# Service difficulty reports: N846UA

A list on [N846UA](https://openairdocs.org/aircraft/N846UA.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 · 115 reports

- [SDR CALA2026091719510](https://openairdocs.org/sdr/CALA2026091719510.md): Fuel Cap · missing · Sep 13, 2026 · N846UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING, CAP FOUND MISSING UPON ARRIVAL. EWR WAS PREVIOUS STATION THEY DID NOT FIND THE CAP AT THIS TIME. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41-400-005-A. REMOVED PLACARD.
- [SDR CALA2025102010306](https://openairdocs.org/sdr/CALA2025102010306.md): Slide · not reported · Oct 20, 2025 · N846UA · Airbus A319131 · Escape Slide
  > COMPLETED REMOVAL OF L2 DOOR SLIDE AND INSTALLED NEW L2 DOOR SLIDE REF 25-62-44-400-006-A. OPS CHECK GOOD AT THIS TIME ACCOMPLISHED INSTALLATION INSPECTION OF L2 DOOR SLIDE REF 25-62-44-400-006-A. OPS CHECK GOOD AT THIS TIME
- [SDR CALA2025102010302](https://openairdocs.org/sdr/CALA2025102010302.md): None · none · Oct 20, 2025 · N846UA · Airbus A319131 · Standard Practices/Structures
  > WATCHED AND VERIFIED ALL TECHNICISNS WORKING ON SLIDE CHANGE HAS WATCHED "AIRBUS DOOR SLIDE - REMOVAL, PREPARATION, INSTALLATION" AND "AIRBUS DOOR SLIDE R&R CRITICAL STEPS" VERIFIED ALL TECHNICIANS AND OBSERVER HAS WATCHED THE NECESSARY VIDEOS PRIOR TO HANDLIN
- [SDR CALA2025102010300](https://openairdocs.org/sdr/CALA2025102010300.md): Slide · unknown · Oct 20, 2025 · N846UA · Airbus A319131 · Escape Slide
  > REF LOG #6564107 REMOVE AND REPLACE L2 DOOR SLIDE PRECAUTIUONARY. REMOVED DOOR 2L SLIDE PER AMM 25-62-44-000-002-A, UP TO AND INCLUDING STEP 4.B.6... NEED TO CONTINUE FROM 4.B.7 ADD EMP:U092776 COMPLETED REMOVAL OF L2 DOOR SLIDE AND INSTALLED NEW L2 DOOR SL
- [SDR CALA2025102010297](https://openairdocs.org/sdr/CALA2025102010297.md): None · no discrepancy · Oct 20, 2025 · N846UA · Airbus A319131 · Standard Practices/Structures
  > DOOR 2L ARMING HANDLE IS IN THE DISARM POSITION AND SAFETY PIN INSTALLED FOR SLIDE IAW AMM 25-62-44-000-002-A REMOVED DOOR ARMING PIN P/N 98D52103500000 FROM DOOR IN REF AMM TASK 25-62-44-400-006-A VERIFIED REMOVAL OF DOOR ARMING PIN P/N 98D52103500000 FROM DO
- [SDR CALA2025101009889](https://openairdocs.org/sdr/CALA2025101009889.md): Cable · failed · Oct 7, 2025 · N846UA · Airbus A319131 · Passenger/Crew Doors
  > 2L DOOR DIFICULT TO DISARM PERFORMED GVI OF DOOR 2L NO OBSTRUCTIONS FOUND ALSO PEFORMED OPS CHECK IAW AMM 52-10-00, DOOR FUNCTIONS NORMAL WITH THE EXCEPTION OF EXCESIVE FORCE NEEDED TO ARM & DISARM. REMOVED FKEXBLE CONTROL CABLE ON DOOR 2L. STIFF & UBABLE TO
- [SDR CALA2025072406870](https://openairdocs.org/sdr/CALA2025072406870.md): Structure · not reported · Jul 21, 2025 · N846UA · Airbus A319131 · Fuselage Structure (General)
