# Service difficulty reports: N847UA

A list on [N847UA](https://openairdocs.org/aircraft/N847UA.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 · 86 reports

- [SDR CALA2026062217251](https://openairdocs.org/sdr/CALA2026062217251.md): Epsu · faulty · Jun 21, 2026 · N847UA · Airbus A319131 · Emergency Lighting
  > DURING TEST OF CABIN EMERGENCY LIGHTS THE FOLLOWING MESSAGE WAS DISPLAYED. EPSU UNIT FWD L. DURING THE TEST THE FWD HALF OF THE CABIN EMERGENCY LIGHTS DID NOT COME ON. REPLACED EPSU 10WL AND BATTERY REF AMM 33-51-38 UP TO AND INCLUDING STEP 4.C.
- [SDR CALA2026020413548](https://openairdocs.org/sdr/CALA2026020413548.md): Outflow Valve · defective · Feb 2, 2026 · N847UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > SAFETY VALVE STUCK OPEN CPC 1 TESTS OK. SUGGEST REPLACING CAB PR SAFTEY VALVE 6HL AND CPC 2. REF AMM 21-31-52/401 CONFIG 00. ENSURE SAFETY VALVE 7HL IS CLOSED UNLESS IT CAN BE POSITIVELY DETERMINED WHICH SAFETY VALVE OPENED, PER TSM 21-31-00-810-808-A, NEED T
- [SDR CALA2025100309579](https://openairdocs.org/sdr/CALA2025100309579.md): Pin · installed · Oct 2, 2025 · N847UA · Airbus A319131 · Standard Practices/Structures
  > INSTALLED L2 DOOR EMERGENCY CONTROL HANDLE SAFETY PIN IN THE DISARMED POSITION TO FACILITATE SCHEDULED L2 DOOR. R & R IAW AMM 52-10-00-860-001-A. REMOVED L2 DOOR EMERGENCY CONTROL HANDLE SAFETY PIN POST-MX ON L2 DOOR SLIDE R&R REF AMM 52-10-00-860-002-A. A
- [SDR CALA2025090808602](https://openairdocs.org/sdr/CALA2025090808602.md): Door · false indication · Sep 4, 2025 · N847UA · Airbus A319131 · Door Warning System
  > DOOR FWD AVIONICS ECAM ON START. CONFIRMED FWD E&E DOOR INDICATION INOPERATIVED, GIVING FALSE INDICATION WITH DOOR CLOSED. DEFERED PER MEL 5270BZ. *DM* REF TSM 52-41-00-810-803-A. PERFORMED FAULT CONFIRMATION FOR FWD AVIONICS DOOR IN REF TO TSM 52-41-00-810
- [SDR CALA2025071006420](https://openairdocs.org/sdr/CALA2025071006420.md): None · none · Jul 6, 2025 · N847UA · Airbus A319131 · Standard Practices/Structures
  > INSTALLED LOCK PIN ASSEMBLY TO THE RH OFF WING INFLATION CYLINDER FOR SLIDE MAINT LOCK PIN REMOVED AND STOWED AS REQD INSPECTION UPDATE: VERIFIED REMOVAL AND STOWAGE OF RIGHT OFFWING SLIDE BOTTLE LOCKOUT PIN AS REQUIRED. REF. GMM 09-25-05.
- [SDR CALA2025043004352](https://openairdocs.org/sdr/CALA2025043004352.md): Blower · faulted · Apr 27, 2025 · N847UA · Airbus A319131 · Air Distribution Fan
  > VENT BLOWER FAULT DISPLAYED IN THE UPPER ECAM SCREEN TECH SUOV UPDATE DURING TAXI TEST WHILE THE NUMBER 1 GEN WAS FLUCTUATING THE VENT BLOWER CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET PLEASE INSPECT CONTACTOR 8HQ FOR ANY SIGNS OF BURNING PERFORMED INSPECTION
- [SDR CALA2025042904319](https://openairdocs.org/sdr/CALA2025042904319.md): Computer · faulted · Apr 26, 2025 · N847UA · Airbus A319131 · Autopilot System
  > ECAM AUTO FLT YAW DAMPR1 RUD TRIM1 CLASS2 F/CTL PERFORMED OPS TEST OF THE RUDDER TRIM FUNCTION AND RESET PER AMM TASK 22-62-00-710-001-A, OPS CHECK GOOD. RUD TRIM 1 FAULT WENT AWAY. AS OF NOW NO AUTO FLT YAW DAMPR 1 MSG ON ECAM. REPLACED FAC 1 PER AMM TASK 22-
- [SDR CALA2025041003673](https://openairdocs.org/sdr/CALA2025041003673.md): Battery Pack · no test · Apr 9, 2025 · N847UA · Airbus A319131 · Emergency Lighting
  > R.H. MID. EMERG LIGHT BATT. IS NOT TESTING. REMOVED AND REPLACED EMERG BATT. PACK AT R.H. MID. LOCATION. OPS. CHECK NORMAL. REF AMM 33-51-38-400-002-A
- [SDR CALA2025031702874](https://openairdocs.org/sdr/CALA2025031702874.md): Computer · faulty · Mar 13, 2025 · N847UA · Airbus A319131 · Flight Control System
  > ELAC 1 PITCH FAULT ON TAKEOFF ROLL. ACP LOW SPEED ABORT R&R'D ELAC 1, OPS NML, REF AMM 27-93-34/401.
