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 YENA2024071100958Intercostal · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL LAYER LOC DOOR STOP 7 FR16RH HOL E H3. CRACK DEPTH 0.063 INCH AND DIRECTION 12 OCLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00024) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR SDR YENA2024071100957Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN BTW FR 12 TO FR 14 LOWER AREA ON LH AVIONIC COMPARTMENT(CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00047) REF AEROMAN N/R 2024-29895, PERFORMED REPAIR TO CORROSION AT THE FWD FUSELAGE LOWER SKIN AT NSDR YENA2024071100956Fuel Tank · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASS ENGER CABIN; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00050) REF AEROMAN N/R 2024-298788, REMOVED CORROSION MECHANICALLY LOCATED ON UPPER SKIN BTW FR41/FR42 LH SIDE SDR YENA2024071100955Shear Web · crackedDURING HEAVY MAINTENANCE: CRACKED SHEAR WEB LOCATED AT FR 71 BTW STR 27R AND 32R IN THE THS COMPARTMENT; REF AEROMAN WO# 2024-177/1 NR# 2024-298723 FOR ALL WORK ACCOMPLISHED REMOVED DAMAGED SHEAR WEB FABRICATED AND INSTALLED NEW WEB IAW A320 SRM 51-41-2, SRM 5SDR YENA2024071100954Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON FITTING BTW FR13- FR14 INTERNAL STRUCTURE LOWER AREA ON LH AVIONICS COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00051) REF AEROMAN NR 2024-298984 WO# 2024-177/1 REMOVED AND REPLACED FITTING AND FASTSDR YENA2024071100953Skin · corrodedDURING HEAVY MAINTENANCE: FUSELAGE/ FWD LOWER SKIN AT NLG/ FR12-13 LH LOWER STGR AT Y520/ CORROSION- TEMPORARY REPAIR (A24-745-01) (CONSIDERED A MAJOR REPAIR)SDR CALA2024070900177Backlight · inoperativeTRANSPONDER BACKLIGHT NOT WORKING. REPLACED ATC CONTROL PNL, REF AMM 34-52-12, CONTROLER OPS CKED OK, BUT LIGHT INOP ON WINDOW THAT SHOWS NUMBER, NINTIME TO TROUBLESHOOT, REQUESTING MEL 3310A. OK TO MEL COMPLIED WITH MEL 3310A. OPS CHECK OF INTEGRAL LIGHTINGSDR YENA2024070500940Engine · failedFLT#153, JFK- PBI. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) .'AFTER T/O A/C HAD A SIGNIFICANT VIBRATION. WHILE TROUBLESHOOTING TOWER ADVISED SEVERAL A/C SAW DEBRIS COME OFF OUR A/C. WE RETURNED AND DIDAN OVERWEIGHT LANDING; FOUND #1 ENG DAMAGE CAUSED BY BISDR AALA202407051973Indicator · false activationAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED AN ENGINE # 2, AGENT 1 DISCHARGE LIGHT ILLUMINATED INFLIGHT. MAINTENANCE FOUND NO INDICATION OF FIRE BOTTLE DISCHARGE OR FAULT ON ENGINE AND APU FIRE PANEL. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL CHESDR CALA2024070500145Thermostat · intermittentAIR ENG2 BLEED ABNORM PR PFR AND BMC 2 BITE SHOWING: PRESS REG-V 4001HA2 OR SOL 10HA2 OR SENSE LINE. T/S REF TSM 36-11-00-810-810-A. PERFORMED LEAK CHECK ON THE #2 ENG PRV BRAIDED SENSE LINE AND RIGID LINES. NO LEAKS NOTED. PERFORMED HEALTH CHECK ON PRV 4001HASDR YENA2024070300931Girt Bar · failedFLT#613, HPN-FLL. 