  > PERFORM PERMANENT REPAIR FOR SAFETY STAY JACK POINT TAIL STRUCTURE PER ECRA 5351-01289 PART 3 ON OR BEFORE 01-20-2026. SEE LOGPAGE 5350387. PERFORM PERMANANT REPAIR OF SAFETY STAY JACK POINT TAIL STRUCTURE PER ECRA 5351-01289 STEP 3 ON OR BEFORE 01-20-26 PART
- [SDR CALA2025063006076](https://openairdocs.org/sdr/CALA2025063006076.md): Steering Sys · false indication · Jun 26, 2025 · N846UA · Airbus A319131 · Landing Gear Steering System
  > STEERING FAULT WHILE TAXIING FOLLOWED BY L/G CONTROL FAULT..LEFT GEAR SHOWS UNLOCKED. PERFORMED FUNCTIONAL TEST OF NWS WITH THE HAND WHEEL REF AMM 32-51-00-720-003-A. NO FAULTS. PERFORMED OPERATIONAL TEST OF THE NOSE WHEEL STEERING WITH THE CFDS REF AMM 32-51
- [SDR CALA2025032703243](https://openairdocs.org/sdr/CALA2025032703243.md): Slide · none · Mar 23, 2025 · N846UA · Airbus A319131 · Escape Slide
  > FORWARD DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0020} - REMOVED R1 DOOR SLIDE FOR REPLACEMENT PER AMM 25-62-44-000-802-A INSTALLED 1R DOOR ESCAPE SLIDE PER AMM 25-62-44-400-802-A. OPS CHECK GOOD.
- [SDR CALA2025030302532](https://openairdocs.org/sdr/CALA2025030302532.md): Fairing · damaged · Feb 27, 2025 · N846UA · Airbus A319131 · Engine Thrust Reverser
  > PDA 2REF LP 4012401. #1ENG RH TR FAIRING PEICE BROKEN OFF. 6IN BY 1/2IN IN SIZE. WEIGHT ESTIMATED ABOVE 3.5OZ BUT BELOW 2.2LBS SDR ACCOMPLISHED REF LP 4012401 FOR REPAIR TO #1 ENG INBOARD REVERSER FAIRING REPAIR.
- [SDR CALA2025021302318](https://openairdocs.org/sdr/CALA2025021302318.md): Girt Bar · dirty · Feb 11, 2025 · N846UA · Airbus A319131 · Emergency Equipment
  > DOOR L2 DIFFICULT TO DIS ARM. CLEANED DEBRIS FROM AROUND GIRT BAR AND GIRT BAR FITTINGS. ACCOMPLISHED DOOR 2L ARM/DISARM OPERATION WITH NO DEFECTS NOTED. REF AMM 25-62-44. OK F/SVC. ADD EMP:U010764,U342413
- [SDR CALA2025012100159](https://openairdocs.org/sdr/CALA2025012100159.md): Skin · cracked · Dec 25, 2024 · N846UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > CREASE ACROSS AFT UNDERS IDE OF FUSELAGE. COMPLETED DAMAGE MAP FOR 8 EA DENTS FR 62-64 BETWEEN STR 41LH-43RH SENT TO ENG FOR SUPPORT LOCKING LOG FOR MX FERRY FOR REPAIR AT GSO PICS ADDED MEASURED GOUGE DEPTH IN DENT #1. MATERIAL LOSS IS 0.017, PERFORMED
- [SDR CALA2024102500930](https://openairdocs.org/sdr/CALA2024102500930.md): Air Data Module · faulted · Oct 25, 2024 · N846UA · Airbus A319131 · Air Data Computer
  > PASSING 10000FT CA AIRSPD INDICATOR VARIED -/+ 20KTS FO AND STDBY IAS OK ACCMP IR1 SYSTEM TEST REF AMM 34-14-00-740-004-A. IR1 FAILS WITH MESSAGE MMR1-GPSSU1(40RT1-1SN1) ADIRU1(1FP1). SLAVED IN NEW ADIRU 1 AND SWAPPED MMR1 AND MMR2 REF TSM 34-36-00-810-874
