Airbus A319-114
Service difficulty reports · 10,218
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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 aircraft_model_key = 'A319114' 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.
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 aircraft_model_key = 'A319114' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2026050102775Cids · faultedAIRCRAFT 3154, EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT ROWS 1-29, EMERGENCY TRAC LIGHTING FLASHING ON AND OFF ON TAKE OFF. PERFORMED CIDS RESET PER AMM 23-73. PERFORMED OPS TEST OF EMERGENCY LIGHTS PER AMM 33-51. CHECKS GOOD. NO 60 DAY HISTORY. (LSDR DALA2026050102761Frame · corrodedCORROSION LEVEL 2 WEB FRAME 16 AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW FR12 TO FR16 AT LEVEL STR23L AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1569531 - AIRCRAFT WAS GROUNDED)SDR DALA2026050102754Display · faultedATO - AT APPROXIMATELY 22 KNOTS DUE TO LOSS OF CAPTAINS PFD. MAINTENANCE IN PROGRESS. (LP: 7794686). AIRCRAFT WAS GROUNDEDSDR DALA2026042902698Shear Plate · corrodedPAX CABIN, AFT SECTION, FLOOR BTWN FR 69 & FR 70, Y-1194.8, SHEAR PLATE CORRODED. REPLACED THE SHEAR PLATE IAW SRM 53-41-17-01A, FIGURE 001, ITEM 310. REV 157. AND INSTALLED IAW DWG D534 74180, SHEET 6, ITEM 74. (LP: 1567232). AIRCRAFT WAS GROUNDED.SDR DALA2026042902697Web · corrodedLEVEL 2 CORROSION WEB BTW FR 69 TO FR 70, STR 23L REPLACED THE WEB IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53474180, ISSUE: AA. MEASUREMENT OF CORROSION: L= 0.7260 INCH, W=0.4440 INCH. AIRCRAFT WAS GROUNDEDSDR DALA2026042902696Web · corrodedLEVEL 2 CORROSION ON WEB FRAME 16, STR 23R. REPLACED THE WEB IAW SRM 51-42-11, SRM 51-72-11, DWG D53918884 & DWG D53114392. CORROSION: L= 0.833INCH W=0.520 INCH. ACFT WAS GROUNDED.SDR DALA2026042902703Battery · inoperativeRT OVERWING EMERGENCY LIGHTS INOP. FWD TO MEL AND PLAC IAW MEL 33-50-04A NEEDS EPSU. R & R RT OVERWING EPSU IAW AMM 31-51. OPS CHECK NORMAL. (LP: 8892318). AIRCRAFT WAS GROUNDEDSDR DALA2026042902702Elec Connector · disconnectedOPS TEST OF EPSU FAULTS EPSU EXT LOAD AFT LT. FOUND CONNECTOR ON SLIDE DISCONNECTED. RECONNECTED IAW AMM 25-62. ONLY SLIDE COVER WAS REMOVED. NO RII STEPS TO C/W. R &R BATTERY ON EPSU (13WL) IAW AMM 33-51. (LP: 8892317). AIRCRAFT WS GROUNDEDSDR DALA2026042902700Unknown · odorFA REPORT FUMES AROUND MID/AFT CABIN. FUMES LASTED A FEW MINUTES AND HAPPENED EXACTLY AT ENGINE START NR 1 ENGINE WAS STARTED WITH APU ON - BLEED ON. C/W MSI STEP STEP A. FLIGHT CREW REPORTED FUEL ODOR WENT AWAY AFTER A FEW MINUTES. C/W STEP (B). MCC CONCURESDR DALA2026042902699Power Supply · no testDURING R1 DOOR SLIDE CHANGE, FAIL OPS TEST OF EPSU. R & R EPSU (11WL) IAW AMM 33-51, OPS CHKD FAILED. OP CHECKS GOOD IAW AMM 33-51. (LP: 8892316). AIRCRAFT WAS GROUNDEDSDR DALA2026042502621Floor Support · corrodedTASK 5320-6010, CPCP 2021-2001. PAX CABIN AFT SECTION, FLOOR STRUCTURE AT FR68 Y512.5 LONGITUDINAL BEAM WITH CORROSION. REPLACED FLOOR STRUCTURE LONGITUDINAL BEAM P/N: 5347219420400 AT FR67 TO FR70, Y512.5 IAW A319 SRM 53-41-14-03A FIG 303, ITEM 180. REV 157.SDR DALA2026042502620Shear Plate · crackedCRACK SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOC. STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWGD53474180 