# Service difficulty reports: N855UA

A list on [N855UA](https://openairdocs.org/aircraft/N855UA.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 · 89 reports

- [SDR CALA2026072417968](https://openairdocs.org/sdr/CALA2026072417968.md): Panel · missing · Jul 22, 2026 · N855UA · Airbus A319131 · Aerodynamic Fairings
  > LEFT WING TO BODY FAIRING PANEL 191DT FOUND MISSING UPON LANDING. REMOVED REMAINING PANEL AND INSTALLED NEW PANEL IAW MM 53-35-11.
- [SDR CALA2026072417965](https://openairdocs.org/sdr/CALA2026072417965.md): Battery · warning message · Jul 21, 2026 · N855UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMER R, 33-51-38, MX MSG DURING EMERGENCY LIGHT TEST ON PTP. REPLACED RIGHT EPSU BATTERY, OPS CHECKED GOOD, IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A.
- [SDR CALA2025072907055](https://openairdocs.org/sdr/CALA2025072907055.md): Fuel Cap · missing · Jul 25, 2025 · N855UA · Airbus A319131 · Fuel Storage
  > PDA 2 RAMP REPORTS FUEL COUPLING CAP MISSING INSTALLED NEW SERVICABLE CAP IAW AMM 28-25-41-400-007-A. CAP STILL REQUIRES PAINT STRIPE INSTALLED NEW FUEL CAP. COUPLING CAP REQUIRES PAINT MARKING IAW ECRA 2820-02404.
- [SDR CALA2025032703240](https://openairdocs.org/sdr/CALA2025032703240.md): Battery · no test · Mar 26, 2025 · N855UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - EPSU 11WL NEEDED CHANGING. REMOVED AND REPLACED EPSU 11WL BATTERY, IAW AMM33-51-38. OPS TESTED NORMAL. OK FOR SERVICE.
- [SDR CALA2025022602484](https://openairdocs.org/sdr/CALA2025022602484.md): Cap · missing · Feb 24, 2025 · N855UA · Airbus A319131 · Fuel Storage
  > PDA 2 REFUEL CAP FOUND MISSING ON ARRIVAL INTO CHS SEE LOG PAGE 3977389 FUEL CAP WAS ALREADY ON CDL 3883611 ALLIED REPORTS - DIFFICULT TO PUT THE FUEL CAP ON FUEL CAP DAMAGED, REQUEST CDL. APPLIED CDL DDP. CDL 28A. DISPATCH DESK: 32 NAME: NW DATE: 15-FEB-25- 2
- [SDR CALA2025012802084](https://openairdocs.org/sdr/CALA2025012802084.md): Connector · damaged · Jan 25, 2025 · N855UA · Airbus A319131 · Emergency Lighting
  > REF LP 3648690. DURING EMERGENCY LIGHT OPS CHECK, FOUND L2 LOWER PATHWAY EXIT SIGN INOP. REPLACED CONNECTOR ON LIGHTED EXIT SIGN AT L2 DOOR IAW ESPM20-44 -00-02, OPS CHECK GOOD.
