# Service difficulty reports: N896UA

A list on [N896UA](https://openairdocs.org/aircraft/N896UA.md).

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

- [SDR CALA2026080518297](https://openairdocs.org/sdr/CALA2026080518297.md): Lamp · corroded · Aug 4, 2026 · N896UA · Airbus A319132 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, PTP SHOWS FAULT EPSU EXT LOAD EMER. RESET POWER TO ASSOCIATED EPSU. NO FIX. COMPLETED BITE OF EPSU UNIT IAW TSM 33-51-00-810-822-A. BITE SHOWED EXTERIOR LIGHTS FAULT. WIRING CHECKED IAW TSM 33-51-00-810-822-A, FOUND RED LED EX
- [SDR CALA2026021813865](https://openairdocs.org/sdr/CALA2026021813865.md): Strut · worn · Feb 15, 2026 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY VERTICAL MEMBER Y765 WORN. REPLACED REINFORCEMENT PLATES ON FWD CARGO BAY VERTICAL MEMBER Y765 IAW SRM 53-21-29-300-002.
- [SDR CALA2026021813863](https://openairdocs.org/sdr/CALA2026021813863.md): Strut · worn · Feb 15, 2026 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY VERTICAL MEMBER Y254 WORN. REPLACED THE REINFORCEMENT PLATES IAW SRM 53-21-29-300-002.
- [SDR CALA2026021813866](https://openairdocs.org/sdr/CALA2026021813866.md): Skin · dented · Feb 7, 2026 · N896UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > RT EXTERIOR FUSELAGE SKIN DENTED JUST FWD OF FR63 BTWN STR 37-38R. PERFORMED DOUBLER REPAIR IAW SRM 53-41-11-300-109.
- [SDR CALA2025102810658](https://openairdocs.org/sdr/CALA2025102810658.md): Pin · damaged · Oct 27, 2025 · N896UA · Airbus A319132 · Light System Wiring
  > FOUND 32CBA EMEGRANCY LIGHT TO BE INOP WHILE TROUBLESHOOTING 11CBA LIGHT WAS WORKING PRIOR REF LP 6750695 FOR TROUBLESHOOTING BITE TESTS PASS ON POTH PTP AND POWER SUPPLY, NO JOY ON OPS TEST OF LIGHT OK TO MEL PLACARD INSTALLED 11CBA BEEN ADDED TO THIS MEL FOU
- [SDR CALA2025082908269](https://openairdocs.org/sdr/CALA2025082908269.md): Hook · missing · Aug 28, 2025 · N896UA · Airbus A319132 · Emergency Equipment
  > R1 SLIDE MISSING CLIP FROM STRAP THAT ATTACHES TO SLIDE DOOR.
- [SDR CALA2025052604941](https://openairdocs.org/sdr/CALA2025052604941.md): Elec Connector · disconnected · May 20, 2025 · N896UA · Airbus A319132 · Light System Wiring
  > FWD CABIN CEILING EMERGENCY EXIT SIGN NOT ILLUMINATING SIGN NOT ILLUMINATING. LIGHT IN CEILING JUST AFT OF SIGN ILLUMINATES. MEL 3350AB UNABLE TO USE 3350AB UPDATED WITH PARTS PART IDENTIFIED. UPDATED M/L WITH M/E NUMBER OF LIGHT NEEDED. FOUND A CONNECTOR NOT
- [SDR CALA2025040803625](https://openairdocs.org/sdr/CALA2025040803625.md): Warning Light · false activation · Apr 4, 2025 · N896UA · Airbus A319132 · Door Warning System
  > DOOR 1R FLASHING ON DOOR PAGE AS IF ITS ARMED THEN DISSARMEDUNABLE TO REPLICATE FAULT ON THE GROUND REF TSM 52-11-00-810-805-A. AND NO FAULTS NOTED ON PREVIOUS TWO LEGS REF LP 4410335. OPS CHECK GOOD AT THIS TIME.
