# Service difficulty reports: N606AR A list on [N606AR](https://openairdocs.org/aircraft/N606AR.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 39LA20150404133](https://openairdocs.org/sdr/39LA20150404133.md): Nut · out of position · Apr 4, 2015 · N606AR · Casa C212CD · Propeller Controlling System > THE 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 L - [SDR 39LA2013072400164](https://openairdocs.org/sdr/39LA2013072400164.md): Bracket · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach Fittings > FOUND 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 39LA2013072400154](https://openairdocs.org/sdr/39LA2013072400154.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin > TWO 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 39LA2013072400144](https://openairdocs.org/sdr/39LA2013072400144.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin > TWO 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 39LA2013072400134](https://openairdocs.org/sdr/39LA2013072400134.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin > WHILE 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 W - [SDR 39LA2013072400124](https://openairdocs.org/sdr/39LA2013072400124.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin > FOUND 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 39LA2013072400114](https://openairdocs.org/sdr/39LA2013072400114.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin > WHILE 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 39LA2013072400104](https://openairdocs.org/sdr/39LA2013072400104.md): Bracket · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach Fittings > FOUND 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 39LA2013072400094](https://openairdocs.org/sdr/39LA2013072400094.md): Web · chafed · Jul 24, 2013 · N606AR · Casa C212CD · Fuel Storage > FOUND 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 39LA2013072400084](https://openairdocs.org/sdr/39LA2013072400084.md): Window Frame · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Structure > DURING 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 39LA2013072400074](https://openairdocs.org/sdr/39LA2013072400074.md): Attach Fitting · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage, Stabilizer Attach Fittings > WHILE 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 BUSH - [SDR 39LA2013072400064](https://openairdocs.org/sdr/39LA2013072400064.md): Frame · gouged · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Frame > FOUND DEEP GOUGE RT SIDE IN FRAME 1F. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2030. - [SDR 39LA2013072400054](https://openairdocs.org/sdr/39LA2013072400054.md): Skin · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin > WHILE 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 39LA2013072400044](https://openairdocs.org/sdr/39LA2013072400044.md): Skin · punctured · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin > LOWER 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 39LA2013072400034](https://openairdocs.org/sdr/39LA2013072400034.md): Frame · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Frame > FOUND 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 39LA2013072400024](https://openairdocs.org/sdr/39LA2013072400024.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin > FORWARD FUSELAGE LT SIDE, 1 DEEP DENT AT FS 3538, WL 33.0. REPAIRED IAW EO 2021032-309 AND EO2012032-424. - [SDR 39LA2013071900014](https://openairdocs.org/sdr/39LA2013071900014.md): Fitting · damaged · Jul 19, 2013 · N606AR · Casa C212CD · Fuselage, Wing Attach Fittings > BS 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 39LA2013071900004](https://openairdocs.org/sdr/39LA2013071900004.md): Skin · dented · Jul 19, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin > BELLY SKIN DENTED BEYOND LIMITS. REPLACED BELLY SKINS IAW EO 2021032-309 AND EO2012032-424. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/aircraft/N606AR/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.