEZE PLUG AND WASHER, INSTALLED IAW 53-41-12. PERFORMED GVI ON R2 DOOR NR 7 DOOR STOP LWR INBD HOLE NO D
- [SDR CALA2026083119100](https://openairdocs.org/sdr/CALA2026083119100.md): Frame · cracked · Jul 6, 2026 · N814UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FRAME 68, STR 22L HORIZONTAL STIFFENER LOWER RADIUS FLANGE CRACKED. INNER FLANGE & HORIZONTAL FLANGE FILLET RADII. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01576 WITHOUT DEVIATIONS.
- [SDR CALA2026083119098](https://openairdocs.org/sdr/CALA2026083119098.md): Frame · corroded · Jul 2, 2026 · N814UA · Airbus A319131 · Fuselage Main, Frame
  > RIGHT FRAME 66, STR 22-23, HAS 7 HOLES WITH REJECTABLE INDICATIONS. HAD VISIBLE CORROSION SURROUNDING IT ON AFT FACE. REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01577 WITHOUT DEVIATION.
- [SDR CALA2026063017456](https://openairdocs.org/sdr/CALA2026063017456.md): Frame · damaged · Jun 28, 2026 · N814UA · Airbus A319131 · Fuselage Main, Frame
  > UPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND FR67 FRAME TO HAVE MULITPLE ELONGATED FASTENER HOLES. REMOVED AND REPLACED RT FR67 FRAME IAW SRM 51-44-11 AND 51-42-11.
- [SDR CALA2026063017430](https://openairdocs.org/sdr/CALA2026063017430.md): Door Sill · corroded · Jun 26, 2026 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > UPON REMOVAL OF R2 DOOR SILL TO FOM FR68 FRAME REPLACEMENT FOUND DOOR SILL TO HAVE CORROSION AND MULTIPLE ELONGATED FASTENER HOL ES. REMOVED AND REPLACED R2 DOOR SILL IAW A319 UAL SRM 51-44-11 AND 51-42-11.
- [SDR CALA2024092600691](https://openairdocs.org/sdr/CALA2024092600691.md): Packing · damaged · Sep 25, 2024 · N814UA · Airbus A319131 · Hydraulic System, Main
  > Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD RECIEVED ECAM ON T/O AFTER POWER BROUGHT UP DEBRIEFED CREW, PUMPS RUN TIME DID NOT EXCEED 5 MINUTES AFTER RUNNING. PERFORMED INSPECTION OF DPI REF 29-00-00-280-006. NO LOW LEVEL WARNING. UPON INSPECTION FOUND
- [SDR CALA2023122803744](https://openairdocs.org/sdr/CALA2023122803744.md): Fuel Cap · missing · Dec 23, 2023 · N814UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING APPLY CDL 28A INOP STICKER APPLIED IN FLIGHT DECK DISPATCH DESK: 24 NAME: RB DATE: 22-DEC-23- APPROVED CDL FOR MISSING FUEL CAP. INSTALLED NEW FUEL CAP AND NOTICED THE ADJUSTMENT IS NOT CORRECT.(SEE PICTURES). NECESSARY ADJUST THE FUEL CAP AS
- [SDR CALA2023092002836](https://openairdocs.org/sdr/CALA2023092002836.md): Bleed Air Sys · warning message · Sep 19, 2023 · N814UA · Airbus A319131 · Engine Bleed Air System
  > ENG 2 BLEED LEAKECAM...SHUT BLEED OFFPER ECAM PERFORMED LEAK CK / ENGINE RUN ON ENG 2. NO LEAKS NOTED. NO MESSAGES, BITE CK OF BMC SHOWED NO FAULTS. PFR SHOWED NO CURRENT FAULTS. ALL WORK IAW AMM 36-22-16. OK FOR CONTINUED SERVICE. PERFORMED LEAK CK / ENGINE R
- [SDR CALA2023071402243](https://openairdocs.org/sdr/CALA2023071402243.md): Door Frame · cracked · Jul 13, 2023 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > R/H EMERGENCY EXIT FWD FRAME CRACKED PER HAECO LCQ N/R 9294845/ 24845 GEN BY REMOVED AND REPLACED RH EMERGENCY EXIT FWD FRAME IAW UAL SRM 51- 72-11-911-001
