# Construcciones Aeronauticas C-212-CC

- Type: Aircraft model (FAA registry)
- Registry code: 2410204
- Manufacturer (registry): CONSTRUCCIONES AERONAUTICAS SA
- Model: C-212-CC
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 28
- 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: 12
- Page: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc

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 2006-15-12](https://openairdocs.org/ad/2006-15-12): Protective liner between the passengers and the cargo. · EADS CASA C-212-CC with STC ST02129AK. Effective Aug 29, 2006
- [AD 2006-15-11](https://openairdocs.org/ad/2006-15-11): Protective liner between the passengers and the cargo. · EADS CASA C-212-CC with STC ST02177AK. Effective Aug 29, 2006
- [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 84-02-03](https://openairdocs.org/ad/84-02-03): Exit Doors Modification · EADS CASA C-212-CB and C-212-CC. Effective Feb 27, 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 (12)

- [N107BH](https://openairdocs.org/aircraft/N107BH): [Bighorn Airways Inc](https://openairdocs.org/faa-owner/BIGHORN%20AIRWAYS%20INC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1979, S/N 165
- [N109BH](https://openairdocs.org/aircraft/N109BH): [Bighorn Airways Inc](https://openairdocs.org/faa-owner/BIGHORN%20AIRWAYS%20INC), [Sheridan, WY](https://openairdocs.org/faa-place/WY/Sheridan), built 1981, S/N 192
- [N1331C](https://openairdocs.org/aircraft/N1331C): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1982, S/N 265
- [N348CA](https://openairdocs.org/aircraft/N348CA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1981, S/N 175
- [N349TA](https://openairdocs.org/aircraft/N349TA): [Bering Air Inc](https://openairdocs.org/faa-owner/BERING%20AIR%20INC), [Nome, AK](https://openairdocs.org/faa-place/AK/Nome), built 1986, S/N 349
- [N352CA](https://openairdocs.org/aircraft/N352CA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 1981, S/N 190
- [N422CA](https://openairdocs.org/aircraft/N422CA): [Bering Air Inc](https://openairdocs.org/faa-owner/BERING%20AIR%20INC), [Nome, AK](https://openairdocs.org/faa-place/AK/Nome), built 1982, S/N 238
- [N426CA](https://openairdocs.org/aircraft/N426CA): [Spitaker Leasing LLC](https://openairdocs.org/faa-owner/SPITAKER%20LEASING%20LLC), [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs), built 1981, S/N 168
- [N440RA](https://openairdocs.org/aircraft/N440RA): [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), S/N 174
- [N758XP](https://openairdocs.org/aircraft/N758XP): [Paraclete Aviation LLC](https://openairdocs.org/faa-owner/PARACLETE%20AVIATION%20LLC), [Raeford, NC](https://openairdocs.org/faa-place/NC/Raeford), built 1981, S/N 138
- [N8517A](https://openairdocs.org/aircraft/N8517A): [Airbus Ds Military Aircraft Inc](https://openairdocs.org/faa-owner/AIRBUS%20DS%20MILITARY%20AIRCRAFT%20INC), [Mobile, AL](https://openairdocs.org/faa-place/AL/Mobile), built 1981, S/N 178
- [N961BW](https://openairdocs.org/aircraft/N961BW): [Construction Helicopters LLC](https://openairdocs.org/faa-owner/CONSTRUCTION%20HELICOPTERS%20LLC), [Howell, MI](https://openairdocs.org/faa-place/MI/Howell), S/N 248

## NTSB investigations (4)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC09LA104](https://openairdocs.org/ntsb/ANC09LA104), Sep 18, 2009: CASA 212-200 (N349TA), Savoonga, AK, substantial damage. Probable cause: The pilot’s failure to maintain directional control during the landing roll in a gusting crosswind.
