# C A S A C-212-CD

- Type: Aircraft model (FAA registry)
- Registry code: 2410201
- Manufacturer (registry): C A S A
- Model: C-212-CD
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 19
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A43EU](https://openairdocs.org/tcds/A43EU) (OpenAirDocs)
- Holder: Airbus Defense and Space S.A.
- Registered aircraft: 1
- Page: https://openairdocs.org/model/c-a-s-a-c-212-cd

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2022-17-06](https://openairdocs.org/ad/2022-17-06): Fuselage · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 29, 2022
- [AD 2020-03-18](https://openairdocs.org/ad/2020-03-18): Flight Controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Apr 2, 2020
- [AD 2018-19-02](https://openairdocs.org/ad/2018-19-02): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Oct 22, 2018
- [AD 2017-01-10](https://openairdocs.org/ad/2017-01-10): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 22, 2017
- [AD 2015-16-04](https://openairdocs.org/ad/2015-16-04): Fire Protection · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 23 more. Effective Sep 15, 2015
- [AD 2013-24-09](https://openairdocs.org/ad/2013-24-09): Engine Controls · EADS CASA C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Jan 21, 2014
- [AD 2009-20-10](https://openairdocs.org/ad/2009-20-10): Auto Flight · EADS CASA C-212-CB, C-212-CC, C-212-CD and 1 more. Effective Nov 17, 2009
- [AD 2009-12-04](https://openairdocs.org/ad/2009-12-04): Navigation · EADS CASA C-212-CB, C-212-CC, C-212-CD and 3 more. Effective Jul 16, 2009
- [AD 2008-06-13](https://openairdocs.org/ad/2008-06-13): Centre wing lower skin · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 17, 2008
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2004-07-17](https://openairdocs.org/ad/2004-07-17): Nose landing gear (NLG) · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective May 11, 2004
- [AD 99-19-15](https://openairdocs.org/ad/99-19-15): AFM - Limitations Section - Ice Protection Systems · EADS CASA C-212-CB, C-212-CC, C-212-CD and 8 more. Effective Dec 27, 1999
- [AD 99-04-02](https://openairdocs.org/ad/99-04-02): Inspect Fuel Pump Cover Plates For Spark Marks · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 17, 1999
- [AD 98-22-04](https://openairdocs.org/ad/98-22-04): Power Quadrant Cover · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Nov 27, 1998
- [AD 98-18-21](https://openairdocs.org/ad/98-18-21): Corrosion Inspection · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 20, 1998
- [AD 98-12-28](https://openairdocs.org/ad/98-12-28): Inspect False Spar Of Wing For Cracking · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 15, 1998
- [AD 98-10-08](https://openairdocs.org/ad/98-10-08): Lower Shaft & Support Structure Of Rudder · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 17, 1998
- [AD 98-06-02](https://openairdocs.org/ad/98-06-02): Inspect Spherical Bearings Of Aileron Control Rod · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 15, 1998
- [AD 97-21-14](https://openairdocs.org/ad/97-21-14): Inspect Restrictor Pistons · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Nov 24, 1997
- [AD 97-03-13](https://openairdocs.org/ad/97-03-13): Rudder Pedal Setting Mechanisms · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 14, 1997
- [AD 96-09-22](https://openairdocs.org/ad/96-09-22): AFM - Icing · EADS CASA C-212-CB, C-212-CC, C-212-CD and 7 more. Effective Jun 11, 1996
- [AD 96-07-14](https://openairdocs.org/ad/96-07-14): Reduced Structural Integrity · EADS CASA C-212-CB, C-212-CC, C-212-CD and 2 more. Effective May 15, 1996
- [AD 92-13-51](https://openairdocs.org/ad/92-13-51): Backup Blocking Device · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 31, 1992
- [AD 91-03-10](https://openairdocs.org/ad/91-03-10): Propeller Speed & Pitch Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 11, 1991
- [AD 89-23-16](https://openairdocs.org/ad/89-23-16): Power Reserve System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Dec 12, 1989
- [AD 89-22-09](https://openairdocs.org/ad/89-22-09): Passenger Door Evacuation · Step and handrails (Fischer Brothers Avn STC SA906GL). Effective Nov 20, 1989
- [AD 89-19-05](https://openairdocs.org/ad/89-19-05): Rear Passenger Seats · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 14, 1989
- [AD 89-21-08](https://openairdocs.org/ad/89-21-08): Trim Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 5, 1989
- [AD 89-02-08 R1](https://openairdocs.org/ad/89-02-08-R1): Wing Flap Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 5, 1989
- [AD 89-05-01](https://openairdocs.org/ad/89-05-01): Wing Flap Control System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Apr 3, 1989
- [AD 88-09-02](https://openairdocs.org/ad/88-09-02): Fuel Shut-Off Valves · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 1, 1988
- [AD 87-16-04](https://openairdocs.org/ad/87-16-04): Stall Warning System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Aug 31, 1987
- [AD 87-10-08](https://openairdocs.org/ad/87-10-08): Crew Door Handle Cover · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jun 19, 1987
- [AD 87-05-07](https://openairdocs.org/ad/87-05-07): Attendant's Seat · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 25, 1987
- [AD 87-05-06](https://openairdocs.org/ad/87-05-06): Propeller Feathering Control · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 25, 1987
- [AD 87-04-10](https://openairdocs.org/ad/87-04-10): Smoke Detector System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 9, 1987
- [AD 87-04-02](https://openairdocs.org/ad/87-04-02): Nose Landing Gear · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 2, 1987
- [AD 87-03-04](https://openairdocs.org/ad/87-03-04): Trim Control Markings & Placards · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 19, 1987
- [AD 86-19-05](https://openairdocs.org/ad/86-19-05): Electrical System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Oct 2, 1986
- [AD 84-12-03](https://openairdocs.org/ad/84-12-03): Structural Flight Controls and Fuel System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Jul 23, 1984
- [AD 83-02-06](https://openairdocs.org/ad/83-02-06): Fuel Filter System · EADS CASA C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Feb 7, 1983