- [SDR CALA2023071002201](https://openairdocs.org/sdr/CALA2023071002201.md): Stringer · corroded · Jul 8, 2023 · N814UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER 31R AT FR65 HAS CORROSION JUST FWD OF OUT FLOW VALVE PER HAECO LCQ N/R 9294579/24579 GEN BY V926223
- [SDR CALA2023071002200](https://openairdocs.org/sdr/CALA2023071002200.md): Door Sill · corroded · Jul 8, 2023 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AT FR66 AND FR68 PER HAECO LCQ N/R 9294633/24633 GEN BY V061603
- [SDR CALA2023033100956](https://openairdocs.org/sdr/CALA2023033100956.md): Connector · leaking · Mar 31, 2023 · N814UA · Airbus A319131 · Hydraulic System, Main
  > HYD RESERVOIR FILL CONNECTOR SPINS UNABLE TO ATTACHED SERVICER SERVICEABLE NON-COSMETIC INT DIP ABLE TO SECURE HYD FILL CONNECTION LOCKING PLATE TANGS FOR CONTINUED SERVICING THRU QUICK DISC SERVICE PORT. REQ CARRY APPROVED PER GMM 05-30-06. AT NEXT MAINTENAN
- [SDR CALA2023032700894](https://openairdocs.org/sdr/CALA2023032700894.md): Reservoir · unknown · Mar 27, 2023 · N814UA · Airbus A319131 · Hydraulic Power System
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD FOUND YELLOW HYDRAULIC SYSTEM VERY LOW, SERVICED WITH 3 GALLONS RAN YELLOW HYDRAULICS FOR 2+ HOURS WHILE CYCLING FLIGHT MAIN WING FUEL TANKS AND INSPECTED FOR POSSIBLE HYDRAULIC HYDRAULIC FLUID. T/S PER T
- [SDR CALA2022090502253](https://openairdocs.org/sdr/CALA2022090502253.md): Fitting · none · Sep 2, 2022 · N814UA · Airbus A300* · Fuselage Main, Frame
  > ON OR BEFORE AIRCRAFT N814UA (4014) ACCUMULATE 37,170 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION OF THE LH WINDOW FRAME CONTINUITY FITTING AREA AROUND THE INSTALLED WASHERS PER PART 2 STEP 1 OF THE LATEST REVISION OF EC 5311-02875, THERE AFTER REPEAT INS
- [SDR CALA2022081002023](https://openairdocs.org/sdr/CALA2022081002023.md): Skin · damaged · Aug 9, 2022 · N814UA · Airbus A319131 · Wing, Control Surface Attach Fittings
  > DEEP SCRATCH FOUND ON RH SLAT NO.3 INBD TRAILING EDGE SIDE CAUSED BY RUBBING ON 622BT PROTRODING SCREW HEAD. REQUIRES FURTHER EVALUATION. LTPR NR# 5001173902-0010. CREATED DMG REF GMM 06-35-05. THIS IS A CAT "A" RPR WITH NO REINSPECTION REQUIRED. PERFORMED REP
- [SDR CALA2021031500321](https://openairdocs.org/sdr/CALA2021031500321.md): Pipe · leaking · Mar 15, 2021 · N814UA · Airbus A319131 · Hydraulic System, Main
  > *EMERGENCY DECLARED* HYD Y RSVR LO LVL ECAM AT CRUISE. LOST YELLOW SYSTEM AND ACCUMULATOR. PYLON LEAKING,PART. # D2901010201200,TUBING REMOVED NEED TO BE INSTALLED. INSPECTED HYDRAULIC LEAK AT #2 ENGINE AND FOUND TUBING IN THE LOCKED FOR POSITIVE FIX. CONTACT
- [SDR CALA2020123001413](https://openairdocs.org/sdr/CALA2020123001413.md): Landing Gear · malfunctioned · Dec 29, 2020 · N814UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. GEAR DOORS OPERATED NOR MALLY UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT NLG FOR ANY OBVIOUS DEFECTS AND REPORT TO TOMC LOCKED FOR GEAR DOWN FERRY.
