# Service difficulty reports: N840UA

A list on [N840UA](https://openairdocs.org/aircraft/N840UA.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 · 102 reports

- [SDR CALA2026061917188](https://openairdocs.org/sdr/CALA2026061917188.md): Apu · odor · Jun 14, 2026 · N840UA · Airbus A319131 · Airborne Auxiliary Power Unit (APU) System
  > MUSTY SOCK SMELL FROM PACKS W APU BLEED RUNNING OILY MUSTY SMELL WITH PACKS RUNNING ON APU. PLACED APU ON MEL MEL 4910B REJECTED NEED TO ADDRESS THE ODOR IN THE CABIN ACP INITIAL TROUBLE SHOOTING PER FIM TASK 05-50-00-810-831-A, CONFIRMED ORDER STRONG WHEN
- [SDR CALA2026060916954](https://openairdocs.org/sdr/CALA2026060916954.md): Light · inoperative · Jun 8, 2026 · N840UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT OUT AT ROW 31CBA, 32CBA REMOVED AND REPLACED SEAT/WALL MOUNT EMERGENCY LIGHT PER AMM 33-51-18. OPS CHECK GOOD
- [SDR CALA2026041015259](https://openairdocs.org/sdr/CALA2026041015259.md): Fuel Cap · missing · Apr 6, 2026 · N840UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTED FUEL CAP MISSING AFTER T-2272 ON ARRIVAL IN MSP FROM SFO.
- [SDR CALA2026032314733](https://openairdocs.org/sdr/CALA2026032314733.md): Apu · faulted · Mar 19, 2026 · N840UA · Airbus A319131 · APU Core Engine
  > SMOKE FUME EVENT DURING ENGINE 1 START AFT CABIN WAS BAD FLT DEC K HAD FUMES TOO. INSPECTED APU IAW TASK 49-00-00-200-816-A, FOUND SMOKE AND OIL RESIDUE IN THE COMPARTMENT. REMOVED HEAT SHIELD AROUND THE AFT TURBINE SECTION FOUND UPPER & LOWER LUBRICATION LI
- [SDR CALA2025120211670](https://openairdocs.org/sdr/CALA2025120211670.md): Battery Pack · no test · Nov 29, 2025 · N840UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMER L, FAULT MESSAGE FROM CIDS WHILE CONDUCTING EMER LIGHT SYSTEM TEST. REMOVED AND REPLACED EPSU BATTERY 11WL, IAW AMM 33-51-38-000-002-A, 33-51-38-400-002-A. OPS CHECKED GOOD, NO FAULT MESSAGES OR DEFECTS NOTED.
- [SDR CALA2025102910677](https://openairdocs.org/sdr/CALA2025102910677.md): Filter · clogged · Oct 27, 2025 · N840UA · Airbus A319131 · Air Distribution System
  > FUMES REPORTED IN AFT GALLEY, ACFT DIVERTED TO RIC. LOCAL FBO TO FOLLOW AMM 05-51-10-200-801-C-1. REMOVED AND REPLACED CABIN RECIRCULATION FILTERS IAW MM 21-21-00, NO ABNORMAL FINDINGS, OK.
- [SDR CALA2025072206829](https://openairdocs.org/sdr/CALA2025072206829.md): Stringer · corroded · Jul 19, 2025 · N840UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT PIT STR 31R CORRODED AT FR 65. RMVD AND RPLD STRINGER 31R FROM FR 64-67 IAW A319 SRM 51-72-11- 911-001.
- [SDR CALA2025070706273](https://openairdocs.org/sdr/CALA2025070706273.md): Fitting · cracked · Jul 6, 2025 · N840UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD LOWER NODE AREA, LEFT CONTINUITY FITTING CRACKED AT HORIZONTAL FLANGE, AFT EDGE. REMOVED/REPLACED LH AND RH CONTINUITY FITTINGS AS DIRECTED BY EA 5310-07675 AND IAW A319 SRM 51-42-14/001 AND AIRBUS REPAIR DRAW INGS R5311-2919 AND R 53113426.
