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 YENA2023041300359Unknown · unknownDURING HEAVY MAINTENANCE: REF AEM NR 2023-68759: CORR INT STRU SPLICE STGR 43L FR30-FR31 FWD CARGO; REF AEM NR 2023-68759 FOR ALL WORK ACP RPL SPLICE PLATE AT STGR43L PER SRM 51-42-11, 51-72-11. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023041300358Unknown · unknownDURING HEAVY MAINTENANCE: REF AEM NR 2023-68753: CORR STRG 43L FR24-FR28 FWD CARGO; REF AEM NR 2023-68753 FOR ALL WORK ACP RPL STGR 43L FR24-FR28 PER SRM 51-42-11, 51-72-11. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023041300357Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / FRAME 41-42 / STIFF 16-17 / CORROSION DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023041300356Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TRAILING EDGE OVERHANG / RIBS 13-16 & 18-20 AND WX3493 & WX4010 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023041300355Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / TRAILING EDGE OVERHANG / BETWEEN GEAR RIB 5 AND RIB 18 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023041300354Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE/AFT LAV VENT OUTLET BTWN FR69/70 & STR29/32/ EXISTING DOUBLER REPAIR/ CORROSION/ PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR CALA2023041201100Lamp · inoperativeINOP EMERGENCY EXIT LAMP AT SR 36C. NEW BULB DID NOT CHANGE ISSU E. NO POWER DETECTED AT CONNECTOR. COORECTED WIRE ISSUE AT SR 36 LH IAW ESPM 20-43-11-01-H. OPC EME RGENCY LIGHTING SYSTEM IAW AMM 33-51-00-710-805-A TEST OK.SDR AALA202304189584Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 68 AND S23T. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5.SDR YENA2023041400399Lgciu · failedFLT#1005, JFK- PDX. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) ' UPON TAKEOFF L/G GEAR NOT UPLOCKED CAUTION MESSAGE APPEARED; REF L/P 3720661, ITEM 2 (GROUND CONFIG AFTER FLT CONFIG W/ ELECT PWR C/W IAW AMM TASK 32-00-00-860-002A, AMM TASK 34-11-00-440-801 ASDR GTIA2023041437111Unknown · unknownFUME EVEN ON DECENT.-PERFORMED DECONTAMINATION OF THE ECS IAW AMM 21-00-00. COULD NOT DUPLICATE FUME SMELL. A/C OK FOR SERVICESDR AALA202304120278Door · out of adjustAIRCRAFT WAS NOT GROUNDED: L1 LAVATORY DOOR HARD TO OPEN. MAINTENANCE ADJUSTED LAVATORY DOOR PER AMM 25-40-00.SDR AALA202304174698Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING FUEL TANK ACCESS PANEL 540LB HAS ELONGATED FASTENER HOLE. REPLACED ACCESS PANEL PER SRM 51-72-11.SDR GTIA2023041437110Transducer · leakingECAM HYD G RSVR LO LVL AT CRUISE BEFORE DESENT. AMBER FUILD LEVEL ON GREEN SYSTEM PAGE-PERDORMED GVI OF A/C FOUND LEAKS ON BRAKE SUPPLY TRANSDUCER (96GG) R/R MANIFOLD IAW AMM 32-42-22-000-001-A AND PERFORMED ENG IDLE RUN IAW AMM 71-00-00 LEAK CHECK GOOD A/C OKSDR CALA2023041201095Power Supply · unknownDURING EMERGENCY LIGHT TEST AMM 33-51-00-710-001-A FAULT EPSU BATTERY AFT L WAS RECORDED. USING TSM 33-51-00-810-802-A VERIFIED AFT L BATTERY OF EPSU 13WL IS AT FAULT. VEREFIED BATTERY REPLACEMENT AND OPS CHECK GOOD REMOVED AND REPLACED BATTERY OF THE EMERGENCSDR