- [SDR CALA2024022700565](https://openairdocs.org/sdr/CALA2024022700565.md): Servo Valve · faulty · Feb 23, 2024 · N846UA · Airbus A319131 · Landing Gear System
  > TEST FLIGHT DISCREPANCY. RT OVERWING EXIT SIDEWALL DUCT CONTINUOUS HIGH AIRFLOW. NO FLOW LEFT OVERWING SIDEWALL. ALSO BRAKES SYS 1 FAULT.APPEARED ON LDG. CREW ALSO REPORTS DIFFERENCE IN AIRFLOW AT RT OVERWING EXIT WHEN COCKPIT TEMP SELECTOR KNOB IS USED. BOROS
- [SDR CALA2023102503167](https://openairdocs.org/sdr/CALA2023102503167.md): Arming Lever · tight · Oct 23, 2023 · N846UA · Airbus A319131 · Emergency Equipment
  > DOOR 2L REPORTED TO BE SUPER DIFFICULT TO ARM/DISARM.PERFORMED 2L DOOR INSPECTION, LUBRICATION AND EMERGENCY HANDEL TENSION PULL REF AMM TASK 52-11-22-820-001-A. OPS CHECK NORMAL.
- [SDR CALA2023070702193](https://openairdocs.org/sdr/CALA2023070702193.md): Manifold · leaking · Jul 6, 2023 · N846UA · Airbus A319131 · Hydraulic System, Main
  > CREW REPORTED AT FL250 GOT ECAM HYD Y RSVR LO LEVEL. CREW FOLLOWED QRH AND SHUT OFF ENG PUMP. QTY WAS SHOWING ZERO. CREW TURNED Y ENG PUMP BACK ON FOR LANDING. CREW REPORTED HYD FLUID RESIDUE BETWEEN BOTH MLG WHEEL WELLS. UPDATED MAA CODE FIX USING VENDOR MAA
- [SDR CALA2023041401123](https://openairdocs.org/sdr/CALA2023041401123.md): Battery · inoperative · Apr 12, 2023 · N846UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REUQIRES REPLACEMENT. LTPR NR# 5001223609-0010 BATTERY REPLACEMENT OF (13WL) PERFORMED IAW AMM: 33-51-38-000- 002 / 33-51-38-400-002 REV 119. M&E P/N: 18-3351-3-0001, S/N OFF: 280637,
- [SDR CALA2023041401122](https://openairdocs.org/sdr/CALA2023041401122.md): Battery · inoperative · Apr 12, 2023 · N846UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REUQIRES REPLACEMENT. LTPR NR# 5001223536-0010 BATTERY REPLACEMENT OF (11WL) PERFORMED IAW AMM: 33-51-38-000- 002 / 33-51-38-400-002 REV 119. M&E P/N: 18-3351-3-0001, S/N OFF: 119508,
- [SDR CALA2023041401113](https://openairdocs.org/sdr/CALA2023041401113.md): Battery · inoperative · Apr 12, 2023 · N846UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REUQIRES REPLACEMENT. LTPR NR# 5001223528-0010 BATTERY REPLACEMENT OF (1OWL) PERFORMED IAW AMM: 33-51-38-000- 002 / 33-51-38-400-002 REV 119. M&E P/N: 18-3351-3-0001, S/N OFF: 123164,
- [SDR CALA2023041401112](https://openairdocs.org/sdr/CALA2023041401112.md): Battery · inoperative · Apr 12, 2023 · N846UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. LTP NR# 5001223572-0010. BATTERY REPLACEMENT OF (12WL) PERFORMED IAW AMM: 33-51-38-000- 002 / 33-51-38-400-002 REV 119. M&E P/N:18-3351-3-0001, S/N OFF: 187368, S/N
- [SDR CALA2022100302654](https://openairdocs.org/sdr/CALA2022100302654.md): Safety Valve · failed · Oct 3, 2022 · N846UA · Airbus A319131 · Landing Gear Door Retract Section