- [NTSB ANC09LA019](https://openairdocs.org/ntsb/ANC09LA019), Feb 14, 2009: Construcciones Aeronauticas C-212-CC (N440RA), Kotzebue, AK, substantial damage. Probable cause: The flight crew's decision to continue flight into adverse weather. Contributing to the accident was blowing snow which limited their visibility during final approach to land.
- [NTSB IAD05FA023](https://openairdocs.org/ntsb/IAD05FA023), Nov 27, 2004: CASA 212-200-CC (N960BW), Bamiyan, Afghanistan, destroyed, 6 fatal. Probable cause: the captain's inappropriate decision to fly a nonstandard route and his failure to maintain adequate terrain clearance, which resulted in the inflight collision with mountainous terrain. Factors were…
- [NTSB DCA87MA022](https://openairdocs.org/ntsb/DCA87MA022), Mar 4, 1987: CASA C-212-CC (N160FB), Romulus, MI, destroyed, 9 fatal

## FAA accident and incident reports (19)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20221015010079I](https://openairdocs.org/incident/20221015010079I), Oct 15, 2022: Construcciones Aeronauticas Sa C-212-CC (N1331C), Unalakleet, AK, No damage. Company casa 212 for [privacy data omitted] was departing runway 33 in Unalakleet, Alaska. VMC conditions -there was a 20 knot crosswind and the runway…
- [Incident 20220926011069I](https://openairdocs.org/incident/20220926011069I), Sep 26, 2022: Construcciones Aeronauticas Sa C-212-CC (N349TA), Kotzebue, AK, Minor damage. While taxing on otz base ramp area after PART135 cargo flight, aircraft cut turn sharp and sruck left wing on a loader parked on the south side of ramp,…
- [Incident 20180326010231I](https://openairdocs.org/incident/20180326010231I), Mar 26, 2018: Construcciones Aeronauticas Sa C-212-CC (N107BH), Sheridan, WY, Minor damage. On March 26, 2018 at 1732 MDT, N107BH a casa 212 taxiing to parking struck the wing tip of another casa 212 N217BH that was parked on the ramp. There were five…
- [Incident 20170308001969I](https://openairdocs.org/incident/20170308001969I), Mar 8, 2017: Construcciones Aeronauticas Sa C-212-CC (N109BH), Sheridan, WY, Minor damage. N109BH, a casa 212, was flight training at shr,WY. Airport; executing touch and go landings on runway 15. After touch down ,the aircraft was re-configured for…
- [Incident 20120307012399I](https://openairdocs.org/incident/20120307012399I), Mar 7, 2012: Construcciones Aeronauticas Sa C-212-CC (N963BW), Bagram, Minor damage. FAA not able to go to scene. All/most information provided by air carrier. When the nose wheel touched during landing the a/c made an immediate left turn and…
- [Accident 20090918049699A](https://openairdocs.org/incident/20090918049699A), Sep 18, 2009: Construccio C-212-CC (N349TA), Savoonga, AK, Substantial damage. The pilots stated that they touched down on runway 05 in Savoonga and the aircraft began to drift to the right. The captain added power on the right engine to…
- [Accident 20090214025049A](https://openairdocs.org/incident/20090214025049A), Feb 14, 2009: Construccio C-212-CC (N440RA), Kotzebue, AK, Substantial damage. Ptrs #AL01200901225FLIGHT 1240 was returning to Kotzebue the ATIS was checked and the visibility was 6 statute miles. The visibility deteriorated to 1 1/4…
- [Incident 20071103826859I](https://openairdocs.org/incident/20071103826859I), Nov 3, 2007: Casa C212CC (N426CA), Houston, TX, No damage. (-23) Parachutist broke his left ankle during a high speed downwind landing during a demonstration mass parachute jump at the ballunar liftoff festival on the…
- [Incident 19870323028559I](https://openairdocs.org/incident/19870323028559I), Mar 23, 1987: Casa C212CC (N346CA), Abilene, TX. Right engine flamed out on landing when propeller was put in reverse thrust. Pilot tube found sheared.