Historical (superseded or no longer in force):

- [AD 2021-16-07](https://openairdocs.org/ad/2021-16-07) (historical): Fuselage · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Sep 28, 2021
- [AD 2017-19-08](https://openairdocs.org/ad/2017-19-08) (historical): Flight controls · Airbus Defense and Space C-212-CB, C-212-CC, C-212-CD and 2 more. Effective Oct 25, 2017
- [AD 2007-05-01](https://openairdocs.org/ad/2007-05-01) (historical): Cracks had been found in the centre wing lower skin. · Construcciones Aeronauticas C-212-CB, C-212-CC, C-212-CD and 4 more. Effective Mar 14, 2007
- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996

## Registered aircraft (1)

- [N606AR](https://openairdocs.org/aircraft/N606AR): [412 Jw Aviation LLC](https://openairdocs.org/faa-owner/412%20JW%20AVIATION%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 1984, S/N 304

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (37)

As reported by operators and repair stations, by the model named in the report.

- [SDR JTAA202308231003](https://openairdocs.org/sdr/JTAA202308231003), Aug 21, 2023: ATTACH FITTING. CRACKED. PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.31 SHOWS REJECTABLE INDICA
- [SDR JTAA202308231002](https://openairdocs.org/sdr/JTAA202308231002), Aug 21, 2023: ATTACH FITTING. CRACKED. PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.31 SHOWS REJECTABLE INDICA
- [SDR JTAA202308231001](https://openairdocs.org/sdr/JTAA202308231001), Aug 21, 2023: ATTACH FITTING. CRACKED. PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.29 SHOWS REJECTABLE INDICA
- [SDR 2016FA0000220](https://openairdocs.org/sdr/2016FA0000220), May 10, 2016: HINGE BRACKET. CORRODED. RT INBD AILERON HINGE BRACKET FOUND TO HAVE EXFOLIATION CORROSION AT AIRFRAME ATTACH POINT, REQUIRING REPLACEMENT OF PART. OTHER CONTROL SURFACE HINGES/ATTACH B
- [SDR 2016F00121](https://openairdocs.org/sdr/2016F00121), May 10, 2016: BEARING. MIGRATED. COPILOT AILERON CONTROL ROD FOUND DISCONNECTED FROM INTERCONNECT BELLCRANK, DUE TO BEARING MIGRATION FROM ROD END. INSTALLATION DID NOT HAVE LARGE DIAMETER WASH
- [SDR 39LA20150404133](https://openairdocs.org/sdr/39LA20150404133), Apr 4, 2015: NUT. OUT OF POSITION. 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 INCI
- [SDR 39LA2014022860](https://openairdocs.org/sdr/39LA2014022860), Feb 28, 2014: CONNECTOR. DAMAGED. DURING CRUISE FLIGHT FROM OASH TO OAIX THE FLIGHT CREW COULD SMELL HOT ELECTRICAL FUMES IN THE FLIGHT DECK. THE QRH WAS COMPLIED WITH, & THE SOURCE OF THE ELECT
- [SDR 39LA2014022459](https://openairdocs.org/sdr/39LA2014022459), Feb 24, 2014: UNKNOWN. FUMES. DURING CRUISE FLIGHT FROM OAMS TO OAIX THE FLIGHT CREW EXPERIENCED FUMES IN THE FLIGHT DECK. O2 MASKS WERE DONNED BY THE CREW & THE QRH WAS COMPLIED WITH. THE E
