# Service difficulty reports: N898UA

A list on [N898UA](https://openairdocs.org/aircraft/N898UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA2026081318571](https://openairdocs.org/sdr/CALA2026081318571.md): Control Module · faulted · Aug 11, 2026 · N898UA · Airbus A319132 · Landing Gear Steering System
  > AFTER NR 1 ENG START LOUD HARMONIC VIBRATION NOISE UNDER FLT DECK FLOOR, STARTED ENGINE 1 & OBSERVED LOW HARMONIC HUM OR BUZZ. STARTED ENGINE 2 BUZZ REMAINED. DESELECTED ENGINE 1 HYD PUMP & THEN ENGAGED PUMP AGAIN. NO FLUCTUATIONS OBSERVED IN GREEN SYS QTY OR
- [SDR CALA2026061617140](https://openairdocs.org/sdr/CALA2026061617140.md): Battery · inoperative · Jun 15, 2026 · N898UA · Airbus A319132 · Emergency Lighting
  > DURING TEST OF EMERGENCY LIGHTS EPSU R BATTERY WAS INOPERATIVE. R & R EPSU R BATTERY. SYSTEM TEST PASSED 33-51-38/401.
- [SDR CALA2026060116718](https://openairdocs.org/sdr/CALA2026060116718.md): Skin · damaged · May 18, 2026 · N898UA · Airbus A319132 · Nacelle/Pylon, Plate/Skin
  > AIR INTAKE COWL SHOWS SIGN OF LIGHTNING STRIKE. PICT AND DIMENSION. 6 O'CLOCK POSITION. DIMENSIONS PER ATTACHED IMAGE: 3/16 INCH WIDE, 1/4 INCH WIDE, 0.024 INCH DEEP. AFT EDGE OF DAMAGE IS 9/16 INCH FORWARD OF AFT EDGE OF INLET COWL. REMOVED AIR INTAKE COWL
- [SDR CALA2026032314792](https://openairdocs.org/sdr/CALA2026032314792.md): Packing · leaking · Mar 20, 2026 · N898UA · Airbus A319132 · Hydraulic System, Main
  > HYD Y RSVR LO LVL ECAM PROCEDURE COMPLIED CONTACT TOMC 847-700-9980 FOUND YELLOW SYSTEM HYDRAULICS DEPLETED. INSPAECTED AIRCRAFT BELLY AND FOUND HYDRAULIC FLUID COVERING BELLY OF AIRCRAFT, MAINLY RH GEAR SIDE PIC ADDED CREW ALSO SAID THEY ACCOMPLISHED THE SHU
- [SDR CALA2026020913643](https://openairdocs.org/sdr/CALA2026020913643.md): Outflow Valve · faulted · Feb 6, 2026 · N898UA · Airbus A319132 · Pressure Regulator/Outflow Valve
  > FOUND BLOWN DUCT ON RT SIDE AFT E&E BAY. PT NO. DOESNT BREAK REMOVED BLOWN DUCT FROM AFT E&E BAY REF IPC 21-26-01-14B, 21-26-01-18A. LEFT DAMAGED DUCT IN AFT E&E. PULLED CIRCUIT BREAKERS D5, D6, Y17, AE02 FOR MX, REF AMM 21-26-11 REMOVED BLOWN DUCT FROM AFT E&
- [SDR CALA2026020313529](https://openairdocs.org/sdr/CALA2026020313529.md): Accumulator · overserviced · Jan 30, 2026 · N898UA · Airbus A319132 · Hydraulic System, Main
  > AT 85 KTS, DURING TAKE OFF ROLL, HYD B ELEC PUMP LOW PRESSURE ECAM. B QTY BELOW RANGE AFTER REJECT. UPON RETURN TO GATE, PRESSURE NORMAL & QTY NORMAL SECOND REJECTED TAKE OFF IN 2 DAYS. ACCUMULATOR PRESSURE 700 PSI. PRESSUIZED HYD B SYS. ONLY GOT 700
- [SDR CALA2026020213490](https://openairdocs.org/sdr/CALA2026020213490.md): Hydraulic System · overserviced · Jan 29, 2026 · N898UA · Airbus A319132 · Hydraulic System, Main
  > HYDRAULIC B LOW PRESSURE ECAM ON TAKEOFF ROLL.. ACCOMPLISHED TBS TASK 29-12-00-810-804-A, FOUND BLUE HYD SYS OVERSERVICED & ACCUMULATOR LOW PRESS. BLED HYD SYS AND SERVICED TO PROPER LEVEL. BLUE HYD ACCUMULATOR TO CORRECT PRESSURE IAW AMM 12-14-29. ACCOMPLISH
- [SDR CALA2025121512115](https://openairdocs.org/sdr/CALA2025121512115.md): Battery Pack · inoperative · Dec 13, 2025 · N898UA · Airbus A319132 · Emergency Lighting
  > AFT LEFT EPSU BATTERY FAULTED. REPLACED AFT LEFT EPSU BATTERY REF AMM 33-51-38. OPS CHECK GOOD REF AMM 33-51-00. NO DEFECTS NOTED.