- [SDR CALA2025012702069](https://openairdocs.org/sdr/CALA2025012702069.md): Switch · out of position · Jan 24, 2025 · N855UA · Airbus A319131 · Emergency Lighting
  > ENROUTE FLIGHT ATTENDANT REPORTED EMERGENCY CABI N LIGHTS ILLUMINATED RANDOMLY FOUND AAP LIGHT EMER PB SWITCH STICKING. CLEANED OUTI OF PB SWITCH AND OP CHECKED. PB SWITCH MOVES FREELY. ACCOMPLISHED EMERGENCY LIGHT OPERATIONAL TEST REFERENCE MM 33-51-00-710-
- [SDR CALA2025012702068](https://openairdocs.org/sdr/CALA2025012702068.md): Switch · out of position · Jan 24, 2025 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS COME ON RANDOMLY IN CRUISE. FOUND NO SMOKING SWITCH IN AUTO POSITION. MOVED NO SMOKING SWITCH TO OFF EMERGENCY LIGHTS OPERATE NORMALLY IAW AMM 33-51-00
- [SDR CALA2025012702066](https://openairdocs.org/sdr/CALA2025012702066.md): Switch · faulted · Jan 24, 2025 · N855UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS COME ON WHEN SWITCH IS PUT IN THE ARM POSITION REMOVED AND REPLACED EMERGENCY EXIT LIGHT SWITCH (4WL). OPS CHK NORMAL. REF. WDM 33-51-01 AND AMM TASK 33-51-00-710-004-A
- [SDR CALA2024070801969](https://openairdocs.org/sdr/CALA2024070801969.md): Cids · intermittent · Jul 6, 2024 · N855UA · Airbus A319131 · Emergency Lighting
  > CABIN ESCAPE PATH LTS ILLUMINATING INTMNTLY. CREW REPORTS CABIN EMERGENCY LIGHTS GOING ON AND OFF THROUGHOUT RERAN TEST. ALL CHECKS GOOD, NO FAULTS. CABIN FOR FIRST 30 MINS OF FLIGHT, REST OF THE FLIGHT OK. UPON ARRIVAL ACP EM LIGHTS TEST PER MM33-51-00-710-00
- [SDR CALA2024070801968](https://openairdocs.org/sdr/CALA2024070801968.md): Oxygen Mask · unwanted deploy · Jul 6, 2024 · N855UA · Airbus A319131 · Passenger Oxygen System
  > O2 MASK FWD GALLEY DROPPED REPACKED MASK PER MM35-21-43-550, DOOR IS SECURE.
- [SDR CALA2024060701718](https://openairdocs.org/sdr/CALA2024060701718.md): Battery · expired · Jun 6, 2024 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT 10WL FWD CABIN BATTERY LIFE EXPIRED REF TO PEMCO NR 15426.0045 REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 10WL IAW A319 AMM 33-51-39-000-007 C1 AND 33-51-39-400-007 C1. OPS CHECK GOOD. IAW A319 AMM 33-51-00-710-002
- [SDR CALA2024060701717](https://openairdocs.org/sdr/CALA2024060701717.md): Battery · expired · Jun 6, 2024 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT 11WL L/H MID CABIN BATTERY LIFE EXPIRED. REF TO PEMCO NR 15426.0046 REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 11WL IAW A319 AMM 33-51-39-000-007C1 AND 33-51-39-400-007-C1. OP S CHECK GOOD IAW A319 AMM 33-51-00-710
- [SDR CALA2024060701716](https://openairdocs.org/sdr/CALA2024060701716.md): Battery · expired · Jun 6, 2024 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT 12WL R/H MID CABIN BATTERY LIFE EXPIRED. REF TO PEMCO NR 15426.0047 REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 12WL IAW A319 AMM 33-51-39-000-007-C1 AND 33-51-39-400-001-C1.
- [SDR CALA2024060701715](https://openairdocs.org/sdr/CALA2024060701715.md): Battery · expired · Jun 6, 2024 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT 13WL AFT CABIN BATTERY LIFE EXPIRED REF TO PEMCO NR 15426.0048 REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL IAW A319 AMM 33-51-39-000-007 C1 AND 33-51-39-400-007-C1.
