Airbus A320-232
Service difficulty reports · 32,653
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 aircraft_model_key = 'A320232' 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 = 'A320232' 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 GTIA2022082636612None · corrodedCORROSION ON BORE OF LH ELEVATOR FITTING # 1, 2, 3 & 5. RAF 01-2803724-2 GENERATED-REPAIRED LH ELEVATOR HINGE FITTING #1, 2, 3 AND 5 IAW SRM 55-26-41-300-004. FIRTS INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS INTERVAL SDR GTIA2022082636611None · corrodedCORROSION ON BORE OF RH ELEVATOR FITTING #4. RAF-012803724-1 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #4 IAW SRM 55-26-41-300-005 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS INTERVAL IS 6 YEARS. INSPECTION TYSDR GTIA2022082636610None · corrodedCORROSION ON BORE OF LH ELEVATOR FITTING # 6. RAF 01-2803725-1 GENERATED-REPAIRED LH ELEVATOR HINGE FITTING #6 IAW SRM 55-26-41-300-006 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT SUBSEQUENT INSPECTIONS INTERVAL IS 6 YEARS INSPECTION TYSDR GTIA2022082636609None · noneLH ELEVATOR INBD & OUTB SERVO CONTROL ACTUATOR BUSHINGS REQUIRE REPLACEMENT-REPAIRED LH ELEVATOR INBD AND OUTBD SERVOCONTROL ACTUATOR FITTING, BUSHINGS REPLACED IAW TI 5513-1602 SRM 55-26-47-300-002 AND CMM 55-21-15-410-801-A01 INSPECTION THRESHOLD IS 6 YEARS SDR GTIA2022082636608None · corrodedCORROSION ON RH ELEVATOR FITTINGS 1, 2, 3 &5. RAF-01 2803723-1 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #1, 2, 3 AND 5 IAW SRM 55-26-41-300-004 FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS AT INTERVALS OF 6 YESDR GTIA2022082636607None · damagedRH SPOILER #3 CENTER HINGE FITTING HAS DAMAGED AND MIGRATING BUSHINGS. RAF-01 2803728-1 OPENED-REPAIRED SPOILER #3 CENTER HINGE FITTING IAW EA #57-0376-22 PANT #1 REV. #0 CAT C REPAIR INSPECTION TIME LINE 6 MONTHS ONE TIMESDR GTIA2022082636606None · noneRH ELEVATOR INBD & OUTBD SERVO CONTROL ACTUATOR BUSHINGS REQUIRE REPLACEMENT. RAF-01 2803727-1 GENERATED-REPAIRED RH ELEVATOR INBD AND OUTBD SERVOCONTROL ACTUATOR FITTING, BUSHINGS REPLACED IAW TI 5513-1602 SRM 55-26-47-300-002 AND CMM 55-21-15-410-801-A01 INSDR AALA202208265637None · noneAIRCRAFT WAS GROUNDED: DURING DESCENT JUST BEFORE GEAR EXT APPROXIMATELY 3000 FT, FLIGHT ATTENDANT REPORTED EXTREME AND PUNGENT CHEMICAL ODOR FROM TAIL TO ROW 16, APU WAS OFF NOT EXHAUST FUMES STILL PRESENT AT GATE WITH ENGINE OFF. **SUPPLEMENTAL REPORT WILL BSDR YENA2022082500818None · noneFLT#285, JFK-RDU. 'MULTIPLE INFLIGHT & FLIGHT DECK CREW REPORTED SMELLING "DIRTY SOCK AND BOX OF CRAYON" SMELL ON DESCENT AND AT THE GATE WITH AND WITHOUT APU BLEED ( APU BLEED AIR SUPPLY SYSTEM ).' (SUPPLEMENTAL TO FOLLOW)SDR YENA2022082500817A/C Pack · odorFLT#1693, FLL-NAS. 