- [SDR CALA2025071106461](https://openairdocs.org/sdr/CALA2025071106461.md): Door Frame · cracked · Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, Structure
  > LH O/W HATCH AFT FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED AFT FRAME SEGMENT ON LH O/W HATCH IAW SRM 51-72-11-911-001, SRM 51-42-11-001, SRM 51-75-12-911-002.
- [SDR CALA2025071106460](https://openairdocs.org/sdr/CALA2025071106460.md): Door Frame · cracked · Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, Structure
  > LH O/W HATCH FWD FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED FWD FRAME SEGMENT ON LH O/W HATCH IAW SRM 51-72-11-911-001, SRM 51-42-11-001, SRM 51-75-12-911-002.
- [SDR CALA2025071106459](https://openairdocs.org/sdr/CALA2025071106459.md): Door Frame · cracked · Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, Structure
  > RH O/W HATCH AFT FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED 1EA FRAME DEGMENT (AFT) AT R/H O/W HATCH IAW SRM 51-42-11-001, SRM 51-72-11-911-001, AND SRM 51-75-12- 911-002.
- [SDR CALA2025071106458](https://openairdocs.org/sdr/CALA2025071106458.md): Door Frame · cracked · Jul 3, 2025 · N840UA · Airbus A319131 · Fuselage Main, Structure
  > RH O/W HATCH FWD FRAME SEGMENT IS CRACKED. REMOVED AND REPLACED 1EA FRAME SEGMENT (FWD) AT R/H O/W HATCH IAW SRM 51-42-11-001, SRM 51-72-11-911-001, AND SRM 51-75-12- 911-002.
- [SDR CALA2025062705994](https://openairdocs.org/sdr/CALA2025062705994.md): Floor Support · corroded · Jun 25, 2025 · N840UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT Y 765 AT FR 64-65 HAS CORROSION AT HARD POINT. REMOVED AND REPLACED 1EA FLOOR BEAM (Y765) AT AFT FUSELAGE L/H S IDE IAW A319 SRM 51-47-11/001 AND A319 SRM 51-72-11-911-001.
- [SDR CALA2025062705992](https://openairdocs.org/sdr/CALA2025062705992.md): Floor Support · corroded · Jun 25, 2025 · N840UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT Y 1292 AT FR 64-65 HAS CORROSION AT HARD POINT. REMOVED AND REPLACED 1EA FLOOR BEAM *Y1292) AT AFT FUSELAGE L/H SIDE IAW A319 SRM 51-42-11/001 AND A319 SRM 51-72-11-911-001.
- [SDR CALA2025051904829](https://openairdocs.org/sdr/CALA2025051904829.md): Cap · missing · May 16, 2025 · N840UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING AS FOUND ON SERVICE CHECK WALKAROUND. NOTIFIED TOMC NEWMAN REF AMM TASK 28-25-41. REPLACED MISSING FUEL CAP AND LANYARD. NO LEAKS OR DAMAGE NOTED. PARTS USED: 31-2825-9-0001,QTY:1 ROTABLE PARTS CHG SN OFF 4040 PN OFF 31-2825-9-0001 IP
- [SDR CALA2025040703576](https://openairdocs.org/sdr/CALA2025040703576.md): Slide · none · Apr 2, 2025 · N840UA · Airbus A319131 · Escape Slide
  > FORWARD DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0020} - SCHEDULED PARTS CHANGE OF L1 DOOR, REMOVED SLIDE PACK. R&R L1 ESCAPE SLIDE. AS PER AMM 25-62-44 C.W RII INSP REQUIREMENTS FOR L1 DOOR REF GMM 09-25-05
- [SDR CALA2025040703575](https://openairdocs.org/sdr/CALA2025040703575.md): Slide · not reported · Apr 2, 2025 · N840UA · Airbus A319131 · Escape Slide
  > FORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - SLIDE DOOR SAFETY ARMING PIN INSTALLED. REMOVED SLIDE DOOR SAFETY ARMING PIN AS PER 25-62-44 AFTER SCHEDULED PARTS CHANGE OF L1 SLIDE C.W WITH IDT INSP REQUIREMENT FOR SLIDE DOOF SAFETY ARMING
- [SDR CALA2024112502947](https://openairdocs.org/sdr/CALA2024112502947.md): Bolt · missing · Nov 24, 2024 · N840UA · Airbus A319131 · Wheel/Ski/Float
  > #1 MLG TIRE MISSING A WHEEL TIRE BOLT.... UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED. PERFORM A GVI MAC RELATED WORK ORDER 000000003123069 AND PRTR OF THE ARE FOR MISSING BOLT. REMOVE AND REPLACE THE MLG TIRE. REMOVED AND REPLACED THE
- [SDR CALA2024083000518](https://openairdocs.org/sdr/CALA2024083000518.md): Vent · unknown · Aug 28, 2024 · N840UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > VENT SKIN VALVE FAULT ACCOMPLISHED RESET PROCEDURE AND AVEC TEST, REF TSM 21-26-00-810-803-A. TEST OK.