- [SDR CALA2023100402937](https://openairdocs.org/sdr/CALA2023100402937.md): Wire · damaged · Sep 30, 2023 · N855UA · Airbus A319131 · Air Conditioning System Wiring
  > VENT EXTRACT FAULT ECAM AEVC TEST SHOWS EXTRACT FAN 18HQ FAULT -- PANEL 123VU C/B AE2 BREAKER OUT FOR EXTRACT FAN, RESET C/B AND IF NEEDED, PARTS ADDED REF IPC 21-26-01-08 ECAM MESSAGES. SEE PHOTO T/S EXTRACTOT FAN 18 HQ FOUND WIRE HARNESS DAMAGED AT CONNECTO
- [SDR CALA2023070502173](https://openairdocs.org/sdr/CALA2023070502173.md): Fuel Cap · missing · Jul 4, 2023 · N855UA · Airbus A319131 · Aircraft Fuel System
  > FUEL CAP MISSING ON ARRIVAL QRO. OK TO CDL CREW APPLIED STICKER DISPATCH DESK: 33 NAME: JP DATE: 04-JUL-23. DEFERRED DIRECTLY BY TOMC. REPLACED FUEL CAP PER AMM 28-25-00. CAP, COUPLING R OFF 31-2825-9-0001 0671 ON 31-2825-9-0001 7070.
- [SDR CALA2022072701889](https://openairdocs.org/sdr/CALA2022072701889.md): Seat Track · corroded · Jul 27, 2022 · N855UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN R/H I/B FLOOR SEAT TRACK HAS CORROSION AT FR-20. REMOVED CORROSION DAMAGE OUT OF LIMITS IAW SRM 53-00-15-283-002. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-11-15 AND SRM 51-42- 11. WORK ACCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR# 32944.
- [SDR CALA2022072001841](https://openairdocs.org/sdr/CALA2022072001841.md): None · corroded · Jul 20, 2022 · N855UA · Airbus A300* · Fuselage Main, Structure
  > AFT CARGO COMPT: AFT CARGO DOORSILL CUTOUT SURFACE FR55A TO FR59 HAS SEVERAL POINT POINT WITH CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00 IS FOUND OUT LIMIT IAW S NSTALLED NEW SHEET THRESHOLD IAW SRM 51-42-11 AND DRAWING PART L RM 53-41-49-283-003, REMO
- [SDR CALA2022072001840](https://openairdocs.org/sdr/CALA2022072001840.md): None · corroded · Jul 20, 2022 · N855UA · Airbus A300* · Fuselage Miscellaneous Structure
  > AFT CARGO CPMT: AFT CARGO DOOR LOWER FRAME WITH COVER SHEET SURF ACE CORRODED FROM FR55A TO FR59. REMOVED AND REPLACED SHEET COVER AT AFT CARGO DOOR LOWER FRAME F ROM FR55 TO FR 59 IAW A319 SRM 51-72-11-911-001. WORK ACCOMPLISH ED AT ST ENGINEERING OF MOBILE A
- [SDR CALA2022071801786](https://openairdocs.org/sdr/CALA2022071801786.md): None · corroded · Jul 16, 2022 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO CPMT: AFT CARGO DOOR LOWER FRAME WITH COVER SHEET SURFACE CORRODED FROM FR55A TO FR59.
- [SDR CALA2022071801783](https://openairdocs.org/sdr/CALA2022071801783.md): Door Sill · corroded · Jul 15, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO COMPT: AFT CARGO DOOR SILL CUTOUT SURFACE FR55A TO FR59 HAS SEVERAL POINT POINT WITH CORROSION.
- [SDR CALA2022071501752](https://openairdocs.org/sdr/CALA2022071501752.md): None · corroded · Jul 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > (SUPPORT TASK) AFT CARGO COMPARTMENT BETWEEN FR61 AND FR62 STR 3 4R HAS CORROSION. DOT 132-87() REMOVED CORROSION ON STR 34R BETWEEN FR61-FR62 IAW SRM 51-74-00 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM O AREA FOUND OUT OF LIMITS IAW SRM 53
- [SDR CALA2022071501750](https://openairdocs.org/sdr/CALA2022071501750.md): Seat Track · corroded · Jul 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > FWD CABIN R/H I/B FLOOR SEAT TRACK HAS CORROSION AT FR-20.