- [Accident 19870304009469A](https://openairdocs.org/incident/19870304009469A), Mar 4, 1987: Casa C212CC (N160FB), Detroit, MI, Destroyed, 9 fatal. Crashed while operating the propeller in the beta mode on final. Too slow plane caused asymetric thrust. Lost control
- [Incident 19851230070419I](https://openairdocs.org/incident/19851230070419I), Dec 30, 1985: Casa C212CC (N352CA), Abilene, TX. During training flight engine was shutdown but propeller control was binding. Repositioned cable after landing.
- [Incident 19850502040659I](https://openairdocs.org/incident/19850502040659I), May 2, 1985: Casa C212CC (N169FB), Kalamazoo, MI. Low oil pressure indication with EGT rise. Engine shutdown and returned. Misalignment of aeroquip fitting.
- [Incident 19840801051779I](https://openairdocs.org/incident/19840801051779I), Aug 1, 1984: Casa C212CB (N348CA), Ft Worth, TX. Copilot lapsed into unconsciousness for a short period during flight. Was reinstated after medical tests.
- [Incident 19840405019939I](https://openairdocs.org/incident/19840405019939I), Apr 5, 1984: Bell 212 (N346CA), Dallas, TX. Departed left side of runway on rollout. Found faulty steering actuator and pressure directional valve.
- [Incident 19831107070469I](https://openairdocs.org/incident/19831107070469I), Nov 7, 1983: Bell 212 (N348CA), Abilene, TX. Fire erupted in engine after run up and shutdown while boarding passengers. Starting procedures to be changed.
- [Incident 19830204007389I](https://openairdocs.org/incident/19830204007389I), Feb 4, 1983: Casa C212200 (N160FB), Columbus, OH, Minor damage. Lost control on landing roll as a wind gust picked up a wing and dragged the other wing on the runway.
- [Incident 19821115065649I](https://openairdocs.org/incident/19821115065649I), Nov 15, 1982: Casa C212200 (N160FB), Romulus, MI, Damage unknown. Left engine failure. Engine was feathered. Normal landing. Suspect a shaft in the nose case failed.
- [Incident 19820627040059I](https://openairdocs.org/incident/19820627040059I), Jun 27, 1982: Bell 212 (N346CA), Abilene, TX. Pilot was testing negative torque system incorrectly. Caused an off airport landing. No defects in nts system.
- [Incident 19820306007099I](https://openairdocs.org/incident/19820306007099I), Mar 6, 1982: Casa C212 (N346CA), Irving, TX. Zt za smoke from panel on climbout. Cut off circuits. Landed ok. Left prop beta light wiring shorted.

## Service difficulty reports (201, newest 50)

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

- [SDR UATA2650916265301](https://openairdocs.org/sdr/UATA2650916265301), Sep 16, 2026: SKIN. DAMAGED. FS 27 LOWER BEAM & LOWER SKINS DAMAGED. REMOVED F27 LOWER BEAM. PREVIOUSLY REPAIRED RT LOWER SKIN SECTION, LT & RT FS27 TO C CHANNEL BRACKETS/CVR BOX MOUNTING S
- [SDR UATA2026072835701](https://openairdocs.org/sdr/UATA2026072835701), Jul 23, 2026: HINGE FITTING. CORRODED. RT & LT INNER FLAP, OTBD PYLON, OTBD HINGE FITTINGS FOUND CORRODED. APPROXIMATE WS 2900. REMOVED DAMAGED FITTINGS. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE 
- [SDR UATA20264105702](https://openairdocs.org/sdr/UATA20264105702), Apr 8, 2026: SKIN. CORRODED. RH INNER FLAP, OUTBOARD PYLON, OUTBOARD SKIN CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WING STATION 
- [SDR UATA1900410265701](https://openairdocs.org/sdr/UATA1900410265701), Apr 8, 2026: HINGE. CORRODED. RH INBOARD FLAP, OUTBOARD PYLON BOTH FLAP HINGE PLATES CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WIN
- [SDR UATA2650406267901](https://openairdocs.org/sdr/UATA2650406267901), Apr 6, 2026: OIL COOLER. FAILED. LEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.
