# Service difficulty reports: N893UA

A list on [N893UA](https://openairdocs.org/aircraft/N893UA.md).

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

- [SDR CALA2026080718362](https://openairdocs.org/sdr/CALA2026080718362.md): Fuel Sys · no discrepancy · Aug 6, 2026 · N893UA · Airbus A319132 · Aircraft Fuel System
  > FUEL BURN WAS DOUBLE WHAT IT SHOULD BE TAXIING TO THE RUNWAY. FAS SAID THEY SMELLED FUEL VAPORS IN THE CABIN WHILE SITTING WAITING FOR TAKEOFF. OPEN AND INSPECTED ENGINES FOUND NO ISSUES, RAN ENGINES FOR 5 MIN NO ISSUES FOUND DURING RUN.
- [SDR CALA2026040615069](https://openairdocs.org/sdr/CALA2026040615069.md): Fuel Line · leaking · Apr 5, 2026 · N893UA · Airbus A319132 · APU Engine Fuel and Control
  > WHEN PACKS ARE RUNNING ON APU BLEED STRONG FUEL OR EXHAUST SMELL INBD CREW REPOERTED ONLY SMELL WHEN USING THE APU. AFTER TAKEOFF SMELL WENT AWAY. WHEN APU STARTED AGAIN IN EWR SMELL CAME BACK. CONFIRMED STRONG FUEL SMEEL THROUGHT THE CABIN. AND FLIGHT DECK. F
- [SDR CALA2025121712199](https://openairdocs.org/sdr/CALA2025121712199.md): Pressure Switch · faulted · Dec 14, 2025 · N893UA · Airbus A319132 · Hydraulic Pump (Electric/Engine), Main
  > HYD G ENG 1 PUMP LO PR ON UPPER ECAM SPOKE WITH CREW & THEY STATED HYD G ENG 1 PUMP LO PR APPEARED ON UPPER ECAM DURING CRUISE.WHEN ECAM MESSAGE APPEARED, IT GAVE A MESSAGE TO TURN OFF THE HYD GREEN ENG 1 PUMP OFF. HYD GREEN PUMP WAS TURNED OFF & CREW WAS USIN
- [SDR CALA2025120211701](https://openairdocs.org/sdr/CALA2025120211701.md): Battery · discharged · Dec 2, 2025 · N893UA · Airbus A319132 · Battery/Charger System
  > MOVE TEAM REPORTED FOUND A/C GND POWER OFF, BOTH BATT SWITCHES IN ON, AND EMERGENCY LIGHT SWITCH IN AUTO/ON POSITION AND NO POWER OR LIGHT ON A/C. NO FAULTS FOUND - ACFT BATTERIES CHARGED WITH NO CURRENT DRAW REF MM 24-38-00 OPS CK GOOD, EMERGENCY LIGHTS OPS C
- [SDR CALA2025112411430](https://openairdocs.org/sdr/CALA2025112411430.md): Control Valve · inoperative · Nov 21, 2025 · N893UA · Airbus A319132 · Cabin Cooling System
  > A/C PACK NR 1 OUTPUT HIGH TEMPS 88F WOULD NOT COOL. LIGHT OIL SMELL IN AIR. OBSERVED HIGH DISCHARGE TEMPERATURE ON PACK 1 AND FAULT P1 FLOW CONT VALVE (23HB). PERFORMED TSM 21-51-00-810-803-A. PACK 1 FLOW CONTROL VALVE REQUIRES REPLACEMENT. REMOVED PACK F
- [SDR CALA2025111711239](https://openairdocs.org/sdr/CALA2025111711239.md): Fuel Cap · missing · Nov 13, 2025 · N893UA · Airbus A319132 · Fuel Storage
  > AIRCRAFT REFUELING CAP AND LANYARD MISSING FROM RT WING UPON ARRIVAL. INSTALLED REFUEL CAP WITH NEW IAW AMM 28-25-41-400-005-A. AND EC2820-02404C..