'ON TAKEOFF STRONG ALL ZONE SMELL AFTER ODOR ISOLATION PROCEDURE WITH PACK 1 OFF SMELL SEEMED TO DISSIPATE; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A (A), ISOLATED FAULT TO TYPE 5, (A), 1, C PER TSM 05-50-00-810-B. AIRCRAFT IS OKSDR AALA202208252778Lamp · inoperativeAIRCRAFT WAS NOT GROUNDED: CABIN ENTRY DOOR L1 EMERGENCY EXIT LIGHT NEEDS RELAMPED. RELAMPED L1 DOOR OVERHEAD EXIT LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR CALA2022082402155Frame · corrodedCOROSSION FOUND ON FRAME 67L CORRECTION , FRAME 70 ,SIX OCLOCK POSITION CORRECT LOCATION OF CORROSION IS FRAME 67- STRINGER 44 PER SRM DAMAGE IS AT STR 44 FR 67 53-41-12-75-A FIGURE C REMOVED 60 FASTNERS COMON TO F,S 67L IN THE 6 OCLOCK POSITION AND L-ANGLE UPSDR CALA2022082402154Stringer · corrodedCORROSION FOUND ON STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70. CORROSION LOCATION IS FRAME 67-STRINGER 27 PER SRM ENGINEERING UPDATE, IT IS STRG 26R 53-41-13-50-A. REMOVED STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70.AND ASSOCIATED FASTNER FWD OF F.S 70 STR SDR CALA2022082402162Spring · missingPDA 3 NOSE GEAR BYPASS LEVER ONE SPRING CLIP MISSING OUT OF TWO...SEE PHOTO PHOTO ADDED INSTALLED NEW SPRING CLIP AT NLG BYPASS LEVER...REF IPC 32-51-12-01E.SDR CALA2022082402160Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV ASDR CALA2022082402159Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA, FR16 RH SIDE; HOLE H4 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393810 TRE ENTRY LOG PAGE NUMBER 9334428. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H4 FWD GALLEY AREA I.A.W. EA 5310-06784 REV SDR CALA2022082402158Crossbeam · crackedCRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H3 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393809 PERFORMED SCEPTRE ENTRY LOG PAGE NUMBER 9334409. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H3 FWD GALLEY AREA I.A.W. EA 531SDR CALA2022082402157Floorbeam · elongatedELONGATED HOLE FLOOR BEAM -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA.SEE AEROMAN NON ROUTINE 2022-393856. INSTALLED NEW FLOOR BEAM Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, DWG #D53472201 AND DWG #D534722 00. PERFOMED SCPETRE ENTRY SDR CALA2022082402156Frame · corrodedFOUND CORROSION AT STR 26R END FITTING AT FRAME FR70. SEE ATTACHED PICTURES. PICS ADDED DAMAGE IS 9 INCHES LONG PROTEUDIMG FORWARD FROM FRAME 70 ON CORROSION LOCATION IS ON FRAME 67-STRINGER 27 SRM ENGINEERING UPDATE, IT IS STR 26R STRINGER 26 R/H 53-41-13-50SDR YENA2022082600821Thermostat · failedFLT#8097, JFK-DEN. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'SHORTLY AFTER T/O, WE RECEIVED A AIR ENG 1 BLEED FAULT. LEVELS AT 8,000 RAN QRC ECAM & QRH PROCEDURES. NEEDED TO AVOID ICING CONDITIONS. WHICH WE WERE UNABLE TO THUS FORCING US TO RETURN TO JFK.SDR YENA2022082600819None · failedFLT#1396, PDX-BOS. 'NOSE STEER FAULT FIRE SYSTEM FAUL GEAR FAULT FLT CTRL FAUL SLAT FAULT FLAP FAULT WOW FAULT EICAS MESSAGES APPEARED IN FLIGHT; REMOVED AND REPLACED LGSCU IAW AMP BD500-A-J32-61-01-01AAA-520A-A ALL OPS TESTS PASSED. A/C OK FOR CONTINUED SERVSDR AALA202208248759Door · lack of lubeAIRCRAFT WAS NOT GROUNDED: L1 DOOR DIFFICULT TO LOCK ONCE DOOR IS FLUSH , FLIGHT ATTENDANT COMPLAINS HANDLE DIFFICULT TO FULLY LOCK. MAINTENANCE CLEANED AND LUBRICATED L1 DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR YENA2022082600820Fire Bottle · failedFLT#28, MCO-EWR. 