Aerospatiale ATR42-500
Service difficulty reports · 548
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 = 'ATR42500' 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 = 'ATR42500' 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 CA190604013Generator · unserviceable(CAN) SHORTLY AFTER TAKEOFF #2 ACW GENERATOR FAILED AND WOULD NOT RESET . UPON ARRIVAL ACW GENERATOR CONTROL UNITS SWAPPED FROM SIDE TO SIDE AND 32 ACW GEN STILL FAILED TO RESET. #2 ACW GENERATOR REPLACED AND GROUND FUNCTION TESTED SERVICABLE. (TC# 20190604013SDR CA190521030Wheel · damaged(CAN) DESCRIPTION: DURING TOWING OF AIRCRAFT A NOISE WAS NOTED FROM #4 MAIN WHEEL. MAIN WHEEL COVER REMOVED AND BROKEN BOLT/NUT WAS DISCOVERED. NOTE: TIRE PRESSURE WAS WITHIN LIMITS. CORRECTIVE ACTION: MAIN WHEEL REMOVED AND AXLE AND BRAKE ASSEMBLY WERE INSPECSDR CA190521036Indicator · failed(CAN) IN FLIGHT TURN BACK DUE TO FAILURE OF F/O`S VSI INDICATOR. AIRCRAFT RELEASED TO SERVICE AFTER REPLACEMENT OF THE VSI. (TC# 20190521036)SDR CA190515012Fitting · corroded(CAN) DURING HMV INSPECTION, CORROSION WAS FOUND ON THE AFT ANCHORAGE FITTING, P/N S53671272200, OF THE PAX DOOR ASSEMBLY. W/O 33421433, NR 00342 INSPECTION CARD 425-536112-DVI-10000-1. REPLACED PART. (TC# 20190515012)SDR CA190515009Fitting · corroded(CAN) DURING HMV INSPECTION, CORROSION FOUND ON THE FWD SPRING FITTING, PART NUMBER S5217670920200, OF THE PAX DOOR ASSEMBLY. W/O 33421433, NR 00336 INSPECTION CARD 425-536112-DVI-10000-1. REPLACED PART (TC# 20190515009)SDR COEA2019051303804Clamp · damagedFLIGHT 619, JHM-HNL: AFTER ARRIVAL AT THE GATE WHILE EXECUTING THE PARKING CHECKLIST, THE CREW DECLARED AN EMERGENCY DUE TO SMOKE ON THE FLIGHT DECK. THE AIRCRAFT WAS EVACUATED AND THE FIRE DEPARTMENT RESPONDED. MAINTENANCE IS CURRENTLY TROUBLESHOOTING. THIS ISDR CA190503025Doubler · cracked(CAN) DURING AN HMV INSPECTION (425-ZL-115GVI-10000-1), A CRACK WAS FOUND ON THE R/H TEAR STRAP DOUBLER AT FR 7 AT THE AFT NLG TO WEB AREA AT STA 20R. REFERENCE WO 33421433 NR 95. PART TO BE REPLACED. PN S53172101205 (TC# 20190503025)SDR CA190503024Angle · cracked(CAN) DURING HMV INSPECTION, A CRACK WAS LOCATED ON THE AFT HOLE OF THE R/H PICK UP ANGLE. P/N S57114282201. INSPECTION TASK CARD W/O 33421433 TASK CARD 425-535141-SDI-10000-1. W/O 33421433 NR 113. PART TO BE REPLACED WITH MADE PART. PN S57114282201 (TC# 20190SDR CA190503027Doubler · cracked(CAN) DURING HMV INSPECTION, (425-ZL-115GVI-10000-1) A CRACK WAS FOUND ON THE LEFT HAND TEAR STRAP DOUBLER AT FR 7 AT THE AFT NLG TO WEB AREA AT STA 20L. REFER