- [SDR CALA2025092209114](https://openairdocs.org/sdr/CALA2025092209114.md): Computer · faulted · Sep 17, 2025 · N893UA · Airbus A319132 · Fuel Indicating System
  > CENTER TANK FLUCTUATE 0 TO 3000 AUTO FEED FAULT FOB CHANGE WITH CENTERFQIC BITE PER AMM28-42-00-740-001-A NO FAULTS INDICATED. LAST LEG REPORT FOR FQIC CH1& CH2 NO FAILURES. CLASS 3 FAULTS CH1 & CH2 L CONDENSICON 19QT, C CONDENSICON 20QT, L CONSENSICON 19QT
- [SDR CALA2025090508481](https://openairdocs.org/sdr/CALA2025090508481.md): Elec Connector · disconnected · Aug 28, 2025 · N893UA · Airbus A319132 · Door System Wiring
  > FRONT CARGO DOOR SHOWS UNLOCKED. GRND CREW HAS OPENED AND CLOSE D IT SEVERAL TIMES PUTTING FWD CARGO DOOL ON MEL 5270J. PERFORMED TSM 52-31-00-810-801-A. FOUND ELEC CONNECTOR TO PROX SENSOR FIN 30WV DISCONNECTED. RECONNECTED CONNECTOR AND OPS CHECKED SENSOR
- [SDR CALA2025050604500](https://openairdocs.org/sdr/CALA2025050604500.md): Pitot Head · malfunctioned · May 2, 2025 · N893UA · Airbus A319132 · Pitot/Static System
  > ON TAKEOFF -60KTS THU AP PROX. 250KNOTS CAPT AIRS EED INDICATOR LAGGED 8-1 0 KT BELW F/O+STDBY A INSPECTION OF CAPT PITOT FOUND DAMAGE INSIDE OF TUBE SEE PHOTO, CAPT PITOT NEEDS REPLACED. PERFORMED FLUSHING OF LINE GOING FROM ADM TO CAPT PITOT NO DEBRIS FOUND
- [SDR CALA2024032900906](https://openairdocs.org/sdr/CALA2024032900906.md): Skin · corroded · Mar 26, 2024 · N893UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > RADIO ALTIMETER ANTENNA HAD BROKEN NUT PLATE, WHILE REPLACING FOUND CORROSION UNDER ANTENNA. CORROSION WAS BLENDED AND DOUBLER INSTALLED PER ECRA 5341-01446. & PART 1.2 REQ''S DIP FOR FUSELAGE SKIN AT FR60-61 BETWEEN STR43R ART 2 OF LATEST REVISION ECRA5341-0
- [SDR CALA2024032700885](https://openairdocs.org/sdr/CALA2024032700885.md): Skin · corroded · Feb 29, 2024 · N893UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > RADIO ALTIMETER ANTENNA #3 HAS 1 BROKEN DOME NUT UPDATED DEFECT STATEMENT AND REPAIR ACTION ON LP7463670. OK TO CLEAR THIS ITEM. RADIO ALTIMETER ANTENNA HAD BROKEN NUT PLATE, WHILE REPLACING FOUND CORROSION UNDER ANTENNA. CORROSION WAS BLENDED AND DOUBLER INS
- [SDR CALA2024031100672](https://openairdocs.org/sdr/CALA2024031100672.md): Stringer · corroded · Feb 29, 2024 · N893UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT FR55 TO FR57 STR 42L HAS CORROSION REMOVED AND REPLACED ANGLES REINFORCE IN CARGO COMPARTMENT FR55 TO FR56 STR 42L IAW SRM 53-41-13-300-010 SRM 51-42-11/001 FORM 4 4-0008.
