# N440RA: Construcciones Aeronauticas C-212-CC

- Status: Valid registration
- Airframe: [Construcciones Aeronauticas C-212-CC](https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc) (registry code 2410204, 28 seats)
- Data sheets: [TCDS A43EU](https://openairdocs.org/tcds/A43EU) (Airbus Defense and Space S.A.) (OpenAirDocs)
- Serial number: 174
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Certificate issued: July 17, 2006
- Expires: April 30, 2028
- Mode S code: A54C15
- Registered owner: [Ryan Air Inc](https://openairdocs.org/faa-owner/RYAN%20AIR%20INC)
- Location: [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage)
- Owner type: Corporation
- Owner's area on the map: 61.1637° N, 149.9966° W: Placed by OpenAirDocs at the center of ZIP code 99502, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=440RA
- Page: https://openairdocs.org/aircraft/N440RA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 44 in force

### Matched by airframe (Construcciones Aeronauticas C-212-CC)

- [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

## Information bulletins (advisory)

None matched.

## NTSB investigations (1)

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 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.

## FAA accident and incident reports (1)

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.

- [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…

## Service difficulty reports (12)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [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 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 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 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 UATA202005155301](https://openairdocs.org/sdr/UATA202005155301), May 11, 2020: FRAME. BUCKLED. UPON SCHEDULED UNDERFLOOR INSPECTION, FOUND FRAME 16F RIB WEBBING AT BL 0.0 SLIGHTLY BUCKLED OR DEFORMED. A DOUBLER WAS FABRICATED, USING 2024 T3 MATERIAL OF 0.
- [SDR UATA202005165301](https://openairdocs.org/sdr/UATA202005165301), May 10, 2020: FRAME. BUCKLED. UPON SCHEDULED INSPECTION FOUND FRAME 14F SLIGHTLY BUCKLED. TECHNICIANS WERE ABLE TO STRAIGHTEN THE BUCKLE, AND FABRICATE A DOUBLER OF ONE GAUGE THICKER THAN OR
- [SDR UATA2020040200001](https://openairdocs.org/sdr/UATA2020040200001), Apr 1, 2020: FLOORBEAM. CORRODED. FOUND FRAME 17 FLOOR BEAM CAP ANGLE CORRODED BETWEEN THE CENTER LINE AND RH BUTT LINE. APPROXIMATELY 29 INCHES WAS REMOVED AND REPLACED WITH A SPLICE REPAIR PER
- [SDR UATA2020040200000](https://openairdocs.org/sdr/UATA2020040200000), Apr 1, 2020: SUPPORT ANGLE. CORRODED. FOUND CORROSION ON A FLOOR BOARD SUPPORT ANGLE UNDER THE COCKPIT FLOOR. ANGLES AT FRAME 5 AND NEAR FRAME 6B WERE SEVERELY CORRODED UNDER NUT PLATES. CORRODED AR

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

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Construcciones Aeronauticas C-212-CC)

- [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/aircraft/N440RA/stcs.md

## Related

- Other Construcciones Aeronauticas C-212-CC aircraft: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc/aircraft.md

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