- [SDR CALA2025111811321](https://openairdocs.org/sdr/CALA2025111811321.md): Skin · dented · Oct 31, 2025 · N898UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > LEFT FWD EXT FUSELAGE, APPROX FR 8,S23L DENTED. EVALUATED DENT BETWEEN FR 9 - 10 LT, DENT IS 3IN AFT OF FR 9 AND 1.37 5IN ABOVE S23L IAW SRM 53-11-11-283-012. DENT IS TYPE 1 AS D=0.025IN, A=1.375IN, D/A = 0.025IN/1.375IN= 0.018IN AND IS LESS THEN 0.100IN. P
- [SDR CALA2025080807476](https://openairdocs.org/sdr/CALA2025080807476.md): Proximity Sensor · faulted · Jul 28, 2025 · N898UA · Airbus A319132 · Landing Gear Position and Warning
  > CHRONIC LEVEL 1 - LGCIU 1 FAULT DUE TO HISTORY OF L/G LGCIU 1 FAULTS WITH AIRMAN REPORTING 32-31 -73 R LG DOOR PROX SNSR 26GA, REF TSM TASK 32-31-00-810-819-A, PERFORM BITE OF LGCIU 1 FOR FAULT CODES. REF ASM 32-31-03 CHECK RESISTANCE AND INSULATION RESISTANCE
- [SDR CALA2025072806943](https://openairdocs.org/sdr/CALA2025072806943.md): Unknown · odor · Jul 27, 2025 · N898UA · Airbus A319132 · Air Distribution System
  > SUSPECTED BURNING RUBBE RY SMELL IN COCKPIT WHEN PACK 1 ON PACK TEMP 165 PACK 1 OFF SMELL LESS PILOT REPORTED PACK TEMP ON #1 165 PACK #2 115 RAN PACK ON BOTH ENG BLEED AIR AND APU BLEED FOUND TO BE OPERATING NORMAL PACK 1 WAS 165 PACK # 2 155 NO BURNING SMELL
- [SDR CALA2025031302798](https://openairdocs.org/sdr/CALA2025031302798.md): Proximity Sensor · faulted · Mar 10, 2025 · N898UA · Airbus A319132 · Door Warning System
  > DOOR R2 IS DIARMED BUT K EEPS INDICATING IN AND O UT OF BEING AR MED DOOR 2R HAS ERRONEOUS SLIDE INDICATIONS ON ECAM DOOR PAGE, HAS HISTORY. REQUEST MEL 2560SR MEL 2560SR REJECTING FOR POSITIVE FIX. LOCKING FOR TELEFLEX ADJ AND VERFICATION OF FLOOR FITTING ARM
- [SDR CALA2025030502598](https://openairdocs.org/sdr/CALA2025030502598.md): Indicator · faulted · Mar 2, 2025 · N898UA · Airbus A319132 · Door Warning System
  > DOOR 2R ARMED LIGHT COMES ON WHEN DOOR DISARMED AND DOOR OPEN DOOR ARMED SWITCH IN FLIGHT DECK AND THE SLIDE ARMED SWITCH ON DOOR NOT WORKNG CORRECTLY. SLIDE ARMED LIGHT COMES ON ANYTIME DOOR IS OPENED REGARDLESS OF ARMED HANDLE POSITION. FLIGHT DECK INDICAT
- [SDR CALA2025030402570](https://openairdocs.org/sdr/CALA2025030402570.md): Light · faulted · Mar 2, 2025 · N898UA · Airbus A319132 · Door Warning System
  > DOOR 2R SHOWS ARMED AFTER FAS DISARMED IT REF. LP 4046596, CHECKED DOOR 2R HANDLE PROXIMITY SENSORS REF. AMM 52-71-00-820-002-A. SENSORS OK. REMOVED AND REPLACED DOOR 2R SLIDE ARMED LIGHT ASSEMBLY REF. AMM 52-73-21-400-002-A OPS CHECK GOOD. INDICATIONS GOOD IN
- [SDR CALA2025030302542](https://openairdocs.org/sdr/CALA2025030302542.md): Indicator · false activation · Feb 27, 2025 · N898UA · Airbus A319132 · Accessory Compartment