- [SDR CALA2024030400631](https://openairdocs.org/sdr/CALA2024030400631.md): Fitting · damaged · Feb 29, 2024 · N893UA · Airbus A319132 · Elevator Structure
  > RH ELEVATOR HINGE FITTING #4 UPPER SAFETY WIRE LUG BROKEN REPAIRED RH ELEVATOR HINGE FITTING #4 I.A.W SRM 55-26-41-300-001 ATTACHED FORM 44-0008 EMP#: V934611 WORK ACCOMPLISHED AT ST ENG INEERING OF MOBILE AT BFM ON NR#: 90359
- [SDR CALA2024031300710](https://openairdocs.org/sdr/CALA2024031300710.md): Seat Track · corroded · Jan 29, 2024 · N893UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SUPPORT AT -Y81 CORRODED AT FR16. REMOVED AND REPLACED FLOOR SUPPORT AT -Y81 I.A.W SRM 51-42-11/00 1 FORM 44-0008 EMP#: V934614 WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 90309
- [SDR CALA2024031800754](https://openairdocs.org/sdr/CALA2024031800754.md): Door Sill · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, DEPTH 0.022", OUT OF LIMITS IAW SRM 51-41-49-283, REMOVED AND REPLACED DOOR SILL PLATE IAW S RM 51-42-11 AND SRM 51-72-11-911-002.
- [SDR CALA2024022800586](https://openairdocs.org/sdr/CALA2024022800586.md): Floor Support · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT Y254 CORRODED AT FR16.
- [SDR CALA2024022600545](https://openairdocs.org/sdr/CALA2024022600545.md): Fitting · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Passenger/Crew Doors
  > L/H AFT PASSENGER DOOR JAMB HAS CORROSION UNDER SCUFF PLATE AT C ENTER FWD UPPER EDGE. REMOVED CORROSION FROM COORNER SILL AND SHAPE SILL I.A.W. A319 S ED I.A.W A319 SRM 51-42-11/001 SFR# 1035253 FORM 44-0008 ATTACHE RM 51-75-00, COORNER SILL D=0.040'' SHAPE S
- [SDR CALA2024022600544](https://openairdocs.org/sdr/CALA2024022600544.md): Seat Track · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK -Y1292 HAS CORROSION AT FR20. REMOVED CORROSION FROM SEAT TRACK -Y1292 AT FR20 IAW SRM 51-74-0 90354 0 FOUND TO BE OUT OF LIMIT IAW SRM 53-11-15. REMOVED AND REPLACE D SEAT TRACK IAW SRM 51-42-11.
- [SDR CALA2024022600543](https://openairdocs.org/sdr/CALA2024022600543.md): Floor Support · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CABIN RH SIDE BETWEEN FR66 AND 67 FLOOR SUPPORT STRUCTURE AT Y-765 HAS CORROSION ON SEVERAL AREA. REMOVED AND REPLACED FLOOR SUPPORT AT -765 I.A.W SRM 51-42-11/00 1 SFR# 1035251 44-0008.
