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 AALA202105089002Damper · faultedAIRCRAFT IN BASE MAINTENANCE: DAMPING FUNCTION OF PASSENGER CREW DOOR 842 FAILED OPERATIONAL TEST. REPLACED DOOR DAMPER CYLINDER IAW AMM 52-13-14-400-001-B, OPS CHECK GOOD.SDR YENA2021050700307Unknown · odorFLT# 1219, BOS-MIA. ODOR OCCURANCE OBSERVED @ TAKE OFF AND APPROACH SEE MX-270 ; C/W THE INFO NOTICE 2017-T015F SEE HOW A AC IS OK FOR SVC MCC MARIO WAS MADE AWARESDR YENA2021050700306Wire Harness · failedFLT# 861, BOS-SJU. ENG 2 EGT OVERLIMIT 720C FOR 90 SECS TOGA TAKE OFF WITH ENG ANTIICE ON.AT 1000FT AFE ECAM APPEARED. THRUST LEVERS RETARDTED TO CLIMB DETENT PER NORMAL SOP.EGT STAYED AT 720C IAW ECAM ENG # 2 THRUST LEVER RETARTED SLIGHTLY EGT RETURNED TO NORSDR GTIA2021050635716Web · crackedPYLON #1 OB WEB BTW RIB 2-3 CRACK RAF -01 273060802 OPENED-REF LTPR 5001066519-0010 REPAIRED #1 ENGINE PYLON CRACK IAW EO 5450-2104 AND RDAF 80902833/003/2021SDR GTIA2021050635715Stringer · corrodedCORROSION FOUND ON STRINGER 41RH 131W FR59 RAF-01 2730611-02 CREATED-COMPLETED NDT AND REPAIR IAW EO 5341-2109 AND RDAF 80906069/007/2021SDR GTIA2021050635714Fitting · scratchedSCRATCHES FOUND ON RUDDER BEARING #6 FITTING RAF 01 2730610 OPENED-ACCOMPLISHED EO 5546-2103SDR GTIA2021050635713Megaphone · malfunctionedFWD MEGAPHONE HAS BEEPING NOISE WHEN DEPRESSED-R+R FWD MEGAPHONE IAW SPIRIT AIRLINES EMF EQUIPMENT LAYOUT DRAWING MANUAL NK320-232-EQ OK TO CONT.SDR GTIA2021050635712Radar · odorSMOKE SMELL CLIMBING FL200 TO FL300 BAD WX ST ELMOS FIRE AT THE TIME OF SMELL ONCE WX GOT BETTER SMELL WENT AWAY. ALL AC INDICATIONS NORMAL. SMELL WENT AWAY AFTER WX. FA SMELLED IN IN THEE BACK TO.-TROUBLESHOOT A/C FOR FUME EVENT IAW TSM 05-50-00. NO FUMES NOTSDR AALA202105049006Support Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT ANGLE LOCATED AT UPPER INBOARD SIDE RIB 7 APROX ON RIGHT PYLON. REPLACED SUPPORT ANGLE LOCATED AT UPPER INBOARD SIDE RIB 7 ON RIGHT PYLON IAW A320 SRM 51-72-11-911; DRAWING D54630462 SHEET 01; DWG-D54630485 AND A320 SDR GTIA2021050335711Compressor · hotCRUISING AT FL350 FLIGHT ATTENDANT REPORTED STRONG SMOKE SMELL (NON-VISABLE) SHORTLY AFTER CAPT AND FO SMELLED SAME ODOR. IT RESEMBLED BURNNG ELECTRICAL SMELL REMOVAL OF SMOKE/FUMES COM PROCEDURE WAS INITIATED. - AFTER CABIN FANS OFF AND PACK FLOW HIGH SMELL BSDR AALA202105069016Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION OF LOWER SPIGOT FITTING BORE ON RH PYLON BETWEEN RIB 4 AND RIB 5, MEASURING L=13.0 IN, W=1.25 IN, D=0.003 IN. REPLACED LOWER SPIGOT FITTING WITH NEW IAW SRM 54-51-12-300-002 AND DRAWINGS R54612042 AND R54612043.SDR AALA202105112800Window · glazedAIRCRAFT IN BASE MAINTENANCE: GLAZED PASSENGER CREW DOOR 831 WINDOW PANE ASSEMBLY PRISMA. REPLACED PASSENGER CREW DOOR 831 WINDOW PANE ASSEMBLY PRISMA PER 56-31-11-400-002-A.SDR AALA202105039667Bottle · failedAIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPING FUNCTION DOES NOT PASS OPERATIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14-400-001-B.SDR GTIA2021050335705Seal · leaking"FUME EVENT ON APROACH / LANDING F/A IN AFT NOTICED IT FIRST THEN THE COCKPIT. ( PACKS A320 WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - FAULT CAUTIONS