- [SDR UATA202603275702](https://openairdocs.org/sdr/UATA202603275702), Mar 20, 2026: SKIN. CRACKED. RIGHT WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS5000 AS MARKED. REPAIRED CRACKED SECTION OF RH FLAP COVE SKIN. SEE 337 DATED 3
- [SDR UATA1740327265701](https://openairdocs.org/sdr/UATA1740327265701), Mar 20, 2026: SKIN. CRACKED. RH WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS4800 AS MARKED. REPAIRED CRACKED SECTION OF RT FLAP COVE SKIN. REMOVED 75MM X 25M
- [SDR UATA202603275304](https://openairdocs.org/sdr/UATA202603275304), Mar 18, 2026: CHANNEL. WORN. WEAR MARK ON C CHANNEL SECTION BETWEEN L/H FRAMES 17-20. R&R WITH P/N: 212-23201-03-1 IRW CASA 212 SRM SECTION IV FIGURE 4.28 PAGES 0A-02 & INSTALLED WITH FASTE
- [SDR UATA1740327265303](https://openairdocs.org/sdr/UATA1740327265303), Mar 18, 2026: DOUBLER. CRACKED. REPAIR DOUBLER AT LOWER END OF FRAME 19 CRACKED (LH SIDE). REPLACED DOUBLER SEE 337 DATED 3/18/2026. CRACK FOUND AT DOUBLER FOR L/H FRAME 19. R&R WITH 2 DOUBLER
- [SDR UATA1740327265301](https://openairdocs.org/sdr/UATA1740327265301), Mar 16, 2026: GUSSET. CORRODED. RH SIDE FR 6 & FR 11 FLOOR SUPPORT GUSSETS NUT PLATES CORRODED. REPLACED F6/F11 JUNCTION BARS. FOUND 4 FUSELAGE JUNCTION FITTINGS CORRODED ON RH AT FRAME 6 & 11
- [SDR UATA1750227265701](https://openairdocs.org/sdr/UATA1750227265701), Feb 27, 2026: SKIN. CRACKED. TWO CRACKS FOUND IN TRAILING EDGE OF LT LOWER INNER FLAP COVE AT APPROXIMATE WS 1800 & 2800. REMOVED 6 1/4 X 2 3/8 SECTION FROM OTBD CRACKED AREA & 4 1/4 X 2 3/
- [SDR UATA2025100605301](https://openairdocs.org/sdr/UATA2025100605301), Sep 25, 2025: FAIRING. CRACKED. FOUND CRACK IN RH WING TO FUSELAGE FAIRING AT FRAME F5. (SEE AOT-C212-53-0001 FOR DETAILS). REPAIRED CRACK DAMAGE AND REINFORCED F5 RH BY INSTALLATION OF SB KIT
- [SDR UATA1750815255701](https://openairdocs.org/sdr/UATA1750815255701), Aug 13, 2025: HINGE. CRACKED. LH AILERON CENTER HINGE STRUCTURE, A PREVIOUS REPAIR PATCH IS CRACKED. REPAIR WAS ACCOMPLISHED AS FOLLOWS: REMOVED THE PREVIOUS CRACKED REPAIR ANGLE. USING THE 
- [SDR UATA1750702255301](https://openairdocs.org/sdr/UATA1750702255301), Jul 2, 2025: CHANNEL. DAMAGED. IMPACT DAMAGE FOUND IN C CHANNEL AFT OF F19. REMOVED DAMAGED C CHANNEL AND INTERCOSTALS AT F18 AND F19 THAT WERE MODIFIED TO ACCEPT A PREVIOUS REPAIR TO OLD C C
- [SDR UATA20205095701](https://openairdocs.org/sdr/UATA20205095701), May 8, 2025: SKIN. CORRODED. CORROSION FOUND ON LOWER SURFACE OF LH WING AT W.S. 3450. REMOVED BRACE STRUT AT APPROXIMATE W.S. 3200 AND SPLICE PLATE AT APPROX. W.S. 3060 FOR ACCESS TO REPAI