'DUE TO T/C A320-26-2300-710-003 FIRE BOTTLE REPLACEMENT REQUIRED; REMOVED AND REPLACED AFT FIRE CARGO BOTTLE IAW AMM 26-23-42 OPS AND LEAK CHECKS GOOD. OK FOR SERVICE.'SDR CALA2022082402168Stringer · corroded(SUPPORT TASK) AFT CARGO FR56 TO FR58 STRINGER 37R CORRODED.(REP LACE P/N: D5347552623000) REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53475580. E MP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34925.SDR YENA2022082300812Lug · brokenFLT#1176, KIN-FLL. 'EMER.LIGHT BETWEEN ROWS 18 AND19 IN CABIN INOP; FOUND GROUND WIRE TERMINAL LUG ON GROUND POST 7261VN BROKEN OFF. REPAIRED AND RE-TERMINATED TERMINAL LUG IAW ESPM 20-48-11. OPS CHECK EMERGENCY LIGHT GOOD IAW AMM33-51-00. OPS CHECK GOOD.'SDR GTIA2022082236600None · noneL1 AND R1 DOOR ASSIST BOTTLE REQ SVC-SVCD L1 AND R1 DOORS ASSIST BOTTLE IAW AMM 52-10-00SDR GTIA2022082236599Megaphone · inoperativeFWD MEGAPHONE INOP-R&R MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD. NO FURTHER DEFECTS NOTEDSDR YENA2022082200810A/C Pack · odorFLT#194, STI-EWR.' ON DESCENT BELOW 1000FT DIRTY SOCK SMELL, TURNED OFF PACK #1 AND THE SMELL DISSIPATED; COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION A(A) ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085B/ TSM 05-50-00-810-085D. A/C OK FORSDR CALA2022081902119Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30SDR CALA2022081902118Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4SDR CALA2022081902120Bottle · noneDOOR EMERGENCY ASSIST BOTTLE AT 2 L & 1R NEED SERVICING. SERVICED DOOR BOTTLES PER AMM 52-10-00-614-001-A.SDR GTIA2022082236597None · noneFUME OR VAPOR OR ODOR EMANATING FROM REAR GALLEY CAUSING CREW & PAX TO BECOME VERY SICK.-PERFORMED INSPECTION TO CHECK FOR ODORS, VAPOR OK FUMES ISOLATED , NO ODORS OR FUMES NOTED. ALL PERFORMED IAW TSN 05-50-00-810-831-A. AC OK FOR SERVICE. MOC # 109053. Q6TRSDR GTIA2022082236596None · fault message"ENG 1 COMPRESSOR VANE MESSAGE IN FLIGHT-PER TSM 75-30-00-810-847-A R+R 2.5 LPC BLEED - MASTER ACTUATOR ON ENG#1 IAW AMM 75-31-42 PB401, OPS TEST GOOD, PER HIGH POWER ASSURANCE TEST REF AMM 71-00-00
TORQUE WRENCH USED: NK1205 / DUE: 23-DEC-22"SDR YENA2022090100847Autopilot Sys · faultyFLT#767, MCO-PSE. (AIRCRAFT DIVERTED TO SJU) 'NAV LS TUNING DISAGREE IN FLIGHT W/ AUTO PILOT #1 DISCONNECT & MAP NOT AVAILABLE ON CAPT'S ND. RAN QRH & RESET DID NOT RESET. MCDU ALSO KEPT INTERMITTENTLY PAUSING WITH A "PLEASE WAIT" MESSAGE. OFF-SIDE FM CONTROL SDR CALA2022081902128Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293704 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOTSDR CALA2022081902127Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293703 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOTSDR CALA2022081902126Frame · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SID E CRACK LENGTH 0.080 INCHES APPROX. CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B". SEE