- [SDR CALA2025031802907](https://openairdocs.org/sdr/CALA2025031802907.md): Cover · disengaged · Mar 13, 2025 · N896UA · Airbus A319132 · Emergency Exits
  > DOOR L EMER EXIT ECAM AT FL330 IN CLIMB DELTA P 6.3 AT 15000 STA BLE DURING CABIN WALK THRU FOUND L EMER EXIT DOOR PANEL COVER DISENGAGED. REATTACHED COVER, ECAM MEAAAGE EXTINGUISHED.
- [SDR CALA2024052201563](https://openairdocs.org/sdr/CALA2024052201563.md): Fuel Cap · missing · May 20, 2024 · N896UA · Airbus A319132 · Fuel Storage
  > PDA 2 FUEL CAP MISSING ON ARRIVAL INTO DEN. REF LOGPAGE 8021929, FUELER REPORTED MISSING FUEL CAP. APPLIED 28A COMPLIED WITH CDL. DISPATCH DESK: 12 NAME: CB DATE: 20-MAY-24- OK TO CDL CAP, COUPLING R OFF 31-2825-9-0001 2463 ON 0000 CAP, COUPLING R OFF 31-2825-
- [SDR CALA2023101703103](https://openairdocs.org/sdr/CALA2023101703103.md): Clamp · missing · Oct 16, 2023 · N896UA · Airbus A319132 · Exterior Lighting
  > PDA 2 RT RETRACT LANDING LIGHTBRETENTION AND BULB DEPARTED ACFT SEE LOG ITEM 6039852 RPL RING AND BULB SEE LOG PAGE 6039852. LENS ON RT LANDING LIGHTMISSING RH LANDING LIGHT. RIGHT LANDING LIGHT ASSY CLAMP IS MISSING AS WELL AS BULB REQUESTING CDL 33G, HIGH SP
- [SDR CALA2023050101291](https://openairdocs.org/sdr/CALA2023050101291.md): Intercostal · cracked · Apr 28, 2023 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L1 DOOR FRAME 16 #7 DOOR STOP UPPER IB HOLE HAS CRACK INDICATION S IN INTERCOSTAL LAYER 4 O''CLOCK POSITION. RMVD AND RPLD L1 DOOR FR16 #7 INTERCOSTAL IAW A319 SRM 51-72-12 AND DWG R53113118.
- [SDR CALA2023050101290](https://openairdocs.org/sdr/CALA2023050101290.md): Intercostal · cracked · Apr 28, 2023 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L1 DOOR FRAME 16 #1 DOOR STOP LOWER IB HOLE HAS CRACK INDICATION IN INTERCOSTAL LAYER 2 O''CLOCK POSITION. RMVD AND RPLD L1 DOOR FR16 #1 INTERCOSTAL IAW A319 SRM 51-72-12 AND DWG R53113118.