- [SDR UATA1740327265302](https://openairdocs.org/sdr/UATA1740327265302), Mar 16, 2025: SEAT TRACK. CORRODED. RH SIDE WALL SEAT RAIL IS CORRODED AT FRAME 5F. REPLACED RH WALL MIDDLE SEAT RAIL SECTION. RH WALL SEAT RAIL SECTION. REMOVED SEAT RAIL. FABRICATED NEW SEAT RAI
- [SDR UATA2025031915701](https://openairdocs.org/sdr/UATA2025031915701), Mar 11, 2025: STIFFENER. CRACKED. CRACKED U CHANNEL IN AFT LH CENTER WING SECTION STATION 2380, AS FLAGGED. REPLACED CRACKED STIFFENER WITH NEW. SEE 337 DATED 03/11/2025 FOR FURTHER INFO. FAA FO
- [SDR UATA2650214255303](https://openairdocs.org/sdr/UATA2650214255303), Feb 14, 2025: WEB. CRUSHED. RH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~4.5 X 9". 
- [SDR UATA2650214255302](https://openairdocs.org/sdr/UATA2650214255302), Feb 14, 2025: WEB. CRUSHED. LH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~ 5.5" X 9.
- [SDR UATA2650214255301](https://openairdocs.org/sdr/UATA2650214255301), Feb 14, 2025: FRAME. PUNCTURED. FOUND A SMALL PUNCTURE IN THE AFT SIDE OF THE RH WEB OF FRAME 11, 2 INCHES ABOVE FLOOR LEVEL. REPAIRED PER CASA ENGINEERING DOC 252EA-00020 REV A. SEE 337 DATED
- [SDR UATA2024101045310](https://openairdocs.org/sdr/UATA2024101045310), Oct 10, 2024: DOOR FRAME. CRACKED. LOWER CARGO DOOR CUTOUT FRAME, LH SIDE "C" CHANNEL HAS A CRACK IN THE UPPER FLANGE JUST AFT OF FRAME 19. INSTALLED AN INTERNAL REINFORCING DOUBLER BEHIND THE CR
- [SDR UATA202410100001](https://openairdocs.org/sdr/UATA202410100001), Oct 10, 2024: DOOR FRAME. CHAFED. LOWER CARGO DOOR CUTOUT FRAME, RH SIDE "C" CHANNEL HAS 2 CHAFE MARKS IN THE UPPER RADIUS, JUST FWD. OF FRAME 19. BLENDED CHAFFED AREAS AND INSTALLED AN INTERNAL
- [SDR UATA202410105308](https://openairdocs.org/sdr/UATA202410105308), Oct 10, 2024: FRAME. MECHANIC ERROR. MECHANIC INDUCED DAMAGE TO FRAME 11 WEB, UNDER THE FLOOR, 5 INCHES LEFT OF CENTER. DRESSED OUT THE DAMAGED AREA & FABRICATED A DOUBLER 2 1/4 INCH BY 3 INCHES OF
- [SDR UATA202410105307](https://openairdocs.org/sdr/UATA202410105307), Oct 10, 2024: FITTING. CORRODED. LH SIDE EXTRUSION ON AFT SIDE OF FRAME 11, UNDER FLOOR HAS EXFOLIATION CORROSION. REPLACED EXTRUSION WITH NEW 212-22406-07-2. SEE FORM 337 DATED 9/20/2024 FOR F
- [SDR UATA202410105306](https://openairdocs.org/sdr/UATA202410105306), Oct 10, 2024: FITTING. CORRODED. RH SIDE EXTRUSION ON FWD. SIDE OF FRAME 11, UNDER FLOOR IS CRACKED. (BOUNDARY LAYER CORROSION). REPLACED EXTRUSION WITH NEW 212-22406-06-1. SEE FORM 337 DATED 9
- [SDR UATA2024101045305](https://openairdocs.org/sdr/UATA2024101045305), Oct 10, 2024: SKIN. CORRODED. LOWER LH SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL.