ASSOCIATED WITH OPERATIVE SIDE NOT DISPLAYED )-R & R LH RECIRCULATSDR CALA2021050300590Servo Valve · failedAFTER TOFF AUTO BRAKESAND NORM BRAKES ECAM AFTER LANDING ANTI SKID AND N/W STRG ECAM LOG PAGE LOCKED BY TOMC.BRAKE SERVO VALVE (17GG) WAS REPLACED AND CAT III LAND VERIFY TEST PASSED. AIRCRAFT IS RESTORED TO FULL CAT III STATUSSDR YENA2021050300304Unknown · odorFLT 135, JFK-ABQ. INFLIGHT REPORTED ACRID/BURNING ODOR THROUGHOUT CABIN PRIMARILY IN THE AFT GALLEY - ROW 17 DURING TAKEOFF / INTIAL CLIMB AND UPON LANDING IN THE FOWARD GALLEY; ACCOMPLISHED TSM 24-00-00-810-823-A. NO DEFECT NOTED COULDN'T DUPLICATE ITEM. AIRCSDR YENA2021050300303Battery · no testDURING 15 DAYINSPECTION (PARKED AIRCRAFT), EMERG LIGHTS AT 11WL & 12WL FAILED TEST; R & R EMERGENCY LIGHT BATTERIES AT 11WL & 12WL IAW AMM 33-51-38. TEST GOOD.SDR YENA2021050300302Battery · no testDURING 15 DAYINSPECTION (PARKED AIRCRAFT), EMERG LIGHTS AT 11WL & 12WL FAILED TEST; R & R EMERGENCY LIGHT BATTERIES AT 11WL & 12WL IAW AMM 33-51-38. TEST GOOD.SDR YENA2021043000298Control Valve · looseFLT # 192, TPA-BOS. LEVEL 2 ODOR EVENT DETECTED BY PREVIOUS FLIGHT CREW AND CURRENTLY DETECTED IN CABIN AND COCKPIT ( APU BLEED VALVE ) ; PER INFO NOTICE 2017-T015F, APPLIED MEL 36-12-02-A CAT C PER MCC. APU BLEED/LOAD CONTROL VALVE SECURED IN THE CLOSED POSISDR CALA2021043000570Skin · corrodedCORROSION ON EXISTING DOUBLER BETWEEN FR63 TO FR64, STR41R -STR42R (MARKED). BLENDED OUT CORROSION, ALODINED AND PRIMED AREAS IN REF SRM 51-74-00/001 VERIFY MATERIAL TO BE USED FOR DOUBLER AS .071-2024T3 PO#9047624 AND FILLER AS .063-2024T3 PO#4325226 REF AVO#SDR CALA2021043000569Stringer · corrodedSTRINGER 41 CORRODED FROM FR 57 TO FR 64. LOCATION IS AIRCRAFT RIGHT. REMOVED CORRODED STRINGER 41R FROM FR57 TO FR64. VERIFIED REPLACEMENT PART AS D5347047120200 PO# 7123438305 M&E 18-5300-3-0007 REF SRM 53-41-13-07B FIG007 ITEM90 VERIFIED REPLACEMENT PART ASSDR CALA2021043000568Stringer · corrodedSTRINGER 40 CORRODED FROM FR 57 TO FR 64. REMOVED THE STRINGER SECTION. PERFORMED NDT HOLE PROBE SCAN ON FASTENER HOLES AT STR. 40R FROM FR56 TO FR64. IAW AVO ESC210411-4294-1C PART B STEP 2(B). NO DAMAGE FOUND. REF L/P6114120 FOR SKIN CORROSION REF AVO#ESC2SDR CALA2021043000565Transceiver · inoperativeRADAR/PRED WS APPEARINOP REPLACED WXR TRANSCEIVER REF MM34-41-33-400-003-A AND IPC 34-41-33-991-00300-C ITM 1B OPS CHECKED NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1993500 SN OFF 2280 TRANSCEIVER, WX OFF 31-2311-9-0001 2280 ON 31-2311-9-0001 2104SDR AALA202104299001Oven · odorAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS ADVISED STRONG BURNING SMELL IN FORWARD GALLEY THAT LASTED APPROXIMATELY 30 TO 40 SECONDS. NO VISIBLE SMOKE. ACCOMPLISHED JOB CARD 26L00021001. REPLACED RIGHT FORWARD GALLEY OVEN PER AMM 25-35-19.SDR AALA202104291796Window · glazedAIRCRAFT IN BASE MAINTENANCE: GLAZED PASSENGER CREW DOOR 841 WINDOW PANEL ASSEMBLY PRISM AT FORWARD GALLEY AREA. REPLACED PASSENGER CREW DOOR 841 WINDOW PANEL ASSEMBLY PRISM AT FORWARD GALLEY AREA PER AMM 56-31-11-400-002-A.SDR CALA2021042800564Door Sill · corrodedAFT CABIN R- 2 DOOR LOWER SILL PLATE CORR @ AFT END FR68 MKD DOT 60-076 REF. AAR N/R:9478800 GENERATED BY: V891378 REMOVED R2 