# Service difficulty reports: N849UA A list on [N849UA](https://openairdocs.org/aircraft/N849UA.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 · 74 reports - [SDR CALA2026081218502](https://openairdocs.org/sdr/CALA2026081218502.md): Fuel Cap · missing · Aug 9, 2026 · N849UA · Airbus A319131 · Fuel Storage > FUEL CAP MISSING. INSTALLED A NEW FUEL CAP IAW AMM 28-25-41. - [SDR CALA2026080318227](https://openairdocs.org/sdr/CALA2026080318227.md): Relay · faulted · Aug 1, 2026 · N849UA · Airbus A319131 · Hydraulic System, Main > HYD Y LO LVL ECAM ECAM PROCEDURES FOLLOWED TSM 29-13-00-810 -816-A. UPON ARRIVAL VERIFIED NO HYD LEAKS. NO FAULTS IN SYS AFTER CYCLING HYD AS A PRECAUTION. AS PRECAUTION RECOMMEND CHANGE RELAYS (3816GX, 6MJ) AND SCCB PWR SUPPLY RELAY 3811GX. ON INITIAL EVALUAT - [SDR CALA2026061517082](https://openairdocs.org/sdr/CALA2026061517082.md): Actuator · faulty · Jun 11, 2026 · N849UA · Airbus A319131 · Compressor Bleed Valve > EGT NR 1 ENG EXCEEDANCE TO WITH ECAM EGT EXCEED POST FLIGHT REPORT & TAKEOFF REPORT ENG GAS PATH ADV REPORT. REF L/P 9219236 FOR ALL WORK PERFORMED AND CLEARING OF FAULT REF TSM AND TECH SUPPORT. DUE TO THE REOCCURING ENG 1 EGT OVER LIMIT AND RELATED CLM'S "C - [SDR CALA2026010212632](https://openairdocs.org/sdr/CALA2026010212632.md): Fuel Cap · missing · Dec 31, 2025 · N849UA · Airbus A319131 · Fuel Storage > ACFT CAME TO GET WITH FUEL CAP MISSING. - [SDR CALA2025111111126](https://openairdocs.org/sdr/CALA2025111111126.md): Battery · discharged · Nov 11, 2025 · N849UA · Airbus A319131 · Emergency Lighting > FWD LH EMERGENCY BATTERY FOUND WITH FAILURE. REPLACED LH FWD EMERGENCY BATTERY AS PER AMM 33-51-38/401 CONFIG 00. OPERATIONAL TEST GOOD. - [SDR CALA2025110911012](https://openairdocs.org/sdr/CALA2025110911012.md): Warning Message · false activation · Nov 6, 2025 · N849UA · Airbus A319131 · Emergency Lighting > EMERGENCY LIGHT TEST FAULTS 'EPSU BATTERY AFT L'. PREFORMED OPS CHECK OF EMERGENCY LIGHT IAW AMM 33-51-00-710-001-A. TEST PASS. NO FAULT FOR EPSU BATT AFT L. - [SDR CALA2025101610172](https://openairdocs.org/sdr/CALA2025101610172.md): Fuel Cap · missing · Oct 14, 2025 · N849UA · Airbus A319131 · Fuel Storage > FUELERS REPORT NO FUEL CAP ON ARRIVAL REPLACED MISSING FUEL CAP PER AMM 28-25-41, - [SDR CALA2025090408473](https://openairdocs.org/sdr/CALA2025090408473.md): Bracket · broken · Sep 1, 2025 · N849UA · Airbus A319131 · Passenger Compartment Equipment > PC POWER INDICATION BRACKET IS BROKEN ON SEAT 7C. WITH LIGHTS MISSING OR STOWED. OK TO APPLY NEF 2522LB SECURED IN SEAT POWER PORTS AND IN USE LIGHTS AS REQ. PLACED ON PLACARD SEAT USEABLE. INSTALLED NEW HOUSING SHROUD ASSY FOR FOR PC POWER AT SEAT 7C. LIGHT - [SDR CALA2025090308443](https://openairdocs.org/sdr/CALA2025090308443.md): Wire · loose · Sep 1, 2025 · N849UA · Airbus A319131 · Light System Wiring > IN SEAT EMERGENCY LIGHT AT SEAT 7 C HAS WIRE LOOSE FROM CONNECTOR. LIGHT IS INOP. BOTH WIRES BROKEN FROM MOLEX CONNECTOR. SEE PIC. UPDATE: FLAGGING