- [SDR 8EKA201309130002](https://openairdocs.org/sdr/8EKA201309130002), Aug 23, 2013: ESCAPE HATCH. DEPARTED. AFTER NORMAL REFUELING OPERATION, REMOVE HATCH AND FUELED FROM TOP OF AIRPLANE, WENT TOPSIDE TO INSPECT THE FUEL CAPS. ON RETURNING TO CABIN, REINSTALLED HATCH.
- [SDR 8EKA201309130001](https://openairdocs.org/sdr/8EKA201309130001), Aug 23, 2013: ESCAPE HATCH. DEPARTED. AFTER THE NORMAL REFUELING, REMOVED HATCH AND FUELED FROM THE TOP OF AIRPLANE, WENT TOPSIDE TO INSPECT THE FUEL CAPS. ON RETURNING TO THE CABIN, REINSTALLED THE
- [SDR 39LA2013072400164](https://openairdocs.org/sdr/39LA2013072400164), Jul 24, 2013: BRACKET. CORRODED. 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 PREFOR
- [SDR 39LA2013072400154](https://openairdocs.org/sdr/39LA2013072400154), Jul 24, 2013: SKIN. DENTED. 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 2012032-20
- [SDR 39LA2013072400144](https://openairdocs.org/sdr/39LA2013072400144), Jul 24, 2013: SKIN. DENTED. 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
- [SDR 39LA2013072400134](https://openairdocs.org/sdr/39LA2013072400134), Jul 24, 2013: SKIN. CORRODED. 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 ENGIN
- [SDR 39LA2013072400124](https://openairdocs.org/sdr/39LA2013072400124), Jul 24, 2013: SKIN. CORRODED. FOUND CORROSION UNDER LT CENTER SECTION EXHAUST FAIRING DURING INSPECTION. CORROSION FOUND TO BE BEYOND MFG LIMITS. REPAIRED IAW EADS TECH INSTRUCTION NR 17 DAT
- [SDR 39LA2013072400114](https://openairdocs.org/sdr/39LA2013072400114), Jul 24, 2013: SKIN. CORRODED. 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 ENGIN
- [SDR 39LA2013072400104](https://openairdocs.org/sdr/39LA2013072400104), Jul 24, 2013: BRACKET. CORRODED. 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 
- [SDR 39LA2013072400094](https://openairdocs.org/sdr/39LA2013072400094), Jul 24, 2013: WEB. CHAFED. 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
- [SDR 39LA2013072400084](https://openairdocs.org/sdr/39LA2013072400084), Jul 24, 2013: WINDOW FRAME. CORRODED. 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 AIR
- [SDR 39LA2013072400074](https://openairdocs.org/sdr/39LA2013072400074), Jul 24, 2013: ATTACH FITTING. CRACKED. WHILE PERFORMING EDDY CURRENT INSPECTION, SUPPLEMENTAL INSPECTION DOCUMENT 20,000 /2,800 FLIGHT SUPPLEMENTAL INSPECTION OF HORIZONTAL STABILIZER, FOUND THAT LT 
- [SDR 39LA2013072400064](https://openairdocs.org/sdr/39LA2013072400064), Jul 24, 2013: FRAME. GOUGED. 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), Jul 24, 2013: SKIN. CRACKED. 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), Jul 24, 2013: SKIN. PUNCTURED. 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), Jul 24, 2013: FRAME. CRACKED. 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), Jul 24, 2013: SKIN. DENTED. 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), Jul 19, 2013: FITTING. DAMAGED. 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 2012032-20