WO 34421433 NR 94. PART TO BE REPLACED. PN S53172101204 (TC# 20190503027)SDR CA190503028Control Cable · damaged(CAN) DURING HMV CHECK, A DAMAGED CABLE WAS DISCOVERED. CABLE REPLACEMENT REVEALED AN ISSUE WITH BOTH THE ADOC MM AND THE ATR.DOC MM. AFTER CONSULTATION WITH ATR, THEY SUPPLIED THE CABLE LENGTH SPECS FOR ALLELEVATOR CABLES. ONE OF THE TWO LONG CABLES IN THE L/SDR CA190430021Door · missing(CAN) UPON ARRIVAL, CREW NOTICED ACCESS DOOR TO HYD BAY MISSING. SNAG ENTERED IN JL BOOK.. MAINTENANCE INSPECTED THE HYD BAY, NO OTHER DAMAGE REPORTED. DMI 373928-1 AND CDL 52-03 RAISED. PARTS ON ORDER (TC# 20190430021)SDR CA190503009Cable · failed(CAN) DURING HEAVY CHECK, A R/H ELEVATOR CABLE WAS FOUND TO BE DAMAGED AT A FWD QUADRANT. AFTER THE CABLE WAS ORDERED, USING THE RELEVANT IPC, THE CABLE CAME IN AND WAS FOUND TO BE WAY TOO LONG. FURTHER INVESTIGATION IN THE REST OF THE AIRPLANE REVEALED SEVERASDR CA190403006Eec · intermittent(CAN) IN CRUISE, CREW NOTICED #2 TORQUE BUG SLOWLY MOVING BETWEEN 40-105%. TORQUE OBSERVED (ISA - 20 DEGREES CELCIUS) WAS #1 ENG = 105%, AND #2 ENG = 95%. ALL OTHER INDICATIONS LED CREW AND MCC TO BELIEVE TQ IND CORRECT. #2 ELECTRONIC ENGINE CONTROLLER REPLACESDR CA190402012Floorbeam · corroded(CAN) DURING HMV INSPECTION 425-536108 GVI 10000-1, CORROSION WAS FOUND IN MULTIPLE LOCATIONS ON FLOOR BEAM S53672409218 AT FRAME 40. CORROSION WAS REMOVED BY BLENDING AND THE REMAINING MATERIAL THICKNESS WAS FOUND UNDER LIMITS IN SEVERAL LOCATIONS. REFERENCE SDR CA190327009Transmitter · leaking(CAN) JUST PRIOR TO STARTING #1 ENGINE, FUEL WAS NOTICED ON GROUND BELOW. MTCE INVESTIGATED AND FOUND THE #1 FUEL FLOW TRANSMITTER LEAKING. FUEL FLOW TRANSMITTER REPLACED IAW JIC 73-31-61 RAI 10000. (TC# 20190327009)SDR CA190327007Floorbeam · corroded(CAN) DURING HMV INSPECTION, CORROSION FOUND ON FLOOR BEAM AT FRAME 33, P/N S53372411200, BETWEEN LBL 13 AND LBL 38. WO 33424191 MR 00090, INSPECTION TASK CARD 425-536108-GVI-10000-1.SDR CA190326019Stringer · cracked(CAN) DURING THE HMV VISIT, UPON INSPECTION (425-ZL-253-GVI-10010-1), CRACK WAS FOUND ON L/H STRINGER 2 (S53671107208) ST FRAME 34 INTERSECTION. REFER TO WO 33424191, NR #00032. SRM REPAIR REQUIRED. (TC# 20190326019)SDR CA190326014Doubler · cracked(CAN) DEFECT- DURING HMV INSPECTION, CRACK FOUND ON RH TEAR STRAP DOUBLER PN S53172101205 AT FRAME 7 OF NLG. W/O 33424191 NR 00028. INSPECTION TASK CARD 425-ZL-115-GVI-10000-1. CORRECTIVE ACTION: PARTS REPLACEMENT (TC# 20190326014)SDR CA190326018Stringer Clip · cracked(CAN) DURING THE HMV VISIT, UPON