N606AR
Service difficulty reports · 18
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N606AR' AND registry_match = 'registration' 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 n_number = 'N606AR' AND registry_match = 'registration' 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 39LA20150404133Nut · out of positionTHE 2 ENG POWER LEVER HAD NO CONTROL OVER THE ENG DURING CRUISE FLIGHT. THE NR 2 ENG WAS SHUTDOWN IN FLIGHT & AN EMER WAS DECLARED. THE ACFT LANDED WITHOUT INCIDENT. INSPECTED NR 2 ENG CONTROL SYS & FOUND THAT THE NUT FOR THE PROPELLER PITCH CONTROL INPUT LSDR 39LA2013072400164Bracket · corrodedFOUND CENTER WING RT OTBD FLAP BRACKET, INBD AND OTBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKINS PN'S 212-13202-05-1 AND 212-13202-05-2. REPAIR PREFORMED IAW EO2012032-309 AND EO2021032-424, AND DWG NR 2012032-2032.SDR 39LA2013072400154Skin · dentedTWO DENTS FOUND ON LOWER SURFACE OF RT WING AT APPROX WING STATION 9350. REPLACED WING SKIN IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG N R 2012032-2033.SDR 39LA2013072400144Skin · dentedTWO UPPER FUSELAGE SKINS REQUIRE REPLACEMENT DUE TO DENTED AREAS BEYOND LIMITS, SEVERAL ELONGATED RIVET HOLES. REPLACED 2 EA UPPER FUSELAGE SKINS IAW EO 2021032-309 AND EO2012032-424.SDR 39LA2013072400134Skin · corrodedWHILE PERFORMING GENERAL VISUAL INSPECTION OF WING (TASK 57.02, ITEM 11 OF 1 YEAR INSPECTION UNDER COMPANY CAMP, WO 124890-5), FOUND FLAP COVE BEHIND NR 2 ENGINE CORRODED. NON ROUTINE DISCREPANCY GENERATED UNDER WO 125651-603. REPLACED FLAP COVE SKINS FROM WSDR 39LA2013072400124Skin · corrodedFOUND CORROSION UNDER LT CENTER SECTION EXHAUST FAIRING DURING INSPECTION. CORROSION FOUND TO BE BEYOND MFG LIMITS. REPAIRED IAW EADS TECH INSTRUCTION NR 17 DATED OCTOBER 1992, EO2012032-309 AND EO2021032-424.SDR 39LA2013072400114Skin · corrodedWHILE PERFORMING GENERAL VISUAL INSPECTION OF WING (TASK 57.02, ITEM 11 OF 1 YEAR INSPECTION UNDER COMPANY CAMP, WO 124890-5), FOUND WING SKIN BEHIND NR 2 ENGINE CORRODED. REPLACED WING T/E SKIN FROM WING STATION 1266 TO WING STATION 3500 WITH 2024-T3, 0.025"SDR 39LA2013072400104Bracket · corrodedFOUND CENTER WING LT OTBD FLAP BRACKET, INBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKIN, PN 212-13202-05-2, IAW EO 2012032-309 AND EO 2012032-424, AND DWG NR 2012032-2032, SUPPORTED BY FAA FORM 8110-3 DATED 31 MAY 2013.SDR 39LA2013072400094Web · chafedFOUND CHAFE DAMAGE TO LT WING FUEL TANK COLLECTOR BOX FORWARD WEB. PERFORMED REPAIR IAW EO2012032-309 AND EO2012032-424, AND DWG NR 12032-2038, SUPPORTED BY FAA FORM 8110-3 DATED 31 MAY 2013.SDR 39LA2013072400084Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE CO-PILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO2012032-309 AND EO2021032-424, AND AIRLIFT DWG 2012032-2036, SUPPORTED BY FAA FORM 8110-3, DATED 31 MAY 2013.SDR 39LA2013072400074Attach Fitting · crackedWHILE PERFORMING EDDY CURRENT INSPECTION, SUPPLEMENTAL INSPECTION DOCUMENT 20,000 /2,800 FLIGHT SUPPLEMENTAL INSPECTION OF HORIZONTAL STABILIZER, FOUND THAT LT HORIZONTAL STABILIZER UPPER AAFT ATTACH FITTING HAS CORROSION AND CRACK INDICATION AROUND MOUNT BUSHSDR 39LA2013072400064Frame · gougedFOUND DEEP GOUGE RT SIDE IN FRAME 1F. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2030.SDR 39LA2013072400054Skin · crackedWHILE PERFORMING GENERAL VISUAL INSPECTION OF WING. FOUND FLAP COVE BEHIND NR 1 ENGINE EXHAUST CRACKED IN 2 PLACES. REPAIRED IAW EO2012032-309 AND EO2012032-424.SDR 39LA2013072400044Skin · puncturedLOWER FUSELAGE SKIN AT BS 5390 - 6966, LBL 20.0 - RBL 20.0 HAS PIERCED SKIN. REPAIRED EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2031.SDR 39LA2013072400034Frame · crackedFOUND CRACKED FRAME AT BS 9650 LT SIDE RAMP AREA FUSELAGE 5TH STRINGER FROM BOTTOM. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND DWG NR 2012032-2029.SDR 39LA2013072400024Skin · dentedFORWARD FUSELAGE LT SIDE, 1 DEEP DENT AT FS 3538, WL 33.0. REPAIRED IAW EO 2021032-309 AND EO2012032-424.SDR 39LA2013071900014Fitting · damagedBS 5744.3 RT SIDE FWD WING MOUNT INSIDE CABIN HAS ONE HOLE DRILLED ACROSS MOUNTING BRACKET. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND DWG NR 2012032-2032.SDR 39LA2013071900004Skin · dentedBELLY SKIN DENTED BEYOND LIMITS. REPLACED BELLY SKINS IAW EO 2021032-309 AND EO2012032-424.
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