CALA2023041001093Flap System · lockedSUPPORT TASK- FLIGHT TEST: F/CTL FLAPS LOCKED WARNING OCCURED WHILE CONFIGURING FOR LANDING. FLAPS PARTIALLY EXTENDED BETWEEN 0-1. SLATS EXTENDED NORMALLY. W/C:51126 PERFORMED TSM 27-51-00-810-818-A, ADJUSTMENT THE INTERCONNECTING 801-A T11230 SEE FORM 44-0008SDR CALA2023041001091Fuel Cap · missingPDA 2, TOW TEAM REPORTED FUEL CAP MISSING FROM AIRCRAFT UPON ARRIVAL. TOMC SMITH INSTALLED SERVICEABLE FUEL CAP. PARTS USED: 1844397,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1844397 SN OFF 7014 CAP, COUPLING R OFF 31-2825-9-0001 7014 ON 31-2825-9-0SDR CALA2023041001087Windshield · failedFO WINDSHIELD SHATTERED.LOOKS LIKE OUTER PANE. REMOVED AND REPLACED WHC 2 (2DG2). OPS TEST GOOD. NO / FAULTS NOTED AT THIS TIME. REMOVED AND REPLACED R1 WINDOW OPS CHECK GOOD.SDR YENA2023041100341Unknown · unknownFLT#607, FLL-LAS. 'FLT ATTENDANT IN AFT CABIN STATES SHE SMELLS CLEANING FLUID IN THE REAR OF THE AIRCRAFT; PERFORMED INFO NOTICE 2017-T15J & TSM 05-50-00 LEVEL A EVENT. NO ABNORMAL ODOR WAS NOTED. A/C OK FOR SERVICE. MCC GAULDA NOTIFIED.'SDR YENA2023041100339Ptu · failedFLT#1270, CHS-LGA. (AIRCRAFT DIVERTED TO JFK) 'Y HYD RSVR LO LVL; FOUND PTU MANIFOLD TO BE AT CAUSE FOR THE LEAK. REMOVED AND REPLACED PTU MANIFOLD IAW AMM 29-13-51. OPS CHECK & LEAK CHECK ARE GOOD. A/C OK TO CONTINUE FOR SERVICE.'SDR CALA2023041001084Flap System · faultyFLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL ECAM FOLLOWED TRAILINGEDGE FLAPS RAMAINED UPLEADING EDGE DEVICES DEPLOYED LOCKED BY TOMC PER TOMC SR MGR CFDS HITS THE FLAP MECH DRIVE UNIT. WHEN DEPLOYING THE FLAP HANDLE THE TORQUE TUBES SPIN A FEW ROTATIONSDR YENA2023041100344Unknown · unknownFLT#1529, JFK-RSW. 'UPON ARRIVAL AT GATE INFLIGHT NOTIFIED ME OF A 'FUME EVENT ' ON DESCENT PASSING THRU 10,000 AND LASTING 5-7 MINUTES. NO ODOR WAS DETECTED IN THE FLIGHT DECK ( APU SYSTEM ).' (SUPPLEMENTAL INFORMATION TO FOLLOW)SDR AALA202304114308Safety Valve · faultedAIRCRAFT WAS GROUNDED: LANDING GEAR DOORS NOT CLOSED ECAM ON LANDING GEAR EXTENSION FOR LANDING. MAINTENANCE REPLACED THE NOSE LANDING GEAR DOOR CLOSING SAFETY VALVE PER AMM 32-31-19 AND TSM 32-51-00-810-826-A. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMSDR CALA2023041001069Web · crackedWHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX .439". RCRAFT N408UA (4108) REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES R PART 2 OF THE LATESDR AALA202304105989Door · stickingAIRCRAFT WAS NOT GROUNDED: LAVATORY A DOOR STICKS HARD TO OPEN. MAINTENANCE LUBED LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR AALA202304100475Power Supply · no testAIRCRAFT WAS NOT GROUNDED: SEATS 13 ABC, 17 ABC, 22 ABC, 26 ABC, LEFT HAND AFT DOOR AND RIGHT HAND AFT DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.SDR GTIA2023041037107Harness · looseLEVEL @ FL380 EPR BEGAN TO FLUCTUATE APPROX 1.23 TO 1.29 EP. AS SUCH FUEL FLOW ALSO BEGAN TO CLUXUATE BEWTWEEN 2050 AND 2300 PER SIDE. THIS OCCURED ON BOTH ENGINES CREATING AN ASSYMETRY. ATTEMPTED MANUAL THRUST CONTROL. UNSECCESFUL-VERIFIED INSTALLATION OF EECSDR CALA2023041001061Fitting · crackedR/H FR 68 STGR 22 HAS A CRACK IN THE RADIUS OF WEB AND FLANGE GE N BY MECH V061632 ON HAECO LCQ NR #9292027(34027) 341-01385. WORK ACCOMPLISHED BY LCQ EMP V061673. ACCOMPLISH INIT ATEST REVISION OF EC/RA 5341-01385 ON OR BEFORE 55,060 TOTAL AIR NOT TO EXCEED 1SDR GTIA2023040637106Unknown · unknownON CLIMBOUT AT 12,000' , FAS REPORTED BURNING RUBBER SMELL NEAR ROW 27C. IT DISSIPATED, BUT ON DESCENT, RETURNED THROUGHOUT ROWS 27-30. WE PERFORMED FUME CHECKLIST AND TURNED OFF PACK 2. FAS REPORTED SMELL WENT AWAY QHICKLY.-PERFORMED TSM 05-50-00-810-831-A. CSDR CALA2023040601059Reservoir · lowG RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD SERVICED GREEN HYD FLUID AND HEAD PRESSURE TO SERVICABLE LIMIT REF AMM 12-12-00. NO FAULTS NOTEDSDR CALA2023040601058Check Valve · lowCREW REPORT: GREEN HYD LOW RES IN FLT FOUND GREEN SYS RESERVOIR EMPTY WITH EVIDENCE OF LEAKING IN LH WHEEL WELL FOUND LEAK AT HP MANIFOLD CHECK VALVE 1059GM O-RINGS ON ORDER. REMOVED AND REPLACED HP MANIFOLD CHECK VALVE 1059GM OPERATION CHECK GOOD NO LEAKS FOUSDR CALA2023040601056Web · crackedR/H FR 68 STGR 22 HAS A CRACK IN THE RADIUS OF WEB AND FLANGE GE N BY MECH V061632 ON HAECO LCQ NR #9292027(34027) 341-01385. WORK ACCOMPLISHED BY LCQ EMP V061673. ACCOMPLISH INIT ATEST REVISION OF EC/RA 5341-01385 ON OR BEFORE 55,060 TOTAL AIR NOT TO EXCEED 1SDR CALA2023040601055Web · crackedWHILE PERFORMING UAL EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491), CRACK WAS FOUND AT FR 68 RHS STGR 22 LOWER WEB HORIZONTAL FLANGE RADIUS. CRACK LENGTH APPROX .439". RCRAFT N408UA (4108) REACHES 50,000 TOTAL AIRCRAFT FLIGHT CYCLES R PART 2 OF THE LATESDR GTIA2023040637102Skin · dented"3 EACH DENTS LOCATED BETWEEN FRAMES 23 TO 24 AND FRAMES 24 TO 25 LH SIDE OF FUSELAGE. RAF-01 3069145-02 HAS BEEN GENERATED.-PERFORMED REPAIR INSTRUCTION ON DENT EXTERNAL SKIN LOC ON FR 23 PLUS 19 INCH AND BTW STRG 24-25 LH UPPER FUSELAGE IAW EA # 53-0722-23 RSDR GTIA2023040637101Unknown · corrodedCORROSION ON LOWER SILL AT FUSELAGE STATION FR 66 TO 68 AND STR 23R RAF -01 3069144-01 GENERATED -PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED FR 68 AT LEVEL STR 23R AT AFT GALLEY AREA IAW SRM A320 53-41-14-300-007 PRINCIPLE 5 FIG 001 THIS REPAIR IS CATEGOSDR GTIA2023040637100Web · cracked"CRACKED WEB FAIRING SUPPORT AT FUSELAGE STATION FR.. 49 AND STR. 27R
RAF-01 3069143-02 GENERATED-PERFORMED PERMANENT REPAIR ON SUPPORT WEB BELLY FAIRING AT LEVEL FR 49 RH SIDE LOWER FUSELAGE IAW A320 SRM 53-45-12-300-010 THIS REPAIR IS CATEGORY A"SDR GTIA2023040637099Unknown · dented"MULTIPLE DENTS ON AFT GALLEY G4 WORKDECK. RAF01-3069139-02 GENERATED-REMOVED AND REPLACED WORKDECK AFT GALLEY AREA IAW EA 25-0111-23