INSPECTION(425-535602-DVI-10000-1), CRACK WAS FOUND ON THE R/H FR.26 UPPER CLIP AT STR. 4. REFER TO WO #3342419 NR #00031. PART TO BE REPLACED (TC# 20190326018)SDR CA190326017Stringer Clip · cracked(CAN) DURING THE HMV VISIT, UPON INSPECTION(425-535602-DVI-10000-1), CRACK WAS FOUND ON THE UPPER CLIP ST STR 4. REFER TO WO #334424191, NR #00029. PART TO BE REPLACED (TC# 20190326017)SDR CA190326021Angle · cracked(CAN) DURING HMV INSP, R/H PICKUP ANGLE, P/N S57114282201, FOUND CRACKED. WO 33424191, NR 00009. INSPECTION TASK CARD 425-535141-SDI-10000-1. PART TO BE REPLACED. (TC# 20190326021)SDR CA190326020Angle · cracked(CAN) DURING HMV INSP, L/H PIKUP ANGLE, P/N S57114282200, FOUND CRACKED. WO 33424191, NR 00008. INSPECTION, TASK CARD 425-535141-SDI-10000-1. PART TO BE REPLACED. (TC# 20190326020)SDR CA190326016Angle · cracked(CAN) DURING THE HMV VISIT, UPON INSPECTION (425-535148-SDI-10000-1), CRACK WAS FOUND ON THE L/H FR.26 SHEAR ANGLE BTW.STR. 12-13. REFER TO WO 33424191 NR #00010. PART TO BE REPLACED. (TC# 20190326016)SDR CA190326015Angle · cracked(CAN) DURING THE HMV VISIT, UPON INSPECTION (425-535148-SDI-10000-1), CRACK WAS FOUND ON THE R/H FR.26 SHEAR ANGLE BTW.STR. 12-13. REFER TO WO 33424191 NR #00011. PART TO BE REPLACED. (TC# 20190326015)SDR CA190326012Doubler · cracked(CAN) DEFECT- DURING HMV INSPECTION, CRACK FOUND ON LH TEAR STRAP DOUBLER PN S53172101204 AT FRAME 7 OF NLG. W/O 33424191 NR 00027. INSPECTION TASK CARD 425-ZL-115-GVI-10000-1 CORRECTIVE ACTION: PARTS REPLACEMENT (TC# 20190326012)SDR CA190322009Skin · corroded(CAN) LH WING SPOILER OUTER PANEL CORRODED ON THREE AREA ON UPPER SURFACE. (TC# 20190322009)SDR CA190321005Skin · corroded(CAN) SURFACE CORROSION ON UPPER SKIN AND ANGLE OF R/H SPOILER. (TC# 20190321005)SDR CA190319011Hinge Fitting · corroded(CAN) VERTICAL STABILIZER REAR SPAR MIDDLE RUDDER HINGE FITTING CORRODED.SDR CA190320013Skin · corroded(CAN) CORROSION FOUND ON LH HORIZONTAL STAB LEADING EDGE LOWER SKIN AT OUTBOARD EDGE. (TC# 20190320013)SDR COEA2019031801804Hinge · corrodedWO 199374 DISCREPANCY: LEVEL 2 CORROSION DISCOVERED ON LT LOWER WING DROP PANEL 532BB PIANO HINGE LE CORRECTIVE ACTION: REPLACEMENT OF HINGE WITH OEM PART. THIS IS A SUPPLEMENTAL TO PREVIOUSLY ISSUED SDR COEA2019031801804 TO CLARIFY THAT THIS IS A MINOR REPAISDR CA190325020Stick Shaker · intermittent(CAN) RESTRICTIONS IN ELEVATOR MOVEMENT FROM NEUTRAL TO NOSE UP POSITION. NORMAL MOVEMENT IN NOSE DOWN POSITION. STICK PUSHER REPLACED IAW JIC 27-36-31 RAI 10000. MFC REPLACED IAW JIC 31-48-81 RAI 10000. SYSTEM