AEROMAN NON ROUTINE 2022-293701SDR CALA2022081902125Frame · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SID E. CRACK LENGTH 0.100 INCHES APPROX.SEE AEROMAN NON ROUTINE 2022 -293702 CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B"SDR CALA2022081902124Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-343198 REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA:L=0.604 IN W=0.485 IN;D=0.079 IN, NOMINAL THICKNESS= SILL PERFORMED VISUAL ISDR CALA2022081902123Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359891. REMOVED AND REPLACED SEAT TRACK Y765 LOC.BTW FR12 TO FR24 AT FWD ION ON AREA AND NOT FOUND ADDITIONAL DAMAGE I.A.W. NTM 51-90- 2023. GALLEY AREA IN PASSENSDR AALA202208185522Life Line · missingAIRCRAFT WAS NOT GROUNDED: LEFT SIDE OVER WING ESCAPE LIFE LINE MISSING. REPLACED OVER WING ESCAPE LIFE LINE PER MM 25-60-00SDR YENA2022081800809None · noneFLT#2822, PBI-BOS. ' FUMES EXPERIENCED ON DESCENT THROUGH 12.000'. NO IMPROVEMENT W/PACK 1 OFF. IMPROVEMENT W/PACK 2 OFF; PREFORMED INFO NOTICE 2017-T015, SECTION A (A) ISOLATED FAULT TO TYPE 10, (A) 1 C PER TSM 05-50-00-810-085-B (D) ACFT OK FOR SERVICE NO SSDR CALA2022081702115Light · inoperativeCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT EMERGENCY BATTERY FAILED CAP TEST REMOVED AND REPLACED AFT EMERGENCY BATTERY. OPS CHECK GOODSDR CALA2022081702112Frame · crackedCRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPASDR GTIA2022081836592Skin · dentedREF LOG PAGE 2740316-1 MWI LWR NOSE DENT RH SIDE. RAF-01 2897215-01 HAS BEEN GENERATED.-REPAIRED FUSELAGE SKIN RH LOWER BETWEEN FR 1-2 PER A320 SRM 53-11-11-300-073. THIS REPAIR IS CAT B REQ REINSPECT AT 60,000FC 120,000FH FROM EMBODIMENT PER A320 SRM 53-11-11SDR YENA2022081800808Unknown · odorFLT#1179, JFK-MBJ. 'REPEAT ITEM: 3430029 3466939 DIRTY SOCK SMELL UPON ARRIVAL WHEN APU SUPPLYING BLEED AIR. THROUGHOUT CABIN AND COCKPIT. SMELL INITIATED WHEN APU BLEED SELECTED ON DURING TAXI IN. THE CABIN SMELL WAS REPORTED STRONG AT THIS POINT AND GETTING SDR YENA2022081800807None · noneFLT#362, BGI-JFK. 'FOUND L2 DOOR EMERGENCY SLIDE MOUNTING BOLT RELEASED WHEN FA REPORT BUSTLE NOT INSTALLED PROPERLY; PERFORMED GVI OF L2 DOOR SLIDE. ALL CONNECTORS AND FWD MOUNT BOLT INSTALLED. AFT MOUNTING BOLT FOUND DETACHED FROM PULL SPRING. REMOVED AND RESDR AALA202208162950Wire Harness · brokenAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT ROW 4ABC INOPERATIVE. MAINTENANCE FOUND WIRE HARNESS BROKEN AND REPLACED IT PER AMM 33-51-19. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.SDR CALA2022081602077Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.THIS PERFORMED PERMANET REPAIR (REPLACED)CONTINUITY FITTING RH SIDE. ROTO TEST INSPECTION OF THE CONTINUITY FITTINGS TO SPLICE FITTINGS 3 FASTENER HOLES.SDR CALA2022081602076Fitting · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SIDE. CRACK LENGTH 0.100 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL RH SIDE.
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