- [SDR CALA2024121803106](https://openairdocs.org/sdr/CALA2024121803106.md): Fitting · corroded · Dec 12, 2024 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAIN CABIN L2 DOOR #1 DOOR STOP OUTBOARD EDGE AT DOOR SEAL CONNE CTOR PLATE CORRODED. INSTALLED L2 FWD LWR CORNER FITTING AT FR66 AT #1 DOOR STOP AREA IAW A319 SRM 51-42-11/001 AND 51-72-11-911-001.
- [SDR CALA2024121603090](https://openairdocs.org/sdr/CALA2024121603090.md): Fitting · cracked · Dec 9, 2024 · N847UA · Airbus A319131 · Fuselage Main, Structure
  > LH WINDSHIELD CONTINUITY FITTING HAS CRACK INDICATION APPROX.40 0 INCH FROM CTR POST. REMOVED AND REPLACED LH AND RH CONTINUITY FITTINGS IAW AIRBUS DWGS R53112919 REV K AN D R53113426 REV F AS DIRECTED BY EA 5310-0765 REV B OPS 004.
- [SDR CALA2024120503021](https://openairdocs.org/sdr/CALA2024120503021.md): Angle · cracked · Dec 4, 2024 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH AFT TI ANGLE CRACKED REPAIR PER EA 5331-01718 OP 8 BEFORE NEX T FLIGHT. REPAIRED PER EA 5331-01718 OP 8 BY REPLACEMENT OF R/H AFT TI-ANGLE.
- [SDR CALA2025012900233](https://openairdocs.org/sdr/CALA2025012900233.md): Frame · cracked · Nov 29, 2024 · N847UA · Airbus A319131 · Fuselage Main, Frame
  > FRAME 68 RH AFT FACE HAS CRACK INDICATION JUST BELOW STR 8 IN RA DIUS, APPROX.200 LONG, ALONG RADIUS JUST ABOVE UPPER SEAL FASTE NER. GEN BY V892444 ON HAECO LCQ NR 9296105 / 30105 CLEARING LP. FOR REPAIR, INSPECTION AND REFERENCE DETAILS, SEE NEW LP''S 36851
- [SDR CALA2023073102371](https://openairdocs.org/sdr/CALA2023073102371.md): Cap · missing · Jul 28, 2023 · N847UA · Airbus A319131 · Aircraft Fuel System
  > FUEL CAP MISSING UPON ARRIVAL AT DFW. PDA DOCUMENTED ON THIS LOGPAGE PER GMM 02-30-95. TOMC NOTIFIED. APPLIED CDL 28A FUEL CAP CAME IN MISSING NOT JUST COVER. PDA FILED AND ESFR ALSO FILED DISPATCH DESK: 11 NAME: E B DATE: 28-JUL-23- OK TO DEFER FUEL CAP PER C
- [SDR CALA2022011800173](https://openairdocs.org/sdr/CALA2022011800173.md): Outflow Valve · fault message · Jan 18, 2022 · N847UA · Airbus A319131 · Cabin Pressure Control System
  > LOSS OF PRESS WHILE IN DESCENT FROM 380 TO 340.MADE DESCENT TO 1 0000. NO ECAM NO MASK.HIGHEST C PFR AND BOTH CPCS BITE TEST GOOD. CREW REPORTS ECAM PRESSURES PAGE POPPED UP WITH NO ECAM WARNING. CABIN ALTITUDE WAS FLASHING AMBER TO GREEN AND INDICATED 9000 F
- [SDR CALA2021052600734](https://openairdocs.org/sdr/CALA2021052600734.md): Fitting · damaged · May 24, 2021 · N847UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LH FR 4 SIDE POST UPPER CORNER FITTING HAS HOLE WITH DAMAGE IN B ORE, SCORING, WEAR & OUT OF ROUND ON HAECO LCQ REF 9296515 AD RE LATED SUPPORT TASK. NR GENERATED BY V892444 REMOVED AND REPLACED LH FR4 SIDE POST UPPER CORNER FITTING IAW U NITED ECRA 5311-02571
- [SDR CALA2021052600733](https://openairdocs.org/sdr/CALA2021052600733.md): Stringer · corroded · May 24, 2021 · N847UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR-35R, BTWN FR59-FR60 IN AFT CARGO COMPARTMENT (L OCATED JUST AFT OF CARGO DOOR AFT DOOR FRAME) {A3NB-53-4-6179} P ER HAECO LCQ N/R 9296737/32737 GENERATED BY V925611. REMOVED AND REPLACED STRINGER BETWEEN FR59-60 STR35R IN AFT CARG O COMPARTMEN
