# N602AR: 1980 EADS CASA C-212-CC-15 AVIOCAR, registration cancelled 2022-03-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 4, 2022 - Status when cancelled: Valid registration - Airframe: [EADS CASA C-212-CC-15 AVIOCAR](https://openairdocs.org/model/eads-casa-c-212-cc-15-aviocar) (registry code 8682005) - Engine: [Honeywell TPE331-10](https://openairdocs.org/engine/honeywell-tpe331-10) (registry code 33977) - Data sheets: [TCDS E4WE](https://openairdocs.org/tcds/E4WE) (OpenAirDocs) - Serial number: 161 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: September 26, 2012 - Certificate issued: October 10, 2019 - Last registry action: October 10, 2019 - Mode S code: A7CEBD - Owner when cancelled: [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N602AR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=602AR - Page: https://openairdocs.org/deregistered/N602AR-2022-03-04 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the EADS CASA C-212-CC-15 AVIOCAR: https://openairdocs.org/model/eads-casa-c-212-cc-15-aviocar.md ## Service difficulty reports (33) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 39LA2019061105182](https://openairdocs.org/sdr/39LA2019061105182), Jun 5, 2019: SKIN. PUNCTURED. DURING SCHEDULED INSPECTIONS, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE TAIL STAND MOUNT. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY - [SDR 39LA2019060311801](https://openairdocs.org/sdr/39LA2019060311801), May 31, 2019: FLOORBEAM. CORRODED. DURING SCHEDULED INSPECTIONS, THE FLOOR BEAM AT LANDING GEAR FRAME 9 WAS FOUND TO HAVE CORROSION AT A FLOORBOARD NUTPLATE. ASSEMBLY OF A TECHNICAL DATA PACKAGE - [SDR 39LA20190531180](https://openairdocs.org/sdr/39LA20190531180), May 31, 2019: ANGLE. CORRODED. DURING SCHEDULED INSPECTIONS, A T-ANGLE WAS FOUND TO BE CORRODED ON THE CARGO/RAMP DOOR. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE RE - [SDR 39LA20181030178](https://openairdocs.org/sdr/39LA20181030178), Oct 30, 2018: CHANNEL. CORRODED. DURING REPAIR ACTIONS TO THE RT INBD FLAP PIVOT CONTROL POINT, THE CHANNEL ATTACHED TO THE SUPPORT BOX WAS FOUND TO BE CORRODED. REF SRM FIG 2-24 POS 3 DWG 212- - [SDR 39LA20181030177](https://openairdocs.org/sdr/39LA20181030177), Oct 30, 2018: FITTING. WORN. DURING INSPECTION, DANAGE WAS NOTED TO THE RT INBD FLAP PIVOT CONTROL POINT. THE LT AND RT FITTING PLATES WERE FOUND WORN BEYOND LIMITS AT THE BOLT HOLES. REF S - [SDR 39LA20151004145](https://openairdocs.org/sdr/39LA20151004145), Oct 4, 2015: BLADE. CRACKED. DURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED. - [SDR 39LA20150902142](https://openairdocs.org/sdr/39LA20150902142), Sep 2, 2015: UNKNOWN. FUMES. DURING CRUISE, WHEN HEATER VLV OPENED, THE FLIGHT CREW NOTICED FUMES IN BOTH THE FLIGHT DECK & CABIN. TESTED GEARBOX FOR POSITIVE PRESS & FOUND NORMAL NEGATIVE - [SDR 39LA20150430134](https://openairdocs.org/sdr/39LA20150430134), Apr 30, 2015: CONTROL