Aerospatiale ATR 72-212
Service difficulty reports · 4,441
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 = 'ATR72212' 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 = 'ATR72212' 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 COEA2016072552801Adc · failedPASSING THROUGH APPROX. 7000FT, THE NR 1 ENGINE SURGED THROUGH APPROX. 95%. CREW ELECTED TO RETURN TO ANC, NO EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: COULD NOT DUPLICATE DURING ENGINE RUNS. OCF PERFORMED TO MONITOR ALL ENGINE PARAMETERSSDR MTNA20160715001Mount · crackedRIGHT INBOARD FLAP CAM GUIDE MOUNT CRACKED BEYOND MANUFACTURER'S ACCEPTABLE LIMITS. REPAIRED IAW AMM JIC 57-52-00RAI 10000.SDR MTNA20160715004Stringer Clip · corrodedINTERIOR CARGO BAY FRAME 23C, STRINGER 16R CORNER BRACKET HAS HEAVY CORROSION. DAMAGE EXCEEDS MANUFACTURER'S ACCEPTABLE LIMITS. REPLACED IAW SRM 51-25-01. FABRICATED IAW SRM 535140-03-A01.SDR MTNA20160715003Stringer Clip · corrodedFRAME 28C, STRINGER 17 HAS CORNER BRACKET WITH EXFOLIATION CORROSION. DAMAGE EXCEEDS MANUFACTURER'S ACCEPTABLE LIMITS. REPLACED THE STRINGER CLIP IAW SRM 51-21-42. FABRICATED NEW CLIP IAW SRM 53514012-A01.SDR MTNA20160713001Stringer · corrodedCORROSION DISCOVERED AT FRAME 33 STRINGER 16L. DAMAGE BEYOND THE ACCEPTABLE LIMITS OF THE MANUFACTURER. REMOVED STRINGER 16L IAW SRM 51-21-42. INSTALLED FABRICATED REPAIR STRINGER IAW SRM 530000-300-825-A01.SDR COEA2016062303803Skin · damagedAFT CARGO DOOR INNER SKIN IS DAMAGED AT LOWER CORNERS AND HAS OVERSIZED HOLES. REPAIRED IAW SRAS DO/TS-5345/05.SDR COEA2016061414807Floorbeam · corrodedFLOORBEAM, FRAME 17 HAS CORROSION. REPAIRED IAW 0043023.SDR COEA2016061413807Floorbeam · corrodedFLOORBEAM 15 HAS CORROSION BETWEEN CENTER SEAT TRACKS. REPAIRED IAW SRM 530000-300-852-A01.SDR COEA2016060315807Skin · crackedFWD CARGO DOOR, FWD LOWER CORNER, INTERNAL SURFACE OF OUTER SKIN HAS MULTIPLE AREAS WITH CRACKS. REPAIRED IAW SRAS S523R0080.SDR COEA2016052601807Generator · faultedFLIGHT 7202, AIR TURN BACK DISCREPANCY. DURING CLIMB OUT THE ACW NR 2 GEN FAULTED. THE CREW RESET THE SYS BUT THE FAULT RETURNED. THE CREW ELECTED TO RETURN & LANDED SAFELY & NO EMER WAS DECLARED. REPLACED THE NR 2 ACW GEN. LEAK & OPERATIONS CHECKED GOODSDR KPVA20160705005Skin · corrodedWHILE UNDERGOING 2 YEAR CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL SURFACE BETWEEN FRAMES 24 AND 25, AND STRINGERS 19 RIGHT AND STRINGER 20 RIGHT. SKIN REPAIRED IAW CETS-2231/16.SDR KPVA20160705004Support Beam · corrodedWHILE UNDERGOING 2 YEAR CHECK INSPECTION, CORROSION WAS FOUND ON RIGHT OUTBOARD FLAP FORWARD SUPPORT BEAM AT WING RIB 18. SUPPORT BEAM FOUND TO BE OUT OF LIMITS. INSTALLED TEMP