- [SDR CALA2024080700380](https://openairdocs.org/sdr/CALA2024080700380.md): Spoiler Sys · faulted · Aug 3, 2024 · N840UA · Airbus A319131 · Drag Control System
  > F/CTL SPOILER FAULT MESSAGE ON ECAM. (L SPLR4 SERVO VLV 31CE7 OR OUTPUT FROM SEC 1)... TOMC SMITH REQUEST MEL, DEACTIVTED LH SPLR 4 REF MEL 2764W DISPATCH DESK: 34 NAME: CO DATE: 03-AUG-24-OK TO APPLY MEL 2764W FOR SPOILER #4 PAIR INOP PLACED ON MEL. *DM* SU
- [SDR CALA2024072602106](https://openairdocs.org/sdr/CALA2024072602106.md): Skin · contaminated · Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS INDICATION OF WATER INGRESS, VISIBLE AREA 2 INCH ES DIA, 71 INCHES FROM IB EDGE, 13 INCHES FROM AFT EDGE, EXTENDI NG UNDER LIGHTENING STRIP, GEN BY MECH V892444 REPAIRED L/H ELEVATOR UPPER SKIN 71 IN FROM I/B 13IN FROM T/E ZO NE A 2 IN DIS IAW
- [SDR CALA2024072302089](https://openairdocs.org/sdr/CALA2024072302089.md): Skin · contaminated · Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR UPPER SURFACE HAS EVIDENCE OF WATER INGRESS 29 INCHE S FROM IB EDGE, 22 INCHES FROM AFT.75 IN DIA., GEN BY MECH V892 444 DRILLED WITNESS HOLES ON R/H ELEVATOR UPPER SKIN 29 IN FROM I/B INSP BY V078632 22IN FROM T/E ZONE A 1.5 IN DIA IAW A319 AMM 5
- [SDR CALA2024072302090](https://openairdocs.org/sdr/CALA2024072302090.md): Skin · contaminated · Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS INDICATION OF WATER INGRESS, 2 INCHES DIA, 117 I NCHES FORM IB EDGE, 13 INCHES FROM AFT EDGE. GEN BY MECH V892444 REPAIRED L/H ELEVATOR UPPER SKIN 77IN FROM I/B EDGE, 12IN FROM T /E ZONE A, 2IN DIA IAW A319 SRM 55-21-11-300-005 PAR 2A CATEGORY
- [SDR CALA2024072302087](https://openairdocs.org/sdr/CALA2024072302087.md): Skin · contaminated · Jul 21, 2024 · N840UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR UPPER SURFACE HAS EVIDENCE OF WATER INGRESS 29 INCHES FROM IB EDGE, 18.5 INCHES FROM AFT EDGE, 1.75 INCH DIA., DRILLED WITNESS HOLES ON R/H ELEVATOR UPPER SURFACE 29IN FROM I/ 75, B 18.5 FROM T/E ZONE A 1.5IN DIA. FOUND NO LIQUID IAW A319 AMM 55-
- [SDR CALA2024011900142](https://openairdocs.org/sdr/CALA2024011900142.md): Fuel Cap · missing · Jan 17, 2024 · N840UA · Airbus A319131 · Fuel Storage
  > REPORTED BY FUELER FUEL CAP MISSING FUEL CAP MISSING WOULD LIKE TO APPLY CDL 28A CAP AND LANYARD MISSING PLACED ON CDL DISPATCH DESK: 37 NAME: MA. DATE: 17-JAN-24- OK TO DEFER FUEL CAP MISSING.