QUADRANT. CORRODED. LEFT AILERON CABLE QUADRANT HAS AN AREA OF EXFOLIATION CORROSION APPROX 1.00 INCH BY .750 INCH BY .125 DEEP. REPLACED LT AILERON CABLE QUADRANT IAW AMM 27-11-02 - [SDR 39LA20150326131](https://openairdocs.org/sdr/39LA20150326131), Mar 26, 2015: FRAME. DAMAGED. FOUND OVERSIZED HOLE IN FRAME 18F, STRINGER 08, ON INSPECTION. REPAIRED IAW EO 14022-300 & DWG 14022-2012. - [SDR 39LA20150326130](https://openairdocs.org/sdr/39LA20150326130), Mar 26, 2015: FLAP. CHAFED. RIGHT WING OTBD FLAP FOUND CHAFED & CRACKED UPON INSPECTION. REPAIRED IAW EO 14022-300 & DWG 14022-2002. - [SDR 39LA20150326129](https://openairdocs.org/sdr/39LA20150326129), Mar 26, 2015: FLAP. DENTED. RIGHT INBD FLAP LE DENTED. REPAIRED IAW EO 14022-2018. - [SDR 39LA20150326128](https://openairdocs.org/sdr/39LA20150326128), Mar 26, 2015: ANGLE. CRACKED. CRACK ABOUT 1/2 INCH ON ANGLE, INSIDE OF LT AILERON ABOVE ACCESS PANEL 540 EB. - [SDR 39LA20150326127](https://openairdocs.org/sdr/39LA20150326127), Mar 26, 2015: SPAR. CORRODED. RIGHT WING LE SPAR WING STATION 7700 FOUND TO HAVE LEVEL 2 EXFOLIATION CORROSION. REPAIRED IAW EO 14022-300. - [SDR 39LA20150326126](https://openairdocs.org/sdr/39LA20150326126), Mar 26, 2015: STRUCTURE. CORRODED. LEFT WING TE FLAP WELL WS 6300 EXFOLIATION CORROSION FOUND DURING HEAVY CHECK INSPECTION. REPAIRED IAW EO 14022-300. - [SDR 39LA20150326125](https://openairdocs.org/sdr/39LA20150326125), Mar 26, 2015: SKIN. CRACKED. INSPECTION OF LT ELEVATOR REVEALED TWO SMALL CRACKS ON LE OF ELEVATOR. REPAIRED IAW DWG 14022-2016 & EO 14022-300. - [SDR 39LA20150326124](https://openairdocs.org/sdr/39LA20150326124), Mar 26, 2015: MOUNT. CHAFED. NUMBER 1 ENG EXHAUST DUCT AFT INBD MOUNT FOUND CHAFED ABOVE & BELOW BASE OF MOUNT STUD. REPLACED WITH SERVICEABLE UNIT IAW MM. - [SDR 39LA20150326123](https://openairdocs.org/sdr/39LA20150326123), Mar 26, 2015: SKIN. CRACKED. LEFT OTBD WING LE CRACKED AT WS 7700. REPAIRED IAW DWG 14022-2011 & EO 14022-300. - [SDR 39LA20150326122](https://openairdocs.org/sdr/39LA20150326122), Mar 26, 2015: BUSHING. CORRODED. RIGHT ENG LOWER ATTACH FITTING BUSHING CORRODED. REPAIRED IAW DWG 14022-2013 & EO 14022-300. - [SDR 39LA20150326121](https://openairdocs.org/sdr/39LA20150326121), Mar 26, 2015: SKIN. DAMAGED. AIRFRAME SKIN AT LT FWD ENTRY DOOR, FS 3150, STRINGER 16L, FOUND DAMAGED UPON INSPECTION. REPAIRED IAW DWG 14022-2001 & EO 14022-300. - [SDR 39LA20150326120](https://openairdocs.org/sdr/39LA20150326120), Mar 26, 2015: SKIN. CORRODED. RIGHT HORIZONTAL STAB LE CORRODED UNDER DE-ICE BOOT. REPAIRED IAW DWG 14022-2010 & EO14022-300. - [SDR 39LA20150326119](https://openairdocs.org/sdr/39LA20150326119), Mar 26, 2015: SKIN. CORRODED. LEFT HORIZONTAL STABILIZER LE CORRODED UNDER DE-ICE BOOT. REPAIRED IAW EO14022-300 & DWG 14022-2009. - [SDR 39LA20150326118](https://openairdocs.org/sdr/39LA20150326118), Mar 26, 2015: DOOR FRAME. PUNCTURED. AIRFRAME SIDE OF EMER ESCAPE HATCH FOUND PUNCTURED 