  > LANDING GEAR DID NOTEXTEND NORMALLY.PERFORMED MANUALEXTENSION TROUBLESHOT L/G AND DOORS REF AMM 32-31-00-810-808-A. FOUND OPS CHECK NORMAL. SAFETY VALVE 49GA FAILED. REPLACED SAFETY VALVE. ACCOMPLISHED 6 GEAR SWING CYCLES AND PERFORMED OPS CHECK OF SAFETY VALV
- [SDR CALA2021120802305](https://openairdocs.org/sdr/CALA2021120802305.md): Fuel Cap · missing · Dec 8, 2021 · N846UA · Airbus A319131 · Aircraft Fuel System
  > PDA 2 REFERENCE LOG 7570430 FUEL CAP WAS REPORTED MISSING NEW CAP WAS INSTALLED CAP WAS REPLACED REFERENCE LOG 7570430 NO FURTURE PDA ACTION REQUIRED
- [SDR CALA2021100601804](https://openairdocs.org/sdr/CALA2021100601804.md): None · missing · Oct 6, 2021 · N846UA · Airbus A319131 · Main Landing Gear Attach Section
  > PDA 3 REF L/P 7172025. LEFT MLG BLANKING PLUG MISSING. SEE PHOTO. REF ECRA 3211-01346 REV A. PERFORMED INTERIM REPAIR PER PART 1. ISSUED DIP TO ACCOMPLISH DAILY INSP. PER PART 2 AND PERMANENT REPAIR PER PART 3 WITHIN 25 FLT. HOURS. OK TO DIP. DAILY INSPECTION
- [SDR CALA2021041600481](https://openairdocs.org/sdr/CALA2021041600481.md): Pump · failed · Apr 16, 2021 · N846UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > Y HYD SYS RSVR OVRHT ON ECAM FOUND YELLOW SYSTEM RESERVOIR OVER SERVICED. DRAINED EXCESS AND SERVICED TO NORMAL LEVEL REF AMM TASK 12-12-29-611-001-A ITEM CORRECTED SEE LOG PAGE NUMBER 6143767. (REMOVED AND REPLACED #2 ENGINE CASE DRAIN FILTER PER AMM 29-11-43
- [SDR CALA2021031200300](https://openairdocs.org/sdr/CALA2021031200300.md): Skin · corroded · Mar 10, 2021 · N846UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > R-2 AFT ENTRY DOOR CUTOUT FWD FR68 AREA UNDER PLANKING PLATE HAS AREAS OF CORROSION A3NB-53-3-6299. PER HAECO LCQ N/R 9296482/22 482. GENERATED BY MECH V311118. REMOVED AND REPLACED R-2 DOOR SILL @ FR 66-68 PER A319 SRM 51-42 -11-801 & D53480009002 REV A. REMO
- [SDR CALA2021031000293](https://openairdocs.org/sdr/CALA2021031000293.md): Door Sill · corroded · Mar 10, 2021 · N846UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R-2 AFT ENTRY DOOR CUTOUT FWD FR68 AREA UNDER PLANKING PLATE HAS AREAS OF CORROSION A3NB-53-3-6299. PER HAECO LCQ N/R 9296482/22 482. GENERATED BY MECH V311118. REMOVED AND REPLACED R-2 DOOR SILL @ FR 66-68 PER A319 SRM 51-42 -11-801 & D53480009002 REV A. REMO
- [SDR CALA2021031000283](https://openairdocs.org/sdr/CALA2021031000283.md): Stringer · corroded · Mar 9, 2021 · N846UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT STRINGER 41RT FR61-64 HAS CORROSION -A3NB-53-3-618 5- GENERATED ON HAECO LCQ N/R 9296557 (22557) BY MECH V052030. REMOVED AND REPLACED STRINGER 41RT FR61-FR64 IAW A319 SRM 51-72- 11-911-002. PERFORMED BY MECH V052030 AND INSPECTED BY V061334.