- [SDR CALA2021052400706](https://openairdocs.org/sdr/CALA2021052400706.md): Fitting · damaged · May 21, 2021 · N847UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LH FR4 SIDE POST I/B HORIZONTAL FITTING HAS ELONGATED HOLE FOUND DURING THE REMOVAL OF THE FITTING TO PERFORM JOB NO 32515 ON HA ECO LCQ REF 9296752 SUPPORT TASK. NR GENERATED BY V061619 REMOVED AND REPLACED LH FR4 SIDE POST I/B HORIZONTAL FITTING IAW A319 SRM
- [SDR CALA2021052400705](https://openairdocs.org/sdr/CALA2021052400705.md): Threshold · corroded · May 21, 2021 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT, DOOR THRESHOLD SILL FRAME 55A-59 STR 38RH HAS C ORROSION A3NB-53-4-6179 PER HAECO LCQ N/R 9296461/32461 GENERATE D BY V061595. REMOVED AND REPLACED AFT CARGO DOOR THRESHOLD SILL IAW A319 SRM 51-72-11-911-001. PERFORMED BY MECH V918284 AND INSP
- [SDR CALA2021052100701](https://openairdocs.org/sdr/CALA2021052100701.md): Web · corroded · May 20, 2021 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT, DOOR THRESHOLD BOX WEB FRAME 55A-59 STR 36-37RH HAS CORROSION. A3NB-53-4-6179 PER HAECO LCQ N/R 9296462/32462 G. REMOVED AND REPLACED TORSION BOX COVER (NEW) PN #D5347715400490 PO #1094477.1 IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2021051700664](https://openairdocs.org/sdr/CALA2021051700664.md): Intercostal · cracked · May 14, 2021 · N847UA · Airbus A319131 · Passenger/Crew Doors
  > AD 2019-20-10: L1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBOARD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING. "REPAIR BE FORE NEXT FLIGHT."CONTACT ENGINEERING FOR APPROVED REPAIR INSTRU CTIONS. PER HAECO LCQ N/R 9296302/32302 GENERATED BY V061633. REPA
- [SDR CALA2021051700663](https://openairdocs.org/sdr/CALA2021051700663.md): Intercostal · cracked · May 14, 2021 · N847UA · Airbus A319131 · Service Doors
  > AD 2019-20-10: R1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBOARD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING. "REPAIR BE FORE NEXT FLIGHT". CONTACT ENGINEERING FOR APPROVED REPAIR INSTR UCTIONS. PER HAECO LCQ N/R 9296304/32304 GENERATED BY V061633. REP
- [SDR CALA2021051700662](https://openairdocs.org/sdr/CALA2021051700662.md): Torsion Box · corroded · May 14, 2021 · N847UA · Airbus A319131 · Fuselage Main, Structure
  > AFT PIT TORSION BOX AT FR56-FR59 TRANSITION PANEL HAS CORROSION DOT L003 SUPPORT TASK- PER HAECO LCQ N/R 9296713/32713 GENERATED BY V061704. REMOVED AND REPLACED WITH NEW TRANSITION PANEL IAW A319 SRM 51-7 2-11-911-001 AT HAECO LCQ REF 9293713/32713 BY MECH V9
- [SDR CALA2021042600544](https://openairdocs.org/sdr/CALA2021042600544.md): Shear Plate · corroded · Apr 25, 2021 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN FR69-70 STR 23R RH SHEAR PLATE HAS CORROSION A3NB-05-3 -6029. LOGPAGE IS OPEN FURTHER DETAILS AWAITED.