SDR REF ESPM 20-56-22-03 AND AMM 33-51-00 RETERMINATED WIRES. PERFORMED OPS TEST OF EMERGENCY LIGHT AT 7C. OPS - [SDR CALA2025090308439](https://openairdocs.org/sdr/CALA2025090308439.md): Battery · no test · Sep 1, 2025 · N849UA · Airbus A319131 · Emergency Lighting > WHILE PERFORMING EMERGENCY LIGHTS TEST ON LP 6125976 FOUND SEAT ROW EMERGENCY PATH LIGHTING INOP FOR ROWS 25, 26, 29, 30, 34 AND 35. FOUND EPSU BATTERY AFT L AND EPSU BATTERY EMER L FAULT. REF TSM 33-51-00-810-802-A REPLACED 11WL AND 13WL BATTERY, REF AMM 3 - [SDR CALA2025082608124](https://openairdocs.org/sdr/CALA2025082608124.md): Display · faulted · Aug 24, 2025 · N849UA · Airbus A319131 · Central Display > PFD FAILED AFTER TAKEOFF STRONG BURNING ODOR FROM CAPT PFD UPON ARRIVAL & AFTER TAKEOFF CAPTS PFD WENT OUT THEN STARTED FLICKERING & A BURNING SMELL OCCURED. NO OTHER ECAM MSGS OR OTHER FAULTS NOTICED. CAPT TURNED OFF DISPLAY & SMELL CEASED, NO OTHER ISSUES E - [SDR CALA2025031102726](https://openairdocs.org/sdr/CALA2025031102726.md): Battery · faulted · Mar 7, 2025 · N849UA · Airbus A319131 · Emergency Lighting > AFT DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0021} - AFTER EMERGENCY LIGHT TEST FOR ESCAPE SLIDE INSTALLATION TEST WAS FOUND A CIDS FAULT EPSU BATTERY AFT L. REQUIRES RII. T/S PER TSM 33-51-00-810-802-A, UP TO AND INCLUDING STEP A (A) 1. NO DISCREPAN - [SDR CALA2024122701668](https://openairdocs.org/sdr/CALA2024122701668.md): Fuel Cap · missing · Dec 23, 2024 · N849UA · Airbus A319131 · Fuel Storage > PDA 2 CDL APPLIED (28A FOR MISSING FUEL CAP) CORRECTIVE ACTION TAKEN ON LP 3291440. - [SDR CALA2024102202703](https://openairdocs.org/sdr/CALA2024102202703.md): Fitting · cracked · Oct 14, 2024 · N849UA · Airbus A319131 · Fuselage Main, Structure > LEFT AND RIGHT WINDSHIELD LOWER NODE CONTUNUITY FITTINGS HAVE CR ACK INDICATIONS ON AFT FACE OF HORIZONTAL FLANGE. REMOVED & REPLACED L/H & R/H WINDSHIELD LOWER NODE CONTINUITY FITTINGS IAW A319 EA 5310-07675 OP004 AND REO-L25218 AND AIRBUS REPA IR DRAWINGS R - [SDR CALA2023082502629](https://openairdocs.org/sdr/CALA2023082502629.md): Cap · missing · Aug 24, 2023 · N849UA · Airbus A319131 · Aircraft Fuel Distribution System > PDA 2 REFERENCE LOGPAGE 5554700. FUEL CAP MISSING UPON ARRIVAL AT DFW. MISSING FUEL CAP NOTED BY MAINTENANCE AND TOMC NOTIFIED. REPLACED MISSING CAP PARTS USED: 31-2825-9-0001,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1509936 SN OFF 0705 - [SDR CALA2023022000497](https://openairdocs.org/sdr/CALA2023022000497.md): Fuel Cap · missing · Feb 20, 2023 · N849UA · Airbus A319131 · Aircraft Fuel System > FUELER REPORTED THAT FUEL CAP IS MISSING. NO DAMAGE NOTE TO COUPLING. REPLACED MISSING REFUEL/DEFUEL COUPLING CAP IAW AMM 28-25-41. PARTS UPDATE ROTABLE PARTS CHANGE WAS INDICATED - TT # 1604407 SN OFF 0937 CAP, COUPLING R OFF 31-2825-9-0001 0937 ON 31-2825 - [SDR CALA2023021600463](https://openairdocs.org/sdr/CALA2023021600463.md): Fuel Cap · unknown · Feb 16, 2023 · N849UA · Airbus A319131 · Aircraft Fuel System > PDA 2 REFERENCE 3861332 AIRCRAFT ARRIVED FROM CVG MISSING FLUEL CAP. GENERATED CDL 28A TO REPLACE CAP. NO LEAKS, NO DAMAGE NOTED. PHOTO UPLOAD. NO CAPS AVALIBLE DEN. FLAGGED SDR REPORT. ITEM BEING TRACKED ON LOG PAGE 3861332. CLOSING THIS LP - [SDR CALA2022032800801](https://openairdocs.org/sdr/CALA2022032800801.md): Bushing · chipped · Mar 28, 2022 · N849UA · Airbus A319131 · Wing Structure > RT WING RIB 5 FWD LUG BUSHING CHIPPED PER HAECO LCQ N/R 9290638/ 22638 GEN BY V061642 PERMANENT REPAIR OF THE RH MLG SUPPORT RIB 5, AFT PINTLE FWD LUG ACFT REACHES 105,000 TTL ACFT FC OR 210,000 TTL ACFT FH, PER PART 3 OF THE LATEST REVISION OF ECRA5720-03262 - [SDR CALA2022032500781](https://openairdocs.org/sdr/CALA2022032500781.md): Bushing · chipped · Mar 24, 2022 · N849UA · Airbus A319131 · Wing Structure > RT WING RIB 5 FWD LUG BUSHING CHIPPED PER HAECO LCQ N/R 9290638/ 22638 GEN BY V061642 - [SDR CALA2022031700679](https://openairdocs.org/sdr/CALA2022031700679.md): None · corroded · Mar 16, 2022 · N849UA · Airbus A319131 · Fuselage Structure (General) > R2 DOOR SILL HAS SEVERAL AREAS OF CORROSION IN FASTENER HOLES BE TWEEN FR.66-68 PER NR9290764/22764 GEN BY V061742 RMVD AND RPLD R2 DOOR SILL P/N D5348004320701 PO 1101622.9 IAW A 319 SRM 51-72-11 51-42-11 PG 1-2 AND PG 7,8 BY MECH V061742 INSP BY V077960 - [SDR CALA2022031400654](https://openairdocs.org/sdr/CALA2022031400654.md): Intercostal · cracked · Mar 12, 2022 · N849UA · Airbus A319131 · Fuselage Main, Frame > LH FWD DOOR STOP AT FR 20 STOP #7 IB UPPER HOLE HAS CRACK INDICA TION IN INTERCOSTAL LAYER PER HAECO LCQ N/R 9290154/22154 GEN BY V892444 REMOVED AND REPLACED INTERCOASTAL AT FR 20 LH DOOR STOP #7 IAW A 319 SRM 51-72-11-911-002. ACMP BY MECH V061742 INSP BY V8 - [SDR CALA2022031400653](https://openairdocs.org/sdr/CALA2022031400653.md): Intercostal · cracked · Mar 12, 2022 · N849UA · Airbus A319131 · Fuselage Main, Frame > RH FWD DOOR STOP FR20 STOP #7 IB UPPER HOLE HAS CRACK INDICATION IN FRAME AND INTERCOSTAL LAYER PER HAECO LCQ N/R 9290150/22150 G EN BY V892444 REMOVED AND REPLACED INTERCOASTAL AT FR 20 RH DOOR STOP #7 IAW A 319 SRM 51-72-11-911-002. ACMP BY MECH V061742 INSP - [SDR CALA2022031400652](https://openairdocs.org/sdr/CALA2022031400652.md): Intercostal · cracked · Mar 12, 2022 · N849UA · Airbus A319131 · Fuselage Main, Frame > LH FWD DOOR STOP AT FR16 STOP #7 IB UPPER HOLE HAS CRACK INDICAT ION IN INTERCOSTAL LAYER PER HAECO LCQ N/R 9290152/22152 GEN BY V892444 REMOVED AND REPLACED INTERCOASTAL AT FR 16 LH DOOR STOP #7 IAW A 319 SRM 51-72-11-911-002. ACMP BY MECH V061742 INSP BY V07 - [SDR CALA2022031400651](https://openairdocs.org/sdr/CALA2022031400651.md): Intercostal · cracked · Mar 12, 2022 · N849UA · Airbus A319131 · Fuselage Main, Frame > RH FWD DOOR STOP FR16 STOP #7 IB UPPER HOLE HAS CRACK INDICATION IN FR LAYER PER HAECO LCQ N/R 9290148/22148 GEN BY V892444 REMOVED AND REPLACED INTERCOASTAL AT FR 16 RH DOOR STOP #7 IAW A 319 SRM 51-72-11-911-002. ACMP BY