- [SDR UATA2024101045304](https://openairdocs.org/sdr/UATA2024101045304), Oct 10, 2024: FRAME. CRACKED. FRAME 19 RH CRACKED BEHIND ACTUATOR ATTACH POINT. REMOVED THE OLD REINFORCEMENT DOUBLER REPAIR. FABRICATED A NEW DOUBLER FROM 2024 T3 ALCLAD ALUMINUM 0.050 THIC
- [SDR UATA2024101045303](https://openairdocs.org/sdr/UATA2024101045303), Oct 10, 2024: FRAME. CRACKED. FRAME 19 CRACKED BEHIND LH ACTUATOR ATTACH POINT. FABRICATED AND INSTALLED NEW LOWER FRAME 19 AND ACTUATOR ATTACH POINT DOUBLER. SEE FORM 337 DATED 9/20/2024 FO
- [SDR UATA1901010245302](https://openairdocs.org/sdr/UATA1901010245302), Oct 10, 2024: FLOORBEAM. CORRODED. UNDER SIDE OF THE UPPER "T" FLANGE AT FRAME 11, THERE IS EXFOLIATION CORROSION UNDER THREE DIFFERENT NUT PLATES (CENTER AREA). REMOVED A 21 INCH SECTION OF THE 
- [SDR UATA1901010245301](https://openairdocs.org/sdr/UATA1901010245301), Oct 10, 2024: SKIN. DAMAGED. LOWER RH SIDE SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL
- [SDR UATA202408024531](https://openairdocs.org/sdr/UATA202408024531), Jul 15, 2024: FAIRING. CRACKED. THE FUSELAGE TO WING FILLET FAIRING, WHERE IT WRAPS AROUND THE FUSELAGE TO ATTACH AT FRAME 5 WAS FOUND CRACKED. THIS IS THE THIRD AIRCRAFT IN OUR FLEET THIS YEA
- [SDR UATA202406105702](https://openairdocs.org/sdr/UATA202406105702), May 3, 2024: PROFILE. CRACKED. FOUND A CRACKED PROFILE ON THE AFT FALSE SPAR OF THE LH WING AT STA 2820. PROFILES AT FURTHER OUT STATIONS HAVE INSPECTIONS REQUIRED BY AN AD NOTE 98-12-28 WHIC
- [SDR UATA202406105301](https://openairdocs.org/sdr/UATA202406105301), May 3, 2024: FITTING. CRACKED. FOUND FLOOR BEAM TO SIDEWALL EXTRUDED FITTINGS TO BE CORRODED AND CRACKED AT FRAME 6 AND 11, BOTH RH AND LH. REPLACING FITTINGS WITH NEW.