- [SDR 39LA2013071900004](https://openairdocs.org/sdr/39LA2013071900004), Jul 19, 2013: SKIN. DENTED. BELLY SKIN DENTED BEYOND LIMITS. REPLACED BELLY SKINS IAW EO 2021032-309 AND EO2012032-424.
- [SDR EHAA20130211002](https://openairdocs.org/sdr/EHAA20130211002), Feb 11, 2013: ENGINE. POWER LOSS. FIFTEEN MINUTES INTO THE FLIGHT, THE NR 1 ENGINE EXPERIENCED A MOMENTARY POWER LOSS OF ABOUT TEN PERCENT TORQUE. ALL THE GAUGES INDICATED THE SAME AND THE ACFT 
- [SDR 39LA2013020600014](https://openairdocs.org/sdr/39LA2013020600014), Feb 5, 2013: ENGINE. POWER LOSS. DURING THE TAKEOFF ROLL, IT WAS DETERMINED THAT THE RT ENGINE WAS NOT MAKING THE PREDICTED POWER. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND ACFT WAS TAXIED B
- [SDR 39LA2013011800001](https://openairdocs.org/sdr/39LA2013011800001), Jan 16, 2013: INDICATOR. MALFUNCTIONED. AFTER DEPARTING, ENROUTE, THE TAWS FAILED. ACFT RETURNED BACK TO DEPARTURE. INSPECTED WIRING AND CONNECTIONS, NO DEFECTS NOTED. PERFORMED GPS AND TWAS SYS OPS A
- [SDR 3PRA201109070001](https://openairdocs.org/sdr/3PRA201109070001), Sep 7, 2011: SWITCH. BURNED. WHILE PERFORMING "BEFORE START" CHECKS WITH GPU CONNECTED AND POWERING SYS, A HEAVY ELECTRICAL BURNING ODOR AND SMOKE CAME FROM OVERHEAD ELECTRICAL PANEL. CREW 
- [SDR P4YA2010031600001](https://openairdocs.org/sdr/P4YA2010031600001), Apr 14, 2010: SKIN. CRACKED. DURING CENTER WING NDI DRIVEN BY THE REPETITIVE INSPECTION REQUIREMENT OF AD 2008-06-03 THROUGH THE INSP REQUIREMENTS OF AOL 212-018 REV2, EDDY CURRENT REVEALED
- [SDR RRI2001F00000](https://openairdocs.org/sdr/RRI2001F00000), Sep 23, 2001: PROPELLER. SEPARATED. PROP HUB SEPARATED AT BOLTS, LEAVING JUST THE AREA OF THE HUB THAT THE BOLTS ATTACH TO. THE HUB WAS NEW AT THE OVERHAUL. THERE WAS NO VIBRATION AT ALL DURING TH
- [SDR 2000ZZZX659](https://openairdocs.org/sdr/2000ZZZX659), Jan 27, 2000: SPAR. DAMAGED. DURING SCHEDULED MAINTENANCE CHECK, THE RIGHT HORIZONTAL STABILIZER AFT SPAR BEAM WAS FOUND CRACKED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. REPLACED AFT BEAM
- [SDR 99ZZZX4495](https://openairdocs.org/sdr/99ZZZX4495), Nov 15, 1999: GEAR. FAILED. THE NUT SECURING BEARING TO IDLER GEAR PN 896806-1 LOOSENED CAUSING GEAR TO BIND IN GEARCASE. THIS BINDING CAUSED THE NR 1 IDLER IN THE TORQUE SENSOR TO SHEER W
- [SDR 2000ZZZX658](https://openairdocs.org/sdr/2000ZZZX658), Nov 15, 1999: GEAR. FAILED. THE NUT SECURING BEARING TO IDLER GEAR, P/N 896806-1, LOOSENED CAUSING GEAR TO BIND IN GEARCASE. THIS BINDING CAUSED TNE NR 1 IDLER IN THE TORQUE SENSOR TO SHEE
- [SDR 99ZZZX1994](https://openairdocs.org/sdr/99ZZZX1994), Apr 13, 1999: PUMP. CRACKED. SIGNS OF DEFECT: LOW OIL PSI, HIGH TEMPERATURE, AND OIL TANK SPEWING OUT OIL (IT WAS BEING PRESSURIZED). INSPECTION (DISASSEMBLY) REVEALED SCAVENGE PUMP WAS CRA