REPAIR IAW CETS-2595/16-28106.SDR KPVA20160705001Attach Angle · crackedWHILE UNDERGOING A 2-YEAR CHECK INSPECTION, A CRACK WAS FOUND ON THE AFT PASSENGER AIRSTAIR DOOR, STAIR STRUCTURE FORWARD LOWER ATTACHMENT ANGLE. THE ATTACH ANGLE WAS REPLACED IAW SRM 51-25-01.SDR KPVA20160705003Attach Bracket · corrodedWHILE UNDERGOING 2 YEAR CHECK INSPECTION, UNDERNEATH HYDRAULIC COMPARTMENT FAIRING PANEL 195GP, FORWARD SUPPORT UPPER ATTACHING BRACKET AT FRAME 28A WAS FOUND CORRODED. THE ATTACHING BRACKET WAS REPLACED IN ACCORDANCE WITH STRUCTURAL REPAIR MANUAL 512504-02-SDR KPVA20160705002Floorbeam · corrodedWHILE UNDERGOING A 2 YEAR CHECK INSPECTION, CORROSION ON THE FLOORBEAM UPPER FLANGE AT FRAME 33, BL 0 WAS FOUND BY VISUAL INSPECTION. THE FLOORBEAM WAS REPAIRED IAW SRM 530000-300-827-A01.SDR MTNA20160512001Skin · crackedMAIN CARGO DOOR FORWARD OUTER LATCH FITTING CRACKED. MAIN CARGO DOOR LOWER INNER SKIN CRACKED AT OUTER LATCH FITTING. REMOVED DAMAGED SECTION OF SKIN, FABRICATED NEW SECTION OF SKIN FROM 2024-T3, PO 198454, .032" FABRICATED 2 EA REPAIR DOUBLERS FROM 2024-T3,SDR MTNA20160422001Control Valve · faultyDURING CRUISE AT FL 190, HOT AIR STARTED COMING OUT OF DUCTS & TEMP CONTINUES TO GET HOTTER, TEMP ABOVE 100 DEGREES. TEMP SWITCHED TO MANUAL MODE & NOTHING CHANGED, RAN THE CHECKLIST, DECLARED AN EMER & RETURNED TO FIELD. R & R NR 1 TEMPERATURE CONTROL VALVESDR COEA2016040417819Stringer · crackedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 1R IS CRACKED AT FRAMES 20 & 17. SPLICE REPAIR ATR72 SRM 530000-300-824-A01.SDR COEA2016040416819Stringer · crackedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 1AR IS CRACKED AT FRAME 20. SPLICE REPAIR ATR72 SRM 530000-300-824-A01.SDR COEA2016040415819Stringer · crackedDURING HEAVY CHECK, STRINGER 2R IS CRACKED AT FRAME 20. SPLICE REPAIR SRM 530000-300-824-A01.SDR COEA2016040414819Stringer · crackedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 1AL IS CRACKED AT FRAME 20. SPLICE REPAIR ATR72 SRM 530000-300-824-A01.SDR COEA2016040413819Stringer · crackedHEAVY CHECK COE & MAJOR REPAIR. STRINGER 2AL CRACKED AT FRAME 20. SPLICE REPAIR ATR72 SRM 530000-300-824-A01.SDR COEA2016033101821Warning System · false activationAIR TURN BACK FLIGHT 7276, DURING CLIMB OUT EN-ROUTE, THE EMER BATTERY CHARGE LIGHT ILLUMINATED. PERFORMED IAW ACFT EMER CHECKLIST. TROUBLESHOOTING, RESET OF SYSTEMS & ENG RUNS. NO FAULTS WERE FOUND.SDR COEA2016031509819Landing · damagedHEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON CTR WING UPPER REMOVABLE PANEL LANDING FOR ACCESS PANEL 522CT. REPAIR IAW SRAS DO TS-531 06 3474 ISSUE E DATED 4 5 2016.SDR COEA2016031508819Landing · damagedHEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON CTR WING UPPER REMOVABLE PANEL LANDING FOR ACCESS PANEL 521DT. REPAIR PER SRAS DO TS 531 06 3474 ISSUE E DATED 4 5 2016.SDR COEA2016030907819Frame Splice · corrodedHEAVY CHECK COE & MINOR REPAIR. FRAME 9 SPLICE HAS LEVEL 2 CORROSION ON LOWER LEG, BETWEEN STRINGERS 21L & 21R. REPLACED WITH OEM PART.SDR COEA2016030903819Panel · corrodedHEAVY CHECK COE & MINOR REPAIR. RT WING, PANEL 623GT, HAS LEVEL 2 SURFACE CORROSION ON EDGE NEXT TO RUBBER SEAL. REPLACED PANEL WITH OEM PART.SDR COEA2016030902803Master Cylinder · inoperativeAFTER ARRIVAL FROM FLIGHT 8299, THE CREW NOTED THE RT FIRST OFFICERS BRAKE WAS INOPERATIVE. REPLACED THE FIRST OFFICERS MASTER CYLINDER, BLED BRAKES. OPERATIONS CHECKED GOOD.SDR COEA2016030801803Unknown · malfunctionedFLIGHT 7299 BRAKE INOPERATIVE WO 159364 DISCREPANCY. DURING TAXI, THE FIRST OFFICERS RT BRAKE FAILED. ACFT WAS TAXIED BACK TO RAMP. OPERATIONS CHECKED BRAKES IAW JIC 32-42-00 OPT 10000-001 & ENG RUN & TAXI CHECKLIST. NO FAULT FOUND. OPERATIONS CHECKED GOOSDR COEA2016030620819Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FUSELAGE CTR SECTION LT LOWER SKIN PANEL HAS LEVEL 2 CORROSION UNDER THE ICE SHIELD, BETWEEN THE BOTTOM EDGE OF THE ICE SHIELD & THE UPPER SKIN PANEL EDGE THAT ARE BEYOND SRM LIMITS. REPAIRED IAW SRAS CE-1282 16 10127 DATED 4 SDR COEA2016030619819Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. FUSELAGE CTR SECTION LT UPPER SKIN PAN HAS AREAS OF LEVEL 2 CORROSION UNDER THE ICE SHIELD, BETWEEN THE BOTTOM OF THE WINDOWS & THE LOWER SKIN PANEL EDGE THAT ARE BEYOND SRM LIMITS. REPAIR IAW SRAS CE-1282 16 10127 DATED 4 19 SDR COEA2016030512819Skin Panel · corrodedHEAVY CHECK COE & MINOR REPAIR. LT WING UPPER SURFACE PANEL 523GT, SURFACE CORROSION ON EDGE NEXT TO RUBBER SEAL. REPLACED WITH OEM PART.SDR COEA2016030510819Landing · damagedHEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON LANDING FOR PANEL 622CT. REPAIR IAW SRAS DO TS-531 06 3474 ISSUE E DATED 4 5 2016.SDR COEA2016030506819Mount Bracket · corrodedHEAVY CHECK COE & MINOR REPAIR. LEVEL 2 CORROSION ON PANEL 632AB MOUNT BRACKET. REPLACED WITH OEM PART.SDR COEA2016030504819Bracket · corrodedHEAVY CHECK COE & MINOR REPAIR. RT ELEVATOR CTR RIB, INBD BRACKET UNDER PANEL 344FT HAS LEVEL 2 CORROSION. REPLACED BRACKET WITH OEM PART.SDR COEA2016030418819Floorbeam · corrodedHEAVY CHECK COE & MINOR REPAIR. INTERIOR CABIN, FLOORBEAM 36 HAS LEVEL 2 CORROSION & AREAS OF MISSING SURFACE PROTECTION. REPLACED WITH OEM PART.SDR COEA2016030411819Threshold · corrodedHEAVY CHECK COE & MINOR REPAIR. AFT CARGO DOOR THRESHOLD, UPPER SURFACE HAS AREAS OF LEVEL 2 CORROSION. REPLACED THRESHOLD