ISSUE: AA RELEASE DATE: 09-SEP-24. TOOK MEASURE OF CRACK ON SHESDR DALA2026042002475Unknown · unknownATB - DUE TO AIRCRAFT PITCHING UP WITH A/P OFF. REPLACED ACCELEROMETER UNIT 12CE4, THS ZERO ADJUSTMENT CHECK, AND ELEVATOR FREE PLAY CHECK. NTF, AND ALL OPS CHECK GOOD. (LP: 7729382). AIRCRAFT WAS GROUNDED.SDR DALA2026042502622Oxygen Bottle · emptyPORTABLE O2 BOTTLE READING ZERO IN AFT RT CABIN LOWER. C/A: REMOVED AND REPLACED O2 PORTABLE BOTTLE PER A 319 AMM 35-30 HYD TEST CURRENT. (LP: 8241176). AIRCRAFT WAS GROUNDEDSDR DALA2026042202552Oxygen Mask · faultedSHIP 3159 DISC: DURING CAPT OXYGEN MASK TEST THE MASK STARTED FLOWING OXYGEN NON - STOP. THE MASK WAS REMOVED. SPINNING THE EMER DIAL AND FLIPPING THE 100% SWITCH HAD NO EFFECT. AFTER ABOUT 45 SECONDS IT SHUT OFF WITH NO OTHER ACTIONS. C/A: R&R CAPT'S O2 MASK SDR DALA2026042202549Oxygen Mask · not reportedREMOVED O2 MASK / SMOKE DETECTOR ACCESS PANEL FROM CEILING OF FWD LAV. REMOVED AND REPLACED AIR EXTRACTION HOOD ABOVE FWD LAV CEILING PANEL AND REINSTALLED PANEL PER CMM 25-40. PERFORMED O2 MASK DROP TEST PER A319 AMM 35-23 AND LAV SMOKE DETECTOR TEST PER A31SDR DALA2026042002463Repair · not reportedREMOVE EXISTING EXTERNAL REPAIR LOCATED BTWN FR1 AND FR3 STRG 34R AND RT LOWER STRG AND PERFORM VISUAL INSPECTION OF THE UNDERLYING STRUCTURE. REPAIRED R/H NOSE FWD FUSELAGE SKIN BETWEEN FRI-FR3 BETWEEN STRG -34R-36R I/A/W DELTA ER/A 633282-14AD REV: ORIGINAL SDR DALA2026042202554Skin · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR SKIN REPAIR INSTALLED AT FR 65 - 66 S31 - 32R IAW ER/A 632717-14. C/A: SECTION I IS LIMITED TO 6MO ( 182 DAYS ) FROM 15APR26. ER/A TO B E REVISED PRIOR TO THIS LIMIT ELSE REMOVED A/C FROM SERVICE. ASSOCIATED ER/SDR DALA2026042002462Skin · dentedUPPER FUSELAGE FR55+470MM BETWEEN STR 6L-7L SKIN PANEL WITH DENT. REPAIRED UPPER REAR FUSELAGE SKIN PANEL WITH DENT FR55+470MM BETWEEN STRG 6LH - 7LH IAW DELTA ER/A 633023-14 REV ORIGINAL DATED 15/APR/26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIR. ASSOCIATED ESDR DALA2026042002461Skin · crackedLOWER FUSELAGE AT FR65+220MM BETWEEN STRG 31R-32R SKIN PANEL CORRODED AND CRACKED. REPAIRED UPPER REAR FUSELAGE SKIN PANEL BETWEEN FR65-FR66 AND STRG 31RH-32RH I/A/W DELTA ER/A 632717-14 REV. ORIGINAL DATED 17 -APR-26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIRSDR DALA2026042002465Lamp · inoperativeCIDS 1 GND SCAN SHOWS EPSU EXT LOAD EMER L. REF A319 SM 33-51-00, REMOVED AND REPLACED EPSU 11WL, NO HELP. FOUND LAMP AT 63WL INOP, CLEANED SOCKET AND RELAMPED, OPS CK OK. (LP: 1547814) AIRCRAFT WAS GROUNDEDSDR DALA2026041702436Door Frame · damagedFR68 DOOR FRAME R/H, DOOR STOP FITTINGS 1,2,3,4,5,6 AND 7 LOCATIONS WERE FOUND THE HOLES (4 HOLES IN EACH FITTING) COMMON TO THE FRAME WEB GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER (6.38MM/0.251") "ACTION REQUIRED PRIOR TO FURTHER FLIGHT, ENGINEERING EVASDR DALA2026041602407Uplock Switch · faultyDECLARED EMERGENCY DUE TO AN LGCIU 1 FAULT WITH AN ASSOCIATED RT MAIN LANDING GEAR UNLOCKED INDICATION. REPLACED RT MAIN LANDING GEAR UNLOCK PROXIMITY SENSOR 14GA AND LGCIU 1. (LP: 7984110) AIRCRAFT WAS GROUNDEDSDR DALA2026042202551Door Frame · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLED AT FR68RH DOOR STOP AREA OF FRAME WEB PER ER/A 633159-14AD. C/A: SECTION I IS LIMITED TO 60000FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA SDR DALA2026042202550Door Frame · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D ON FRAME WEB FR68RH AT DOOR STOPS PER ER/A 633159-14AD. SECTION I IS LIMITED TO 37900FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01SDR DALA2026042202553Door Frame · damagedER/A 633159-14AD ISSUED FOR REPAIR TO FR68 RT FRAME WEB AT DOOR STOPS. FOLLOW ON ACTION REQUIRED. PERFORM SECTION II EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1545988). AIRCRAFT SDR DALA2026042002460Skin · not reportedDAMAGE TOLERANCE EVALUATION (DTE) REQUIRED FOR FUSELAGE SKIN R EPAIR INSSTALLED AT FR56 AND S-6/7LH PER ER/A 633023-14. SECTION I IS LIMITED TO 6MO (182) DAYS FROM 10APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 1SDR DALA2026041602406Bleed Air Sys · warning messageDIV - TO RDU DUE TO A RT WING BLEED LEAK MESSAGE WITH THE LT ENG BLEED SYSTEM ALREADY ON MEL AND THE CABIN PRESSURE CLIMBING. MASKS DID NOT DEPLOY. REPLACED LT AND RT EBAS TLT. (LP: 7729686) AIRCRAFT WAS GROUNDEDSDR DALA2026041602405Computer · faultyATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. ENG 1 G HYD MON C/B WAS FOUND POPPED. REPLACED ELAC 2.SDR DALA2026041502383Stringer · corrodedAFT CARGO BAY, BETWEEN FR 59 & FR 60, STR 43L, STRINGER EXISTING COUPLING REPAIR CORRODED. REPAIRED FUSELAGE S43L BTWN FR 58 - 61. IAW ER/A 633052-14, REV. ORIGINAL. MAJOR REPAIR.SDR DALA2026042002464Lug · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF LUG B ORE AT RH WING OUTBOARD FLAP PER ER/A 633290-14. SECTION I LIMITED TO 6 MONTHS FROM 09APR26 ON FTN 1X6843. ER/A T O BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE COMPONENT FROM SERV ICE. ASSOCIATEDSDR DALA2026041302313Guide Vane · damagedUPON WALK AROUND NOTED BIRD STRIKE IN NR 2 ENGINE. CLEANED BIRD REMAINS FROM NBR 2 ENG. PERFORMED BIRD STRIKE INSPECTION PER AMM 05-51-14 AND 72-00-00. BIRD REMAINS DID NOT GO THROUGH CORE OF ENGINE. FOUND OUTLET GUIDE VANE ON NBR 2 ENG AT 2 O'CLOCK POSITION SDR DALA2026041202309Roller · looseL/G DOORS NOT CLOSED AFTER TAKEOFF FOLLOWED ECAM PROCEDURE. INSPECTED NLG AND FOUND UPLOCK ROLLER AND LOCKSTAY ASSY LOOSE AND OF OUT RIG. PERFORMED ADJUSTMENT OF NLG UPLOCK ROLLER AS PER A319 AMM 32-21. GEAR CYCLED SEVERAL TIMES W/ GOOD UP LOCK INDICATION ANDSDR DALA2026041202307Window Frame · crackedREQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, LH/RH CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. REPLACED CONTINUITY FITTINGS (LH P/N D5311107720200) (SDR DALA2026041202310Oxygen Mask · no testF/O O2 MASK FAILED TEST. SOUND OF O2 LEAKING AFTER TEST. RESEAT F/O'S O2 BOX DOORS. NOW OPS NORM PER A319 AMM 35-12-41. OKAY FOR SERVICE. (LP: 8590161) AIRCRAFT WAS GROUNDEDSDR DALA2026041202308Tire · failedBLOWN TIRE ON MAIN LANDING GEAR #4 WITH VISIBLE FLUID ON MAIN GEAR ASSEMBLY 7 WHEEL WELL. R&R #4 MLG WHEEL ASSY PER A320/319 AMM 32-41-11. #4 MLG WHEELASSY OK FOR CONT. SERVICE. (LP: 8676597) AIRCRAFT WAS GROUNDEDSDR DALA2026040902270Seat Track · corrodedPASSENGER CABIN AFT SECTION AT FR65, Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTSDR DALA2026040902269Seat Track · corrodedPASSENGER AFT CABIN AT FR 65, -Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 -Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040902268Seat Track · corrodedPASSENGER AFT CABIN AT FR66, Y=765 SEAT TRACK WITH CORROSION. C/A: REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 Y=765 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040902267Seat Track · corrodedPASSENGER AFT CABIN AT FR 65, -Y=765 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 -Y=765 WET -AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040802237Brake Sys · faultedDECLARED EMERGENCY INTO DTW DUE TO A BRAKES SYSTEM 1 FAULT ALONG WITH AN AUTO BRAKE FAULT AND A NORMAL BRAKES SERVO VALVE (18GG) FAULT. MLG #4 WHEEL FLAT SPOTTED AND FAILED DURING THE ROLL OUT. HYDRAULIC LEAK ABOVE THE MAIN LANDING GEAR WAS ALSO DISCOVERED. SDR DALA2026040902256Computer · faultyATO - AT THROTTLE UP DUE TO AN ELAC 2 PITCH FAULT. REPLACED ELAC 2. (LP: 8410558) AIRCRAFT WAS GROUNDEDSDR DALA2026040802238Engine · no discrepancySUCKED UP PLASTIC BAG IN NR 2 ENGINE PRIOR TO TAKE OFF ON RWY. INSPECTED NR 2 ENG IAW AMM 72-00. NO DAMAGE OR DEFECT WAS NOTED. ACFT OK FOR SVC. IAW AMM 05-51-19-200-001-A. MCC NOTIFIED. INSPECTED NR 2 ENG IAW AMM 05-51-19-200-001-A. NO DAMAGE OR DEFECT WAS NSDR DALA2026040802234Fitting · crackedCOCKPIT WINDSHEILD RIGHT CONTINUITY FITTING CRACKED AT UPPER OUTBOARD SIDE OF RADIUS. C/A: COMPLIED WITH PRI 633309-14AD, AWAITING FINAL ERA. (LP: 1532865) AIRCRAFT WAS GROUNDEDSDR DALA2026040802233Fitting · crackedCOCKPIT WINDSHEILD, LEFT CONTINUITY FITTING CRACKED AT UPPER OUTBOARD SIDE OF RADIUS. COMPLIED WITH PRI 633309-14AD, AWAITING FINAL ERA. (LP: 1532850) AIRCRAFT WAS GROUNDEDSDR DALA2026040802236Coffeemaker · damagedAFTER PUSHBACK AND ENGINE START AFT FA'S CALLED TO REPORT AN ELECTRICAL BURNING SMELL. NO VISIBLE SMOKE OR FIRE REPORTED. PASSENGER IN 29DEF ALSO REPORTED THE ODOR. WALK AFT NOTICED THE SMELL BEGINNING AROUND ROW 15. AND A STRONGER ODOR IN THE AFT GALLEY NEAR SDR DALA2026040802235Plenum · contaminatedOIL ODOR THROUGHOUT CABIN & COCKPIT ON ACFT ENTRY. APU LEAK CHK & INSP FOR CONTAMINATION C/W ON LOG 8044937, COMPLETES SMOKE AND FUMES WORKCARD 0550-2002 AND 0550- 2001 AND DUE TO PREVIOUS HIS ON NR 2 ENG. COMPLETED ENG 1 & 2 BOROSCOPE WORKCARD 7900-2001. REISDR DALA2026040802232Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT AT Y-1720MM BETWEEN FR 20 & FR 21, WEB AND SUPPORT ANGLES (2EA) WITH CORROSION. REPLACED WEB P/N 5311278520300 AND SUPPORT ANGLE P/N D5311278620101 IAW A319 SRM 53-11-14-07B FIG 007 ITEMS 186A AND 190 AND A319 SRM 51-72-911-001 PSDR DALA2026040902271Cover · missingCREW REPORTS FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. FWD TO CDL 27-00-16 "M" PROCEDURE C/W. WILL RQ ONCE EACH FLIGHT DAY REP CHK. DISP APPROVED. PLACARD INSTALLED. OK FOR SVC. "M" PROCEDURES REVERSED. INSATLLED FAIRING PIVOT COVER ON LEFT INBOARD MOVSDR DALA2026040602161Support Angle · corrodedLOWER FUSELAGE LT AVIONICS BAY, FR 13 BTWN STRINGERS 31L & 34L, VENTILATION DUCTS SUPPORT STRUCTURE INNER ANGLE WITH CORROSION. REPLACED ANGLE AT L/H AVIONICS COMPARTMENT FR 13 BETWEEN STGR 31L AND STGR 34L I.A.W A319 SRM 51-72-11-911- 001 REV. 155.00 DATED 1
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