- [SDR CALA2021041900495](https://openairdocs.org/sdr/CALA2021041900495.md): Door Sill · corroded · Apr 18, 2021 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN LH SIDE FR68 STR 23L DOOR SILL IB EDGE HAS CORROS ION A3NB-05-3-6029 AT HAECO LCQ REF 9296545 GENERATED BY MECH V9 17055 ACCOMPLISHED L2 DOOR SILL BEAM REPAIR IAW A319 SRM 53-41-300-001 FIGURE 001 SHETT 03 REPAIR PRINCIPLE 5 DETAIL H. REMOVED DO
- [SDR CALA2021041900494](https://openairdocs.org/sdr/CALA2021041900494.md): Door Sill · corroded · Apr 18, 2021 · N847UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT MAIN CABIN RH SIDE R2 DOOR SIL FR 66 FWD TAB HAS CORROSION A 3NB-05-3-6029 AT HAECO LCQ REF 9296538 GENERATED BY V917055 REMOVED AND REPLACED R2 DOOR SILL IAW A319 SRM 51-72-11-911-001 REMOVED DOT B294 MECH BY V915153 INSP BY V892443
- [SDR CALA2020070401036](https://openairdocs.org/sdr/CALA2020070401036.md): Battery · discharged · Jul 2, 2020 · N847UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILS FOR ESPU BATTERY EMER R PER NR 9298007. REMOVED AND REPLACED 12WL BATTERY IAW AMM 33-51-38-000-002- A AND 33-51-38-400-002-A. OP CHECK GOOD IAW AMM 33-51-00-71 0-001-A.
- [SDR CALA2019110501907](https://openairdocs.org/sdr/CALA2019110501907.md): Door Frame · cracked · Oct 28, 2019 · N847UA · Airbus A319131 · Fuselage Main, Structure
  > L/H AFT PAX DOOR FR68, L/H FRAME 68 AT STRINGER 8 LOCATION HAS CRACK INDICATION IN RADIUS. REPAIRED L/H AFT PAX DOOR FRAME AT FR689 STGR 8 IAW SRM 53-41- 12-300-012. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR IMBODIM ENT 36200 FC, SUBSEQUENT INSPECTION AT IN
- [SDR CALA2019110501906](https://openairdocs.org/sdr/CALA2019110501906.md): Door Frame · cracked · Oct 28, 2019 · N847UA · Airbus A319131 · Fuselage Main, Structure
  > L/H AFT PAX DOOR FR68, L/H FRAME 68 AT STGR 8 CRACK INDICATION IN RADIUS (FREEZE PLUG REPAIR). REPAIRED L/H AFT PAX DOOR FRAME AT FR 68 STGR 8 WITH FREEZE PLUG REPAIR IAW SRM 53-41-12-300-012 & SRM 51-73-12-801. INSPECT ION THRESHOLD FROM TIME OF ADL/REPAIR EM
- [SDR CALA2019102501824](https://openairdocs.org/sdr/CALA2019102501824.md): Plug · missing · Oct 25, 2019 · N847UA · Airbus A319131 · Passenger/Crew Doors
  > A3NB-52-3-6001 A-27-001 L2 DOOR, DOOR ASSIST PRESSURE GAUGE MISS ING RUBBER PLUG REMOVED AND REPLACED L2 DOOR DAMPER CYLINDER IAW A319 AMMS 52-13 -14-000-001, 52-13-14-400-001. A319 AMM 52-13-14-400-001 STEP 4. E AND F. CHARGING OF CYLINDER AND CHECKING CYLIND
- [SDR CALA2019102501823](https://openairdocs.org/sdr/CALA2019102501823.md): Wire · broken · Oct 25, 2019 · N847UA · Airbus A319131 · Light System Wiring
  > (SUPPORT TASK) A-13 DOT 011. L/H PANEL 261WW EXIT LIGHT WIRE IS BROKEN. AAR NONROUTINE 9303669 REMOVED AND REPLACED EMER-EXIT MARKER LIGHT 90WL5 AND TERMINATED WIRES ON L/H PANEL 261WW. IAW A319 ESPM 20-48-25-0101-2, AMM 33 -51-13-000-001-A, 33-51-13-400-001-A
- [SDR CALA2019102501822](https://openairdocs.org/sdr/CALA2019102501822.md): Cylinder · eroded · Oct 25, 2019 · N847UA · Airbus A319131 · Passenger/Crew Doors
  > CUSTOMER REQUEST, PETE LAMENDOLA, L1 DOOR DAMPER SYLINDER PRESSU RE GAUGE GROMMET ERRODED. REMOVED AND REPLACED L1 DOOR DAMPER CYLINDER IAW A319 AMM''S 52-1 1-14-000-001, AND 52-11-14-400-001. CHARGING OF CYLINDER ACCOMPL ISHED ON ROUTINE CARD 17-2500-1-9909 S
- [SDR CALA2019061000922](https://openairdocs.org/sdr/CALA2019061000922.md): Relay · failed · Jun 10, 2019 · N847UA · Airbus A319131 · Fuel System Wiring
  > C/B A14 - SMOKE CONFIG PUMP CONTROL - POPPED, FUEL PUMP CB A14 TRIPPING IN CRUISE, REPLACE RELAYS 63QA AND 64QA. M+E 18-2821-3-0062.