DOOR LOWER SILL PLATE AND INSTALLED NEW R2 DOOR LOWER SILL PLATE IAW A320 SRM 51-42-11 AND 53-41-14-80A, AND RECONECTED DRAIN HOSES LSDR AALA202105149633Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORE OF FORWARD LUG OF AFT DOOR LOCK FITTING, MEASURING DIAMETER= 1.289 INCH AND W= 0.641 INCH, BETWEEN FR26 AND FR27 AT STR 39R AT FORWARD CARGO COMPARTMENT DOOR. REPLACED LOCK FITTING REF A320 SRM 51-41-11-801SDR AALA202105141934Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORES OF FORWARD LUG OF AFT DOOR LOCK FITTING, MEASURING DIAMETER = 1.251 INCH AND W = 0.646 INCH, AT FR27 AND STR 39. REPLACED LOCK FITTING LOCATED FR27 FORWARD CARGO COMPARTMENT DOOR REF A320 SRM 51-41-11-801 SDR AALA202105139904Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND ON BORE OF FORWARD LUG (DIAMETER: 1.269 INCHES, WIDTH: 0.650). REPLACED LOCK FITTING BETWEEN FR 27 AND FR 28 FORWARD CARGO COMPARTMENT PER SRM 51-42-11-801.SDR YENA2021043000300Unknown · odorFLT # 473, BOS-AUA. STRONG FUMES AFT ON CLIMBOUT WHICH DISAPPEARED @ CRUISE IN DESCENT FUMES STRONG OBSERVED COCKPIT AND CABIN FOLLOWED ALL FROM V1 SUPP PROCEDURES COCKPIT CABIN ODOR RECOGNITION & ISOLATION QRH PROCEDURES ; INFO NOTICE 2017-T015F LVL ODOR COMPSDR YENA2021043000299Unknown · odorFLT # 473, BOS-AUA. STRONG FUMES AFT ON CLIMBOUT WHICH DISAPPEARED @ CRUISE IN DESCENT FUMES STRONG OBSERVED COCKPIT AND CABIN FOLLOWED ALL FROM V1 SUPP PROCEDURES COCKPIT CABIN ODOR RECOGNITION & ISOLATION QRH PROCEDURES ; INFO NOTICE 2017-T015F LVL ODOR COMPSDR AALA202104289006Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 LOWER MIDDLE ATTACH BOLT. REPLACED ATTACH BOLT PER TASK CARD 26C61057005 .SDR CALA2021042800557Skin · corrodedSKIN CORROSION AT FR65-FR66 BETWEEN STR39R TO STR40R PER AVO ESC210415-4294-1 COMPLIED WITH STEP 6 DETAILED US INSPECTION AND MAPPING OR REWORKED AREA. PER AVO ESC210415-4294-1 COMPLIED WITH STEP 6 DETAILED US INSPECTION AND MAPPING OR REWORKED AREA. REMOVED FSDR AALA202105110042Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261AG MEASURING L=47.00 INCHES W=7.00 INCHES AT FR64 TO FR66 AND -Y254 TO Y254. REPLACED FLOOR PANEL 261AG REF A320 SRM 53-02-00-300-011 & IRM 9701 REV K.SDR YENA2021043000297Unknown · odorFLT # 1225, JFK-TPA. FL EXPERIENCED A TINGLY FEELING IN HER MOUTH. ODOR POSSIBLY BURNING ELECTRIC,DETECTED BY CREW MOSTLY (STRONGEST) IN AFT CABIN ; ACCOMPLISHED LEVEL 1 ODOR PER INFO NOTED 2017-T015F SECTION C. A/C IS OK FOR SERVICE. ACCOMPLISHED DECONTAMINSDR CALA2021042800554Stop Fitting · crackedPER NR 9294159/40159 AD 2018-03-12: L2 DOOR FR68 STOP FITTING NO .1 INBOARD LOWER HOLE IS CRACKED THE IN THE WEB AT 6:00. "REPAIR BEFORE NEXT FLIGHT". GENERATED BY V061633 ACCOMLISHED THE FINAL REAM OF THE L-2 DOOR FRAME 68 DOOR STOP FITTING #1 INBOARD LOWER HSDR CALA2021042800553Fitting · crackedPER NR 9294160/40160 AD 2018-03-12: R2 DOOR FRAME 68 STOP FITTIN G NO. 1 INBOARD LOWER HOLE IS CRACKED IN THE WEB AT 6:OO. "REPAI R BEFORE NEXT FLIGHT". GENERATED BY V061633 ACCOMPLISHED THE FINAL REAM OF THE R-2 DOOR FRAME 68 DOOR STOP FITTING #1 INBOARD LOWESDR CALA2021042800555Door Sill · corrodedAFT CABIN R- 2 DOOR LOWER SILL PLATE CORR @ AFT END FR68 MKD DOT 60-076 REF. AAR N/R:9478800 GENERATED