IAE V2522-A5

Service difficulty reports · 3,460

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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 engine_model_key = 'V2522A5'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026080318227Relay · faultedHYD 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 EVALUATAug 1, 2026 · N849UA · Airbus A319131 · Hydraulic System, MainSDR CALA2026082418829Fitting · crackedRIGHT CONTINUITY FITTING CRACKED 1 INCH FROM CENTER LINE, 1 00% SCREEN HEIGHT. MAJOR REPAIR, REMOVED AND REPLACED LT & RT CONTINUITY AS DIRECTED BY REO L25 980 AND IAW REPAIR DWG'S R53112919 AND R53113426 AND EC/R A 5311-03457.Jul 31, 2026 · N839UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026080218151Tie Down · corrodedAFT PIT FR 57 STR 42-41L. TIE DOWN PROFILE HAS CORROSION. REMOVED AND REPLACED PROFILE PLATE IAW SRM 51-42-11.Jul 30, 2026 · N839UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026080218153Seal · damagedAFT CARGO, FR 53, STR 31-32L, VERTICAL PROFILE HAS SCRIBE MARK DOWN THE CENTER. REMOVED AND REPLACED SECTION SEALING AT AFT FR 53 STR 31-32L IAW 51-43-11.Jul 30, 2026 · N839UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026080218155Panel · corrodedAFT CARGO, FR 59-62, S38R, FLOOR PROFILE HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED CORRODED PROFILE PANEL WITH A NEW PROFILE PANEL. APPLIED SURFACE PROTECTION COATING.Jul 30, 2026 · N839UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2026061517082Actuator · faultyEGT 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 "CJun 11, 2026 · N849UA · Airbus A319131 · Compressor Bleed ValveSDR CALA2026042715738Spinner · leakingENG1 SOURCE OF FUMESDURING T/O AND CLIMBINTERRIGATED E1 UPON ARRIVAL AT GATE, FOUND STRONG FUEL SMELL IN E1 IN COMPARISON TO E2. RAN BOTH PACKS APROX 5 MIN. NO OIL SMELLS NOR SMOKE IN CABIN NOR NEAR E1 AT THIS TIME. REQ FURTHER TROUBLESHOOTING REF. AMM 71-00-0Apr 15, 2026 · N804UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2026031814641Solenoid · corrodedPRESURIZATION SYS V/S FLUCTUATES + - 800FT CONSTANTLY CONSTANT LY IN FLIGHTCAPT REPORTS THE V/S FT/MN INDICATION ON CAB PRESS PAGE KEPT FLUCTUATING UP AND DOWN WHEN SWITCHED TO MANUAL MODE INDICATION WENT FULLY CLOSED. CAPT ALSO REPORTS BLEED 2 INDICATION WMar 16, 2026 · N839UA · Airbus A319131 · Air Conditioning SystemSDR 2026FA0000060Engine · faultedCONFIGURATION ERROR WAS DETECTED IN ESN V12188 (OPERATED BY BAW BRITISH AIRWAYS), THE FIRST STANDARD MOTOR RELEASED POST SB 72-0716. THIS WAS CERTIFIED ON MAY 12, 2025, BEEN INSTALLED A POST SB 72-0716 P/N FOR HPC STAGE 3 BLADE. THE INSTALLED P/N WAS 6C8403 (SJan 27, 2026 · Engine (Turbine/Turboprop)SDR CALA2026011412967Nozzle · faultedAT 11 OCLOCK POSITION IN AFT SECTION OF NR 2 ENG A PIECE OF LINE R APPEARS TO BE MISSING. DIMENSIONS OF DAMAGED AREA ARE ROUGHLY 10"X8". REMOVED & REPLACED NR 2 ENGINE COMMON NOZZLE ASSEMBLY IAW AMM TASK 78-11-11-400-010-A. ALL CHECKS GOOD.Jan 12, 2026 · N850UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR CALA2025120511814Eec · faultedSETTING TAKEOFF POWER. ENG 1 LAGGED IN POWER. ABORTED TO. WHILE RETURN ENG 1 EPR MODE FAULT PERFORMED TSM TASK 73-22-00-810-857-A LOSS OF THE P4.9 (P5) INPUT