- [SDR CALA2023022400545](https://openairdocs.org/sdr/CALA2023022400545.md): Valve · failed · Feb 24, 2023 · N840UA · Airbus A319131 · Trailing Edge Flap Control System
  > UPON ACFT ARRIVAL GATE RETURN VERBALLY ADVICED BY FLIGHT CREW FLAP SYST 2 FAULT. PFR SHOWING FLP2 PCU VALVE BLOCK 24CV VALVE SENSOR. SEE TSM PICTURE OF PFR 27-51-00-810-852-A. 27-54-53-000-001-A VERIFIED VALVE BLOCK OF THE POWER CONTROL UNIT (FLAP) WAS REMOV
- [SDR CALA2022112803243](https://openairdocs.org/sdr/CALA2022112803243.md): Oxygen Mask · leaking · Nov 28, 2022 · N840UA · Airbus A319131 · Crew Oxygen System
  > CREW SYSTEM LOW CREW OXYGEN SYSTEM-LOW... RECORD PRESSURE PRIOR TO SERVICING 820PSI AFTER TAKEOFF PRESSURE WAS 870 ON GROUND MARTIN, ERIC (V907926) TROUBLESHOT PER TSM 35-10-00-810-813A. FO UND LARGE LEAK COMING FROM LH OBSERVERS MASK. REMOVED OBSERVER MASK AN
- [SDR CALA2022091402357](https://openairdocs.org/sdr/CALA2022091402357.md): Intercostal · none · Sep 12, 2022 · N840UA · Airbus A300* · Fuselage Main, Frame
  > AD RELATED SUPPORT TASK (AD 2022-02-11): RH FR16 STOP #7 HOLE #3 (IB LOWER) HAS CRACK INDICATION IN INTERCOSTAL @10 O''CLOCK. AT HAECO LCQ NON ROUTINE 9294266/24266 GENERATED BY V892444. REMOVED DAMAGED INTERCOSTAL & REPLACED WITH A NEW INTERCOSTAL @ R/H FR16
- [SDR CALA2022082602187](https://openairdocs.org/sdr/CALA2022082602187.md): Fitting · none · Aug 25, 2022 · N840UA · Airbus A300* · Fuselage Main, Frame
  > RH WINDSHIELD SIDE POST UPPER ATTACHMENT, HOLE ON VERTICAL POST HAS CRACK INDICATION: AD RELATEDE SUPPORT TASK (A3NB-53-4-0068) GENERATED BY V892444 AT HAECO LCQ PER NR 9294532 (24532) PERFORMED CUT OUT OF CRACK AND REPLACED UPPER ATTACHMENT FITTING ON THE RH
- [SDR CALA2019012100129](https://openairdocs.org/sdr/CALA2019012100129.md): Fastener · sheared · Jan 19, 2019 · N840UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR FR68 R2 DOOR SILL AFT GIRT BAR SUPPORT HAS SHEARED FASTNER A3NB-53-3-6222 ON LCQ NR 9298248 REMOVED AND REPLACED R2 DOOR SILL BETWEEN FR66-FR68 IAW SRM 51-72-11-911-001.
- [SDR CALA2019012100128](https://openairdocs.org/sdr/CALA2019012100128.md): Support Angle · corroded · Jan 19, 2019 · N840UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN FR68 L2 DOOR SILL SUPPORT ANGLE HAS CORROSION SPOTS ON UPPER SURFACE A3NB-53-3-6222 ON LCQ NR 9298263 INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-41-14. ALODINE AND PRIMED IAW SRM 51-21-11-001. INSTALLED GIRT BAY ASSY IAW IPC 53-46-04-81 AND AMM 52
- [SDR CALA2017120304301](https://openairdocs.org/sdr/CALA2017120304301.md): Director · malfunctioned · Dec 3, 2017 · N840UA · Airbus A319131 · Lighting System
  > EMERG EXIT LIGHTS ON. RESEAT CIDS DIRECTOR SYST OP OK
- [SDR CALA2017052601598](https://openairdocs.org/sdr/CALA2017052601598.md): Battery · faulted · May 26, 2017 · N840UA · Airbus A319131 · Emergency Lighting
  > DURING AN EMERGENCY LIGHTS TEST, MESSAGE FOR THE EPSU BATTERY AFT LT. REPLACED THE BATTERY. OPS CHECKED GOOD.