## STCs that may be installed (OpenAirDocs) (37)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST04105NY](https://openairdocs.org/stc/ST04105NY): Installation of Flight Data Recorder, Flight Data Acquisition Unit, Traffic Advisory Altering System and Navigation Suite. CASA Flight Tech LLC
- [STC ST04109NY](https://openairdocs.org/stc/ST04109NY): Update of COMBI. CASA Flight Tech LLC
- [STC ST02257AK](https://openairdocs.org/stc/ST02257AK): Modify the aircraft configuration from 23 passenger seats to a combined cargo and passenger configuration. CASA Flight Tech LLC
- [STC ST02414AK](https://openairdocs.org/stc/ST02414AK): Reduction/limitation of passenger seats to 19 or fewer. Erickson Incorporated
- [STC ST00065MC](https://openairdocs.org/stc/ST00065MC): Installation of a Ballistic Protection System (BPS). Erickson Incorporated
- [STC ST09907AC](https://openairdocs.org/stc/ST09907AC): Installation of Hartzell 5-blade carbon composite propellers. BS Designs Inc
- [STC ST03558AT](https://openairdocs.org/stc/ST03558AT): Installation of a Collins TCAS-4000 (TCAS II) System (Version 7.0) with dual Collins TVI-920D VSI/TA/RA Indicators and associated hardware. Woven Electronics, LLC
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST02548AK](https://openairdocs.org/stc/ST02548AK): Installation of Main Gear Gravel Deflectors. Aero Twin Inc
- [STC ST04200NY](https://openairdocs.org/stc/ST04200NY): Installation of 19 Martin Baker Aircraft Company Inc. Seat. Carson Helicopters Inc
- [STC ST02540AK](https://openairdocs.org/stc/ST02540AK): Fabrication and installation of Aero Twin, Inc., Rudder Gust Lock Kit No. 4111-212. Aero Twin Inc
- [STC ST04248AT](https://openairdocs.org/stc/ST04248AT): Replacement of OEM metric flight control cables assemblies for the ailerion, elevator, rudder, ailerion trim tab, elevator trim tab, and rudder trim tab with MIL-SPEC standard cables assemblies. Bighorn Airways Inc
- [STC ST02433LA](https://openairdocs.org/stc/ST02433LA): Installation of LifePort Triple Litter Stacking System (TLSS). LifePort LLC
- [STC ST02099SE](https://openairdocs.org/stc/ST02099SE): Installation of a Supplemental Lighting System; manufactured and installed. Aviation Specialties Unlimited Inc
- [STC ST03993AT](https://openairdocs.org/stc/ST03993AT): Installation of a Universal Avionics EFI-890R Electronic Flight Instruments System (EFIS). Air Data Consulting Group, Inc
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST04157AT](https://openairdocs.org/stc/ST04157AT): Installation of Concorde lead acid batteries to replace nickel-cadmium (NiCd) batteries along with associated hardware. AAR Airlift Group
- [STC ST04178AT](https://openairdocs.org/stc/ST04178AT): Replace original equipment Nickel-Cadmium (NiCd) main and auxiliary batteries with Concorde Lead-Acid, main and auxiliary batteries along with associated hardware. Concorde Battery Corporation
- [STC ST02401AK](https://openairdocs.org/stc/ST02401AK): Installation of a Nose Gear Gravel Deflector. Aero Twin Inc
- [STC SA3686SW](https://openairdocs.org/stc/SA3686SW): Installation of floor proximity lighting system. BF Goodrich Aerospace
- [STC ST00673WI-D](https://openairdocs.org/stc/ST00673WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation. Rockwell Collins Inc
- [STC ST02559AK](https://openairdocs.org/stc/ST02559AK): Installation of Aero Twin, Inc. CASA 212 Exhaust Deflector, part number AT-CASA-EXDF-1001. Aero Twin Inc
- [STC SA1315SO](https://openairdocs.org/stc/SA1315SO): Installation of refreshment center. Aeronautical Engineers, Inc. Lists C-212 Series
- [STC ST00335NY](https://openairdocs.org/stc/ST00335NY): Remove existing starter-generator and install Aircraft Parts Corporation (APC) starter generator P/N. Shurka Aerospace Inc
- [STC ST03274AT](https://openairdocs.org/stc/ST03274AT): Passenger seating reconfiguration to 9 seats. Fayad Enterprises, LLC
- [STC ST01142WI-D](https://openairdocs.org/stc/ST01142WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc
- [STC ST03305AT](https://openairdocs.org/stc/ST03305AT): Installation of a SINGLE Class-A Sandel ST3400 Terrain Awareness Warning System (TAWS), pilot and co-pilot annunciator panels, and Air Data Computer (ADC) . Presidential Airways Inc
- [STC ST01394WI-D](https://openairdocs.org/stc/ST01394WI-D): Modification of a Collins CTL-23 or CTL-23C VHF COMM/NAV Control Panel System installation. Rockwell Collins Inc
- [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc
- [STC ST10215SC](https://openairdocs.org/stc/ST10215SC): Installation of Honeywell Mark VI Enhanced Ground Proximity Warning System (EGPWS) equipped with a HOneywell KMD 850 Multi-Function Display (MFD). Bighorn Airways Inc
- [STC SA5603NM-D](https://openairdocs.org/stc/SA5603NM-D): Installation of a Fairchild A100/A100A cockpit voice recorder. Learjet Inc
- [STC SA01900AT](https://openairdocs.org/stc/SA01900AT): Installation of a 9 seat passenger configuration. Gryphon Group International, Inc. Lists C-212 Series
- [STC SA971NE](https://openairdocs.org/stc/SA971NE): Installation of a single trimble TNL-3000 GPS/LORAN navigationsystem. Summit Aviation, Inc. Lists C-212 Series
- [STC SA3903NM](https://openairdocs.org/stc/SA3903NM): Installation of pedestal covers. American Casa Distributor Inc
- [STC SA2135NM](https://openairdocs.org/stc/SA2135NM): Class B aft baggage compartment -9G bulkhead, coat closet, baggage storage and refreshment service unit. Flight Structures Inc. Lists C-212 Series
- [STC SA2570CE](https://openairdocs.org/stc/SA2570CE): Replace the original generator control units with Phoenix Aerospace, Inc., Model GC-1010-24-3B solid state generator control units. Phoenix Aerospace Inc. Lists C-212 Series