PART 1 AND PART 2"SDR GTIA2023040637098Box Beam · dentedDENT LOWER SURFACE OB FLAP ON RH WING RAF 3069146-01 GENERATED -PERFORMED PERMANENT REPAIR ON OB FLAP LOWER SURFACE OH RH WING IAW EC# EA 5753-2319 REVISION 00, EA # 57-0117-23 #1 COVER EA 57-0117-23 PART #1 AND A320 SRM 57-53-00-300-055 THIS REPAIR IS CATEGORSDR CALA2023040601047Plate · corrodedAFT CARGO SHEAR PLATE AT STR38L BETWEEN FR62-FR63 HAS CORROSION ON UPPER FLANGE. GEN AT HAECO LCQ BY V061609 PER NR 9292592 (345 92) REMOVED REPLACED AND REPROTECTED SHEAR PLATE AT STR 38L BETWEEN FR 62-63 IAW A320 SRM 51-72-11-911-002. ACMP BY MECH V061609 INSDR YENA2023040700336Unknown · unknownFLT#1867, HPN-PBI. '"DIRTY SOCK SMELL" VERY STRONG ON DESCENT APU WAS OFF; COMPLIED WITH INFO NOTICE 2017-T015, SECTION A, ISOLATED FAULT TO TYPE 10, (A), 1, C PER TSM 05-50-00-810-085-B, D. A/C IS OK FOR SERVICE. NO DEFECTS OR ODOR PRESENT.'SDR GTIA2023040637091Skin · dentedREF MWI 3003068-1. DENT ON FUSELAGE FR 70 STR 39-41. RAF 01 GENERATED.-ACCOMPLISHED REPAIR OF FUSE SKIN FR70 STR 39-42 RH AS PER REPAIR INSTRUCTIONS REF REO L24358 AND RDAF 81177563/093/2023#A. THIS IS LIFE LIMITED TO 6MO PER RDAF 81177563/093/2023#A.SDR AALA202304050118Power Supply · no testAIRCRAFT WAS NOT GROUNDED: MID RIGHT EMERGENCY POWER SUPPLY UNIT COMMUNICATION FAULT MESSAGE DISPLAYED ON FLIGHT ATTENDANTS PANEL DURING SYSTEM TEST. MAINTENANCE REPLACED MID RIGHT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPSDR AALA202304054163Power Supply · no testAIRCRAFT WAS NOT GROUNDED: FORWARD EMERGENCY POWER SUPPLY UNIT COMMUNICATION FAULT MESSAGE DISPLAYED ON FLIGHT ATTENDANTS PANEL DURING SYSTEM TEST. MAINTENANCE REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATSDR CALA2023040401040Actuator · warning messageFLIGHT CREW REPORTS VIA ARINC PACK 1 +2 FAULT ON ECAM , PACK 1 ALREADY ON MEL REF LOG PAGE 4192703. PACK 2 SHOWING CFDS ATA 21-61-52 P2 RAM AIR OUT ACTUATOR SOURCE TEMP CTL. DECLARED AND EMERGENCY, DESCENDED TO TO FL 100. DIVERTED TO MCI.VARGAS TOMC UPDATED MASDR CALA2023040401039Flange · crackedWHILE PERFORMING EA5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. 22 INNER CAP AND WEB HORIZONTAL FLANGE PER THE LATEST REVISION 22 INNER CAP AND WEB HORIZONTAL FLANGE PER THE LATEST SDR CALA2023040401038Flange · crackedWHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 31-SEPT-2023. EXPECTED TO BECOME A PERMANENSDR CALA2023040401037Flange · crackedWHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 O REACHES 49,948 TOTAL FLIGSDR CALA2023040401025Frame · crackedWHILE PERFORMING EA 5341-01231 REV B OP 001 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 RH STGR 22 WEB HORIZONTAL FLANGE RADIUS. SOLUTION WITH INSPECTION REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 31-SEPT-2023. EXPECTED TO BECOME A PERMANENSDR CALA2023040401024Frame · crackedWHILE PERFORMING EA 5341-01231 REV B OP 1 (AIRBUS SB A320-53-1491 REV 00), CRACKS WERE FOUND AT FR68 LHS STGR 22 WEB HORIZONTAL FLANGE RADIUS AND IN A STOP FITTING HOLE. EMENTS. ACCOMPLISH INITIAL INSPECTION REQUIREMENTS PER PART 2 O REACHES 49,948 TOTAL FLIGSDR AALA202306223482Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FORK END FITTING WORN AND BUSHING HAS MIGRATED AT FR 24 AT S32R. REPLACED FORK END FITTING PER EA 343789.SDR AALA202306228316Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FORK END FITTING WORN AND BUSHING HAS MIGRATED AT FR 24 AT S32L. REPLACED FORK END FITTING PER EA 343789.
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