- [SDR CALA2021031000282](https://openairdocs.org/sdr/CALA2021031000282.md): Stringer · corroded · Mar 9, 2021 · N846UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO PIT, ON STR37R, NEXT AT FR64 HAS CORROSION. -A3NB-53-4 -6179-. GENERATED ON HAECO LCQ N/R 9296639 (22639) BY MECH N0783 39. REMOVED AND REPLACED STRINGER 37 RT FROM FR61-FR63 IAW A319 SRM 51-72-11. DOT REMOVED. PERFORMED BY MECH V052030 AND ISNPECTED
- [SDR CALA2021030300253](https://openairdocs.org/sdr/CALA2021030300253.md): Skin · corroded · Mar 2, 2021 · N846UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > L-2 AFT ENTRY DOOR CUTOUT FWD FR68 AREA UNDER PLANKING PLATE HAS AREAS OF CORROSION (3NB-53-3-6299). REMOVED CORROSION AT L-2 ENTRY DOOR CUTOUT. HFEC OF BLENDED AREA HICKNESS OF BLENDED AREA IAW NTM 51-10-04 FOUND TO BE IN LIMITS IAW A319 SRM 53-41-14-283-002
- [SDR CALA2021030100239](https://openairdocs.org/sdr/CALA2021030100239.md): Stringer · corroded · Feb 26, 2021 · N846UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT, BETWEEN FR61 TO 62 ON STR39L COUPLING HAS CORROSION. REMOVED AND REPLACED EXISTING STRINGER 39L COUPLING BETWEEN FR 6 1-62 IAW A319 SRM 53-00-13-300-001. DOT REMOVED.
- [SDR CALA2021030100238](https://openairdocs.org/sdr/CALA2021030100238.md): Stringer · corroded · Feb 26, 2021 · N846UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO PIT, BETWEEN FR61 TO 62 ON STR39L COUPLING HAS CORROSION. REMOVED AND REPLACED EXISTING STRINGER 39L COUPLING BETWEEN FR 6 1-62 IAW A319 SRM 53-00-13-300-001. DOT REMOVED.
- [SDR CALA2019081001344](https://openairdocs.org/sdr/CALA2019081001344.md): Fuel Cap · missing · Aug 9, 2019 · N846UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTED FUEL CAP MISSING. INSPECTED COUPLING, NO LEAKS NOTED. NO ADDITIONAL DAMAGE. INSTALLED NEW FUEL CAP.
- [SDR CALA2019072801257](https://openairdocs.org/sdr/CALA2019072801257.md): Fastener · missing · Jul 25, 2019 · N846UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > PDA 3. MISSING FASTENER DEFERRALS, REF L/P''S 3846484- ONE FASTENER MISSING ON BELLY PANEL 5 FEET AFT OF LWR BEACON. L/P 3646009- ONE FASTENER MISSING ON CORNER OF PANEL NEXT TO APU DRAIN. AND L/P 3846011- ONE FASTENER MISSING ON LEADING EDGE CORNER OF PNL 471
- [SDR CALA2018100802069](https://openairdocs.org/sdr/CALA2018100802069.md): Control Lever · faulty · Oct 8, 2018 · N846UA · Airbus A319131 · Landing Gear System
  > AFTER T/O LDG GEAR WOULD NOT RETRACT. ALL SYS INDICATIONS NORMAL. R TRND TOORD-NORMAL LANDING CONTACT TOMC WITH FINDINGS ORDMM REPORTS NO FAULTS ON GEAR SWING AFTER REPLACING THE GEAR LEVER ASSY. UNLOCKING THIS ITEM. TROUBLESHOT PER TSM32-31-00-810-885-A, NO D
- [SDR CALA2018021600665](https://openairdocs.org/sdr/CALA2018021600665.md): Power Supply · faulted · Feb 16, 2018 · N846UA · Airbus A319131 · Emergency Lighting
  > DURING A NR 2 SERVICE EMERGENCY LIGHT CHECK, FAULTED TO THE LT OVERWING POWER SUPPLY UNIT. REPLACED THE POWER SUPPLY AND BATTERY IAW MM 33-51-38, NO FAULTS NOTED.