ON ENGINE 1, NO DAMAGED FOUND ON P5 PRESSURE TUBES, REMOVED AND REPLACED E1 EEC IAW AMM 73-22-34/401Dec 3, 2025 · N835UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2025112811582Anti-Ice Valve · warning messageANTI ICE ENG2 VALVE OPEN IN FLIGHT CREW REPORTS THEY CYCLED NR 2 ANTI ICE SWITCH SWITCH ON GROUND AND MESSAGE CLEARED. NO MESSAGE ON ARRIVAL AT GATE. REF AMM 30-21-00/001 CONFIG 13Nov 24, 2025 · N835UA · Airbus A319131 · Engine Anti-Icing SystemSDR CALA2025102410498Actuator · faultedENG 1 COMPRESSOR VANEECAM CREW REPORTED THAT ABORTED T-OFF AT 70 KNOTS. (LOW SPEED). DUE TO #1 ENG SN. V10406 (TSI= 1990 HRS / 1082 CYC) DUE TO ENG1 COMP VANE ECAM. FADEC 1A SHOW ENG1 COMP VANE CH. A VSV ACT / HC/ EEC1 CELL 38 (FAULT CODE SVATK). AHM SHOW DURIOct 20, 2025 · N822UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2025101610189Actuator · faultedENGINE 1 COMPRESSOR VANE ECAM REJECTED T.O. LESS THAN 50KTS ADDED. R & R NUMBER 1 ENG VSV ACTUATOR PER 75-32-41-400-010-010-A AFTER INSTALLATION PERFORMED LEAK CHECK AND POWER ASSURANCE RUN NO LEAKS AND NO ECAM MESSAGE NOTED.Oct 14, 2025 · N836UA · Airbus A319131 · Compressor Bleed ControlSDR CALA2025092209104Engine · making metalENG 1 STALL CREW REPORTED TO LOCAL MAINTENANCE THAT THE ENG-1 STALLED 3 TIMES IN CRUISE ENGINE RECOVERED AND FLIGHT CREW KEPT IT AT IDLE ALL THE WAY DOWN. #1 ENG HPC UPPER BLEED VALVE HAS METAL SHARDS IN THE SCREEN AND METAL INSIDE THE VALVE. REF JOB TASK CARDSep 19, 2025 · N819UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2025082508092Scavenge Pump · faultedENG2/INNER EXHAUST HAS FLUID LEAKING AT THE 6 OCLOCK POSITION. SUSPECT FUEL PUDDLE, DID NOT GLOW FROM UV LIGHT AND DOES NOT HAVE A SMELL. IN CONCURRANCE WITH TOMC ENGINE DESK, SUSPECT #5 ENGINE BEARING OIL SCAVENGE TUBE MAY BE BLOCKED INTERNALLY & CAUSING THEAug 21, 2025 · N830UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2025081107527Exciter · faultedHUNG START ON NUMBER 1 ENGINE AFTER STARTER CUT OUT. STRONG FUEL ODOR IN FLTDECK AFTER CRANK CLASS 3 FUEL DEPULSE ACTIVATED 1. LEADS TO TSM 80-00-00-810-819-A. ENG START INITIAL TO IDLE SPEED TOOK 2 PLUS MINUTES ON 2 STARTS. ODOR OF FUEL SMELL IN FLIGHT DECK UAug 11, 2025 · N838UA · Airbus A319131 · ExciterSDR CALA2025080407251Actuator · faultedENG 1 COMPRESSOR VANE. CHA/CHB VSV ACT/HC/EEC1 FOUND WITH FAULT ACRONYM OF SVATK, REF TSM'S 75-30-00-810-843-A AND 75-30-00-810-845, PERFORMED TSM 75-30-00-810-805B FOUND ENGINE 1 VSV BOTH CHANNELS DEFECTED. REMOVED AND REPLACED ENGINE 1 VSV REF AMM 75-32-Aug 1, 2025 · N852UA · Airbus A319131 · Compressor Bleed ControlSDR CALA2025073107120Exhaust Cone · crackedENG1 HAS GASH TEAR ON EXHAUST. LIGHT SMOKE OBSERVED FROM FRONT & BACK. OIL OR FUEL ODOR NOTICED. INSPECTED WELDED DOUBLER TO ENSURED NO ADDITIONAL DAMAGE PRESENT. TWO CRACKS MEASURING 2 & 4 INCHES. VERIFIED CRACK OUTSIDE OF WELDED DOUBLER IAW ECRA 7811-01Jul 28, 2025 · N812UA · Airbus A319131 · Engine Collector/Tailpipe/NozzleSDR CALA2025051504703Bleed Valve · faultedENG 2 STALL ON CLIMBOUT. NOTICABLE YAW. ECAM CLEARED ITSELF. NO SHUTDOWNOPENED UP ENGINE NUMBER 2 FOR BOROSCOPE INSPECTION PER TSM 71-00-00-810-809-A STEP D2(A).PLEASE NOTE I ONLY BROKE LOOSE BOROSCOPE PLUGS 3 TO 7 PER