- [SDR CALA2022062401559](https://openairdocs.org/sdr/CALA2022062401559.md): Floor Support · corroded · Jun 22, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > DURING INSPECTION EA 5310-06784 REV A, WAS FOUND FLOOR STRTUCTUR E WEB IN FR16 NEAR TO DOOR RH WITH CORROSION.
- [SDR CALA2022062401558](https://openairdocs.org/sdr/CALA2022062401558.md): Seat Track · corroded · Jun 22, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > FWD CABIN R/H O/B SEAT TRACK HAS CORROSION AT FR20.
- [SDR CALA2022061701528](https://openairdocs.org/sdr/CALA2022061701528.md): Stringer · gouged · Jun 17, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSEALGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 12 RMEOVED GUSSET PLATE AT FR66 STGR12 IAW SRM 51-44-11; RECEIVED N EW GUSSET PLATE TRAVELER# T22/1620912 P/N UAD5348002075900 BATCH # 0003819824 AND INSTALLED NEW GUSSET PLATE A
- [SDR CALA2022061701527](https://openairdocs.org/sdr/CALA2022061701527.md): Stringer · gouged · Jun 17, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 14 REMOVED GUSSET PLATE AT FR66. STGR 14. IAW SRM 51-44-11; RECEIVE D NEW GUSSET PLATE TRAVELER# T22/1620915 P/N UAD5348002075900; B ATCH# 0003819824 AND INSTALLED NEW GUSSET PLA
- [SDR CALA2022061701526](https://openairdocs.org/sdr/CALA2022061701526.md): Stringer · gouged · Jun 17, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOUGE FROM STRINGER 10 REMOVED GUSSET PLATE AT FR66 STRINGER 10 IAW SRM 51-44-11; RECEI VED NEW GUSSET PLATE TRAVELER# T22/1620904, P/N UAD5349002075900 BATCH# 0003819824 AND INSTALLED NEW GUSSET PLA
- [SDR CALA2022061501505](https://openairdocs.org/sdr/CALA2022061501505.md): Plate · gouged · Jun 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 14
- [SDR CALA2022061501504](https://openairdocs.org/sdr/CALA2022061501504.md): Plate · gouged · Jun 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSEALGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 12
- [SDR CALA2022061501503](https://openairdocs.org/sdr/CALA2022061501503.md): Plate · gouged · Jun 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > RIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 10
- [SDR CALA2022061501501](https://openairdocs.org/sdr/CALA2022061501501.md): Beam · corroded · Jun 14, 2022 · N855UA · Airbus A319131 · Fuselage Main, Structure
  > FWD CABIN FROM CENTER L/H I/B SUPPORT #1 HAS CORROSION AT FR16 REMOVED CORROSION IN TRACK ASSY AND FOUND WITHOUT LIMITS D=0,060 " MAX D=0,047" T93987. REMOVED AND REPLACED TRACK ASSY IAW SRM 5 1-42-11/001. EMP: V935975 WC: 32949 STA: ST ENG BFM SFR# 1028831
- [SDR CALA2019111601971](https://openairdocs.org/sdr/CALA2019111601971.md): Door Sill · corroded · Nov 11, 2019 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 PAX DOOR SILL FRAME 68 STR 23RH IB SIDE HAS CORROSION FOR NR 9294303 SUPPORT TASK GEN AT HAECO LCQ. RMVD AND RPLD R2 PAX DOOR SILL FR68 STR 23RH IAW SRM 51-42-11-80 1 REF RDAS 80703194-003-2019, REPAIR REF TD 80703194-012-2019 NO.A, ECRA # 5331-02502