- [SDR CALA2020080901090](https://openairdocs.org/sdr/CALA2020080901090.md): Battery Pack · discharged · Aug 5, 2020 · N814UA · Airbus A319131 · Emergency Lighting
  > BATTERY PACK FOR 13WL WILL NOT PASS CAPACITY CHECK. REMOVED AND REPLACED THE BATTERY PACK 13WL AND OP CHECKED GOOD IAW AMM 33-51-38-000-002-A & 33-51-38-400-002-A.
- [SDR CALA2020020800345](https://openairdocs.org/sdr/CALA2020020800345.md): Pressure Deck · cracked · Feb 5, 2020 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > REF EA 5330-05216 REV A STEP 3.2 #4 HOLE IS CRACK ON THE ALUMINUM PRESSURE DECK PANEL ONLY. REPAIRED #4 HOLE ON PRESSURE DECK PANEL REF. EC/RA#: 5331-02602. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5331-02602 ON OR BEFORE THE AIRCRAFT REA
- [SDR CALA2019071501207](https://openairdocs.org/sdr/CALA2019071501207.md): Pedestal · inoperative · Jul 15, 2019 · N814UA · Airbus A319131 · Weather Radar System
  > WX RADAR INOP.WR ANT AND WR R/T MSGON BOTH NDS WXR R/T PN ON: 066-50008-0409 SN ON: 10041 SN OFF: 10065 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1365535 SN OFF 0065 TRANSCEIVER, WX OFF 31-2311-9-0001 0065 ON 31-2311-9-0001 8041 REMOVED AND REPLACED WEATHER
- [SDR CALA2019011300073](https://openairdocs.org/sdr/CALA2019011300073.md): Selector · faulty · Jan 10, 2019 · N814UA · Airbus A319131 · Landing Gear Brake System
  > HAD AUTOBRAKE FAULT ECAM. WHICH SHOWED NORM BRAKES INOP WHICH I S NAGAINST MEL. INTERVIEWED CREW: FLIGHT CREW STATED THAT ECAM MESSAGE CAME ON DURING CRUISE AND THEN WENT AWAY. MESSAGE RETURNED AGAIN DURING LANDING/ROLL OUT. ALSO, THERE IS A NOTICEABLE
- [SDR CALA2018081701808](https://openairdocs.org/sdr/CALA2018081701808.md): Transmitter · failed · Aug 15, 2018 · N814UA · Airbus A319131 · Landing Gear Brake System
  > BRAKES SYS NR 1 FAULTED. RESET THE NOSE WHEEL STEERING ONCE, MESSAGE STILL DISPLAYED. RAN BSCU SYSTEM TESTS. FAULTS ON BSCU 1 BRAKE PEDAL TRANSMITTER 9GG. REPLACED THE BRAKE PEDDAL TRANSMITTER IAW MM 32-42-47. BITE TESTED BSCU 1 AND 2. NO FAULTS.
- [SDR CALA2018071001581](https://openairdocs.org/sdr/CALA2018071001581.md): Fitting · corroded · Jun 25, 2018 · N814UA · Airbus A319131 · Passenger/Crew Doors
  > L2 DOOR AFT LOWER CORNER FITTING HAS CORROSION. REMOVED AND REPLACED L2 DOOR AFT LOWER CORNER FITTING IAW SRM 51-42-11-001.
- [SDR CALA2018041601167](https://openairdocs.org/sdr/CALA2018041601167.md): Power Supply · no test · Apr 16, 2018 · N814UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS FAILED TO TEST, EPSU REMOVED & REPLACED IAW AMM 33-50-00, OPS CHECKED GOOD.
- [SDR CALA2017122904664](https://openairdocs.org/sdr/CALA2017122904664.md): Battery Pack · inoperative · Dec 29, 2017 · N814UA · Airbus A319131 · Emergency Lighting
  > FOUND SEVERAL EMERGENCY LIGHTS NOT WORKING, REPLACED L1 AND LEFT EMERGENCY DOOR BATTERY PACKS. SYSTEM OPS NORMAL.
