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 CALA2022081602075Fitting · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SIDE CRACK LENGTH 0.080 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL LH SIDE.SDR CALA2022081602074Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.PERFORMED PERMANENT REPAIR (REPLACED)CONTINUITY FITTING LH SIDE.SDR CALA2022081602073Floorbeam · elongatedELONGATED HOLE FLOORBEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA. REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA.SDR CALA2022081602072Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA.SDR AALA202208170792Bulb · inoperativeAIRCRAFT WAS GROUNDED: DURING EMERGENCY LIGHTING SYSTEM TEST, A FORWARD LEFT EMERGENCY POWER SUPPLY INTERNAL LOAD FAULT MESSAGE DISPLAYED. MAINTENANCE FOUND INOPERATIVE BULBS ON THE FORWARD-FACING EXIT SIGN AND REPLACED THEM. A SATISFACTORY OPERATIONAL CHECK WSDR AALA202208175884Bulb · inoperativeAIRCRAFT WAS GROUNDED: DURING EMERGENCY LIGHTING SYSTEM TEST, A EMERGENCY LEFT EMERGENCY POWER SUPPLY INTERNAL LOAD FAULT MESSAGE DISPLAYED. MAINTENANCE FOUND INOPERATIVE BULBS ON THE MID CABIN FORWARD-FACING EXIT SIGN AND REPLACED THEM. A SATISFACTORY OPERATISDR AALA202208168304Battery · inoperativeAIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT FLOOR ROW 11 ABC HAS BATTERY FAULT WHEN TESTED. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY AT FLOOR ROW 11 ABC. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS. REFERENCE AMM 33-51-38.SDR CALA2022081602099Stringer · corroded(A3NB-05-3-6029) AFT CARGO, FRAME 61-62, STR 37R HAS CORROSION.( ) STRINGER OUT OF LIMITS IAW SRM 53-41-13, REPLACED WITH NEW STRIN GER P/N: D5347048700000, IAW SRM 51-72-11-911-001. INSTALLED IAW SRM 51-42-11. EMP# V936191 WORK ACCOMPLISHED AT ST ENGINEERING SDR AALA202208158544Wire Harness · defectiveAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT SEAT 11ABC. REPLACED SIDE WALL CONNECTOR ELECTRICAL HARNESS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.SDR CALA2022081602093Floorbeam · corrodedCORROSION FLOOR BEAM +Y765 LOCATED FR68 TO FR70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM Y765 AND FASTENERS LOC FR66 TO F P/N: 20915A22 S/N: 003591 DUE DATE 30-MAY-2023 R70 AT AFT GALLEY AREA IAW SRM A320 51-42-11, DWG D53472000, DWG 53472092 AND DWGSDR GTIA2022081536587Megaphone · inoperativeFWD MEGAPHONE IN-OP-R&R FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOODSDR YENA2022081500795Door · leakingFLT#1411, FLL-AUA. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) 'LOUD HISSING NOISE AND POP L1 DOOR ON ASCENT; ACCOMPLISHED PRESSURIZATION TEST FOR SPECIFIC AREA IAW AMM: 05-53-00. FOCUS AREA L1 DOOR & FWD ACCESS DOORS. NO LEAKS OR NOISES WERE NOTED. AS PRECASDR CALA2022081602069Doubler · unserviceableDURING HMV VISIT REMOVED AND REPLACED DOUBLER REPAIR AT FR52-53 STR 24-26L CAT B MAJOR REPAIR IAW SRM 53-41-11-300-019. LOG CREATED FOR SRI DIP PURPOSE. METHOD OF ULTRASOUND/HFEC SEE SRI FIG. 001 FOR SPECIFIC NTM CHAPTERS. INSPECTIONS DUE AFTER REPAIR EMBODIMESDR