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 AALA202209208390Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM BETWEEN FR 64 AND FR 66 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR AALA202209072781Wire · brokenAIRCRAFT WAS GROUNDED: CANNON PLUG FOR EMERGENCY LIGHT AT SEAT 13ABC WIRE IS BROKEN. REPAIRED BROKEN WIRE PER ESPM 20-48-21 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA202210122172Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22L. REPAIRED FRAME PER EA 339017.SDR AALA202210118568Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 68 AND S22R. REPAIRED FRAME PER EA 339016.SDR AALA202209067979Tire · blownAIRCRAFT WAS GROUNDED: # 3 TIRE BLEW ON LANDING . NORMAL LANDING 200-300 FPM ON TOUCH DOWN. MAINTENANCE REPLACED THE #3 MAIN LANDING GEAR WHEEL ASSEMBLY PER AMM 32-41-11.SDR AALA202209066789Tire · blownAIRCRAFT WAS GROUNDED: # 4 MAIN LANDING GEAR TIRE BLOWN ON LANDING. MAINTENANCE REPLACED THE #4 MAIN LANDING GEAR WHEEL ASSEMBLY PER AMM 32-41-12.SDR CALA2022090202252Skin · noneA3NB-51-4-6001 DURING LOCATED FR59-60 STR 37R SRM 53-00-11 FIG 2 04 USED NOT LOCATED IN CURRENT SRM. DOES NOT COMPLY WITH 14 CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 3() REMOVED AND REPLACED DOUBLER IAW ECRA 5341-01331. EMP# V935774 W ORK ACCOMPLISHESDR AALA202209292577Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING AILERON #5 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.SDR YENA2022090600876None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, LH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408601 WO 2022-178/1 REMOVED AND REPLACED CONTINUITSDR YENA2022090600875None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING, RH SIDE, CRACK LENGTH IS 0.200 INCHES APPROX IN COCKPIT (1 EA); REF AEROMAN N/R 2022-408602 WO 2022-178/1 REMOVED AND REPLACED CONTINUISDR YENA2022090600874None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT OVERWING EMERGENCY EXIT DOOR (AFT LH EEH DOOR 834) CRACK L=0.250 INCH APPROX; ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 834 FOR REPLACEMENT OF FRAME REINFORCE DOOR STRUCTURE REF AEROMAN NSDR YENA2022090600873None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT THE OVERWING EMERGENCY EXIT DOOR (FWD LH EEH DOOR 833) CRACK L=0.196 INCH APPROX; REF AEROMAN N/R 2022-408533 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 833 FOR REPLACEMENT OSDR YENA2022090600872None · noneDURING HEAVY MAINTENANCE: CRACK INDICATIONS WERE FRAME SEGMENTS 1 AT THE OVERWING EMERGENCY EXIT DOOR (FWD RH EEH DOOR 843) CRACK L=0.194 INCH APPROX; REF AEROMAN N/R 2022-408535 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 843 FOR REPLACSDR YENA2022090600871None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FRAME SEGMENT 1 AT OVERWING EMERGENCY EXIT DOOR (AFT RH EEH DOOR 844) CRACK L=0. 