'L2 DOOR GIRT BAR STAYS ENGAGED; REMOVED AND REPLACED L2 DOOR GIRT BAR IAW AMM 52-13-22. OPS CHECK GOOD.'SDR YENA2024070800959Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 7 O'CLOCK AND CRACK DEPTH IS 0.092 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00026) REF AEROMAN WO 2024 1SDR YENA2024070800958Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.076 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00027) REF AEROMAN WO 2024 1SDR YENA2024070800957Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH LAYER FROM LOWER INBOARD HOLE OF Ñ1 DOOR STOP FITTING AT AFT GALLEY AREA (CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.076 INCH); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00027) REF AEROMAN WO 2024 1SDR YENA2024070800956Intercostal · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON INTERCOSTAL FROM LOWER INBOARD HOLE COMMON TO N7 DOOR STOP FITTING AND FR16LH LEVEL AT FWD GALLEY AREA; (RESOLVED ON W/O: 1301763 TASKCARD: NR-00029) REF AEROMAN WO 2024 159/1 NR 2024-277092, REMOVED AND REPLACED ISDR YENA2024070800955Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE CROSSBEAM SPLICING AREA, AT OPEN FASTENER HOLE H2, CRACK DIRECTION IS 1 OCLOCK, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1301763 TASKCARD: NR-00046) REF AEROMAN WO 2024 159/1 NR 2024-277058, PESDR YENA2024070800954Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE UPPER DOUBLE JOGGLE AREA, AT OPEN FASTENER HOLE C, CRACK DIRECTION IS 3 OCLOCK, CONFIRM INDICATION USIN G BOROSCOPE VIEW AS PER NTM 51-90-00, AT FWD GALLEY AREA (1 EA); (RESOLVED ON W/O: 1301763 TASDR YENA2024070800953Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FACE OF FR35 AT LEVEL OF STGR 30L. CRACK LENGTH 1.5 INCH APPROX; (RESOLVED ON W/O: 1301763 TASKCARD: NR-00052) REF AEROMAN WO 2024 159/1 NR 2024-277195 PERFORMED REPAIR AT FRAME 35 BTW STGR 30L TO STGR 31SDR YENA2024070800952Fitting · unknownDURING HEAVY MAINTENANCE: REMOVE AND REPLACE CONTINUITY FITTINGS LH AND RH SIDE LOCATED BTW FRAM E 1 AND FRAME 2 IN COCKPIT DUE TO AIRBUS DOSSIER REFERENCE 81254114; (RESOLVED ON W/O: 1301763 TASKCARD: NR-00053) REF AEROMAN WO 2024 159/1 NR 2024-277245 REMOVE SDR YENA2024070800951Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHME NT, INTERNAL AREA, LH SIDE VERTICAL FLANGE, FROM UPPER TENSION BOLT, C RACK DIRECTION IS 2 OCLOCK, CRACK LENGTH IS 0.120 INCH APPROX., IN COC KPIT (1 EA); (RESOLVESDR YENA2024070800950Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON SPIGOT FITTING PYLON LH; REF AEROMAN WO 2024 159/1 2024-277250, REMOVED AND REPLACED SPIGOT ON PYLON LH IAW A320 SRM 54-51-12-300-002. THIS REPAIR IS CATEGORY A. NO REQUIRED FURTHER INSPECTION TOOL USED CALIPER P/N 500-19SDR YENA2024070800949Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON SPIGOT FITTING PYLON RH; REF AEROMAN WO 2024 159/1 NR 2024-277249, REMOVED AND REPLACED SPIGOT FITTING ON PYLON RH IAW A320 SRM 54-51-12-300-002 THIS REPAIR IS CATEGORY A NO REQUIRED FURTHER INSPECTION. TOOL USED CALIPER SDR YENA2024070800948Pressure Blkhd · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE BULKHEAD @ FR 35 & STR30L / CRACKS AT FASTENER HOLES – TIME LIMITED REPAIR (A24-725-01) (CONSIDERED A MAJOR REPAIR)SDR YENA2024070800947Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FORWARD FUSELAGE / WINDSHIELD FRAME / CENTER POST LH UPPER FASTENERS AREA / CRACK - PERMANENT REPAIR (A24-716-01) (CONSIDERED A MAJOR REPAIR)SDR CALA2024070501963Fitting · crackedRH MLG DOOR ACTUATOR FWD FITTING HORIZONTAL FLANGE HAS GOUGE ADJACENT TO OB FASTENER. REMOVED AND REPLACED RH MLG DOOR ACTUATOR FWD FITTING HINGE FITT ING AND CONNECTING PLATE IAW AIRBUS REPAIR DWG R533-70501 ISSUE F AND R533-70500 ISSUE F, AS DIRECTED BY ECSDR AALA202407031145Proximity Sensor · dirtyAIRCRAFT WAS NOT GROUNDED: CABIN DOOR R1 SHOWED OPEN WITH DOOR ARMED AT SHUTDOWN. CLEANED R1 DOOR PROXIMITY SENSOR.SDR GTIA2024070238213Ecs · contaminated"FA'S SMELLED BURNING SMELL AROUND ROW 7,8,9-PERFORMED TSM 05-50-00-810-831-A FOR ELECTRICAL BURNING SMELL. PERFORMED OPS CHECK AND VISUAL AND PHYSICAL ISNP OF THE RECIRC FANS IAW AMM 21-21-00. OPS CHECK GOOD. PERFORMED IDLE RUN OF ENG 1 & 2 IAW AMM 71-00-00SDR GTIA2024070238209Unknown · fumesFUME EVENT ON ARRIVAL DESCENDING THROUGH 4,000 FEET.-PERFORMED TSM 05-50-810-831. NO DEFECTS NOTED. A/C GOOD FOR CONTINUED SERVICE.SDR GTIA2024070238208Megaphone · inoperativeAFT MEGA PHONE INOP-R/R AFT MEGA PHONE IAW A320 EMER-EQUIP DRAWING.SDR CALA2024071602044Skin · dentedBIRD STRIKE. INSPECTION REQUIRED PER AMM. HIT UNDER CAPT NOSE UNDRSCREEN AT 210KTS 7K FT. FWD DENT EDGE IS X = 13" AND Y = 10" FROM THE CENTER AREA OF THE STATIC PROBE PORT CLOSE UP DENTS ARE ABOUT 6 IN LONG 3IN WIDE 1/4 DEEP AND 5 IN APART DENT 1 FWD DENT SDR AALA202407056384Proximity Sensor · false indicationAIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT PASSENGER COMPARTMENT EMERGENCY EXIT ECAM FAULT MESSAGE. MAINTENANCE REPLACED THE RIGHT HAND AFT OVERWING EMERGENCY EXIT PROXIMITY DETECTOR SWITCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-11.SDR AALA202407036384Warning Message · illuminatedAIRCRAFT WAS NOT GROUNDED: RIGHT HAND AFT PASSENGER COMPARTMENT EMERGENCY EXIT ECAM FAULT MESSAGE. (OPEN)SDR YENA2024070100925Computer · failedFLT#2065, BOS-RSW. (AIRCRAFT DIVERTED TO RIC). 'ELAC 2 FAULT IN FLT ALONG WITH BURNING ODOR . DID NOT RESET AND BURNING ODOR STAYED; REMOVED AND REPLACED ELAC 2 COMPUTER PER AMM 27-93-34. OPS CHECK GOOD AT THIS TIME REF LP 4048103-1 9PER TSM 05-50-00-810-831-ASDR CALA2024070101930Anti-Ice Valve · faultedREPLACE THE LT PACK ANTI-ICE VALVE IAW AMM 21-61-41 PB.401 DUE TO PACK OUTPUT TEMP INDICATION ALWAYS SHOWING BELOW FREEZING.ALSO PURGE THE REMOVED SENSE LINES USING COMPRESSED AIR TO REMOVE POSSIBLE DEBRIS OR BLOCKAGE. REMOVED AND REPLACED LH PAC ANTI-ICE VALSDR CALA2024070900178Anti-Ice Valve · faultedREPLACED LT PACK ANTI-ICE VALVE IAW AMM 21-61-41 PB.401, DUE TO PACK OUTPUT TEMP INDICATION ALWAYS SHOWING BELOW FREEZING. REMOVED AND REPLACED LH PAC ANTI-ICE VALVE REF AMM 21-61-41-400-001-A. PURGED THE REMOVED SENSE LINES, ACCOMPLISHED PACK OPS TEST IAW SDR AALA202407018671Bearing · lack of lubeAIRCRAFT WAS IN BASE MAINTENANCE: DOOR L1 HARD TO CLOSE. PERFORMED LUBRICATION OF HINGE ARM SUPPORT FITTING BEARINGS ON PASSENGER CREW DOOR 831.SDR AALA202407019105Buffer · out of adjustAIRCRAFT WAS IN BASE MAINTENANCE: L1 DOOR GUST LOCK DOES NOT ENGAGE. PERFORMED ADJUSTMENT OF