  > DOOR 2R DISARMED SLIDE INDICATION ON ECAM FLASHING SLIDE ECAM MSG ERRONEOUS. DOOR 2 R ARMS AND DISARM OPERATES NORMALLY. INDICATION PROBLEM ONLY. APPROVED OK TO MEL 2560SR *DM* REF TSM 52-13-00-810-804-A FOR T/S ASSISTANCE. CANNOT REDUPLICATE FLASHING SLIDE ON
- [SDR CALA2025022402426](https://openairdocs.org/sdr/CALA2025022402426.md): Battery · no test · Feb 23, 2025 · N898UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - ALL 4 BATTERY PACKS FAIL 30 MINUITE TEST, MUST BE REPLACED. EMERGENCY BATTERY PACK TESTED ALL 4 NEW BATTERY PACKS IAW W / C A3NB-33-3-0002, NO FAULTS NOTED, ALL EMERGENCY LIGHTS OP
- [SDR CALA2024111101103](https://openairdocs.org/sdr/CALA2024111101103.md): None · pax error · Nov 10, 2024 · N898UA · Airbus A319132 · Smoke Detection
  > MASTER WARNING ECAM LAV SMOKE DISAPPEARED AFTER 30 SECONDS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CREW REPORTED ECAM CLEARED ON ITS OWN. NO FAULTS ON ARRIVAL TO ACFT. VERIFIED NO SMELL IN ANY LAVS. SUSPEC
- [SDR CALA2024091602437](https://openairdocs.org/sdr/CALA2024091602437.md): Control Unit · faulted · Sep 13, 2024 · N898UA · Airbus A319132 · Landing Gear System Wiring
  > ON DEPT REPEAT WRITEUP LG LGCIU 1 FAULT DEBRIEF FLIGHT CREW ON ARRIVAL TO GATE. REPORTED 3 MINUTES AFTER RETRACTING LANDING GEAR ON TAKE OFF, LGCIU 1 FAULT. ALSO HAD WIND SHEAR, GPWS DIED, AND REV 1 FAULT. STILL HITTING 27 GA.IPC 32-31-03-24. POST FLIGHT REPOR
- [SDR CALA2024010200011](https://openairdocs.org/sdr/CALA2024010200011.md): Oil System · leaking · Dec 26, 2023 · N898UA · Airbus A319132 · Turbine Engine Oil System
  > TEST FLIGHT DISCREPANCY.. 1 ENG LOW OIL PRESSENG SHUTDOWN ADDED SDR ENGINE WAS SHUT DOWN DUE TO LOW OIL PRESSURE AT 58 PSI, MIN. 60 PSI REQUIRED. ENGINE THEN WINDMILLED FOR 43 MINUTES; HOWEVER, WE DO NOT KNOW HOW LONG IT WINDMILLED BELOW 5PSI. OIL PRESSURE.
- [SDR CALA2023112703471](https://openairdocs.org/sdr/CALA2023112703471.md): Stringer · corroded · Nov 22, 2023 · N898UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO, UNDERFLOOR COMPARTMENT, FR 65 R/H STR 31 CORROSION. G EN BY V920443 ON HAECO LCQ NR 9294346/32346 REMOVED AND REPLACED STR 31 AND FRAME 64-67- AFT CARGO IAW SRM 5 7-42-11/001 DUE TO CORROSION ACMP BY MECH V061630 AND INSP V8992 60
- [SDR CALA2023112003436](https://openairdocs.org/sdr/CALA2023112003436.md): Intercostal · cracked · Nov 16, 2023 · N898UA · Airbus A319132 · Fuselage Main, Structure
  > L1 DOOR FR16 DOOR STOP #7 UPR INBD HOLE #1 HAS CRACK INDICATIONS IN THE INTERCOASTAL LAYER AT THE 3:, AND 5:OCLOCK POSITION. GEN BY V062335 ON HAECO LCQ NR# 9294288/32288
- [SDR CALA2023112003434](https://openairdocs.org/sdr/CALA2023112003434.md): Door Frame · cracked · Nov 16, 2023 · N898UA · Airbus A319132 · Fuselage Main, Structure
  > L1 DOOR FR16 DOOR STOP #1 LWR INBD HOLE #3 HAS A CRACK INDICATIO N IN THE FRAME LAYER AT THE 2:OCLOCK POSITION.