THE AMM 72-00-00-200-016-B. BOROSCOPE PLMay 12, 2025 · N818UA · Airbus A319131 · Compressor Bleed ValveSDR CALA2025050104378Oil System · leakingWITHIN 3 CYCLES, DUE TO REPEAT OILY SMELL IN COCKPIT ON DESCENT (ONLY, NO ODORS IN CABIN), COMPLETE TROUBLE SHOOTING PER THE TSM 71-00-00-810-801-A. NOTE DUE TO REPORT OF COCKPIT ODOR ONLY START WITH THE LT ENGINE AND PACK FIRST.DOCUMENT ALL FINDINGS.CARRIEApr 28, 2025 · N824UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2025032703256Eec · faultedENG 2 COMPRESSOR STALL A T CRZ ALT FL370 ENG 2 STALL ECAM ENG 2 EPR MODE FAULT CREW REPORTED MULTIPLE LOUD BANGS FOLLOWED BY STALL AND EPR MODE ECAM, ENGINE WAS REDUCED TO IDLE & RAN REMAINDER OF FLIGHT AT IDLE. CREW REPORTED ONE MORE LOUD BANG AFTER LANDING PMar 24, 2025 · N837UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2025030302532Fairing · damagedPDA 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.Feb 27, 2025 · N846UA · Airbus A319131 · Engine Thrust ReverserSDR CALA2025020502215Vsv · failedENG2 FAIL ON T/O ROLL. NO INDICATION NOTICED PRIOR TO FAILURE ENG 2 STALL WITH CFDS VSV MECH/BLD VLV/LPC2 REFERENCE TSM 71-00-00-810-809-A, ALSO SUGGEST MCD INSPECTION PER AMM 79-22-45-000-010-A TO DETERMINE ENGINE SERVICEABILITY. TOMC-MEREDITH FLAGGING SDRFeb 3, 2025 · N837UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2025012402005Pressure Switch · crackedHYD Y ENG 2PUMP LO PR ECAM/RAN ECAM WE DID HAVE PRESSURE FLUCTUA TION AIRCRAFT WAS AT 29K FEET IN CLIMB OUT. WHEN AIRCRAFT ARRIVED AT GATE, YELLOW SYSTEM WAS BELOW NORMAL LIMITS. PRESSURE FLUCTUATION DROPPED AS LOW AS 2300 PSI. FOUND ENG 2 HYDRAULIC PRESSURE SJan 23, 2025 · N842UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), MainSDR CALA2024101100814Eec · faultedFADEC FAULT DISPLAYED ON UPPER ECAM SCREEN. ENGINE FAIL CONFIRM ED ENGINE SHUTDOWN. - ENG 1 REF LP 9512804 FOR WORK PERFORMED. INSTALLED NEW EEC. ALL TESTS GOOD E1 ESN V10546 - PLEASE R&R THE EEC PER AMM TASK 73-22-34/401 CONFIG 13. FOR THE REMOVED EEC, PLEASEOct 10, 2024 · N806UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2024093000716Engine · bird ingestionDURING BIRD STRIKE INSPECTION FOUND EVIDENCE OF BIRD REMAINS IN #1 ENGINE INTAKE AND EXHAUST. UPON BIRDSTRIKE BSI OF THE #1 ENGINE PER AMM 72-00-200-010-A FOUND MISALIGNED STAGE 3 CLAPPER TO BE OUT OF LIMITS IAW AMM 72-00-00-200-016-B PARA D.2(4)WHICH IS MORESep 26, 2024 · N850UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2024080600378Actuator · failedCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGI NE PARAMETE RS NORMAL. - ENG 2 65KTS ENG2 COMP VANEON ECAM. INITIATEDABORT 70KTS. MAX SPD85KTS. SHUT ENG2 DOWN FOUND #2 ENGINE VARIABLE STATOR VANE ACTUATOR FAILED REF TSM 75-30-00-810-846-A. REMOVED #2 ENGIAug 6, 2024 · N844UA · Airbus A319131 · Compressor Bleed ControlSDR CALA2023122003673Engine · failedLOW SPEED ABORT LESS THAN 30 KNOTS. LOUD BANGAND AC VEERED TO RIGHT. ENGINE 2 FAIL ECAM. SEE L/P 6568330 FOR CORRECTIVE ACTION. SCHEDULED PARTS CHANGE"M&E P/N: 31-7200-9-0001 S/N: XXXXXXXXXXXX X. IF S/N FOUND, REMOVE AND REPLACE. IF THE PART REPLACED REQUI RESDec 13, 2023 · N823UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2023112703472Engine · warning messageSTART VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 1 CFDS FAULT AUTOSTART GROUP SOL/EEC1, START VALVE AND EEC PREVIOUSLY REPLACED. REF TSM 80-00-00-810-807-A FOR TROUBLESHOOTING, POSITIVE FIX REQUIRED. TOMC-MEREDITH PERFORMED WIRE CHECK. FOUND WIRING TO BNov 24, 2023 · N415UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR 2023FA0000346Disk · damagedSCRAP OF A PVL BEFORE THE END OF LIMITED LIFE. NICKS, DENT IN AREA A4 MORE THAN SERVICEABLE/REPARAIBLE LIMIT IN ACCORDING WITH SUBTASK 72-50-31-220-020 B(1)(B) AND TASK 72-50-31-300-004 REPAIR004 (VRS4157) SUBTASK 72-50-31-350-054 B(1) AREA A1 NO BLENDS PERMITJun 30, 2023 · N830UA · Airbus A319131 · Turbine SectionSDR CALA2023062802050Engine · inoperativeENG 2 FAIL. ABRUBT YAWLOUD BANG. FIRST ECAMWAS ENG STALL. THEN ENG2 FAIL. EGT RED. REPLACED #2 ENG.PER W/C 317100-1-4900 GROUND RUN LEAK CHECKED NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1809185 SN OFF 0046. DUE TO ENGINE 2 REPLACEMENT, PERFORMED TEST Jun 25, 2023 · N850UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR 2023FA0000022Shaft · damagedHPC REAR SHAFT,GALLING LOC.2 IAW SUBTASK 72-41-13-220-189 NOT PERMITTED. LLP TO BE RETIRED WITH 12843 CYCLES SINCE NEW (LIFE LIMIT WAS 20000 CYCLES)Jan 6, 2023 · N823UA · Airbus A319131 · Turbine Engine Compressor SectionSDR 2022FA0000774Turbine Wheel · crackedCRACKED IN AREA A1 OVER REPAIR VRS4018 LIMITS (SUBTASK 72-50-00-230-071). MINIMUM REMAINING KNIFE EDGE HEIGHT LESS THAN 0.0177 IN. (0.45 MM) (SUBTASK 72-50-00-350-061). NON REPAIRABLE. LIFE LIMITED PART TO BE SCRAPPED WITH 12843 CYCLES (LIFE LIMIT 20000 CYCLESDec 23, 2022 · N823UA · Airbus A319131 · Turbine SectionSDR CALA2022091202343Eec · inoperativePILOT REPORTS E1 REV FAULT. DIVERSION INTO BNA. THRUST REVERSER HAS BEEN DEACTIVATED AND SECURED IN THE FWD THRUST (STOWED AND LOCKED) POSITION. REMOVED AND REPLACED #1 ENGINE EEC. ACCP IDT INSPECTION OF EEC INSTALLATION SAFETY AND SECURITY. IDT EEC OP CHK PASSep 12, 2022 · N815UA · Airbus A300* · Engine Exhaust SystemSDR CALA2022071901811Actuator · warning messageCOMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGINE PARAMETERS NORMAL. LOW SPEED ABORTED TAKEOFF. REMOVED AND REPLACED VARIABLE STATOR VANE (VSV) ACTUATOR. PERFORMED DRY MOTORING OF #1 ENG. LEAK CHECK PASSED. ACP TEST # 11 HIGH POWER ASSURANCE TEST, ACP 2 EJul 19, 2022 · N821UA · Airbus A319131 · Compressor Bleed ValveSDR CALA2021090301503Eec · failedONE TLA FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 INTERMITTENT IN FLIGHT7 OR 8 TIMES USE TSM 76-00-00-810-802-B TO TROUBLESHOOT THE WIRING. PFR ATTACHED. CHECK CFDS ENG 2 FADEC A&B FOR FAULT CODE "TRAL" AND CHECK WIRING PER ABOVE FIM. CODE TRAL PER FIM TASSep 3, 2021 · N836UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2020051700972Engine · fireDURING POST HMV-3 ENGINE RUN #1 ENGINE OIL QTY DECREASED RAPIDLY FOLLOWED WITH SMOKE AND FLAMES COMING FROMTHE TURBINE AREA. ENGI NE WAS MOTORED UNTIL FIRE DEPT RESPONED. FIRE WAS PUT OUT WITH W ATER AND PURPLE-K DRY CHEMICAL SUPPRESSING AGENT. THIS OCCURED D May 17, 2020 · N836UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2020050200885Engine · leakingSCHEDULED PARTS CHANGE, M&E P/N: 31-7200-9-0001 S/N: 0043 ENGINE, V2500-A5 (KIT) POSITION E1 1 ENG NHA POSITION E1 1 ENG IF SCHED ULED S/N NOT FOUND VERIFY S/NS IN ALL OTHER POSITIONS OR CONTACT TOMC PRIOR TO FLIGHT. IF S/N IS FOUND, RMV/RPLC. REMOVEDMay 1, 2020 · N836UA · Airbus A319131 · Turbine Engine Oil SystemSDR CALA2019042900672Seal · damagedPDA 2 ENGINE 2 INBOARD FLEX SEAL SEGMENT IS BENT, BROKEN, CRACKED, WITH PIECE MISSING.Apr 29, 2019 · N816UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2018062101474Line · wornNR 1 ENGINE DID NOT SPOOL UP WHEN THE THRUST LEVERS WERE SET TO FLEX MCT. REMOVED THE PB SENSE LINE ON THE NR 1 EEC, DISCONNECTED THE DOWNSTREAM END ADJACENT TO LOWER MOISTURE TRAP. APPLIED AIR PRESSURE AND LEAK CHECKED GOOD. FOUND PB LINE SUPPORT CLAMP MJun 14, 2018 · N836UA · Airbus A319131 · Fuel Controlling SystemSDR CALA2017100203366Seal · leakingACRID, ELECTRICAL ODOR IN COCKPIT AND 1ST CLASS. NOTICABLE AT LOW DIFF PRESSURES. CHECKED AFT, FWD,AND BOTH SIDE E & E AREAS, NO SMOKE ODOR. PERFORMED AVEC TEST IAW AMM 21-26-00, NO FAULTS FOUND, PERFORMED BCL 1 AND 2 BITE TEST IAW AMM 24-38-00, NO FUALTSOct 2, 2017 · N823UA · Airbus A319131 · Drag Control ActuatorSDR GTIA2017033101850Seal · leakingDESCENDING THROUGH 10,000 FT. SMELLED A DIRTY SOCK AND MUSTY ODOR. TURNED OFF PACKS, BLEEDS & VENTILATED CABIN WITH RAM AIR. R & R DEOILER SEAL ASSY IAW AMM 72-60-31 ON THE RT AND LT ENGINES. R & R THE HEPA FILTERS IAW AMM 21-21-41. PERFORMED A PACK BURNOMar 31, 2017 · N606NK · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2016110295888Skin · crackedRT FUSE SKIN AT FR35 STR 30R HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM RPR ACP IAW ECRA 5330-05813 PART 1.Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016110295889Skin · crackedLT FUSE SKIN AT FR35 STR 30L HAS A CRACK INDICATION ON HOLE MARKED 2. INTERIM REPAIR ACP IAW EC RA5330-05813 PART 1.Oct 30, 2016 · N814UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016102495851Threshold · corrodedFWD CARGO THRESHOLD WEB HAS CORROSION AND FOUND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 53-21-13 PG 101-104.Oct 24, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2016102495852Skin · dentedFUSELAGE SKIN DENTED AT FRAME 23 BETWEEN STRINGERS 24 AND 25L FOUND OUT OF LIMITS. INSTALLED DOUBLER REPAIR PER SRM53-00-11 FIG 232Oct 24, 2016 · N821UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016103195877Fitting · corrodedR1 DOOR SILL FWD GIRT BAR FITTING AREA CORROSION AROUND FWD OUTBD, AFT INBD, & AFT OUTBD HOLE AT FR20 STR23. REMOVED CORROSION BY SPOT FACING ALL 3 HOLES ON FR20 .017 .025 .020 MATERIAL REMOVED & FOUND TO BE IN LIMITS IAW A319 SRM53-11-14 FIG 108 PARA 7B FABOct 24, 2016 · N814UA · Airbus A319131 · Fuselage Main, Attach FittingsSDR CALA2016102495837Doubler · dentedMAJOR REPAIR. DOUBLER REPAIR AFT OF DOOR 1L IS DENTED AT FRAME 23 JUST ABOVE FLOOR LEVEL. INSTALLED DOUBLER IAW SRM 53-11-11 FIG 211. MAJOR REPAIR.Oct 22, 2016 · N819UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2016101995833Door Sill · corrodedL2 DOOR CUTOUT FWD LOWER CORNER HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW SRM 51-42-11.Oct 18, 2016 · N814UA · Airbus A319131 · Fuselage Miscellaneous Structure
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