WITH OEM PART.SDR COEA2016030405819Floor Support · crackedHEAVY CHECK COE & MAJOR REPAIR. RT LONGITUDINAL FLOORBEAM CRACKED AT FRAME 28. REPAIRED IAW EO 5315-02.SDR COEA2016030409819Floor Support · crackedHEAVY CHECK COE & MAJOR REPAIR. RT LONGITUDINAL FLOORBEAM AT FLOORBEAM 29 IS CRACKED. REPAIR IAW EO 5315-02.SDR COEA2016030402819Floor Support · crackedHEAVY CHECK COE & MAJOR REPAIR. LT LONGITUDINAL FLOORBEAM AT FLOORBEAM 29 IS CRACKED. REPAIR IAW EO 5315-02.SDR COEA2016022601819Unknown · malfunctionedFLIGHT 200 EN-ROUTE FOR HEAVY CHECK & AIR TURN BACK DISCREPANCY. CREW REPORTED LOSS OF CABIN PRESS IN AUTO MODE. ELECTED TO RETURN ACFT. NO EMER WAS DECLARED. ACFT LANDED WITHOUT INCIDENT. ITEM DEFERRED. ACFT NOW IN HEAVY CHECK.SDR KPVA201602120001Channel · corrodedLEFT AILERON FIXED T/E CHANNEL HAS CORROSION, FOUND WHILE AT 2YE CHECK. REPLACED LT AILERON FIXED T/E CHANNEL WITH NEW IAW SRM 51-25-03, PARA 3, REV 34. APPLIED SURFACE PROTECTION IAW SRM 51-21-32.SDR KPVA2016020500004Bearing · corrodedTWO HINGES FOUND CORRODED, EXFOILIATIONON LT AILERON TAB, WHILE IN 2YE CHECK. HINGES THAT WERE FOUND CORRODED ON LT AILERON TAB WERE REPLACED IAW SRM 51-25-03, R94.SDR KPVA201602050003Door Sill · corrodedFRAME 39 RT HAS INTERGRANULAR CORROSION AT RT AFT SERVICE DOOR SILL, FOUND AT 2YE CHECK AT BASE. FRAME 39 RT AT RT AFT SERVICE DOOR SILL REPLACED IAW SRM 51-25-01, R94.SDR KPVA201602050002Channel · corrodedLEFT AILERON TAB CLOSING CHANNEL HAS CORROSION, PITTING FOUND WHILE AT 2YE CHECK.SDR KPVA201602040001Seat Track · corrodedCORROSION FOUND ON THE RT SEAT TRACK SEGMENT BETWEEN FRAMES 37 AND 39, WHILE AT 2YE CHECK. SEAT TRACK REPLACED IAW SRM 51-25-04, R94.SDR KPVA2016020200003Floorbeam · corrodedFLOORBEAM AT FRAME 39 LT BETWEEN LBL 325 AND LBL 960 HAS INTERGRANULAR CORROSION, FOUND WHILE AT 2YE CHECK. FLOORBEAM AT FRAME 39 LT BETWEEN LBL 325 AND LBL 960 HAS BEEN REPLACED IAW SRM 51-25-01 AND SRM 51-25-04, R94.SDR KPVA2016020200002Angle · corrodedUPON REMOVAL OF FLOORBEAM AT FRAME 39 UNDER ANOTHER NON-ROUTINE, INTERCOSTAL BRACKET BELOW PASSENGER DOOR SILL CORRODED, EXFOLIATION - WHILE AT 2YE CHECK. INTERCOSTAL BRACKET BELOW PAX DOOR SILL REPLACED IAW SRM 51-25-01, R94.SDR KPVA2016012900002Intercostal · corrodedMLG FAIRING FRAME AT FRAME 25 INTERCOSTAL, CRACKED AT APPROXIMATELY LBL 900 WHILE AT 2YE CHECK. MLG FAIRING FRAME AT FRAME25 INTERCOSTAL CRACKED AT APPROXIMATELY LBL 900, REPLACED IAW SRM 512501-02-001-A01.SDR COEA2016012950801Splice Plate · damagedHEAVY CHECK COE & MAJOR REPAIR. DAMAGE TO FWD PRESS BULKHEAD SPLICE PLATE AT STIFFENER 3LT. REPAIRED IAW SRAS CE 437 16 10002 DATED 2 25 16.
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