- [SDR CALA2019111601970](https://openairdocs.org/sdr/CALA2019111601970.md): Intercostal · cracked · Nov 11, 2019 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R1 DOOR FR 20 NO. 7 STOP UPPER I/B HOLE HAS CRACK INDICATION ON THE INTERCOSTAL ON HAECO LCQ REF 9296085 SPEC A3NB-53-4-6054 AD RELATED AD 2015-05-02. REMOVED & REPLACED WITH NEW INTERCOSTAL IAW A319 SRM 51-72-11, A 319 SRM 51-42-11 AT HAECO LCQ ON HANGAR NR
- [SDR CALA2019110981929](https://openairdocs.org/sdr/CALA2019110981929.md): Hinge Arm · worn · Nov 6, 2019 · N855UA · Airbus A319131 · Rudder Structure
  > ELONGATED HOLES ON RUDDER - #4 HINGE ARM ASSY''. (MX/CUST REQ) (A 3NB-27-3-6014) REF HAECO LCQ NR 9296315 AND GENERATED BY V925611 REMOVED & REPLACED RUDDER NO. 4 HINGE ARM ASSY IAW A319 SRM 55-3 6-42-300-003 AT HAECO LCQ ON HANGAR NR 9296315 PERFORMED BY MECH
- [SDR CALA2019030800360](https://openairdocs.org/sdr/CALA2019030800360.md): Unknown · malfunctioned · Mar 5, 2019 · N855UA · Airbus A319131 · Emergency Lighting
  > PER 9617511 AND T/C 18-0550-1-0002 (SPEC A3NB-33-3-6012) CAB IN EMERGENCY LIGHT CHECK FROM PTP FAILS WITH MSG "EPSU BATT AFT L" AND "EPSU BATT EMER L" RESET EPSU BATT AFT L AND BATT EMER L IAW AMM 33-51-38-400- 001A, PERFORMED BITE TEST IAW AMM 33-51-38-400-00
- [SDR CALA2017102303745](https://openairdocs.org/sdr/CALA2017102303745.md): Unknown · odor · Oct 23, 2017 · N855UA · Airbus A319131 · Air Distribution System
  > MUSTY, OIL SMELL IN CABIN ON DESCENT, SMELL DISSIPATES WITH PACK 2 OFF. PERFORMED TROUBLESHOOTING OF CABIN OIL FUMES, IAW A319/A320 TSM 49-00-00-810-921A12. PERFORMED PRE-CONDITIONING WITH APU. NO FUMES IN CABIN IAW A319/A320 AMM 12-33-21-618-001-A.
- [SDR CALA2017031700647](https://openairdocs.org/sdr/CALA2017031700647.md): Power Supply · malfunctioned · Mar 17, 2017 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS FAILED AN OPS CHECK, MESSAGE FOR EPSU UNIT FWD LT. RESET THE POWER SUPPLY AT THE L1 DOOR. TESTED OK IAW AMM 33-51-00-501
- [SDR CALA2016081295640](https://openairdocs.org/sdr/CALA2016081295640.md): Power Supply · malfunctioned · Aug 9, 2016 · N855UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS CAME ON IN CABIN WHEN SEATBELT SIGN TURNED ON. CYCLED ON/OFF AND OPS NORMAL. OP TEST OF CABIN SIGNS IAW AMM GOOD. R & R EPSU.
- [SDR CALA2016081195621](https://openairdocs.org/sdr/CALA2016081195621.md): Power Supply · no test · Jun 17, 2016 · N855UA · Airbus A319131 · Emergency Lighting
  > SYSTEM TEST SHOWED FWD LT POWER SUPPLY UNIT AND AFT L BATTERY FAILED. REPLACED FWD L POWER SUPPLY UNIT AND AFT L BATTERY. SYSTEM TESTED GOOD.
- [SDR CALA2015060493854](https://openairdocs.org/sdr/CALA2015060493854.md): Contactor · faulty · Jun 1, 2015 · N855UA · Airbus A319131 · AC Generation System
  > LOSS OF ELEC ESSENTIAL POWER BUSS ON CLIMB OUT. REPLACED 15XE CONTACTOR IAW WD 24-24-06 AS PRECAUTION IAW AMM 24-24-55-401. WIRES CHECKED IAW TSM 24-50-00-810-814-A & BOTH 15XC,16XC RELAYS REPLACED.