CALA2022081602063Stringer · corrodedA3NB-53-4-6175 AFT CARGO COMP STR 41R HAS CORROSION BET FR58-64.REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53470332. E MO# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34948.SDR CALA2022081602067Frame · corrodedDURING HMV VISIT AFT CARGO COMPT. PREVIOUS REPAIR HAS CORROSION BETWEEN FR 63-64 & STR. 41L-42L, NEW REPAIR ACCOMPLISHED PER SRM 53-00-11-300-029. LOG CREATED FOR DIP TO BE ACCOMPLISHED PER SRI 53-00-11-205-017. SUBSEQUENT INSPECTIONS AT INTERVALS OF 2200FC/44SDR CALA2022081602066Frame · corrodedAFT CARGO, FRAME 60-62, STR40R HAS CORROSION 20 SRM 51-72-11-911 TREATED AND PRIMED IAW A320 SRM 51-21-11/001 ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR@ APPLIED TOP COAT IAW A320 SRM 51-23-11/001. EMP# V935833 WORK # 34536. REPAIRED STRINSDR CALA2022081602065Stringer · corrodedDURING HMV VISIT AFT BULK CGO. STR FOUND CORRODED @ FR 60-62 STR. 40R. STRINGER REPAIR WAS ACCOMPLISHED PER SRM 53-00-13-300-001 FIG. 001. LOG CREATED FOR INSPECTION TRESHOLD DIP. INTERVALS: TBD, METHOD: TBD, IAW SRI 53-00-13-205-001 TABLE 004. INSPECTION TRESDR GTIA2022081536584Oxygen Mask · leaking"FO OXYGEN MASK HAD A CONTINOUS LEAK WHEN STOWED -R/R OF THE FO,S 02 MASK DUE TO LEAKING IAW AMM 35-12-41 LEAK CK GOOD SEVICED THE CREW 02 IAW GMM 3-12-7 AND AMM 35-12-41. OPS CHECK GOOD A/C OK FOR SERVICE AT THIS TIME
"SDR GTIA2022081536583None · noneDURING WEEKLY CHECK FOUND R2 DOOR ASSIST REQ SERVICE-SERVICED R2 DOOR ASSIST IAW AMM 52-10-00SDR GTIA2022081536582None · noneVENT AVNCS SYSTEM FAULT ( SKIN AIR OUTLET VALVE )-PERFORMED AEVC TEST IAW AMM 21-26-00 OPS CHECK GOOD AT THIS TIME DMI # 2909979-1 REMAINS OPEN A/C OK FOR CONT SERVICESDR AALA202208153856Door Latch · unsecureAIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE SECURED LAVATORY DOOR LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR CALA2022081202059Relay · inoperativeAUTO FLT ''A-THR OFF''DISPLAYED ON UPPER ECAM SCREEN. AUTO THRUST FAIL TROUBLESHOT PER TSM 22-31-00-810-812-A. PERFORMED GROUND SCAN OF THE AFS AND REPLACED RELAYS 17CA1, 17CA2, 18CA1, 18CA2, 5CA1, AND 5CA2. ENG 2 EEC WAS ALSO REPLACED FOR ANOTHER PROBLEM, SEESDR CALA2022081202057Fastener · missingFASTENER MISSISNG INBOARD SIDE NBR 2 PYLON REPLACED MISSING SCREW ON INBD SIDE OF #2 PYLON AS REQUIREDSDR CALA2022081202056Seat 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 CALA2022081202055Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359890. REMOVED AND REPLACED SEAT TRACK-Y1292 LOC. BTW FR12 TO FR24 AT DITIONAL DAMAGE I.A.W. NTM 51-90-00. PERFORMED SCEPTRE ENTRY INE 2022-359890. FWD GALLEY ASDR CALA2022081202054Stringer · corrodedA3NB-53-4-6175 AFT CARGO COMP STR 41R HAS CORROSION BET FR58-64. () REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53470332. E MO# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34948.SDR CALA2022081202053Stringer · 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 YENA2022081600803Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE AREA CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH APROXIN COCKPIT(1EA); REMOVED AND REPLACED CONTINUITY FITTING LH SIDE ON FRAME 2 WINDSHIELD CENTER POST LOWER NOSDR YENA2022081600802Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH APPROX IN COCKPIT(1EA); REMOVED AND REPLACED CONTINUITY FITTING RH SIDE ON FRAME 2 WINDSHIELD CENTER POST LOWER SDR YENA2022081600801Frame · crackedDURING HEAVY MAINTENANCE: CRACK (2EA): FR16LH DOOR STOP 7 INBD. UPPER HOLE (1 O'CLOCK - 0.148") AND INBD. LOWER HOLE (1 O'CLOCK - 0.075"); REF AEROMAN NR 2022-376934 AND 2022-376938 W/O: 2022 174/1: REMOVED AND REPLACED INTERCOSTAL AT FR16 LH SIDE DOOR STOP 7 SDR YENA2022081600800Intercostal · crackedDURING HEAVY MAINTENANCE: CRACK (2EA): FR 16 RH DOOR STOP 7 INBD. UPPER HOLE (9 O'CLOCK - 0.112") AND INBD. LOWER HOLE (9 O'CLOCK - 0.070"); REF AEROMAN NR 2022-376943 AND 2022-376944 W/O: 2022 174/1: REMOVED AND REPLACED INTERCOSTAL AT FR16 RH SIDE DOOR STOP SDR YENA2022081600799Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 16 RH / DOUBLE JOGGLE AREA / HOLES 4 & 6 / CRACK DAMAGE – TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022081600798Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 16 LH / DOUBLE JOGGLE AREA. HOLES 6, 8, B & C / CRACK DAMAGE. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022081200792Pump · failedFLT#2319, FLL- SLC. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO FLL AND DECLARED AN EMERGENCY) 'AFTER T/O HYD YELLOW RSVR LOW LEVEL - RSVR COMPLETELY EMPTIED TO CAUSE YELLOW SYSTEM FAILURE; REMOVED AND REPLACED #2 ENG EDP IAW AMM 29-13-51-000-010-A. OPS CHECK GOODSDR AALA202208120411Power Supply · noneAIRCRAFT WAS NOT GROUNDED: FORWARD LEFT EMERGENCY POWER SUPPLY COM FAULT DISPLAYED. REPLACED EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.SDR YENA2022081200791A/C Pack · dirtyFLT#1709, FLL-PAP. (AIRCRAFT PERFORMED AN AIR TURN BACK TO FLL) ' DURING CLIMB OUT AIRFLOW FROM ALL COCKPIT SOURCES STOPPED COMPLETELY. COCKPIT TEMP ROSE QUICKLY TO AN UNBEARABLE LEVEL. FLOW RETURNED APPROXIMATELY 5-7 MINUTES LATER.' (SUPPLEMENTAL TO FOLLOW)SDR CALA2022081202040Skin · noneDURING HMV VISIT FUSELAGE DOUBLER REPAIR ACCOMPLISHED AT FR23 STR10-11L IAW SRM 53-11-11-300-041 CAT B MAJOR REPAIR WITH RE-INSPECTIONS PER SRI ZONE 1 TABLE 001. "NOT APPLICABLE" SEE NOTE 2. RE-INSPECTION METHOD "NOT CASE OF A/CLIFE EXXTENSION MORE THAN 60000FSDR CALA2022081202039Skin · noneDURING HMV VISIT A DOUBLER REPAIR WAS ACCOMPLISHED AT FR6-7 LHS NEAR TAT SENSOR IAW SRM 53-11-11-300-052 CAT B MAJOR REPAIR REQUIRES DIP FOR REPETITIVE INSPECTIONS IAW SRI 53-11-11-205-051 ZONE A. REF. SRI 53-11-11-205-051 TABLE 001 ZONE A. FLOW CHART 3. INSPSDR YENA2022081200794A/C Pack · dirtyFLT#321, BOS-PBI. 