## PMA parts (OpenAirDocs) (268, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [LSM-500-122](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195333909020260909145848.0001): Parmetheus Pro Instl. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 22, 2026
- [LSM-500-116](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182431779620260909145847.0001): Boom Beam Instl, Casa. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 22, 2026
- [M23065-1470](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174779225620241113171048.0001): Fan Cover. Miraj Corporation · PMA PQ0870NE · Replaces 23065-1470 · Nov 8, 2024
- [M06-201100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195622496020241022163146.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-201100 · Oct 10, 2024
- [SMR5028-09](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193731374620241115132847.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-09 · Sep 19, 2024
- [SMR5028-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185115321820241115132847.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-04 · Sep 19, 2024
- [SMR5028-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171978906820241115132846.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-01 · Sep 19, 2024
- [SMR5028-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165017066320241115132848.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-10 · Sep 19, 2024
- [SMR5028-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147943599320241115132846.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-03 · Sep 19, 2024
- [SMR5028-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139801511620241115132846.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-02 · Sep 19, 2024
- [SMR5028-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123114250420241115132847.0001): Pneumatic De-icer. SMR Acquisition LLC dba SMR Technologies Inc · PMA PQ0845NE · Replaces 25S7D5028-07 · Sep 19, 2024
- [AF9536741](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196094035920240612184642.0001): SPRING, DISK. Airforms LLC · PMA PQ2644CE · Replaces 9536741 · May 13, 2024
- [AF9536259](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195796865120240612184642.0001): RING, DISK DRIVE. Airforms LLC · PMA PQ2644CE · Replaces 9536259 · May 13, 2024
- [AF5000483](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189418556920240612184641.0001): WHEEL HUB, INBOARD. Airforms LLC · PMA PQ2644CE · Replaces 5000483 · May 13, 2024
- [AFGY165MS36](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177883572520240612184643.0001): BOLT, HIGH STRENGTH. Airforms LLC · PMA PQ2644CE · Replaces GY165MS36 · May 13, 2024
- [AF5000728](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171295839220240612184642.0001): PLUNGER, TEE BAR. Airforms LLC · PMA PQ2644CE · Replaces 5000728 · May 13, 2024
- [AF5004387](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156476123420240612184643.0001): SEAL. Airforms LLC · PMA PQ2644CE · Replaces 5004387 · May 13, 2024
- [AF5000485](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149935582220240612184641.0001): WHEEL HUB, OUTBOARD. Airforms LLC · PMA PQ2644CE · Replaces 5000485 · May 13, 2024
- [AF5000485-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141634036820240612184641.0001): WHEEL HUB, OUTBOARD. Airforms LLC · PMA PQ2644CE · Replaces 5000485-2 · May 13, 2024
- [AF5006586](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139940080820240612184639.0001): MAIN WHEEL ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 5006586 · May 13, 2024
- [AF9533857](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136084406720240612184643.0001): SEAL. Airforms LLC · PMA PQ2644CE · Replaces 9533857 · May 13, 2024
- [AF5000482](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116995737520240612184641.0001): WHEEL SUBASSEMBLY, INBOARD. Airforms LLC · PMA PQ2644CE · Replaces 5000482 · May 13, 2024
- [AF5006586-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104525460820240612184640.0001): MAIN WHEEL ASSEMBLY. Airforms LLC · PMA PQ2644CE · Replaces 5006586-2, 5006586-1 · May 13, 2024
- [AFGWA182-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102289087520240612184643.0001): WASHER, DOUBLE-RECESSED. Airforms LLC · PMA PQ2644CE · Replaces GWA182-5 · May 13, 2024
- [M06-200001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140100423620240223153731.0001): Label. Miraj Corporation · PMA PQ0870NE · Replaces Safran 06-200001 · Feb 15, 2024