BY: V891378 REMOVED R2 DOOR LOWER SILL PLATE AND INSTALLED NEW R2 DOOR LOWER SILL PLATE IAW A320 SRM 51-42-11 AND 53-41-14-80A, AND RECONECTED DRAIN HOSES LSDR CALA2021042800552Stringer · corrodedSTRINGER 40R CORROSION BETWEEN FR64 TO FR66. VERIFIED STRINGER REPLACEMENT AS D5348020220201 M&E18-5341-3-0035 PO#UB96850010 SRM 53-41-13-50A FIG14 ITEM850 VERIFIED STRINGER REPLACEMENT PART AS D5348020220201 M&E18-5341-3-0035 PO#UB96850010 SRM 53-41-13-50A FISDR AALA202105069020Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT CENTER WINDOW POST CONTINUITY FITTING CRACKED AT FR2 AND -Y20. REPLACED CONTINUITY FITTING PER EO 5319Y017 AND REPAIR DRAWINGS R53112919 AND R53112958.SDR AALA202105069019Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT CENTER WINDOW POST CONTINUITY FITTING CRACKED AT FR2 AND Y20. REPLACED CONTINUITY FITTING PER EO 5319Y017 AND REPAIR DRAWINGS R53112919 AND R53112958.SDR GTIA2021042635701Flashlight · inoperativeCAPTAIN FLASHLIGHT IS INOP ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R CAPTAIN FLSH LIGHT IAW FOM 9.2.2 THIS CLEARS MDDR 3442 MOC NOTIFIEDSDR CALA2021042600545Stop Fitting · crackedL1 DOOR FRAME 16 AND STOP FITTING #7 LOWER INBOARD HOLE IS CRACK ED IN THE INTERCOSTAL FITTING. REPAIR BEFORE NEXT FLIGHT CONTAC T ENGINEERING FOR APPROVED REPAIR INSTRUCTIONS. LOGPAGE OPEN FURTHER DETAILS AWAITED.SDR YENA2021042800291Slide · out of positionFLT 717, AUS-LAX. R/H OVERWING SLIDE ( 7505MM ) NOT FLUSHED WITH FUSELAGE AND MISSING FASTENER; R & R R/H OVERWING SLIDE (7505) PER AMM 25-62-42.SDR CALA2021042600531Battery Pack · dischargedPER NR 9294161/40161 ALL CABIN EMERGENCY LIGHTS FAIL TO ILLUMINA TE WITH THE SWITCH IN THE ARMED POSITION AND THE CIRCUIT BREAKER S PULLED (SYSTEM TESTS OK FROM THE PTP ON CONSECUTIVE TESTS) REMOVED AND REPLACED EPSU EMERGENCY BATTERY/OWL. OPS CHECK OF TH E ESDR YENA2021042700289Slide · deformedDURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA; (REF AEROMAN N/R 2021-156407) R & R ESCAPE SLIDE RAFT DOOR 832 IAW AMM 25-62-44-000-012-A AND AMM 25-62-44-400-007-A AND PERFORMED OPERATIONAL TEST IS OKSDR YENA2021042700288Slide · deformedDURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 842 AT AFT GALLEY AREA; (REF AEROMAN N/R 2021-156406) R & R ESCAPE SLIDE RAFT DOOR 842 IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A AND PERFORMED OPERATIONAL TEST IS OKSDR YENA2021042700287Slide · deformedDURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 841 AT FWD GALLEY AREA; (REF AEROMAN N/R 2021-156408) R & R ESCAPE SLIDE RAFT DOOR 841 IAW AMM 25-62-44-000-804-A AND AMM 25-62-44-400-803-A AND PERFORMED OPERATIONAL TEST IS OKSDR YENA2021042700286Slide · deformedDURING HEAVY MAINTENANCE, DEFORMATION SLIDE RAFT PASSENGER CREW DOOR 831 AT FWD GALLEY AREA; (REF AEROMAN N/R 2021-156409)R & R ESCAPE SLIDE RAFT DOOR 831 IAW AMM 25-62-44-000-012-A AND AMM 25-62-44-400-007-A AND PERFORMED OPERATIONAL TEST IS OKSDR AALA202104269005Smoke Detector · false activationAIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ECAM ALERTED TWICE IN FLIGHT ERRONEOUSLY. ACCOMPLISHED TEST OF SMOKE DETECTION CONTROL UNIT. ALL TESTS OK IAW AMM 26-17-00. NO FAULTS FOUND.
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