- [SDR CALA2018021600664](https://openairdocs.org/sdr/CALA2018021600664.md): Battery Pack · no test · Feb 16, 2018 · N846UA · Airbus A319131 · Emergency Lighting
  > DURING AN EMERGENCY LIGHT CHECK, FAULTED TO THE FWD LT POWER SUPPLY BATTERY. REPLACED THE BATTERY PACK IAW MM 33-51-38, NO FAULTS NOTED.
- [SDR CALA2017120104282](https://openairdocs.org/sdr/CALA2017120104282.md): Light · malfunctioned · Dec 1, 2017 · N846UA · Airbus A319131 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS IN CABIN STUCK ON. UNDER TOMC GUIDANCE, CREW CYC H5, H6, H7 AND V7. LIGHTS REMAINED ON. CYC NO SMOKING SWITCH, LIGHTS WENT OUT.
- [SDR CALA2017100603527](https://openairdocs.org/sdr/CALA2017100603527.md): Slide · delaminated · Oct 6, 2017 · N846UA · Airbus A319131 · Escape Slide
  > LEFT OVERWING SLIDE HAS DELAMINATION AT TOP AFT CORNER. NEW SLIDE INSTALLED.
- [SDR CALA2017091103152](https://openairdocs.org/sdr/CALA2017091103152.md): Bulb · inoperative · Sep 11, 2017 · N846UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TEST, CIDS MESSAGE FOR THE EPSU RT EXTERIOR LOAD. REPLACED THE BULB ON TH ERIGHT OVERWING DOOR IAW AMM 33-51-15. OPS GOOD.
- [SDR CALA2017080802545](https://openairdocs.org/sdr/CALA2017080802545.md): Battery · no test · Aug 8, 2017 · N846UA · Airbus A319131 · Emergency Lighting
  > EPSU EXT LOAD EMERGENCY AND EPSU BATTERY FAULTS WHEN PERFORMING THE EMERGENCY LIGHTS TEST. REPLACED CENTER RT EPSU BATTERY IAW AMM 33-51-38.
- [SDR CALA2017050501249](https://openairdocs.org/sdr/CALA2017050501249.md): Proximity Sensor · faulty · May 5, 2017 · N846UA · Airbus A319131 · Landing Gear Position and Warning
  > LGCIU 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. EMERGENCY DECLARED. PERFORMED TSM TASK 32-31-00-810-819-A FOR CFDS FAULT MSG "R LG DOOR CLOSED PROX SNSR (26GA)/LGCIU (5GA1)" CODE 32-31-73. REPLACE D 26GA SENSOR IAW AMM32-31-73-000-001-A/400-001-A. BITE TEST, AN
- [SDR CALA2017040700903](https://openairdocs.org/sdr/CALA2017040700903.md): Battery Pack · no test · Apr 7, 2017 · N846UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS FAILED TO TEST. REPLACED THE AFT LEFT POWER SUPPLY BATTERY PACK. OP CHECKED NORMAL.
- [SDR CALA2016021695105](https://openairdocs.org/sdr/CALA2016021695105.md): Wire · damaged · Feb 12, 2016 · N846UA · Airbus A319131 · Light System Wiring
  > RIGHT OVERWING SLIDE INDICATOR LIGHT STAYS ILLUMINATED. REPAIRED WIRE 5273-1001, FWD OF RT OVERWING ESCAPE HATCH LOWER SIDE.