- [SDR CALA2024021900450](https://openairdocs.org/sdr/CALA2024021900450.md): Floor Support · corroded · Jan 27, 2024 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CABIN LH SIDE BETWEEN FR67 AND 68 FLOOR SUPPORT STRUCTURE AT Y 1292 HAS CORROSION. AREA FOUND TO BE OUT OF LIMITS I.A.W (SRM 53-41-14-283-009) D-"0 SUPORT I.A.W (51-44-11/001 SRM). TREATED & PRIMED HOLES I.A.W (S AT BFM ON NR#: 90298.063" MAX "0.031" REMO
- [SDR CALA2024031300711](https://openairdocs.org/sdr/CALA2024031300711.md): Stringer · corroded · Jan 25, 2024 · N893UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > (A3NB-53-4-6179) DOT 206-11 AFT CARGO COMPARTMENT FR57 TO FR65 L /H STGR 42 SURFACE CORROSION. W/C:90087 REMOVED AND REPLACED FASTENER WITH SIGNAL CORROSION, AND REMOVED SRM 51-42-11/001 T04797 INSTUMENT MEASUREMENT FOR 44-0008 ATTACH AND REPLACED PAINT STEIGE
- [SDR CALA2024021300411](https://openairdocs.org/sdr/CALA2024021300411.md): Floor Support · corroded · Jan 24, 2024 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > (A3NB-05-3-6056) DOT #91-026 AFT CABIN RH SIDE BETWEEN FR66 & 69 FLOOR SUPPORT STRUCTURE AT Y-1292 HAS CORROSION ON SEVERAL AREA. W/C:90301 REMOVED AND REPLACED FLOOR BEAM AT Y-1292 I.A.W SRM 51-42-11. EM P: V934614 WC: 90301 STA: ST ENG BFM
- [SDR CALA2023100602965](https://openairdocs.org/sdr/CALA2023100602965.md): Line · leaking · Oct 4, 2023 · N893UA · Airbus A319132 · Hydraulic Reservoir, Main
  > HYD G RSVR LO LVL FOUND GREEN HYD QTY LOW AT SERVICE PANEL. FOUND ON GVI WALK EVIDENCE OF SKYDROL FROM #1 ENGINE PYLON TAIL DRAIN & BEHIND 415BL PICTURES ATTACHED. LEAK APPEARS TO BE IN CLAMP BLOCK UNDER #1 ENGINE #1 FIRE BOTTLE. LINES FWD OF CLAMP BLOCK ARE D
- [SDR CALA2023070302143](https://openairdocs.org/sdr/CALA2023070302143.md): Fuel Cap · missing · Jul 2, 2023 · N893UA · Airbus A319132 · Fuel Storage
  > PDA 1 FUEL CAP MISSING UPON ARRIVAL IN DFW REPLACED MISSING FUEL CAP WITH SERVICEABLE UNIT AMM 28-25-41. ADDED ROTABLE PART CHANGE. INSTALL ONLY. ROTABLE PARTS CHANGE WAS INDICATED - 1405270
- [SDR CALA2022123003530](https://openairdocs.org/sdr/CALA2022123003530.md): Door Frame · cracked · Dec 29, 2022 · N893UA · Airbus A319132 · Fuselage Main, Structure
  > FR68 LH, DOOR STOP FITTING NR 1 BOTTOM INBOARD HOLE HAS 2 REJECTABLE CRACK INDICATIONS.
- [SDR CALA2022123003533](https://openairdocs.org/sdr/CALA2022123003533.md): Door Frame · corroded · Dec 28, 2022 · N893UA · Airbus A319132 · Fuselage Main, Structure
  > RH DOORSTOP FITTING HOLES, DOORSTOP #1 LOWER INBOARD HOLE CORRODED. REPAIR BEFORE NEXT FLIGHT REPAIRED DOORSROP FITTING 1 I/B HOLE #3 PER UAL EC/RA 5341-01360 AND FINAL EA 319-5341-13-A310,
- [SDR CALA2022111603149](https://openairdocs.org/sdr/CALA2022111603149.md): Fuel Cap · missing · Nov 16, 2022 · N893UA · Airbus A319132 · Fuel Storage
  > FUEL CAP MISSING, INSTALLED FUEL COUPLING CAP, 28-25-41.
- [SDR CALA2021092801720](https://openairdocs.org/sdr/CALA2021092801720.md): Drain Mast · cracked · Sep 28, 2021 · N893UA · Airbus A319132 · Powerplant System
  > #1 ENG DRAIN MAST HARD LINE CRACKED ( ACOC) APROX 180 DEGREES AROUND LINE WHERE BRAZED INTO MAST. UPDATED TO SDR. REMOVED AND REPLACED #1 ENGINE DRAINS MAST I.A.W. A319 AMM 71-71-42.
- [SDR CALA2021042200525](https://openairdocs.org/sdr/CALA2021042200525.md): Battery Pack · failed · Apr 22, 2021 · N893UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: - EEL PATH LIGHT TEST FAILS EPSU FWD LEFT ATA 38-51-38. REPLACED BATTERY PACK IN THE FWD LEFT POSITION IAW AMM 33-51-38-400-002-AO. OPS. TEST GOOD.