MECH V061742 INSP BY V077960 - [SDR CALA2022022200480](https://openairdocs.org/sdr/CALA2022022200480.md): Skin · debonded · Feb 21, 2022 · N849UA · Airbus A319131 · Elevator, Plate/Skin > LEFT ELEVATOR TOP SKIN PANEL HAS A DISBOND 1.0" DIA 57.5"FROM IN BD 19" FROM T/E PER N/R 9290233 GEN BY V061671 REPAIRED DISBOND AREA ON LH ELEVATOR TOP SKIN I/B 19" FROM T/E I AW A319 SRM 55-21-11-300-005 BY MECH V061767 INSP BY V061647 - [SDR CALA2018011900244](https://openairdocs.org/sdr/CALA2018011900244.md): Power Supply · no test · Jan 19, 2018 · N849UA · Airbus A319131 · Emergency Lighting > EMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED THE EPSU AND BATTERY AT 11WL IAW AMM 33-51-38. OK FOR SERVICE - [SDR CALA2018011200172](https://openairdocs.org/sdr/CALA2018011200172.md): Lens · missing · Jan 12, 2018 · N849UA · Airbus A319131 · Emergency Lighting > MISSING EMERGENCY EXIT LIGHT PROTECTIVE LENS AT BOTH SEATS 34A AND 30A. INSTALLED THE LENS CAP. - [SDR CALA2017092503322](https://openairdocs.org/sdr/CALA2017092503322.md): Unknown · odor · Sep 25, 2017 · N849UA · Airbus A319131 · Air Distribution System > AFT LAVATORY HAS AN ODOR LIKE BURNED PETROLEUM OR BURNED HYD FLUID. COULD NOT DETECT THE ODOR, ANYTHING ON OR AROUND AFT LAVATORY DOOR. CHECKED GOOD. - [SDR CALA2017041701029](https://openairdocs.org/sdr/CALA2017041701029.md): Warning System · false activation · Apr 17, 2017 · N849UA · Airbus A319131 · Emergency Lighting > ON 2 SERVICE CHECK. DURING EMERGENCY LIGHTS OPS CHECK PTP DISPLAYED EPSU INT LOAD EMER L FAULT. WAITED A FEW HOURS. ACCOMPLISHED OPERATIONAL TEST OF EMERGENCY LIGHTS REF MM 33-51-00, TEST OK. - [SDR CALA2016101795805](https://openairdocs.org/sdr/CALA2016101795805.md): Seat Track · corroded · Oct 12, 2016 · N849UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings > CABIN SEAT TRACK CORRODED AT FRAME C23 BL Y-1292. REMOVED AND REPLACED SEAT TRACK FROM FR 12- FR24 BL Y-792 IAW SRM 51-42-11 PG 31 PAR A B AND PG 46 PARA D. - [SDR CALA2016072895591](https://openairdocs.org/sdr/CALA2016072895591.md): Light · unsecure · Jul 25, 2016 · N849UA · Airbus A319131 · Emergency Lighting > EMERGENCY EXIT LIGHT FALLING OUT AT SEAT 35C SECURED THE LIGHT, OPS CHECKED GOOD - [SDR CALA2014062091310](https://openairdocs.org/sdr/CALA2014062091310.md): Door Sill · corroded · Jun 18, 2014 · N849UA · Airbus A319131 · Fuselage Miscellaneous Structure > CORROSION ON L2 DOOR SILL AT FRAME 66 - 68 IN AFT WET AREA. A 1 SECTION OF THE FLANGE WAS CUT OUT & A REPAIR INSTALLED IAW SRM 53-41-14 PARA 5 A FIG 201, REPAIR PRINCIPAL 5. - [SDR CALA2014062091309](https://openairdocs.org/sdr/CALA2014062091309.md): Door Sill · corroded · Jun 17, 2014 · N849UA · Airbus A319131 · Fuselage Miscellaneous Structure > R2 DOOR SILL INBD FLANGE WAS FOUND CORRODED AT FRAME 68. A 1 SECTION OF THE FLANGE WAS CUT OUT & A REPAIR INSTALLED. REPAIR REQUIRES INSPECTION IAW SRI53-41-14-2-001-00 PARA 3 A TBL 202. - [SDR CALA2014062091308](https://openairdocs.org/sdr/CALA2014062091308.md): Spar · chafed · Jun 17, 2014 · N849UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/Rib > NUMBER 2 PYLON LOWER SPAR FOUND CHAFED AT LOWER SPAR RIB 5. REPAIR ACCOMPLISHED. THIS IS A CAT B REPAIR & REQUIRES SUBSEQUENT INSPECTIONS. - [SDR CALA2014061791297](https://openairdocs.org/sdr/CALA2014061791297.md): Spar · chafed · Jun 16, 2014 · N849UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/Rib > NUMBER 2 PYLON SHOWS SIGNS OF CHAFING AT FIREWALL SEAL LOWER SPAR RIB 5. ACCOMPLISHED REPAIR TO NR 5 RIB SPAR ON NR 2 PYLON IAW SRM54-51-12 FIG 202. SRI INSPECTIONS WILL BE ACCOMPLISHED AS REQUIRED. - [SDR CALA2013123094029](https://openairdocs.org/sdr/CALA2013123094029.md): Panel · unsecure · Dec 27, 2013 · N849UA · Airbus A319131 · Passenger Compartment Equipment > PCU UNIT FELL OUT OVER ROW 11DEF. NOT PSU PANEL, AIR PANEL WAS LOOSE & HANGING DOWN AT SEAT ROW 11DEF. SECURED PANEL IAW AMM, CHECKED OK TO CONTINUE. - [SDR CALA2013100291662](https://openairdocs.org/sdr/CALA2013100291662.md): Unknown · odor · Oct 1, 2013 · N849UA · Airbus A319131 · Air Distribution System > ELECTRICAL FLOOR OUTLET AT 1R HAS ELECTRICAL SMELL. INBOUND CAPT CONFIRMED IT WAS ONLY A SMELL THAT WAS OZONE ELECTRICAL IN NATURE. OKAYED FOR SERVICE. PERFORMED A VISUAL INSPECTION WITH POWER ON OVENS, COFFEEMAKERS, WARMERS, CHILLER & CONNECTED AC ADAPTER - [SDR UALA2013051403356](https://openairdocs.org/sdr/UALA2013051403356.md): Cover · missing · May 13, 2013 · N849UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK COVER MISSING AT ROW 27DEF. INSTALLED NEW SEAT TRACK COVER. - [SDR UALA2012120707109](https://openairdocs.org/sdr/UALA2012120707109.md): Unknown · odor · Dec 6, 2012 · N849UA · Airbus A319131 · Air Distribution System > F/A SMELLED BURNING PLASTIC SMELL ON TAXIOUT. RETURNED TO GATE. ACCMP'D AN INSPECTION CHECK AS PER AMM(S). NO SMOKE NEITHER FUMES WERE OBSERVED. NO OBJECTS BURNED FOUND. FLIGHT CREW FILLED FORM 46-6020 OUT (SMOKE-ODOR IN THE PLANE QUESTIONNAIRE). DUE TO - [SDR UALA2012051002685](https://openairdocs.org/sdr/UALA2012051002685.md): Unknown · odor · May 9, 2012 · N849UA · Airbus A319131 · Air Distribution System > CREW REPORTED ODOR IN ACFT ON DESCENT. SMELLS ROTTEN, NOT ELECTRICAL. NO SMOKE NOTED. ACCOMPLISHED CHECK OF ALL E/E COMPARTMENTS. ALL OK. ACCOMPLISHED PACK BURN OUT PER AMM 21-00-00 AND NO ODOR DETECTED IN CABIN. NO ODORS WERE DETECTED ON FIRST ARRIVAL O - [SDR UALA2012050702652](https://openairdocs.org/sdr/UALA2012050702652.md): Unknown · odor · May 4, 2012 · N849UA · Airbus A319131 · Air Distribution System > ELECTRICAL ODOR. CAN'T DETERMINE SOURCE. - [SDR UALA2012050402650](https://openairdocs.org/sdr/UALA2012050402650.md): Bulb · unsecure · May 4, 2012 · N849UA · Airbus A319131 · Emergency Lighting > ELECTRIC ODOR. CAN'T DETERMINE SOURCE. INSPECTED AIRCRAFT FOUND SEAT ELECTRONICS BOX UNDER SEAT 23ABC OFF OF ITS MOUNT. INSPECTED WIRES AND FOUND GOOD. REINSTALLED BOX. FOUND CEILING LIGHT AT 23-25 INOPERATIVE. RESECURED BULBS LIGHT WORKS, NO ODOR. AL - [SDR UALA2012043002534](https://openairdocs.org/sdr/UALA2012043002534.md): Computer · malfunctioned · Apr 30, 2012 · N849UA · Airbus A319131 · Autopilot System > AUTO FLT 'FCU 1 FAULT' DISPLAYED ON UPPER ECAM SCREEN. ATTEMPTED RESET PERFORM 13.50.3 CYCLED FCU1 FCU2 CB`S, NO FIX. PERFORMED FULL RESET OF FCU CB`S B5-M21. FCU 1 FAULT CLEARED. - [SDR UALA2012031901778](https://openairdocs.org/sdr/UALA2012031901778.md): Stowage Box · leaking · Mar 16, 2012 · N849UA · Airbus A319131 · Crew Oxygen System > CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW O2 LEAKING MORE THAN 20 PSI PER HOUR. USING LEAK CK, CHECK PRESS REG XMITTER, DISTRIBUTION MANIFOLD, AND LINES AT O2 BOTTLE FITTINGS. REMOVED CAPT O2 ACCESS PANEL FOR O2 BOXES AND CHECK LINES - [SDR UALA2012022801216](https://openairdocs.org/sdr/UALA2012022801216.md): Stringer Clip · crushed · Feb 28, 2012 · N849UA · Airbus A319131 · Fuselage Main, Attach Fittings > CLIP CRUSHED AT FRAME 65, 5 O`CLOCK POSITION. CLIP REMOVED. NEW CLIP IN CARGO PIT. DRILLED NEW CLIP. AWAITING FASTENERS. REPLACED STR CLIP AT FRA 65 STR 40R. - [SDR UALA2012021300861](https://openairdocs.org/sdr/UALA2012021300861.md): Skin · punctured · Feb 13, 2012 · N849UA · Airbus A319131 · Fuselage Main, Plate/Skin > UPON INSPECTION OF LAV TRUCK DAMAGE FOUND 2EA 1INCH LONG PUNCTURES THRU OUTER SKIN OF LAV SERVICE PANEL DOOR. REF SMC16 FOR DAMAGE REMOVED. REMOVE FUSELAGE SKIN FASTENERS REF SMC16 & PTT 3582009 & PTT 3582026. GOING TO REPLACE SKIN PER AIRBUS. REMOVED FASTE - [SDR UALA2011122207063](https://openairdocs.org/sdr/UALA2011122207063.md): Bleed Valve · stuck · Dec 22, 2011 · N849UA · Airbus A319131 · Compressor Bleed Valve > NR 1 ENGINE HAD A HUNG START. FOUND 10TH STAGE BLEED VALVE STUCK IN THE CLOSED POSITION. VALVE REPLACED. - [SDR UALA2011120506677](https://openairdocs.org/sdr/UALA2011120506677.md): Actuator · malfunctioned · Dec 2, 2011 · N849UA · Airbus A319131 · Rudder Control System > CAPTAIN'S RUDDER PEDAL SPRING IS NOT RETURNING PEDALS TO OUT POSITION. REPLACED CAPTAIN'S PEDAL POSITION ACTUATOR. CHECKED OPERATION FOUND GOOD. - [SDR UALA2011111106175](https://openairdocs.org/sdr/UALA2011111106175.md): Actuator · faulty · Nov 10, 2011 · N849UA · Airbus A319131 · Rudder Control System > F/O RUDDER PEDALS DO NOT MOVE TOWARD PILOT WITHOUT MANUAL ASSISTANCE. REPLACED PEDAL ADJUSTER ACTUATOR, OPS CHECK NORMAL. - [SDR UALA2011083004650](https://openairdocs.org/sdr/UALA2011083004650.md): Aileron · damaged · Aug 30, 2011 · N849UA · Airbus A319131 · Ailerons > 2 RT AILERON DAMAGED 12 INCHES FROM INBD T/E CORNER. RT AILERON DAMAGED 12 INCHES FROM INBD TRAILING EDGE CORNER. SHOP TO EVAL FIRST B4 ROBBING. REPAIRABLE ON-WING PER SHOP. DAYS SHOP TO MFG REPAIR. REMOVED LWR PANELS AND LOCKS FROM ATTACH HARDWARE. SHOP Next page: https://openairdocs.org/aircraft/N849UA/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 = 'N849UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N849UA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.