- [SDR CALA2017032500720](https://openairdocs.org/sdr/CALA2017032500720.md): Altimeter · faulty · Mar 25, 2017 · N814UA · Airbus A319131 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER INDICATION ERRONEOUS AT FL370 STBY ALT READS FL358. ACCOMPLISHED FUNCTIONAL TEST REF AMM34-21-00. STBY ALT NEEDLE STICKS. REPLACED STBY ALTIMETER REF AMM34-21-22 OPS CHECKS NORMAL.
- [SDR CALA2016110295889](https://openairdocs.org/sdr/CALA2016110295889.md): Skin · cracked · Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LT FUSE SKIN AT FR35 STR 30L HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM REPAIR ACP IAW EC RA5330-05813 PART 1.
- [SDR CALA2016110295888](https://openairdocs.org/sdr/CALA2016110295888.md): Skin · cracked · Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RT FUSE SKIN AT FR35 STR 30R HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM RPR ACP IAW ECRA 5330-05813 PART 1.
- [SDR CALA2016103195877](https://openairdocs.org/sdr/CALA2016103195877.md): Fitting · corroded · Oct 24, 2016 · N814UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > R1 DOOR SILL FWD GIRT BAR FITTING AREA CORROSION AROUND FWD OUTBD, AFT INBD, & AFT OUTBD HOLE AT FR20 STR23. REMOVED CORROSION BY SPOT FACING ALL 3 HOLES ON FR20.017.025.020 MATERIAL REMOVED & FOUND TO BE IN LIMITS IAW A319 SRM53-11-14 FIG 108 PARA 7B FAB
- [SDR CALA2016102495851](https://openairdocs.org/sdr/CALA2016102495851.md): Threshold · corroded · Oct 24, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO THRESHOLD WEB HAS CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-21-13 PG 101-104.
- [SDR CALA2016101995833](https://openairdocs.org/sdr/CALA2016101995833.md): Door Sill · corroded · Oct 18, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR CUTOUT FWD LOWER CORNER HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11.
- [SDR CALA2016101995818](https://openairdocs.org/sdr/CALA2016101995818.md): Door Sill · corroded · Oct 17, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FR68 HAS CORROSION AROUND THE LAST TWO NUT PLATE HOLES AFT END AT DOOR SILL. REMOVED CORROSION AND FABBED REPAIR DOUBLER AND INSTALLED IAW SRM 53-41-14 PARA 5A FIG201 REPAIR PRINCIPLE 5.
- [SDR CALA2016101395796](https://openairdocs.org/sdr/CALA2016101395796.md): Shear Plate · corroded · Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR 70 STR 23 RT, AFT CORNER LOWER PANEL HAS CORROSION ON PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11.
- [SDR CALA2016101395795](https://openairdocs.org/sdr/CALA2016101395795.md): Door Sill · corroded · Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL CORROSION NUMEROUS AREAS BETWEEN FR59 & FR56. REMOVED AND REPLACED AFT CARGO SILL IAW SRM 51-42-11.
- [SDR CALA2016101395794](https://openairdocs.org/sdr/CALA2016101395794.md): Structure · corroded · Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT THRESHOLD CONNECTION HAS CORROSION. REMOVED AND REPLACED AFT PIT THRESHOLD SHEET CONNECTION IAW 51-42-11.
- [SDR CALA2016101395793](https://openairdocs.org/sdr/CALA2016101395793.md): Plate · corroded · Oct 10, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY SUPPORT PLATE JUST INBD OF DOOR SILL CORRODED AROUND FWD-TIE DOWN AT FR56. REMOVED AND REPLACED WITH NEW THRESHOLD PLATE AT AFT CARGO LOWER DOOR FROM FR55.5 TO FR59 IAW SRM 51-42-11.
- [SDR CALA2016101395800](https://openairdocs.org/sdr/CALA2016101395800.md): Support Frame · corroded · Oct 8, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RT WW SHEAR PLATE SUPPORT FRAME BETWEEN FR69-FR90 FOUND TO HAVE CORROSION. REMOVED AND REPLACED RT SHEAR PLATE SUPPORT FRAME IAW SRM 51-72-11.