'FUMES THROUGH 6000FT GOT WORSE ON GROUND; INSPECTED APU AND FOUND EVIDENCE OF OIL ON INTAKE DIFFUSER. REMOVED LOAD COMPRESSOR PLUG IAW AMM 49-20-00, AND FOUND OIL. REINSTALLED PLUG AS REQUIRED. CLEANED AREA W/ EVIDENCE OF OIL PER AMM 49-20-0SDR CALA2022081202037Frame · corrodedCORROSION LOWER SILL FR 66 RH SIDE AT AFT GALLEY AREA, SEE AEROMAN NON ROUTINE 2022-293845 PERFORMED PERMANENT REPAIR ON LOWER SILL RH SIDE AT AFT GALLEY L=2.755IN, W=1.984IN, D=0.087IN, EDDY CURRENT DONE ON REWORKED ULTRASONIC THICKSNESS MEASURES ON REWORKED SDR CALA2022081002009Sensor · faulty**RTBL** LOW SPEED RTO ENGINE 1 ACCELERATION ABNORMAL TROUBLESHOOT NO FAILURE MESSAGES ON MAINTENANCE POST FLIGHT REPORT AFFILIATED WITH NUMBER 1 ENGINE. GROUND SCANNING AND LAST LEG REPORT SHOWS NO FAULT. SCHEDULED MAINTENANCE REPORT HAS P2 T2/ ADIRS1/2/EESDR AALA202208110730Bulb · noneAIRCRAFT WAS NOT GROUNDED: DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND FAULT MESSAGE ON FLIGHT ATTENDANT PANEL EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD FORWARD LEFT AND FAULT MESSAGE EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD EMERGENCY RIGHT / EMERGENCY LESDR AALA202208116627Bulb · noneAIRCRAFT WAS NOT GROUNDED: DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND FAULT MESSAGE ON FLIGHT ATTENDANT PANEL EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD FORWARD LEFT AND FAULT MESSAGE EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD EMERGENCY RIGHT / EMERGENCY LESDR AALA202208115376Bulb · noneAIRCRAFT WAS NOT GROUNDED: DURING PERIODIC SERVICE CHECK MAINTENANCE FOUND FAULT MESSAGE ON FLIGHT ATTENDANT PANEL EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD FORWARD LEFT AND FAULT MESSAGE EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD EMERGENCY RIGHT / EMERGENCY LESDR CALA2022081002033Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR68 LEVEL STRG23L IN PASSENGER CABIN (1 EA) REMOVED AND REPLACED FLOOR STRUCTURE ANGLE AND FASTENERS AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED LOCATED FR68 AT LEVEL STR 23L IN PASSENGER CABIN IAW A320 SCEPTRE SDR CALA2022081002032Dummy Rail · corrodedCORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA SDR CALA2022081002022Engine · fireDURING HIGH POWER RUN OBSERVED #2 ENGINE FIRE WARNING INDICATION ALONG WITH CONTROL TOWER VISUAL CONFIRMATION. SHUTOFF FUEL CONTROL LEVER AND DEPLOYED #2 ENGINE FIRE SWITCH. CRANKED ENGINE UNTIL FIRE WARNING EXTINGUISHED. FIRE BOTTLES WERE NOT DEPLOYED. VISUALSDR CALA2022081002021Doubler · inadequateDURING HMV VISIT FOUND DOUBLER LOCATED AT FR28-29 STR 38L-39L THAT DOES NOT COMPLY WITH CURRENT SRM. ACCOMPLISHED REPAIR PER SRM 53-21-11-300-090 AND 51-42-11. LOG CREATED FOR DIP REPETITIVE INSPECTION REQUIREMENTS. INSPECTION IAW SRI 53-21-11-205-071 ZONE A.SDR CALA2022081002012Stringer · corroded(A3NB-51-4-6001) AFTER REMOVAL OF DOUBLER FR59 ST36R-38R FOUND S TR38R FR58-62 AND COUPLING FR58 HAS SIGNS OF CORRSION. REMOVED AND REPLACED STRINGER 38R FR58 TO FR64 IAW SRM 51-42-11, DWG D53470339. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OSDR YENA2022080900785Light · inoperativeDURING HEAVY MAINTENANCE: EMERGENCY LIGHT TEST DID NOT PASS TEST; REF AE NR 2022-385859, W/O 2022-165/1. FOUND R1 DOOR SLIDE AT FAULT. REMOVED AND REPLACED DOOR SLIDE IAW AMM 25-62-44-000-804-A AND 25-62-44-400-803-A.
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