- [SDR UATA202406105701](https://openairdocs.org/sdr/UATA202406105701), Apr 24, 2024: FAIRING. LOOSE. OB FLAP, IB HINGE FWD FAIRING BECAME LOOSE AND CHAFED INTO THE BOTTOM SKIN OF THE RH WING, JUST FORWARD OF THE HINGE. THE DAMAGE SPECIFICATIONS WERE SENT TO AIR
- [SDR UATA202403183483](https://openairdocs.org/sdr/UATA202403183483), Feb 9, 2024: SKIN. CRACKED. WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.5" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE IN
- [SDR UATA202402023312](https://openairdocs.org/sdr/UATA202402023312), Jan 23, 2024: SKIN. CRACKED. WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.070" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE 
- [SDR UATA202401043521](https://openairdocs.org/sdr/UATA202401043521), Jan 3, 2024: SKIN. CRACKED. WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.719" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE 
- [SDR UATA202312214394](https://openairdocs.org/sdr/UATA202312214394), Dec 21, 2023: FRAME. CRACKED. WHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.75" WAS FOUND IN THE AREA OUTLINED. THE AIRCRAFT WAS REPAIRED B
- [SDR UATA202312013483](https://openairdocs.org/sdr/UATA202312013483), Nov 22, 2023: SKIN. CORRODED. DURING MAINTENANCE, SEVERE CORROSION WAS FOUND IN THE UPPER SKIN OF THE R/H WING BETWEEN STA. 2380 AND STA. 2900, CENTERED OVER STRINGER #1. UNDER THE ENGINE NA
- [SDR 2023F00302](https://openairdocs.org/sdr/2023F00302), Oct 10, 2023: FITTING. CRACKED. WHILE INVESTIGATING HORIZONTAL FITTINGS ON FUSELAGE SIDE DUE TO CRACKS IN FITTINGS, FOUND MATING FITTINGS ATTACHED TO HORIZONTAL STABILIZERS CRACKED AS WELL WHE
- [SDR JTAA20230803001](https://openairdocs.org/sdr/JTAA20230803001), Aug 3, 2023: FITTING. CRACKED. DURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN 
- [SDR JTAA20230803003](https://openairdocs.org/sdr/JTAA20230803003), Aug 3, 2023: FITTING. CRACKED. DURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN 
- [SDR JTAA20230803002](https://openairdocs.org/sdr/JTAA20230803002), Aug 3, 2023: FITTING. CRACKED. DURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN 
- [SDR UATA202309124392](https://openairdocs.org/sdr/UATA202309124392), Jul 18, 2023: CASTING. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE FOUND A CRACK IN THE R/H MLG UPPER FORWARD LANDING GEAR ATTACH POINT CASTING. REMOVED AND REPLACED CASTING. THIS SCHEDULED 
- [SDR UATA202306013481](https://openairdocs.org/sdr/UATA202306013481), Mar 23, 2023: FAIRING. LOOSE. UPON SCHEDULED MAINTENANCE INSPECTION, FOUND FIBERGLASS FLAP HINGE FAIRING LOOSENED, AND SUBSEQUENTLY CHAFED THE FLAP ATTACH PYLON BEYOND LIMITS.
- [SDR 2022F00329](https://openairdocs.org/sdr/2022F00329), Aug 11, 2022: ENGINE. FAILED. UNCOMMANDED RH ENGINE SHUTDOWN.
- [SDR UATA202203243311](https://openairdocs.org/sdr/UATA202203243311), Mar 24, 2022: SKIN. GOUGED. A FORKLIFT LOADING THE AIRCRAFT SLIPPED ON ICE, AND HIT THE AFT UPPER CARGO DOOR AS WELL AS THE AIRCRAFT STRUCTURE DIRECTLY AFT OF THE DOOR, CAUSING GOUGING, AS
- [SDR UATA202203243482](https://openairdocs.org/sdr/UATA202203243482), Feb 23, 2022: ATTACH FITTING. CRACKED. DURING SCHEDULED MAINTENANCE, FOUND A CRACK IN THE R/H WING LOWER OUTBOARD ATTACH FITTING USING X-RAY METHOD.
- [SDR UATA2021122242416](https://openairdocs.org/sdr/UATA2021122242416), Nov 15, 2021: SKIN. CORRODED. LOWER WING SKIN SECTION @ WING STATION 2800 UNDER FLAP PYLON WAS FOUND TO HAVE SEVERE PITTING CORROSION. FABRICATED NEW SKIN AS PER ORIGINAL, AND REPLACED PER A
- [SDR UATA2021111142415](https://openairdocs.org/sdr/UATA2021111142415), Nov 11, 2021: SPAR CAP. CRACKED. CRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.