197 INCH APPROX; REF AEROMAN N/R 2022-408536 WO 2022-178/1 ACCOMPLISHED EC# A320-52-1144 ON EMERGENCY EXIT DOOR 844 FOR REPLACEMENT OF SDR GTIA2022090236633None · noneDURING WEEKLY CHECK FOUND R2 DOOR ASSIST NEEDS SERVICE-SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00SDR GTIA2022090236631None · noneFWD L1 PASSENGER DOOR NEEDS SERVICNG DOOR ASSIST.-SERVICE FWD L1 DOOR ASSIST IAW AMM 52-11-00. NO FURTHER DEFECTS NOTED AT THIS TIME. LEAK CK GOOD.SDR YENA2022090200865None · noneFLT#679, JFK-MKE. 'ON DESCENT. THROUGH 10,000 FEET FLIGHT ATTENDANTS SUSPECTED A FUME EVENT; ACCOMPLISHED INFO NOTICE 2017-T015I. TROUBLESHOOT TO APU BLEED. REF LOG PAGE # 3439401ITEM 2. PACK BURN ACCOMPLISHED. APU INSPECTION ACCOMPLISHED STSLMQ6TR841X.'SDR YENA2022090200862None · noneFLT#120, MCO-ALB. 'ODOR PRESENTED AT 10'K ON DESCENT. IT PERSISTED THROUGHOUT THE LANDING AND WAS REPORTED TO GET WORSE ONCE PARKED AT GATE. PRESENT MOSTLY IN THE AFT GALLEY AREA. BUT REPORTS IN FRONT GALLEY/ CABIN ALSO. ( BLEED AIR SUPPLY SYSTEMS); SEE L/P 34SDR CALA2022090202247Intercostal · noneR/H FR 16 #7 DOOR STOP HOLE #1 CRACK IN INTERCOSTAL AT 10 O''CLOC K AND HOLE #3 INTERCOSTAL AT 1 O''CLOCK (AD 2022-02-11) PER HAECO LCQ N/R 9290235/30235 GEN BY V061632 RMVD AND RPLD INTERCOSTAL AT R/H FR 16 #7 IAW A320 SRM 51-42-11/ 001 AND APPLIED PROTECTIVESDR CALA2022090202244None · noneFORWARD CARGO THRESHOLD SILL PLATE HAS CORROSION FR25-FR28 REMOVED CORROSION AT DOOR SILL PLATE AT FWD CARGO IAW SRM 51-74- 51-42-11. EMP: V935834 WC: 36166 STA: ST ENG BFM 00 CHECK LIMITS ORIG. MAT 0.063" D=0.019" L=3.5" W=1" MAT. REMAI NING 0.042" (T93968) FSDR CALA2022090202243Beam · nonePASSENGER CABIN, BETWEEN FR16 AND Y518, RAIL DUMMY HAS CORROSION RMEOVED CORROSION ON RAIL DUMMY AT FR16 T518 IAW SRM 51-74-00, F SRM 51-75-12. EMP: V933986 WC: 36250 STA: ST ENG BFM OUND WITHOUT OF LIMITS IAW SRM 51-11-14-203-007, MEASURE: L=1.90 0", W=1.4", SDR AALA202210218013Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD RIGHT HAND FRAME CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA INBOARD VERTICAL FLANGE CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 338782.SDR AALA202210211281Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD LEFT HAND SIDE FRAME CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA INBOARD VERTICAL FLANGE LOWER RADIUS CRACKED AT FR 2 AND Y0. REPAIRED FRAME PER EA 338792.SDR AALA202210198968None · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. MAINTENANCE REPLACED CONTINUITY FITTING PER EA 338792.SDR AALA202210190157None · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. MAINTENANCE REPLACED CONTINUITY FITTING PER EA 338792.SDR YENA2022090200860None · noneFLT#777, BOS-LAS. 'LEVEL 1 ODOR EVENT REPORTED BY INFLIGHT IN CRUISE SMELLED LIKE PAINT MID CABIN FIRST THEN AFT WOULD COME AND GO BRIEFLY NO SMOKE OBSERVED. CA ALSO SMELLED IN DESCENT AT 18KFT AND PERFORMED ECOM ISOLATION W X BLEED SHUT AND PACK 1 OFF AND ODOSDR GTIA2022083036627None · nonePASSENGER/CREW DOOR L1/L2/R1/R2 DOOR ASSIST BOTTLE NEED SERVICING.