1" FWD OF LOCK MOUNT HOLE. REPAIRED IAW EO 14022-300 & DWGS 14022-2004, 14022-2005, 14022-2006 & 14022-2007. - [SDR 39LA20150326117](https://openairdocs.org/sdr/39LA20150326117), Mar 26, 2015: SKIN. CORRODED. LEFT LOWER WING SKIN EXFOLIATED AT WING STATION 2485. REPAIRED IAW EO 14022-300 SECTION 8 15. - [SDR 39LA20150326116](https://openairdocs.org/sdr/39LA20150326116), Mar 26, 2015: STRINGER. CORRODED. LEFT WING CTR SECTION STRINGER FOUND CORRODED AT WING STATION 3296, THIRD STRINGER FWD. REPAIRED IAW EO 14022-300 SECTION 8 14. - [SDR 39LA20150326115](https://openairdocs.org/sdr/39LA20150326115), Mar 26, 2015: SKIN. DENTED. MULTIPLE DENTS FOUND IN ACFT SKIN ON BOTTOM OF FUSELAGE. REPAIRED IAW EO 14022-300. - [SDR 39LA20150326114](https://openairdocs.org/sdr/39LA20150326114), Mar 26, 2015: THRESHOLD. CORRODED. LEFT AFT ENTRANCE DOOR THRESHOLD FOUND CORRODED. REPLACED WITH SERVICEABLE IAW EO14022-300 & DWG 14022-2017. - [SDR 39LA20150326113](https://openairdocs.org/sdr/39LA20150326113), Mar 26, 2015: FLOORBEAM. CORRODED. FLOORBEAM UPPER T CAP SHOWED EXFOLIATION CORROSION AT LT SEAT TRACK, FS 6250. REPLACED UPPER T CAP WITH SERVICEABLE IAW EO 14022-300 & DWG 14022-2008. - [SDR 39LA20150326112](https://openairdocs.org/sdr/39LA20150326112), Mar 26, 2015: FLOORBEAM. CORRODED. FLOORBEAM UPPER CAP LT SIDE AT FS 8326, BL 20 FOUND CORRODED. REPAIRED IAW EO 14022-300, ITEM 8 16. - [SDR 39LA20150326111](https://openairdocs.org/sdr/39LA20150326111), Mar 26, 2015: BRACKET. CRACKED. RIGHT WING OUTER FLAP INBD STANCHION CAREEN LE CHAFED & CRACKED. REPAIRED IAW EO 14022-300. OPERATIONAL & FUNCTIONAL CHECKS SATISFACTORY IAW 212-200 MM. - [SDR 39LA20150326110](https://openairdocs.org/sdr/39LA20150326110), Mar 26, 2015: CAP. CORRODED. RIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300. - [SDR 39LA2013112725](https://openairdocs.org/sdr/39LA2013112725), Nov 27, 2013: UNKNOWN. ODOR. DURING FLIGHT WITH ENG BLEED AIR ON, OIL SMELL IN CABIN WITH SMOKE DETECTORS BEING SET OFF. ENG BLEED AIR TURNED OFF, SMOKE SMELL DISSIPATED & SMOKE DETECTORS S - [SDR KGBR2012101000001](https://openairdocs.org/sdr/KGBR2012101000001), Oct 10, 2012: SKIN. CORRODED. CORROSION FOUND ON TOP OF CENTER WING SKIN AT CWS 2380 & 2900 LT, IN THE AREAS OF THE ENGINE FAIRING. - [SDR KGBR2012070600001](https://openairdocs.org/sdr/KGBR2012070600001), Jul 6, 2012: SPAR. CORRODED. LT WING, UPPER FWD SPAR AFT HORIZONTAL LEG, EXFOLIATED AT APPROX WS 3496, ALSO PROBABLE EXFOLIATION AT WS 2130 TO 2450 AND POSSIBLE EXFOLIATION AT WS 2900 TO 30 ## Other aircraft with N602AR - [Cancelled 1996-05-22](https://openairdocs.org/deregistered/N602AR-1996-05-22): Boeing 727-228, S/N 20075. Triennial form not returned. Owner: [Aar Financial Services Corp](https://openairdocs.org/faa-owner/AAR%20FINANCIAL%20SERVICES%20CORP), [Elk Grove Village, IL](https://openairdocs.org/faa-place/IL/Elk%20Grove%20Village) --- 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.