- [SDR CALA2023050101289](https://openairdocs.org/sdr/CALA2023050101289.md): Intercostal · cracked · Apr 28, 2023 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FR16 DOOR STOP #7 HOLE H-1 I/B UPPER HAS A CRACK IN INTERCOSTAL AT 6 O''CLOCK AND 10 O''CLOCK PER HAECO LCQ N/R 9292450/28450 GEN BY V061632 RMVD AND RPLD RH FR16 #7 INTERCOSTAL IAW A319 SRM 51-72-12 AND DWG R53113118 BY MECH V061742 INSP BY V061334
- [SDR CALA2023042801271](https://openairdocs.org/sdr/CALA2023042801271.md): Beam · corroded · Apr 27, 2023 · N896UA · Airbus A319132 · Fuselage Main, Structure
  > R2 DOOR SILL AT FR68 HAS CORROSION PER NR9292559 GEN BY V061680 RMVD AND RPLD NEW DOOR SILL ON R2 DOOR RH FR66 TO FR68 IAW SRM 5 1-72-11-001 BY MECH V914538 INSP BY V061334
- [SDR CALA2023042601253](https://openairdocs.org/sdr/CALA2023042601253.md): Fitting · corroded · Apr 25, 2023 · N896UA · Airbus A319132 · Fuselage Structure (General)
  > R2 DOOR CUTOUT LOWER AFT CORNER FITTING HAS CORROSION AT FASTENE R HOLE. LOWER AFT CORNER FITTING FOUND TO HAVE CORROSION BEYOND ALLOWABL E LIMITS IAW SRM 53-41-74-283-002. FITTING WAS REMOVED AND REPLA CED IAW SRM 51-72-11-711-001. PROTECTIVE FINISH RESTORED
- [SDR CALA2023032000809](https://openairdocs.org/sdr/CALA2023032000809.md): Unknown · unknown · Mar 20, 2023 · N896UA · Airbus A319132 · Flight Control System
  > ON TAKEOFF-F/CTL FLAP+SLAT/SYS2 FAULTS-SLOW TO RETRACT/4 MINAPPR OX TO CLR ECAM. R & R SFCC 2, ALL TESTS PASSED. DUE TO SINGLE SFCC REPLACEMENT, CAT III TEST NOT REQUIRED. ACFT REMAINS CAT III FO. PARTS USED: 1615586,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED
- [SDR CALA2022082602183](https://openairdocs.org/sdr/CALA2022082602183.md): None · none · Aug 26, 2022 · N896UA · Airbus A300* · Hydraulic System, Main
  > ECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD FOUND LEFT MLG DOOR ACTUATOR LEAKING AND MLG DOOR BYPASS VALVE STUCK IN BYPASS. DOOR ACTUATOR M&E 31-3231-9-9003 IPC REF 32-31-03-60B. BYPASS VALVE M&E 31-3231-9-9002 IPC REF 32-31-03-46 ITEM 90. REMOVED
- [SDR CALA2022020700340](https://openairdocs.org/sdr/CALA2022020700340.md): Cabin Pressure · failed · Feb 7, 2022 · N896UA · Airbus A319132 · Cabin Pressure Control System
  > SYS 2 PRESSURE FAULT AT360 PERFORMED CK REF AMM 21-31-00 CPC 2 FAILED REPLACED #2 CPC CONTROLLER TEST PASSED FOR BOTH CPC 1&2. REF AMM 21-31-34-400-001-A. PART S CHANGED SERIAL NUMBER OFF 0354510 AND ON PART SN 0654904 ROTABLE PARTS CHANGE WAS INDICATED - TT #
- [SDR CALA2021112502171](https://openairdocs.org/sdr/CALA2021112502171.md): Bolt · loose · Nov 25, 2021 · N896UA · Airbus A319132 · Ailerons
  > OPENED AND TAGGED C/B B11 AT 49VU PANEL, A01 AND A02 AT 105VU PANEL, AND R20 AT 121VU PANEL FOR AILERON SERVO-CONTROL SERO VALVE MAINTENANCE REF AMM 27-14-51-400-003-A PER TOMC REQUEST, REPLACE LEFT AILERON BLUE SYTEM SERVO FOR VIBRATION ISSUE. REMOVED LEFT O/
- [SDR CALA2020120401323](https://openairdocs.org/sdr/CALA2020120401323.md): Computer · failed · Dec 4, 2020 · N896UA · Airbus A319132 · Autopilot Computer
  > AUTO FLT ''RUD TRV LIM 1'' DISPLAYED ON UPPER ECAM SCREEN. FOLLOWING MAINT, PERFORMED IN LOGPAGE 5552302 (FMGC2 REPLACEMENT), PERFORMED OPERATIONS TEST OF RUDDER LIMITING FUNCTION AND RUDDER TRIM FUNCTIONS, REF AMM 22-61-00 AND 27-22 -00. BOTH SYSTEMS OPERAT
- [SDR CALA2020020800366](https://openairdocs.org/sdr/CALA2020020800366.md): Cids · faulted · Feb 7, 2020 · N896UA · Airbus A319132 · Emergency Equipment
  > EVAC ALARM CAME ON ONTAKEOFF. WOULD NOT STOPUNTIL LANDIG PER TSM 23-73-00-810-955-A, REMOVED AND REPLACED CIDS DIRECTORS #1 AND #2 PER AMM 23-73-34. ACCOMPLISHED BITE TEST OF #1AND #2 GOOD. POST FLIGHT REPORT SHOWED CIDS #1 FAULT, BUT REPLACED BOTH CIDS. AFTER
- [SDR CALA2017081802732](https://openairdocs.org/sdr/CALA2017081802732.md): Frame · dented · Aug 18, 2017 · N896UA · Airbus A319132 · Fuselage Main, Frame
  > DENT ON FRAME 63 STRINGER 30L. REPAIRED THE FRAME IAW SRM 53-00-12-300-001, FIG 20101.