- [SDR CALA2015051193763](https://openairdocs.org/sdr/CALA2015051193763.md): Computer · malfunctioned · May 7, 2015 · N855UA · Airbus A319131 · Autopilot Computer
  > LOSS OF NR 1 ILS, FLIGHT MGMT & GUIDANCE CMPT FMGC NR 2 INOPERATIVE. ACCOMPLISHED RESET OF FMGC 1/2. ACCOMPLISHED AFS TEST IAW AMM 22-96-00-501. AUTOLAND DOWNGRADED.
- [SDR CALA2015022093163](https://openairdocs.org/sdr/CALA2015022093163.md): Power Supply · inoperative · Feb 17, 2015 · N855UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY FWD LIGHT MSG WHEN PERFORMING EMER LIGHT TEST. REPLACED BATTERY SUPPLY IAW AMM 33-51-00. OPERATIONS CHECKED OK.
- [SDR CALA2014082692029](https://openairdocs.org/sdr/CALA2014082692029.md): Door Sill · corroded · Aug 24, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L1 DOOR SILL BEAM WAS CORRODED AROUND THE FWD GIRT BAR FITTING AFT INBD ATTACH HOLE & THE AFT FITTING AFT INBD & OTBD ATTACH HOLES. HOLES WERE SPOT FACED & REPAIR WASHERS INSTALLED IAW SRM 53-11-14 PARA 4 E FIG 108. MINIMUM MATERIAL THICKNESS AT SPOT FACES I
- [SDR CALA2014082692028](https://openairdocs.org/sdr/CALA2014082692028.md): Door Sill · corroded · Aug 24, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R1 DOOR SILL BEAM WAS CORRODED AROUND THE FWD & AFT GIRT BAR FITTING HOLES & AROUND THE FWD DRAIN HOLE. CORROSION WAS REMOVED & AREA BLENDED AROUND THE DRAIN HOLE. FWD GIRT BAR FITTING AFT OTBD HOLE & ALL 4 HOLES AT THE AFT GIRT BAR FITTING WERE SPOT FACED &
- [SDR CALA2014082692025](https://openairdocs.org/sdr/CALA2014082692025.md): Door Sill · corroded · Aug 23, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > 2R DOOR SILL CORRODED UNDER THE GIRT BAR PLATES. DOOR SILL REPLACED IAW SRM 51-42-11 & SRM 51-44-11.
- [SDR CALA2014082592014](https://openairdocs.org/sdr/CALA2014082592014.md): Door Sill · corroded · Aug 21, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL & AFT CORNER FITTING CORRODED BETWEEN FRAME 66 & 68. DOOR SILL & AFT CORNER FITTING R & R IAW SRM 51-42-11.
- [SDR CALA2014082192002](https://openairdocs.org/sdr/CALA2014082192002.md): Skin · dented · Aug 20, 2014 · N855UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT REPORTED BY FLIGHT CREW & CATERING AFT OF DOOR 2L. FUSELAGE DENTED BETWEEN FRAME 69 & 70 AT STRINGER 21. DENT ABOVE STRINGER IS.040 INCHES DEEP,.23 INCHES FROM NEAREST RIVET ROW, 2.66 INCHES X 1.24 TOTAL AREA. DENT BELOW STRINGER IS 3 X 1.25,.010 I
- [SDR CALA2014081891997](https://openairdocs.org/sdr/CALA2014081891997.md): Door Sill · corroded · Aug 17, 2014 · N855UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL HAS SPOTS OF CORROSION BETWEEN FRAME 66 & 68. BLENDED CORROSION, AFTER BLENDING ALL AREAS WERE WITHIN LIMITS EXCEPT FOR NUTPLATE AT INBD FLANGE ON FRAME 68 IAW SRM 53-41-14 FIG 101.

Next page: https://openairdocs.org/aircraft/N855UA/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 = 'N855UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N855UA/reports

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