All 201: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc/reports.md

## STCs that may be installed (OpenAirDocs) (66, first 50)

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 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 ST02083AK](https://openairdocs.org/stc/ST02083AK): Installation of a BFGoodrich Aerospace Traffic alert and collision avoidance system I, Model TCAS 791. Erickson Incorporated
- [STC ST02129AK](https://openairdocs.org/stc/ST02129AK): Reduction/limitation of passenger seats to 19 or fewer. Erickson Incorporated
- [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 ST02434AK](https://openairdocs.org/stc/ST02434AK): Limit passenger seating to nineteen (19) or less. Samaritan Purse
- [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 ST02382AK](https://openairdocs.org/stc/ST02382AK): Reduction / Limitation of passenger seats to nine (9), in accordance with Bighorn Airways, Inc., Document Number BIG-C-212-AFMS, Revision IR, dated June 15, 2011, or later FAA approved revisions. Bighorn Airways Inc
- [STC ST02251AK](https://openairdocs.org/stc/ST02251AK): Reduction / Limitation of passenger seats to nine (9). Bighorn Airways Inc
- [STC ST00682WI-D](https://openairdocs.org/stc/ST00682WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I 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 in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions. 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 ST02317AK](https://openairdocs.org/stc/ST02317AK): Reduction/limitation of passenger seats to nineteen (19) or fewer. Samaritan Purse
- [STC ST03274AT](https://openairdocs.org/stc/ST03274AT): Passenger seating reconfiguration to 9 seats. Fayad Enterprises, LLC
- [STC ST511CH](https://openairdocs.org/stc/ST511CH): Eliminate 27,000 landing cycle life limit of the landing gear by placing aircraft on an inspection program described by the Murray Aviation document titled CASA C212-200 Series Aircraft Landing Gear Continued Airworthiness Limitations , no revision, dated January 23, 1996, or later FAA Approved Revision. Presidential Airways 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 ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies
- [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 ST02243AK](https://openairdocs.org/stc/ST02243AK): Installation of a Honeywell MK-VI EGPWS (TAWS). Jim Air 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 ST00609NY-D](https://openairdocs.org/stc/ST00609NY-D): Installation of replacement Lead Acid Batteries. Bering Air, Inc
- [STC SA5603NM-D](https://openairdocs.org/stc/SA5603NM-D): Installation of a Fairchild A100/A100A cockpit voice recorder. Learjet Inc
- [STC SA1670NM](https://openairdocs.org/stc/SA1670NM): Two (2) 400 gallon bulk liquid cargo tanks. F. S. Air Service
- [STC ST02177AK](https://openairdocs.org/stc/ST02177AK): Reduction/limitation of passenger seats to nine (9) or fewer and installation of a cargo net restraint system using Flight Alaska Drawing No. FA-C212-CC-01, original issue dtd 6/5/01, or later FAA approved revision. Flight Alaska, Inc
- [STC SA01900AT](https://openairdocs.org/stc/SA01900AT): Installation of a 9 seat passenger configuration. Gryphon Group International, Inc. Lists C-212 Series
- [STC ST00608NY-D](https://openairdocs.org/stc/ST00608NY-D): Installation of cargo smoke detector system. CASA Aircraft USA, Inc
- [STC ST00613NY-D](https://openairdocs.org/stc/ST00613NY-D): Installation of replacement hydraulic indicators and sensors. CASA Aircraft USA, Inc
- [STC ST02117AK](https://openairdocs.org/stc/ST02117AK): Reduction/limitation of passenger seats to 9 or fewer. Bering Air, Inc
- [STC ST02098AK](https://openairdocs.org/stc/ST02098AK): Reduction/limitation of seating to required flight crew only. Arctic Transportation Services, Inc
- [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 SA717NE](https://openairdocs.org/stc/SA717NE): Installation of a single Delco Carousel IV-E inertial navigation system. Summit Aviation, Inc
- [STC SA698NE](https://openairdocs.org/stc/SA698NE): Installation of auxiliary equipment bay door system. Summit Aviation, Inc
- [STC SA695NE](https://openairdocs.org/stc/SA695NE): Auxiliary power modification. Summit Aviation, Inc

All 66: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc/stcs.md

## PMA parts (OpenAirDocs) (407, 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/construcciones-aeronauticas-c-212-cc/pma.md

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