- [SDR CALA2015091894368](https://openairdocs.org/sdr/CALA2015091894368.md): Computer · malfunctioned · Sep 15, 2015 · N814UA · Airbus A319131 · Fuel Indicating System
  > CENTER FUEL TANK PUMPS WILL NOT TURN ON AFTER FLAP SLAT RETRACTION. CYCLING OF AUTO FUEL FEED PB SWITCH FROM AUTO TO MANUAL, NO HELP. UNABLE TO MOVE FUEL OUT OF CTR FUEL TANK. NO INFLIGHT RESET AVAILABLE, ACFT DIVERTING, BOTH CTR TANK GFIS & FQIC WERE REPLA
- [SDR CALA2015062494020](https://openairdocs.org/sdr/CALA2015062494020.md): Hydraulic System · low · Jun 22, 2015 · N814UA · Airbus A319131 · Hydraulic System, Main
  > CREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS, CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSEL
- [SDR CALA2015062294004](https://openairdocs.org/sdr/CALA2015062294004.md): Fluid · low · Jun 22, 2015 · N814UA · Airbus A319131 · Hydraulic System, Main
  > CREW REPORT, HYD GREEN ENG 1 PUMP LO PSI WITH HYD GREEN RSVR LO LEVEL. FLIGHT CREW SHUTDOWN GREEN SYS BEFORE QTY EMPTIED IAW QRH. SERVICED GREEN HYD SYS & CHECKED FOR HYD LEAKS. PERFORMED FLIGHT CONTROL CHECK, NO LEAKS NOTED. NO LEAKS NOTED ON ACFT ON FUSE
- [SDR CALA2015051993800](https://openairdocs.org/sdr/CALA2015051993800.md): Sensor · corroded · May 15, 2015 · N814UA · Airbus A319131 · Landing Gear Position and Warning
  > CREW RETURNED TO THE FIELD DUE TO MLG NOT RETRACTING WHEN SELECTED UP. AHM IS FAULTING THE LT GEAR EXTEND PROX SENSOR 21GA. REPLACED 21GA SENSOR DUE TO CORROSION. REPLACED LT MLG MAIN GEAR HARNESS CONNECTOR INSIDE J BOX. REPLACED LT 1M HARNESS, LT 2M ENHAN
- [SDR CALA2015021293119](https://openairdocs.org/sdr/CALA2015021293119.md): Door Sill · corroded · Feb 11, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AT FRAME 66. REPLACED R2 DOOR SILL IAW SRM 51-44-11 & 51-42-11.
- [SDR CALA2015021293146](https://openairdocs.org/sdr/CALA2015021293146.md): Door Frame · cracked · Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT NR 2 DOOR FRAME 68, NR 7 DOOR STOP, LOWER INBD HOLE HAS CRACK INDICATION. REAMED HOLE IAW SRM 52-41-12 FG 202, NDT INSPECTION IAW 51-10-01 & NO CRACK NOTED. FABRICATED FREEZE PLUG & WASHER & INSTALLED IAW 53-41-12.
- [SDR CALA2015021293145](https://openairdocs.org/sdr/CALA2015021293145.md): Door Sill · corroded · Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SHAPE SILL ON R2 DOOR SILL IS CORRODED. R & R DOOR SILL IAW SRM 53-41-14 FIG 101.
- [SDR CALA2015021293144](https://openairdocs.org/sdr/CALA2015021293144.md): Fitting · corroded · Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR CUT OUT AFT CORNER FITTING AT FRAME 68 IS CORRODED. REMOVED & REPLACED FITTING IAW SRM 53-41-14 FIG 101.
- [SDR CALA2015021293143](https://openairdocs.org/sdr/CALA2015021293143.md): Fitting · corroded · Feb 9, 2015 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FRAME 66 R2 DOOR FWD CORNER FITTING CORRODED. R & R CORNER FITTING IAW SRM 53-41-14 FIG 101.

Next page: https://openairdocs.org/aircraft/N814UA/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 = 'N814UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N814UA/reports

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