- [394390-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194442988120231221185038.0001): Flow Divider Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394390-1-1 · Apr 13, 2023
- [394230-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172944965920231221185038.0001): Fuel Solenoid. Honeywell International Inc. · PMA PQ1222NM · Replaces 394230-4-1 · Apr 13, 2023
- [978944-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161625104920231221185038.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 978944-1-1 · Apr 13, 2023
- [394408-10-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157199329620231221185038.0001): Flow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394408-10-1 · Apr 13, 2023
- [319980-6-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139156544320231221185037.0001): Shutoff Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 319980-6-1 · Apr 13, 2023
- [394396-1-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134852963620231221185038.0001): Flow Divider Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 394396-1-1 · Apr 13, 2023
- [C212-TCAS-900](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168728984620230504173355.0001): TCAS 4000 INSTALLATION TOP KIT. Woven Electronics, LLC · PMA PQ00009EB · Replaces C212-TCAS-900 · Dec 1, 2022
- [MG94A-902-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137070962420220916174319.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 23093-1305 · Aug 29, 2022
- [M23088-1348](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152168509320220808113437.0001): Brush, Electrical Contact. Miraj Corporation · PMA PQ0870NE · Replaces 300SGL1009-5 · Jul 18, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137843162120220809130823.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183136835520220809102459.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155429232820220408135717.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022
- [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102545922820220408135653.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022
- [111608-1MIT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID910291084820220208124954.0001): Pin. Mitchell PMA, LLC · PMA PQ04379CE · Replaces 111608-1 · Jan 13, 2022
- [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141640838920220408135615.0001): Gasket, Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157368644820220408135729.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111242205720220408140205.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG843000-17](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID936553775020211110110424.0001): Gasket-UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Aug 9, 2021
- [212-201-05-COV](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID876796333120210608151243.0001): 2.00 CHANNEL ASSEMBLY COVER. Carson Helicopters, Inc. · PMA PQ4181NE · Modification part · May 26, 2021
- [MGDC-212](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166914142420210617193111.0001): Main Gear Gravel Deflector Kit. Aero Twin Inc · PMA PQ2503CE · Modification part · Apr 19, 2021
- [AG358000-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID572734396202107271951110.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 11, 2020
- [858886JP-14](https://drs.faa.gov/browse/excelExternalWindow/B9B5C70564E8693086258656006EB8DB.0001): Diaphragm Assembly. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 858886-14 · Nov 26, 2020
- [AG843000-79](https://drs.faa.gov/browse/excelExternalWindow/7C47B4B54B5941DF862586240047DC8E.0001): Gasket - UHF / AM / IFF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2020
- [AG477000-35](https://drs.faa.gov/browse/excelExternalWindow/CAA7A03C831CF5A78625861F004520E1.0001): Gasket - GPS ANTENNA. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 11, 2020
- [4111-212](https://drs.faa.gov/browse/excelExternalWindow/94038EDF0BB9A08A862586260044AD64.0001): Rudder Gust Lock Kit. Aero Twin Inc · PMA PQ2503CE · Modification part · Nov 8, 2020

All of them: https://openairdocs.org/model/c-a-s-a-c-212-cd/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Construcciones Aeronauticas C-212-CD](https://openairdocs.org/model/construcciones-aeronauticas-c-212-cd): 1 registered aircraft, registry code 2410209

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