- [SDR CALA2017081402686](https://openairdocs.org/sdr/CALA2017081402686.md): Plate · corroded · Aug 14, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT CARGO THRESHOLD PLATE IN SEVERAL PLACES REMOVED AND REPLACED AFT CARGO COMPARTMENT THRESHOLD PLATE/COVER SHEET FRAME 55 TO FRAME 59 RIGHT AND SIDE IAW SRM 51-42-11- 001 PARA D, E, AND F.
- [SDR CALA2017081402677](https://openairdocs.org/sdr/CALA2017081402677.md): Attach Fitting · corroded · Aug 12, 2017 · N896UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > AFT CARGO BAY FRAMES 55-56, STRINGER 38R ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 57-4 2-11-001, AND 57-44-11-001.
- [SDR CALA2017081402670](https://openairdocs.org/sdr/CALA2017081402670.md): Threshold · corroded · Aug 12, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD HAS CORROSION. REMOVED AND REPLACED THE THRESHOLD IAW SRM 51-42-19-001, PARA D, E, AND F.
- [SDR CALA2017080802506](https://openairdocs.org/sdr/CALA2017080802506.md): Support Fitting · corroded · Aug 6, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD SUPPORT BRACKET, HOLE CORRODED AND OUT OF ROUND. REMOVED AND REPLACED THE SUPPORT FITTING IAW SRM 51-42-11-001 PARA D AND F.
- [SDR CALA2017080802505](https://openairdocs.org/sdr/CALA2017080802505.md): Threshold · corroded · Aug 5, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR THRESHOLD HAS CORROSION. REMOVED & REPLACED THE THRESHOLD PLATE IAW SRM 51-42-11-001, PARAGRAPH D, E & F.
- [SDR CALA2017080802504](https://openairdocs.org/sdr/CALA2017080802504.md): Support Bracket · corroded · Aug 5, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SILL SUPPORT BRACKET BETWEEN FRAMES 27A-28 HAS HOLES REAM TO MAX. DIA. WITH CORROSION STILL PRESENT. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-42-11-001, PARA D, E, AND F.
- [SDR CALA2017080802503](https://openairdocs.org/sdr/CALA2017080802503.md): Fitting · corroded · Aug 5, 2017 · N896UA · Airbus A319132 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD CORNER FITTING HAS CORROSION. REMOVED AND REPLACED THE CORNER FITTING IAW SRM 51-42-11-001
- [SDR CALA2017080802502](https://openairdocs.org/sdr/CALA2017080802502.md): Threshold · corroded · Aug 5, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD, HOLE CORRODED AND OUT OF ROUND. INSTALLED REPLACEMENT IAW SRM 51-42-11.