- [SDR CALA2021041200441](https://openairdocs.org/sdr/CALA2021041200441.md): Idg · failed · Apr 12, 2021 · N893UA · Airbus A319132 · AC Generator-Alternator
  > ELEC IDG 2 OIL LO PH/OVHT. REPLACED #2 IDG AND FLUSHED LINES REF AMM 24-21-51. ENGINE RUN GOOD, NO LEAKS, GENERATOR OPD CHECK NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1171879 SN OFF 0505 GENERATOR, INTE OFF 31-2411-9-0001 0505 ON 31-2411-9-0001 018
- [SDR CALA2019020400210](https://openairdocs.org/sdr/CALA2019020400210.md): Beam · corroded · Feb 4, 2019 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT WET AREA LEFT SILL BEAM AT Y1732 FR68 HAS CORROSION AROUND FASTENER HOLE. INSTALLED AND REPAIR AT SILL BEAM AT AFT WET AREA AT Y 1732, IAW SRM 53-41-14-300-001 FIG 01 PAGE 8-15.
- [SDR CALA2019012100139](https://openairdocs.org/sdr/CALA2019012100139.md): Shear Plate · corroded · Jan 21, 2019 · N893UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > REF NR 99829305 SUPPORT TASK (A3NB-53-3-6222) MAIN CABIN SHE AR PLATE HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED MAIN CABIN RIGHT SHEAR LOCATED AND DRILLED NEW SHEAR PLATE FWD OF FR70 IRW SRM 51-42-11-001, SRM 51-44 -11. REMOVED AND REINSTALLED
- [SDR CALA2017063002020](https://openairdocs.org/sdr/CALA2017063002020.md): Control Unit · faulty · Jun 30, 2017 · N893UA · Airbus A319132 · Landing Gear Steering System
  > BRAKES ANTI SKID NWS FAULT. EMERGENCY DECLARED. FOUND BSCU CHANNEL 1, NO RESPONSE. REPLACED BSCU. SYSTEM OPS CHECKED NORMAL IAW AMM 32-42-34.
- [SDR CALA2017050801300](https://openairdocs.org/sdr/CALA2017050801300.md): Battery Pack · no test · May 8, 2017 · N893UA · Airbus A319132 · Emergency Lighting
  > EMERGENCY LIGHT CHECK FAILED EPSU BATTERY FWD AND AFT POSITIONS. REPLACED BATTERY 10WL, 12WL (FWD & AFT) IAW AMM33-51-38-40 0. TESTED OK ON FAP. ACP IDT INSPECTION TEST AND LIGHT OPS CHECKED GOOD.
- [SDR CALA2017041400989](https://openairdocs.org/sdr/CALA2017041400989.md): Attach Fitting · broken · Apr 14, 2017 · N893UA · Airbus A319132 · Escape Slide
  > R1 DOOR SLIDE RAFT SAFETY STRAP ATTACHMENT IS BROKEN. REMOVED & REPLACED THE R1 DOOR SLIDE RAFT IAW AMM 25-62-44-000- 804-A, & AMM 25-62-44-400-803-A
- [SDR CALA2017041000938](https://openairdocs.org/sdr/CALA2017041000938.md): Frame · corroded · Apr 9, 2017 · N893UA · Airbus A319132 · Fuselage Main, Frame
  > AFT CARGO UNDER FLOOR AREA AT FR59 HAS SURFACE CORROSION UNDER PROFILE PANEL ABOVE STR 38R. REPAIRED FR59 BETWEEN STR 37R & 43R IAW ECRA 5340-01769 AND REO L20692 REV IR ACCOMPLISH A PERMANENT REPAIR ON FRAME 59 BETWEEN S-37R & S-43R PER PART 3 OF ECRA 5340-01

## 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 = 'N893UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N893UA/reports

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