-SERVICED PASSENGER/CREW DOOR L1/L2/R1/R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.SDR YENA2022083000832Frame · corrodedDURING HEAVY MAINTENANCE: FUSELAGE - REAR / AFT LAVATORY VENT / FR 68-70 & STGR 31R-32R / CORROSION DAMAGE. TEMPORARY REPAIR (CONSIDERED AS A MAJOR REPAIR)SDR AALA202208307043None · low pressureAIRCRAFT WAS NOT GROUNDED: L1 CABIN DOOR DAMPER/ASSIST BOTTLE PRESSURE LOW. SERVICED L1 DOOR ASSIST BOTTLE PER AMM 52-10-00.SDR AALA202208309432Battery · noneAIRCRAFT WAS NOT GROUNDED: FORWARD LEFT EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD FAULT MESSAGE DISPLAYED DURING TEST. REPLACED FORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.SDR YENA2022082900825None · failedFLT#1457, JFK-AUA. (AIRCRAFT PERFORMED AN AIR TURN BACK AND DECLARED AN EMERGENCY INTO JFK) DURING THE CLIMB A BLACK FLUID BEGAN LEAKING OUT OF FWD GALLEY FLOOR. FLUID HAS A STRONG SMELL OF HUMAN WASTE; FOUND LAV A TOILET ASSY LEAKING. REMOVED AND REPLACED LAVSDR GTIA2022083036621None · noneCAPT FOOT WELL FLASHLIGHT INOP LEAKING BATTERY ACID FROM TAIL CAP -R&R CA FLASHLIGHT ASY IAW SA A320 EMERGENCY EQUIP DRAWINGSDR YENA2022083000831Skin Panel · corrodedDURING HEAVY MAINTENANCE: TRANSFERRED FROM 3451484-1 FOUND CORROSION ON AFT LAV VENT SKIN PANEL; REF FLIGHTSTAR WO FS220050 N/R 00004 REPAIRED FUSE SKIN AT AFT LAV VENT OUTLET IAW A320 SRM 53-41-11.SDR YENA2022083000842Skin Panel · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE BETWEEN RIB1 TO RIB2 ON LH WING (REFER TO THE MPD TASK ZL-500-03 ); ACCOMPLISHED REPAIR OF THE CORROSION ON THE LH WING TOP SKIN PANEL 2 UPPER SURFACE AT LEVEL OF RIBS 1 AND 2 AND STRINGER 16 IAW SDR YENA2022083000841Window Post · crackedDURING HEAVY MAINTENANCE: CRACK: FR2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LH SIDE L=0.160"; REF AEROMAN NR 2022-400154 W/O: 2022 182/1: REMOVED AND REPLACED LH AND RH CONTINUITY FITTINGS FR1-2 IAW SRM 51-72-11-911-001 AND REPAIRSDR YENA2022083000840Coupling · damagedDURING HEAVY MAINTENANCE: PERFORM REPAIR FR43 FOOT COUPLING LH; REF AEROMAN NR 2022-400417 W/O: 2022 182/1: REPAIRED FRAME FOOT COUPLING AND SUPPORT FR43LH IAW JB EC A320-53-1269-02 AND REPAIR INSTRUCTION R53370233.SDR YENA2022083000839Coupling · crackedDURING HEAVY MAINTENANCE: CRACK: FR43 FOOT COUPLING STR21-22RH; REF AEROMAN NR 2022-400387 W/O: 2022 182/1: REMOVED AND REPLACED FRAME FOOT COUPLING FR43 STR18-24RH IAW SRM 51-42-11, 51-72-11, JB EC A320-53-1269-02, AND REPAIR INSTRUCTION R53370232.SDR YENA2022083000838Stop Fitting · crackedDURING HEAVY MAINTENANCE: CRACK HOLE 5 DOUBLE JOGGLE AREA FR20RH AND #7 DOOR STOP FITTING LEVEL AT FWD GALLEY (D=0.061" 2 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400196 W/O: 2022 182/1: REPAIRED HOLE #5 DOUBLE JOGGLE AREA FR20RH AND #7 DOOR