- [SDR CALA2017051201363](https://openairdocs.org/sdr/CALA2017051201363.md): Interface Unit · faulted · May 12, 2017 · N840UA · Airbus A319131 · Central Display
  > CONSTANT/MULTIPLE FALSE ECAM ALERTS. FADEC/DUAL ENG FAIL/NAV.. EMERGENCY DECLARED. REPLACED CFDIU IAW AMM 31-32-34-400-001-A.AND NR 2 FWC IAW AMM 31- 53-34 OPS CHECK OK. PERFORMED LAND VERIFY IAW AMM 22-97-00 LAND TEST OK. AIRCRAFT REMAINS FULL AUTOLAND STAT
- [SDR CALA2017031700609](https://openairdocs.org/sdr/CALA2017031700609.md): Arm · gouged · Mar 16, 2017 · N840UA · Airbus A319131 · Horizontal Stabilizer Structure
  > LEFT HORIZONTAL STABILIZER NR 4 HINGE ARM GOUGED UNDER LOCK FASTENER COLLAR AT FWD OTBD UPPER ATTACH FLANGE. REMOVED AND REPLACED THE ARM IAW SRM 51-72-11, PG. 12.
- [SDR CALA2016101000736](https://openairdocs.org/sdr/CALA2016101000736.md): Check Valve · inoperative · Oct 7, 2016 · N840UA · Airbus A319131 · Hydraulic System, Main
  > ACFT LOST GREEN HYD QTY OK FOR SERVICE, HYDRAULIC RESERVOIR DID NOT EMPTY, SERVICED TO FULL AFTER LEAK FIXED
- [SDR CALA2016100700731](https://openairdocs.org/sdr/CALA2016100700731.md): Check Valve · leaking · Oct 7, 2016 · N840UA · Airbus A319131 · Hydraulic System, Main
  > LOST GREEN HYD FLUID, FOUND CHECK VALVE PTU MANIFOLD LEAKING. REMOVED AND REPLACED THE CHECK VALVE AND O-RING. LEAK CHECKED, NO LEAKS FOUND.
- [SDR CALA2016092095754](https://openairdocs.org/sdr/CALA2016092095754.md): Selector Valve · malfunctioned · Sep 18, 2016 · N840UA · Airbus A319131 · Landing Gear Brake System
  > AIRCRAFT EXCURSION FROM TAXIWAY. CREW REPORTED LOSS OF BRAKES AND STEERING. PFR SHOWS BRAKE SELECTOR VALVE 23GG FAULT ALONG WITH MLG HYDRAULIC PIPE MESSAGE. TEST RUN ON BSCU CHANNEL 1 & 2. BSCU CHAN 1 LAST LEG REPORT - "BRK SELECTOR VALVE (23GG)/L G HYDRAULI
- [SDR CALA2016060795438](https://openairdocs.org/sdr/CALA2016060795438.md): Pump · leaking · Jun 6, 2016 · N840UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > AIR RETURN DUE TO YELLOW HYD SYS QTY LOSS. REPLACED MAIN YELLOW SYS ENG PUMP. INSPECTED FILTERS & DPI'S, FOUND NO CONTAMINANTS. SERVICED SYS, PRESS & LEAK CHECKED GOOD.
- [SDR CALA2016060195421](https://openairdocs.org/sdr/CALA2016060195421.md): Skin · punctured · May 28, 2016 · N840UA · Airbus A319131 · Wing, Plate/Skin
  > .75 INCH PUNCTURE ON FIXED LE SKIN ABOVE FUEL DOOR UNDER RT NR 3 LE SLAT. ACCOMPLISHED REPAIR IAW SRM 57-41-11-2015A.
- [SDR CALA2016052095377](https://openairdocs.org/sdr/CALA2016052095377.md): Battery Pack · defective · May 20, 2016 · N840UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY POWER SUPPLY UNIT FWD LT, FAULT MSG DISPLAYED ON EMER LIGHT SYS TEST. REPLACED BATTERY PACK AT FWD EPSU POSITION 10WL.