- [SDR CALA2014090392050](https://openairdocs.org/sdr/CALA2014090392050.md): Battery · discharged · Aug 30, 2014 · N846UA · Airbus A319131 · Emergency Lighting
  > DURING SERVICE CHECK OF EMER LIGHTS FOUND EPSU FWD L DISPLAYED ON FWD FLIGHT ATTENDANT PANEL. REPLACED THE EPSU & BATTERY ON 10WL IAW MM 33-51-38-401.
- [SDR CALA2014061691284](https://openairdocs.org/sdr/CALA2014061691284.md): Mmr · faulted · Jun 12, 2014 · N846UA · Airbus A319131 · Landing and Taxi Aids
  > GPWS GLIDESLOPE DEVIATION, MODE 5, HAS BEEN DEFERRED IAW MEL CARD 34335. TROUBLE SHOT IAW TSM34-48- 00-810-815-A. ACCOMPLISHED OPERATIONAL TEST OF THE ENHANCED GPWS GND SELF-TEST FUNCTION, OPERATIONS CHECKED GOOD. NO FAULTS DURING EPGWS FAULT REVIEW, NR 1 M
- [SDR CALA2014060291185](https://openairdocs.org/sdr/CALA2014060291185.md): Door Frame · cracked · May 29, 2014 · N846UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68 WEB CRACKED AT DOOR 2L AFT LOWER STOP FITTING LOWER INBD HOLE. HOLE ENLARGED TO 0.510 INCHES & FREEZE PLUG REPAIR ACCOMPLISHED IAW SRM 53-41-12 PARA 5 C & PARA 5 F FIG 205. REQUIRES INSPECTION IAW SRI53-41-12-2-005-00 PARA 3 E TABLE 206, FIG 201. FI
- [SDR CALA2014110792659](https://openairdocs.org/sdr/CALA2014110792659.md): Frame · corroded · May 22, 2014 · N846UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 20RT INBD FLANGE BETWEEN Z=-520 & Z=-460 IS CORRODED AT FLOOR LEVEL IN THE MAIN CABIN, DF9035. REMOVED CORROSION IAW ECRA 5311-01689 & SRM 51-74-00. NDT NOTED NO CRACKS. AIRBUS APPROVED THIS AS INTERIM MAJOR REPAIR WITH 6 MONTHS LIFE LIMIT FROM REPAIR
- [SDR CALA2014052291121](https://openairdocs.org/sdr/CALA2014052291121.md): Frame · corroded · May 22, 2014 · N846UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 20RH INBD FLANGE BETWEEN Z=-520 & Z=-460 IS CORRODED AT FLOOR LEVEL IN THE MAIN CABIN. REMOVED CORROSION IAW ECRA 5311-01689 & SRM 51-74-00. NDT NOTED NO CRACKS. AIRBUS APPROVED THIS AS INTERIM MAJOR REPAIR WITH 6 MONTH LIFE LIMIT FROM REPAIR EMBODIMEN
- [SDR CALA2014051991059](https://openairdocs.org/sdr/CALA2014051991059.md): Skin · corroded · May 19, 2014 · N846UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT WING LOWER FUEL TANK PANEL LANDINGS 540 NB HOLES C & F & 540HB HOLE N WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 4360
- [SDR CALA2014051991058](https://openairdocs.org/sdr/CALA2014051991058.md): Skin · corroded · May 19, 2014 · N846UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT WING LOWER FUEL TANK PANEL LANDINGS 650 AB HOLE B & 640 MB HOLE K WERE FOUND CORRODED. HOLES WERE BUSHED & BRIDGING PLATES INSTALLED IAW SRM 57-21-11 PARA 5 B FIG 202. INSPECTION REQUIRED IAW SRI 57-21-11-2-002-00 3 B TBL 203. FIRST INSPECTION 43600FC

Next page: https://openairdocs.org/aircraft/N846UA/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 = 'N846UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N846UA/reports

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