- [SDR CALA2023112003432](https://openairdocs.org/sdr/CALA2023112003432.md): Door Frame · cracked · Nov 16, 2023 · N898UA · Airbus A319132 · Fuselage Main, Structure
  > R1 DOOR FR20 DOOR STOP #1 LWR INBD HOLE #3 HAS A CRACK INDICATION IN THE FRAME LAYER AT THE 3:OCLOCK POSITION. GEN BY V062335 ON HAECO LCQ NR#9294274/32274 REMOVED AND REPLACED DISCREPANT #1 STEP FR20 INTERCOSTAL A319 SR M 51-42-11-001 AND DWG R53113118 ACMP B
- [SDR CALA2023112003430](https://openairdocs.org/sdr/CALA2023112003430.md): Intercostal · cracked · Nov 16, 2023 · N898UA · Airbus A319132 · Fuselage Main, Structure
  > R1 DOOR FR16 DOOR STOP #7 LWR INBD HOLE #3 HAS A CRACK INDICATIONS IN THE INTERCOASTAL LAYER AT THE 7: AND 8: POSITIONS. GEN BY V062335 ON HAECO LCQ NR# 9294576/32276
- [SDR CALA2023061401854](https://openairdocs.org/sdr/CALA2023061401854.md): Control Unit · warning light · Jun 12, 2023 · N898UA · Airbus A319132 · Landing Gear System
  > BRAKES HOT ECAM AFTER TOFF. LEFT SIDE 380 - RIGHT SIDE 85. ACFT PULLED SLIGHTY TO LEFT ON TOFF UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. REF TSM 32-42-00-810-922-A, CHECK PFR FOR ANY FAULTS, CONTACT TOMC DEBRE
- [SDR CALA2023050501381](https://openairdocs.org/sdr/CALA2023050501381.md): Sdac · inoperative · May 5, 2023 · N898UA · Airbus A319132 · Indicating/Recording System
  > FUEL L TK 1 AND 2 LO PRCAME ON IN FLIGHTALSO FWS SDAC 2 FAULT SDAC2 REPORTED MULTIPLE ERRONEOUS FAULTS IN CONCURRENCE WITH THE ACFT EXPERIENCING AN AC1 BUS FAULT ( REFERENCE LOGPAGE 4493538). PERFORMED GROUND SCAN OF CFDS WITH NO FAULTS FOUND. REPLACED SDAC1 &
- [SDR CALA2022110203017](https://openairdocs.org/sdr/CALA2022110203017.md): Sensor · faulted · Nov 2, 2022 · N898UA · Airbus A319132 · Landing Gear Position and Warning
  > *EMERGENCY LANDING* IN FLIGHT SHORTLY AFTERTAKEOFF L/G LGCIU 1FAULT ECAM PRECEEDED B YLOUD THUMPING NOISE FOUND SENSOR 26GA FAULTED.REMOVED AND REPLACED SENSOR GEAR DOOR INDICATION RETURNED TO NORMAL.REF AMM 32-31-73. REPLACED LGCIU #1 DUE TO ECAM MESSAGE REF
- [SDR CALA2022082602182](https://openairdocs.org/sdr/CALA2022082602182.md): None · none · Aug 26, 2022 · N898UA · Airbus A300* · Engine Temperature Indicating System
  > CAPTAIN REPORTS A REJECTED TO AT APPROX 80 KTS FOR A E2 EGT OVER LIMIT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. AMM77-21-43-700-010. 3 OF 4 PROBES VERY HIGH RESISTANCE. REPLACED ALL 4 EGT PROBES. REF AMMTASK
- [SDR CALA2022062901605](https://openairdocs.org/sdr/CALA2022062901605.md): None · none · Jun 28, 2022 · N898UA · Airbus A300* · Leading Edge Slat Position Indicating System
  > FLIGHT CREW REPORTS VIA ARINC DISPATCH F/CTL SLATS FAULT. VARGAS TOMC CFDS ATA 27-80-00 SLT 1 SYSTEM JAMCHECK SLT MECH DRIVE, SLT 2 SYSTEM JAMCHECK SLT MECH DRIVE, TSM 27-81-00-810-810-A. VARGAS TOMC
- [SDR CALA2022061501510](https://openairdocs.org/sdr/CALA2022061501510.md): None · none · Jun 15, 2022 · N898UA · Airbus A319132 · Powerplant System
  > FOUND LIGHTNING STRIKE DAMAGE TO THE RH ENGINE INNER COWL FIN (PLACARDED WITH NO GRAB) IAW AMM 05-51-18 REMOVED THE #2 ENGINE STRAKE PER REF AMM 71-13-19-000-010-B.