FOUND TO OPERATE NORMALLY WITH NO FURTHER FAULTS SDR COEA2019031401806Hinge · corrodedWO 199113 NR 3 DISCREPANCY: LEVEL 2 CORROSION DISCOVERED ON LOWER LT WING ACCESS PANEL 523BB PIANO HINGE LE CORRECTIVE ACTION: REMOVE AND REPLACE PIANO HINGE. THIS IS A SUPPLEMENTAL TO PREVIOUSLY ISSUED SDR COEA2019031401806 TO CLARIFY THAT THIS IS A MINOR REPSDR COEA2019031302Skin · corrodedWO 199374 MAJOR REPAIR/DISCREPANCY: LEVEL 2 CORROSION FOUND ON LT LOWER WING SKIN BETWEEN RIBS 22-30. CORRECTIVE ACTION: REPAIRED PER SRAS ES-3588/15...9735 ISSUE F, DATED 3/18/2019.SDR CA190312012Bulkhead · corroded(CAN) REAR PRESSURE BULKHEAD CORRODED AT RH LAP JOINT PN S53871407202. OUTSIDE/EXTERNAL COVER CORRODED PN S53871411200. RH WEB AT LAB JOINT AND STIFFENER CORRODED PN S53871407202. (TC# 20190312012)SDR CA190313007Skin · corroded(CAN) CORROSION FOUND ON LH WING LOWER SKIN AFT EDGE AT RIB 22.SDR CA190313011Rib · corroded(CAN) CORROSION FOUND ON LH WING RIB 1 LOWER FITTING FOOT BETWEEN STIFFENER 1-2.SDR CA190314002Skin · corroded(CAN) CORROSION FOUND ON LOWER FUSELAGE SKIN BETWEEN FRAME 38-42 AND BETWEEN STR 17-21. (TC# 20190314002)SDR CA190311032Web · corroded(CAN) WEB CORRODED AT SERVICE DOOR TRESHOLD.SDR CA190311031Web · corroded(CAN) PAX DOOR THRESHOLD CORRODED.SDR CA190312002Doubler · corroded(CAN) LAVATORY PRESSURE BOX INNER DOUBLER CORRODED. AFTER INVESTIGATION FOUND INTERCOSTAL (P/N S53671402200) AND STRINGER #21 (P/N S53671407214020) BTW FR 40-42 CORRODED.SDR CA190311016Skin · corroded(CAN) L/H AFT LOWER FUSELAGE SKIN CORRODED AROUND POTABLE WATER SERVICE DOOR CUT OUT. (TC# 20190311016)SDR CA190311002Floorbeam · corroded(CAN) AFT CARGO AT FR 41, LOWER FLOOR BEAM CORRODED. (TC# 20190311002)SDR CA190313021Rib · corroded(CAN) BOTH VERTICAL LOWER TRAILING EDGE RIB ASSY CORRODED . P/N S5537497300406 & S5537497300651.SDR CA190311011Skin · corroded(CAN) LH WING LOWER SKIN CORRODED BETWEEN RIB 9 AND 10 AT T/E AREA.SDR CA190308014Rib · corroded(CAN) UPPER RUDDER MACHINED RIB CORRODED.SDR CA190311026Seat Track · corroded(CAN) CORROSION FOUND ON RH INB SEAT TRACK BETWEEN FRAME 29-35 (TC# 20190311026)SDR CA190311021Floorbeam · corroded(CAN) CABIN ENTRANCE FLOOR BEAM AT FRAME 36 CORRODED. (TC# 20190311021)SDR CA190311003Seat Track · corroded(CAN) RH AFT CARGO SEAT TRACK BETWEEN FRAME 41 & 44 CORRODED.SDR CA190308021Skin · corroded(CAN) CORROSION FOUND ON LH OUTER WING LOWER SKIN AT RIB 15.SDR CA190308011Floorbeam · corroded(CAN) CABIN ENTRANCE FLOOR BEAM AT FRAME 38 CORRODED.
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