- [SDR CALA2019021700258](https://openairdocs.org/sdr/CALA2019021700258.md): Reservoir · low · Feb 14, 2019 · N847UA · Airbus A319131 · Hydraulic Reservoir, Main
  > GREEN HYD SYSTEM WAS JUST ABOVE THE LOW LEVEL AFTER GEAR RETRACTION SERVICED GREEN SYSTEM HYDRAULICS, ACP LEAK CHECK OF GREEN SYSTEM HYDRAULICS, NO ACTIVE LEAKS AT THIS TIME.
- [SDR CALA2017120804366](https://openairdocs.org/sdr/CALA2017120804366.md): Unknown · unknown · Dec 8, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ON WITH FLT DECK SWITCH IN THE ARM POSITION CYCLED POWER AND EMER. EXIT LT. SWITCH. EMER. LIGHTS FUNCTION NORMALLY
- [SDR CALA2017092203300](https://openairdocs.org/sdr/CALA2017092203300.md): Battery Pack · no test · Sep 22, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY FWD LT MESSAGE APPEARED DURING CABIN EMERGENCY LIGHTS OPS CHECK. ACCOMPLISHED TEST SEVERAL TIMES WITH SAME RESULTS. REPLACED THE BATTERY IN THE POWER SUPPLY IAW AMM 33-51-38-401. OPS CHECKED GOOD.
- [SDR CALA2017063002060](https://openairdocs.org/sdr/CALA2017063002060.md): Battery Pack · no test · Jun 30, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > FOUND FWD LEFT EMERGENCY LIGHT BATTERY FAILED DURING TEST. REPLACED THE BATTERY PACK. TEST PASSED
- [SDR CALA2017051201376](https://openairdocs.org/sdr/CALA2017051201376.md): Cover · loose · May 12, 2017 · N847UA · Airbus A319131 · Emergency Exits
  > L OVERWING EXIT ECAM DISPLAYED DURING CRUISE FOR ABOUT 5 MINUTES NO CABIN PRESSURE CHANGES NOTED UPPER EMERG EXIT DOOR HANDLE COVER CAME LOOSE AND FLIGHT ATTENDANT REINSTALLED COVER. REMOVED COVER AND VERIFIED DOOR ARMING MECHANISM SECURE. REINSTALLED AND SECU
- [SDR CALA2017032600737](https://openairdocs.org/sdr/CALA2017032600737.md): Epsu · defective · Mar 26, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > ESCAPE PATH LIGHTS ROW 10-11 INOP. T/S FOUND EMERGENCY POWER SUPPLY UNIT 10WL DEFECTIVE. REMOVED AN D REPLACED EPSU AMM 33-51-38. OPS CKS GOOD.
- [SDR CALA2017031700646](https://openairdocs.org/sdr/CALA2017031700646.md): Relay · faulted · Mar 17, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS FLASHING INTERMITTENTLY AFTER ENGINE SHUTDOWN. CONTINUED EVEN AFTER TROUBLESHOOTING IAW TSM 33-51-00-810-819A, REPLACED THE RELAY 8WL IAW ASM 33-51-00, OP CHECKED OK.
- [SDR CALA2017022400478](https://openairdocs.org/sdr/CALA2017022400478.md): Power Supply · faulty · Feb 24, 2017 · N847UA · Airbus A319131 · Emergency Lighting
  > AFTER EMER LTS TEST, RESULT EPSU FWD LT. REPLACED FWD EPSU AND BATTERY PER MM 33-51-38. OPS CK GOOD.