BUFFER ON PASSENGER CREW DOOR 831.SDR GTIA2024062938200Door Sill · corrodedINSIDE CABIN AFT WET AREA R2 DOOR SILL BEAM HAS LIGHT CORROSION AROUND FASTENER HOLE RAF-01 CREATED -ACCOMPLISHED REPAIR ON HAECO S/O 12202 OPS 26308-CAT A REPAIR NO RE-INSPECTSDR GTIA2024062938199Skin · dentedLEFT SIDE OF FUSELAGE DENT JUST FORWARD OF FRAME 3 JUST BELOW LEFT SIDE STRINGER. RAF-01 CREATED-ACCOMPLISHED INSPECTION SOLUTION PER AIRBUS RDAF 81417892/002/2024 A. NO ADDITIONAL REQUIREMENTS. CAT A PERMANENT REPAIR PER AIRBUS RDAF 8141792/002/2024 A PAGE 2 SDR YENA2024062700917Landing Gear · malfunctionedFLT#305, EWR- FLL. (AIRCRAFT PERFORMED AN AIR TURN BACK). 'DURING CLIMB OUT AT 3000' LAND GEAR DOOR (NOSE) COULD BE HEARD BANGING / CLOSING REPEATEDLY NO ECAM; PERFORMED CLEARANCE CHECK ON NLG DOORS ALL WITHIN LIMITS INSPECTED ALL AVIONICS COMPARTMENT FOR POSSSDR YENA2024062700916Wire · damagedFLT#745, JFK-PSE. ' DOOR 2L EXIT LIGHTS INOP; PERFORMED SPLICE REPAIR APPROX 12 INCHES FROM 45WL 2 EXIT DOOR SIGN WIRE -A IAW AMM ESPM 20-53-21-02 AND REPLACED TERMINAL WIRE 1 IAW ESPM 20-56-22. OPS CHECK OF 2L EXIT DOOR EMERGENCY LIGHT OK 33-51-00. MDDR CLEARSDR AALA202406269598Girt Bar · bentAIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT THE 2R DOOR SLIDE ARMING BAR BENT. MAINTENANCE FOUND THE FLOOR ARMING INDICATOR OUT OF ALIGNMENT AND RE-ALIGNED IT PER AMM 52-10-00. A SATISFACORY OPERATIONAL CHECK WAS ACCOMPLISHED.SDR GTIA2024062438195Controller · faultedCAB PR FAULT 2 -PREFORMED OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING OF CPC1 IAW 21-31-00 TEST OK NO DEFECTS NOTED VERIFIED CPC2 FAULTED SEE LOG PAGE 3455847-2 FOR CORRECTIVE ACTIONSDR GTIA2024062438194Switch · faultyON TAKEOFF ECAM: HYD Y RSVR LO LVL-AS PER TSM 29-13-00-810-816-A R&R SWITCH LOW LEVEL REF: AMM 29-13-41. OPS CHECK GOOD MESSAGE CLEAREDSDR YENA2024062400898Battery Pack · inoperativeFLT#161, JFK-SMF. ' LH OVERWING EMERGENCY EXIT LIGHT INOP ( INTERIOR AND EXTERIOR EMERGENCY LIGHTING SYSTEMS (WITHOUT PASSENGERS) ); REMOVED AND REPLACED BATTERIES ON EPSU 10WL, 11WL, 12WL, 13WL. REPLACED ESPU 11WL. IAW AMM 31-51-38. OPS CHECKED GOOD ON GROUNDSDR GTIA2024062438193A/C Pack · odorFUME EVENT ON DECENT (PACK 1)-PERFORMED TSM 05-50-00-810-831-A. IDENTIFIED SOURCE OF ODOR TO BE PACK 1. SEE LP 3445741-2 FOR CORRECTIVE ACTION.SDR AALA202406241058Lamp · no testAIRCRAFT WAS IN BASE MAINTENANCE: CHECK EMERGENCY EXIT DOOR LIGHT LEFT-HAND SIDE NEED RELLAMPED IN PASSENGER CABIN. INSTALLED EMERGENCY EXIT DOOR LIGHT PER AMM 33-51-16-400-001.SDR AALA202406249812Power Supply · faultedAIRCRAFT WAS IN BASE MAINTENANCE: FAULT EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT 12WL IN PASSENGER CABIN.SDR AALA202406245330Power Supply · faultedAIRCRAFT WAS IN BASE MAINTENANCE: FAULT EMERGENCY POWER SUPPLY UNIT 10WL AT FWD GALLEY AREA. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL AT FORWARD GALLEY AREA.SDR AALA202406243086Power Supply · no testAIRCRAFT WAS NOT GROUNDED: EMERGENCY EPSU BATTERY CHECK FAIL AT FWD LH POS. REMOVED AND REPLACED EPSU UNIT FWD LH I.A.W. AMM. 33-51-38. TEST OK.
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