STOP FITTING IAW RESDR YENA2022083000837Stop Fitting · crackedDURING HEAVY MAINTENANCE: CRACK (2EA): FR16RH DOOR STOP FITTING #7 UPPER INBD HOLE (D=0.080 6 O'CLOCK DIRECTION) AND LOWER INBD HOLE (D=0.124" 8 & 10 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400210 & 400211 W/O: 2022 182/1: REMOVED AND REPLACED INTERCOSTAL FR16SDR YENA2022083000836Stop Fitting · crackedDURING HEAVY MAINTENANCE: CRACK (2EA): FR16LH DOOR STOP FITTING #7 UPPER INBD HOLE (D=0.094" AT 5 O'CLOCK DIRECTION) AND LOWER INBD HOLE (D=0.123" AT 4 & 12 O'CLOCK DIRECTION); REF AEROMAN NR 2022-400205 & 400207 W/O: 2022 182/1: REMOVED AND REPLACED INTERCOSTSDR YENA2022083000835Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOCATED BTW FRAME 56 AND FRAME 57 IN AFT CARGO COMPARTMENT (CPCP RELATED MPD TASK 534107-01); REMOVED AND REPLACEDSTRINGER 43L AND FASTENERS LOCATED BTW FRAME 54AND FRAME 60 IN AFT CARGO COMPARTMENT AS PER A320SDR YENA2022083000834Window Post · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCHES, IN COC KPIT (1 EA); REF AE NR 2022-420038, WO 2022-175/1. REMOVED AND REPLACED CONTINUITY FITTING SDR YENA2022083000833Battery · inoperativeDURING HEAVY MAINTENACE: FAULT EPSU EMERGENCY POWER SUPPLY UNIT BATTERY 10WL, 11WL,12WL, 13WL IN PASSENGER CABIN (4EA); REF: ARM W/O 2022 175/1 NR 2022-420207 REMOVED AND REPLACED EPSU EMERGENCY POWER SUPPLY UNIT BATTERY 10WL, 11WL, 12WL, 13WL IN PASSENGER CABSDR YENA2022082900826None · noneFLT#2226, POP-EWR. 'ENGINE EXHAUST SMELL IN FLIGHT DECK DISSIPATED WITH PAC 1 OFF; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A (A), ISOLATED FAULT TO TYPE 2 TSM 05-50-00-810-085-B. FOUND OIL LEAKAGE OF DE-OILER CARBON SEAL. REMOVED AND REPLACED DE-OILER CASDR GTIA2022082636616None · noneL2 JUMPSEAT FLASHLIGHT NOT TESTING-R+R L2 JUMPSEAT FLASHLIGHT ,TETS OK IAW EMMERGENCY EQUIPMENT LAYOUT DRAWING NNK320 -232-EQSDR YENA2022082600822Slide · failedFLT#392, TPA-BOS. ' INADVERTENT RIGHT OVERWING SLIDE DEPLOYMENT; REMOVED AND REPLACED RIGHT OVERWING SLIDE IAW AMP 25-63-02.'SDR AALA202209085637O-Ring · leakingAIRCRAFT 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 FOR AASDR GTIA2022082636615None · crackedCRACK FOUND ON MILLED FRAME AT FR43L STGR 24L TO 18L. RAF-01 2803718-01 OPENED. REF EO 5331-2059.-REPLACED FRAME 43LH (FOOT FRAME) IAW EA 53-0355-22 AND EO 5331-2241 REF AEROMAN NR 2022-391291SDR GTIA2022082636614None · corrodedCORROSION ON BORE OF RH ELEVATOR FITTING #6. RAF 01 2803723-2 GENERATED-REPAIRED RH ELEVATOR HINGE FITTING #6 IAW SRM 55-26-41-300-006, FIRST INSPECTION THRESHOLD IS 6 YEARS AFTER COMPONENT FIRST FLIGHT, SUBSEQUENT INSPECTIONS AT INTERVAL OF 6 YEARS, INSPECTISDR GTIA2022082636613None · corrodedCORROSION ON BORE OF LH ELEVATOR FITTING # 4. RAF 01-2803725-2 GENERATED-REPAIRED LH 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 TY
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