- [SDR CALA2016110700863](https://openairdocs.org/sdr/CALA2016110700863.md): Pump · unserviceable · Nov 7, 2016 · N847UA · Airbus A319131 · Fuel Boost Pump
  > EMERGENCY DECLARED. PUMP INDICATION, LEFT TANK PUMP 1 INOP & RIGHT TANK PUMP 1 INOP ON FUEL SYSTEM ECAM. FOUND LT WING TANK PUMP1 AND PUMP 2 LOW PRESSURE. RESET CB A14. FOUND PUMP 1 TO OPERATE NORMALLY. PUMP 2 FOUND TO BE INTERMITTENT. REPLACED BOTH LT W
- [SDR CALA2016072595583](https://openairdocs.org/sdr/CALA2016072595583.md): Power Supply · no test · Jul 23, 2016 · N847UA · Airbus A319131 · Emergency Lighting
  > IAW CHECK CARD 4-2020 STEP 34 EMERGENY LIGHT BATTERY CAP TEST, RECEIVED A MESSAGE EPSU ARMED-ON FWD L REPLACED LEFT OVERWING EPSU IAW MM33-51-38, OPS NORMAL.
- [SDR CALA2016072595580](https://openairdocs.org/sdr/CALA2016072595580.md): Fitting · no test · Jul 22, 2016 · N847UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > L1 DOOR, AFT GIRT BAR FITTING STOP LEVER FAILS CHECK PER 'A' CHECK JOB 4-2060 STEP 10, AND AMM 53-11-00-210-034-A. REMOVED AND REPLACED THE GIRT BAR FLOOR FITTING. ADJUSTED AND SEALED AMM 52-11-00
- [SDR CALA2014071191441](https://openairdocs.org/sdr/CALA2014071191441.md): Actuator · malfunctioned · Jul 9, 2014 · N847UA · Airbus A319131 · Compressor Bleed Valve
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENG PARAMETERS NORMAL. R & R VSV ACTUATOR IAW AMM 75-32-41. LEAK & OPERATIONS CHECK WERE GOOD OK TO CONTINUE.
- [SDR CALA2014061691278](https://openairdocs.org/sdr/CALA2014061691278.md): Wire · damaged · Jun 13, 2014 · N847UA · Airbus A319131 · Light System Wiring
  > FORWARD CABIN EWIS RED & BLACK WIRES DAMAGED AT SEAT TRACK ROW 12 LT. REPAIRED RED & BLACK EMER LIGHT WIRES DAMAGED AT SEAT ROW 12 LT IAW ESPM 20- 53-21. INSULATION WAS DAMAGED ON WIRES FROM CONNECTOR 7260VC5-A 3330-0872-1673-18N & 3330-08702-1673-18.
- [SDR CALA2014060991240](https://openairdocs.org/sdr/CALA2014060991240.md): Stringer · corroded · Jun 7, 2014 · N847UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > STRINGER 44 BETWEEN FRAME 64 - 65 HAS CORROSION. REMOVED CORROSION & INSTALLED REPAIR ANGLE IAW SRM 53-00-13 FIGURE 202 SHEET 2. NO SRI REQUIRED.
- [SDR CALA2013121893786](https://openairdocs.org/sdr/CALA2013121893786.md): Sensor · malfunctioned · Dec 9, 2013 · N847UA · Airbus A319131 · Landing Gear Position and Warning
  > LGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CYCLED CB LGCIU SYS 2 IAW FM RESET PROCEDURE, ECAM STILL DISPLAYED. REPLACED SW 23GA IAW AMM 32-31-73 ALL MESSAGES CLEARED, AC RETURNED TO NORMAL. ECRA 3231-01117 CREATED FOR FERRY FLT TO MAINT BAS FOR GEAR EXTE
- [SDR CALA2013112593250](https://openairdocs.org/sdr/CALA2013112593250.md): Screw · loose · Nov 24, 2013 · N847UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SCREW LOOSE ON PANEL 192KB. SCREW & NUT PLATE NEED TO BE REPLACED. IAW AMM REPLACED NUTPLATE & SCREW.
- [SDR CALA2013110192570](https://openairdocs.org/sdr/CALA2013110192570.md): Power Supply · failed · Oct 31, 2013 · N847UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHT SYSTEM FAILED SELF-TEST. REPLACED LT OVERWING EXIT EPSU & BATTERY IAW MM, EMERGENCY LIGHT TESTED, NOW PASSES.

Next page: https://openairdocs.org/aircraft/N847UA/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 = 'N847UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N847UA/reports

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