- [SDR CALA2021120802281](https://openairdocs.org/sdr/CALA2021120802281.md): Stringer · none · Dec 6, 2021 · N898UA · Airbus A319132 · Fuselage Structure (General)
  > REFERENCE LP7570706 INTERIM REPAIR PLANNING TO CONTACT ENGINEERI NG AFTER 03MAY2022 BUT BEFORE 15MAY-2022 FOR THE ECRA 5330-06892 PART 3 - PERMANENT REPAIR. REFERENCE LP7570706 INTERIM REPAIR PLANNING TO CONTACT ENGINEERI NG AFTER 03MAY2022 BUT BEFORE 15MAY-20
- [SDR CALA2021120802280](https://openairdocs.org/sdr/CALA2021120802280.md): Plate · corroded · Dec 6, 2021 · N898UA · Airbus A319132 · Fuselage Structure (General)
  > CORROSION ON AFT CARGO DOOR THRESH HOLD PER 9298350/26350 GEN V8 92443 REMOVED AND REPLACED D5347715400600 SHEET COVER ASSY AT AFT CARG O DOOR THRESHOLD IAW A319 SRM 51-42-11/001 AND 51-72-11-911-001 BY MECH V078599 INSP BY V892442 REMOVED AND REPLACED D534771
- [SDR CALA2021120602255](https://openairdocs.org/sdr/CALA2021120602255.md): Cable Assy · failed · Dec 5, 2021 · N898UA · Airbus A319132 · Emergency Exits
  > L/H OVERWING EXIT RELEASE CABLE INNER SLEEVE FAILED OPERATIONAL TEST STEP B.4 PAGES 3&4 OF TASK CARD 17-5221-1-7905. PER HAECO L CQ N/R 9298085/26085 GENERATED BY V916370. REMOVED L/H O/W EXIT RELEASE CABLE, LUBED AND REINSTALLED RELEAS FUNSTIONAL CHECK GOOD.
- [SDR CALA2021120602254](https://openairdocs.org/sdr/CALA2021120602254.md): Cable Assy · none · Dec 5, 2021 · N898UA · Airbus A319132 · Emergency Exits
  > R/H OVERWING EXIT RELEASE RIGID CABLE INNER SLEEVE FAILED OPERAT IONAL TEST STEP B.4 PAGES 3&4 OF TASKCARD 17-5221-1-7906. PER HA ECO LCQ N/R 9298084/26084 GENERATED BY V916370. REMOVED R/H O/W EXIT RELEASE CABLE LUBED AND REINSTALLED RELEASE FUNCTIONAL CHECK
- [SDR CALA2021120102210](https://openairdocs.org/sdr/CALA2021120102210.md): Skin · corroded · Nov 30, 2021 · N898UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > REFERENCE ECRA 5330-06888 FUSELAGE SKIN AT FR27-FR28 BETWEEN STR 43R-STR44 CORROSION INTERIM REPAIR. PER PART 1 STEP 2 GENERATE DIP, "ACCOMPLISH A PERMANENT REPAIR ON THE FUSELAGE SKIN AT FR27 -FR28 STR43R-STR44 PER PART 3 OF THE LASTEST REV OF ECRA5330-068 88
- [SDR CALA2020062201025](https://openairdocs.org/sdr/CALA2020062201025.md): Fuel Cap · missing · Jun 22, 2020 · N898UA · Airbus A319132 · Fuel Storage
  > FUEL CAP MISSING DEFER FUEL CAP MISSING REF CDL 28A, NO FUEL LEAKING FROM COUPLING. CHANGED SFR TO YES.