- [SDR CALA2017080802501](https://openairdocs.org/sdr/CALA2017080802501.md): Fitting · corroded · Aug 5, 2017 · N896UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FWD CARGO DOOR SILL, CORRODED ON FWD SILL PLATE. REMOVED AND REPLACED FORWARD CARGO DOOR SILL, SILL PLATE FITTING IAW SRM 51-42-11-001, PARA E AND F
- [SDR CALA2017080802500](https://openairdocs.org/sdr/CALA2017080802500.md): Fitting · gouged · Aug 5, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR THRESHOLD, FWD SUPPORT BRACKET HAS A GOUGE, FWD LOWER SIDE OF BRACKET. REMOVED AND REPLACED THE SUPPORT FITTING AT FRAME 55A IAW SRM 51-42-11-001, PARA F.
- [SDR CALA2017080802479](https://openairdocs.org/sdr/CALA2017080802479.md): Bracket · corroded · Aug 2, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SILL SUPPORT BRACKET BETWEEN FRAMES 25A - 26 HAS HOLES REAM TO MAX. DIA. WITH CORROSION STI LL PRESENT. REMOVED AND REPLACED FWD CARGO DOOR SILL SUPPORT BRACKET IAW SRM 51-42-11-001, REV 118, 51-44-11-001, 51-72- 11-911-001, 51-72-11-911-002,
- [SDR CALA2017080802478](https://openairdocs.org/sdr/CALA2017080802478.md): Bracket · corroded · Aug 2, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR SILL SUPPORT BRACKET BETWEEN FRAMES 26A - 27 HAS HOLES REAM TO MAX. DIA. WITH CORROSION STILL PRESENT. REMOVED AND REPLACED THE FWD CARGO DOOR SILL SUPPORT BRACKET IAW SRM 51-42-11-001, REV 118, 51-44-11-001, 51-72 -11-911-001, 51-72-11-911-002
- [SDR CALA2017080802469](https://openairdocs.org/sdr/CALA2017080802469.md): Fitting · corroded · Jul 31, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FWD DOOR CORNER FITTING HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED THE FITTING AT FRAME 55 IAW SRM 51-72-1 1-911-001, AND 53-41-49-300-004.
- [SDR CALA2017080802467](https://openairdocs.org/sdr/CALA2017080802467.md): Fitting · corroded · Jul 31, 2017 · N896UA · Airbus A319132 · Cargo/Baggage Doors
  > AFT CARGO DOOR AFT CORNER FITTING HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-42-11-001.
- [SDR CALA2017072902438](https://openairdocs.org/sdr/CALA2017072902438.md): Fitting · worn · Jul 29, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > LEFT SIDE AFT UPPER DOG HOUSE FITTING AT FRAME 20 DUCT/PLUMBING SUPPORT BRACKET ATTACH BUSHING WORN. REMOVED AND REPLACED DISCREPANT LT AFT UPPER DOG HOUSE FITTING IAW SRM 51-42-11-001, 51-44-11-001, 51-49-00-001, AND IPC 53-13-01-02B. APPLIED PRIMER AND TOPCO
- [SDR CALA2017072802400](https://openairdocs.org/sdr/CALA2017072802400.md): Door Sill · corroded · Jul 27, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL UPPER SURFACE HAS CORROSION AT FR 68 NEAR IB EDGE CONTINUING FWD 6". PERFORMED R2 DOOR SILL REPAIR AT FR68 IAW SRM 53-41-14-300- 300-001 PARA 2 AND FIGURE 20101 DETAIL G.
- [SDR CALA2017072402354](https://openairdocs.org/sdr/CALA2017072402354.md): Fitting · corroded · Jul 24, 2017 · N896UA · Airbus A319132 · Fuselage Main, Attach Fittings
  > FWD CARGO BAY DOOR AFT CORNER FITTING HAS CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-48-11-00.
- [SDR CALA2017072402353](https://openairdocs.org/sdr/CALA2017072402353.md): Door Sill · corroded · Jul 24, 2017 · N896UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL UPPER SURFACE HAS CORROSION AT FRAME 68 NEAR THE INBD EDGE CONTINUING FWD 6 INCHES. REMOVED CORROSION AND INSTALLED A REPAIR IAW SRM 53-41-14-300-001, FIG 6.

## 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 = 'N896UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N896UA/reports

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