- [SDR CALA2015121494878](https://openairdocs.org/sdr/CALA2015121494878.md): Power Supply · inoperative · Dec 9, 2015 · N840UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED ON 2 SERVICE. REPLACED EMER LIGHT POWER SUPPLY & BATTERY IAW AMM 33-51-38 AT OVERWING EXIT LT SIDE, OPERATIONS CHECKED GOOD.
- [SDR CALA2014122392857](https://openairdocs.org/sdr/CALA2014122392857.md): Fan · faulty · Dec 18, 2014 · N840UA · Airbus A319131 · Air Distribution Fan
  > FLIGHT ATTENDANT`S REPORTED SMOKE & BURNING SMELL. ACCOMPLISHED AMM TASK 05- 51-10-S00-801C1. DETERMINED THAT NR 2 CABIN RECIRC FAN 14HG IS AT FAULT IAW SEQ 1032003 FOR PART CHANGE.
- [SDR CALA2013122393906](https://openairdocs.org/sdr/CALA2013122393906.md): Door · broken · Dec 23, 2013 · N840UA · Airbus A319131 · Crew Oxygen System
  > FIRST OFFICER`S OXY MASK DOOR BROKEN. IAW GMM 05-30-06 REPLACED FIRST OFFICER`S OXY MASK DOOR.
- [SDR CALA2013120293373](https://openairdocs.org/sdr/CALA2013120293373.md): Microphone · defective · Nov 27, 2013 · N840UA · Airbus A319131 · Audio Integrating System
  > UNABLE TO TRANSMIT FIRST OFFICER`S SIDE, RADIO HANDSET & MIC. TROUBLE SHOT TO A BAD MIC FIRST OFFICER`S POSITION. R & R MIC, PERFORMED ADJUSTMENT TEST IAW MM, OPERATIONS CHECKED GOOD.
- [SDR CALA2013111892981](https://openairdocs.org/sdr/CALA2013111892981.md): Power Supply · faulty · Nov 15, 2013 · N840UA · Airbus A319131 · Emergency Lighting
  > EPSU INTERNAL LOAD EMERGENCY RT & EPSU UNIT EMERGENCY LIGHT FAULTS WHEN PERFORMING EMERGENCY LIGHTS CHECK IAW 2SV. REPLACED BATTERY PWR SUPPLY 12L RT SIDE, OPERATIONS CHECKED SYSTEM & OPERATIONS CHECKED NORMAL.
- [SDR CALA2013111392888](https://openairdocs.org/sdr/CALA2013111392888.md): Tire · damaged · Nov 13, 2013 · N840UA · Airbus A319131 · Tire
  > CHUNK OF RUBBER MISSING FROM LT NOSE WHEEL, CORD SHOWING. REPLACED TIRE IAW AMM.
- [SDR CALA2013102892413](https://openairdocs.org/sdr/CALA2013102892413.md): Rudder · dented · Oct 25, 2013 · N840UA · Airbus A319131 · Rudder Structure
  > RT SIDE OF RUDDER HAS DENT-DELAMINATION 47" FROM THE BOTTOM & 20.5" FROM THE TE. CUTOUT DENTED & DELAMINATION AREA, REMOVED HONEYCOMB CORE FULL DEPTH, PREPPED, CLEANED, BONDED HONEYCOMB. APPLIED REPAIR & RESTORED FINISH IAW SRM 51-77-11, AIRBUS TD-G2-S2-0055
- [SDR CALA2013102892412](https://openairdocs.org/sdr/CALA2013102892412.md): Sill · corroded · Oct 25, 2013 · N840UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL CORRODED AT FR 68. RII INSP ACP.
- [SDR CALA2013101692094](https://openairdocs.org/sdr/CALA2013101692094.md): Skin · corroded · Oct 15, 2013 · N840UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT FUEL TANK LANDING HAS CORROSION 640BB BETWEEN RIBS 6 & 7. REMOVED CORROSION & BLENDED AREA. FOUND WITHIN LIMITS IAW SRM 57-21-11 PG 106-110, STEP 4-H.

Next page: https://openairdocs.org/aircraft/N840UA/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 = 'N840UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N840UA/reports

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