- [SDR CALA2020021640417](https://openairdocs.org/sdr/CALA2020021640417.md): Shear Tie · corroded · Feb 11, 2020 · N898UA · Airbus A319132 · Fuselage Internal Mounting Structure
  > CORROSION FWD PIT CLEAT AT FR34 BETWEEN STR43L AND STR42L PER HA ECO LCQ NON ROUTINE 9298270 GENERATED BY V892443 REMOVED AND REPLACED DAMAGED CLEAT, FR34 STR42L-43L IAW A319 IPC 53-21-12-11A, SRM 51-42-11-801 SRM 51-74-00-801 SRM ASNA 3042, SRM 51-72-11-911 S
- [SDR CALA2018012600301](https://openairdocs.org/sdr/CALA2018012600301.md): Connector · damaged · Jan 23, 2018 · N898UA · Airbus A319132 · Landing Gear System Wiring
  > SUPPORT TASK POST TEST FLT. ON TO ROLL AT 100 KTS RECEIVED A L/G GEAR NOT UP LOCKED ECAM AND ALL THREE RED UNLOCKED LIGHTS, GEAR WOULD NOT RETRACT. GEAR INDICATED DOWN WITH DOORS CLOSED. FOUND TWO PUSHED PINS ON 281 VAC, REPLACED BOTH PINS IAW AMM 32-61-01.
- [SDR CALA2018011300182](https://openairdocs.org/sdr/CALA2018011300182.md): Fitting · corroded · Jan 12, 2018 · N898UA · Airbus A319132 · Emergency Equipment
  > CORROSION ON THE R2 DOOR AFT GIRT BAR FITTING, FRAME 68. REMOVED AND REPLACED GIRT BAR FITTING IAW SRM 51-42-11-001, AND 51-44-11-001.
- [SDR CALA2018011200139](https://openairdocs.org/sdr/CALA2018011200139.md): Door Sill · corroded · Jan 12, 2018 · N898UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS CORROSION FRAMES 58 - 59. REMOVED & REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001.
- [SDR CALA2018010500014](https://openairdocs.org/sdr/CALA2018010500014.md): Fitting · corroded · Dec 31, 2017 · N898UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FWD CARGO DOOR SURROUND FWD LATERAL FRAME AT 24.5 HAS CORROSION AROUND FASTENERS, REMOVED AND REPLACED THE FWD CARGO DOOR FRAME FITTING IAW SRM 51-72-11-911-001.
- [SDR CALA2018010500013](https://openairdocs.org/sdr/CALA2018010500013.md): Cleat · corroded · Dec 31, 2017 · N898UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FWD CARGO BAY FRAME 28 BETWEEN STRINGERS 40 - 41R, INSIDE THRESHOLD CLEAT HAS CORROSION, REMOVED AND REPLACED THE FWD CARGO CLEAT IAW SRM 51-72-11-911-001.
- [SDR CALA2017122904677](https://openairdocs.org/sdr/CALA2017122904677.md): Rub Strip · chafed · Dec 29, 2017 · N898UA · Airbus A319132 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT PYLON LOWER SPAR RIB NR 5 HAS A RUB STRIP WORN. REMOVED & REPLACED THE RUB STRIP IAW SRM 54-51-12-300-003, PARA 2, FIG 2010 2.
- [SDR CALA2017122704624](https://openairdocs.org/sdr/CALA2017122704624.md): Skin · chafed · Dec 27, 2017 · N898UA · Airbus A319132 · Nacelle/Pylon, Plate/Skin
  > LEFT PYLON RIB 5 BOTTOM SKIN, LOWER SURFACED CHAFED. REMOVED & REPLACED DOUBLER ON THE NR 1 PYLON RIB 5 BOTTOM SKIN IAW SRM 54-51-12-300-003, PARA 2A. FIG 20102.
- [SDR CALA2017121704484](https://openairdocs.org/sdr/CALA2017121704484.md): Plate · corroded · Dec 16, 2017 · N898UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > SPEC. NO. JE17-5341-1-2710, L2 DOOR SILL PLATE AT FR68L CORRODED AFT OF GIRT BAR PLATE, REMOVED CORROSION ORIGINAL THICKNESS 0.03 MATERIAL LOSS.0.037 M AX MATERIAL LOSS 0.0157 FOUND TO BE OUT OF LIMITS IAW A319 SRM 5 3-41-14-283-002 FIG. 10101. REPAIRED L-2 D

## 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 = 'N898UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N898UA/reports

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