# N392CA: 1989 CASA 300 - Status: Valid registration - Airframe: [CASA 300](https://openairdocs.org/model/casa-300) (registry code 241030A, 19 seats) - Engine: [Honeywell TPE331-10R](https://openairdocs.org/engine/honeywell-tpe331-10r) (registry code 33988) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.), [TCDS E4WE](https://openairdocs.org/tcds/E4WE) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 398 - Year built: 1989 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: December 19, 2024 - Certificate issued: October 6, 2026 - Expires: October 31, 2033 - Mode S code: A48A6A - Registered owner: [International Air Services Inc Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20TRUSTEE) - Location: [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City) - Owner type: Corporation - Owner's area on the map: 39.2227° N, 119.7016° W: Placed by OpenAirDocs at the center of ZIP code 89706, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=392CA - Page: https://openairdocs.org/aircraft/N392CA 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): 53 in force ### Matched by airframe (CASA 300) - [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2022-03-23](https://openairdocs.org/ad/2022-03-23): Rudder Control System · Garmin G1000 Integrated Avionics System and GFC 700 Automatic… (STC SA01535WI-D). Effective Feb 22, 2022 - [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 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 2005-01-18](https://openairdocs.org/ad/2005-01-18): Fuselage stringers · Textron 200, 200C, 200CT and 24 more. Effective Mar 1, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005 - [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004 - [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004 - [AD 2004-08-15](https://openairdocs.org/ad/2004-08-15): TAWS8000 terrain awareness warning systems (TAWS) · Cessna 421, 500, 501 and 18 more. Effective Jun 7, 2004 - [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003 - [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003 - [AD 99-09-10](https://openairdocs.org/ad/99-09-10): Landing Gear Hand Pump · Textron 200CT, 300, A200CT (C-12D) and 19 more. Effective Jun 7, 1999 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 98-21-35](https://openairdocs.org/ad/98-21-35): Actuator Clevis Assembly in Main Landing Gear · Textron 200T, 300, A200CT (C-12D) and 15 more. Effective Nov 23, 1998 - [AD 98-08-20](https://openairdocs.org/ad/98-08-20): Autopilot Servo Actuators · Alliedsignal Avionics Autopilot Servo Actuators, Mystere-Falcon 20 - C5, Mystere-Falcon 20 - D5 and 17 more. Effective Jun 2, 1998 - [AD 98-04-24](https://openairdocs.org/ad/98-04-24): AFM - Limitations Section - Icing · Textron 100, 300, 58 and 13 more. Effective Mar 13, 1998 - [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998 - [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998 - [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997 - [AD 94-01-06](https://openairdocs.org/ad/94-01-06): Traffic Alert and Collision Avoidance System II Processors · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 176 more. Effective Feb 4, 1994 - [AD 93-04-02](https://openairdocs.org/ad/93-04-02): Transponders · BAE Systems ATP, CL-600-2A12 (CL-601), DHC-8-101 and 23 more. Effective Mar 26, 1993 - [AD 93-01-20](https://openairdocs.org/ad/93-01-20): Aft Cowling Doors · Textron 300. Effective Mar 10, 1993 - [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992 - [AD 92-06-11](https://openairdocs.org/ad/92-06-11): Autopilot/Flight Director System Wiring · Textron 1900C, 300, B200 and 2 more. Effective Mar 30, 1992 - [AD 91-12-11](https://openairdocs.org/ad/91-12-11): Side Windows · Textron 200, 200C, 200CT and 7 more. Effective Jul 15, 1991 - [AD 91-12-10](https://openairdocs.org/ad/91-12-10): Wing Spar Attachment · Textron 300, 300LW, B200 and 2 more. Effective Jul 15, 1991 - [AD 89-19-04 R1](https://openairdocs.org/ad/89-19-04-R1): Wing Fuel Bay Skin Panels · Textron 200, 200C, 200CT and 6 more. Effective Jul 9, 1990 - [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990 - [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990 - [AD 89-22-14](https://openairdocs.org/ad/89-22-14): Aileron Flutter · Textron 200, 200C, 200CT and 9 more. Effective Nov 17, 1989 - [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987 ### Matched by engine (Honeywell TPE331-10R) - [AD 2018-22-01](https://openairdocs.org/ad/2018-22-01): Turbine Section · Honeywell International TPE331-10, TPE331-10N, TPE331-10R and 8 more. Effective Dec 10, 2018 - [AD 2018-17-15](https://openairdocs.org/ad/2018-17-15): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 39 more. Effective Oct 22, 2018 - [AD 2018-13-05](https://openairdocs.org/ad/2018-13-05): Turbine Engine Reduction Gear · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 18 more. Effective Jul 26, 2018 - [AD 2016-21-07](https://openairdocs.org/ad/2016-21-07): Fuel control drive · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Nov 28, 2016 - [AD 2016-18-17](https://openairdocs.org/ad/2016-18-17): Compressor impeller · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 22 more. Effective Nov 4, 2016 - [AD 2015-18-03](https://openairdocs.org/ad/2015-18-03): Engine propeller shaft coupling failures · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 8 more. Effective Nov 13, 2015 - [AD 2012-02-06](https://openairdocs.org/ad/2012-02-06): First stage turbine disks · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 12 more. Effective Mar 15, 2012 - [AD 2011-18-51 R1](https://openairdocs.org/ad/2011-18-51-R1): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more. Effective Oct 19, 2011 - [AD 2009-17-05](https://openairdocs.org/ad/2009-17-05): First stage turbine disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Sep 1, 2009 - [AD 2006-14-03](https://openairdocs.org/ad/2006-14-03): New flight cycle counting method for first, second, and third-stage turbine rotors · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 48 more. Effective Aug 9, 2006 - [AD 2004-09-29](https://openairdocs.org/ad/2004-09-29): First Stage Turbine Disks · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 20 more. Effective Jun 15, 2004 - [AD 2002-25-02](https://openairdocs.org/ad/2002-25-02): First stage compressors implellers · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 35 more. Effective Jan 21, 2003 - [AD 98-12-09](https://openairdocs.org/ad/98-12-09): Fuel Manifold · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more. Effective Aug 7, 1998 - [AD 97-15-10](https://openairdocs.org/ad/97-15-10): Engine Inlet Ice Protection · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 39 more. Effective Sep 22, 1997 - [AD 95-16-08](https://openairdocs.org/ad/95-16-08): Life Limited Turbine Components · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 62 more. Effective Sep 5, 1995 - [AD 94-26-07](https://openairdocs.org/ad/94-26-07): Fuel Control Governor Drive · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 32 more. Effective Apr 18, 1995 - [AD 93-15-11](https://openairdocs.org/ad/93-15-11): Propeller Pitch Control (PPC) Gasket · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 58 more. Effective Sep 7, 1993 - [AD 93-02-01](https://openairdocs.org/ad/93-02-01): Stratoflex Fuel Manifold Assemblies · Honeywell International TPE331-10, TPE331-10A, TPE331-10B and 21 more. Effective Mar 18, 1993 - [AD 89-07-07 R1](https://openairdocs.org/ad/89-07-07-R1): Oil Scavenge Pump Assembly · Honeywell International TPE331-1, TPE331-10, TPE331-10R and 26 more. Effective Oct 30, 1989 - [AD 84-10-06 R1](https://openairdocs.org/ad/84-10-06-R1): Fuel Pump Assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10B and 45 more. Effective Dec 26, 1984 ### Historical (superseded or no longer in force) - [AD 98-15-13](https://openairdocs.org/ad/98-15-13) (historical): Fuel Hose · Raytheon 100 Model or Series (all), 200 Model or Series (all), 200C and 32 more. Effective Aug 28, 1998 - [AD 96-17-10](https://openairdocs.org/ad/96-17-10) (historical): Outflow/Safety Valve · Raytheon 200 Model or Series (all), 2000, 300 and 5 more. Effective Sep 24, 1996 - [AD 93-25-07](https://openairdocs.org/ad/93-25-07) (historical): Fuselage Stringers · Raytheon 200 Model or Series (all), 200C, 200CT and 22 more. Effective Feb 15, 1994 - [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989 - [AD 2018-02-14](https://openairdocs.org/ad/2018-02-14) (historical): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 38 more. Effective Feb 28, 2018 - [AD 2015-12-04](https://openairdocs.org/ad/2015-12-04) (historical): Fuel control unit (FCU) · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Jul 22, 2015 - [AD 2011-18-51](https://openairdocs.org/ad/2011-18-51) (historical): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more - [AD 2006-15-08](https://openairdocs.org/ad/2006-15-08) (historical): Woodward fuel control unit (FCU) assemblies · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 26 more. Effective Aug 24, 2006 - [AD 88-12-10](https://openairdocs.org/ad/88-12-10) (historical): Turbine Rotor · Honeywell International TPE331-10, TPE331-10R, TPE331-10U and 6 more. Effective Jun 6, 1988 - [AD 92-02-19 PL](https://openairdocs.org/ad/92-02-19-PL) (historical): Fuel Manifold Assembly Leak · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more ## Information bulletins (advisory) (10 in force) - [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015 - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 - [SAIB CE-06-27](https://openairdocs.org/saib/CE-06-27): . Issued Jan 30, 2006 - [SAIB CE-03-43R1](https://openairdocs.org/saib/CE-03-43R1): . Issued Sep 23, 2003 - [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002 - [SAIB CE-02-11R1](https://openairdocs.org/saib/CE-02-11R1): . Issued Feb 22, 2002 - [SAIB CE-00-16](https://openairdocs.org/saib/CE-00-16): . Issued Feb 4, 2000 - [SAIB ACE-96-15](https://openairdocs.org/saib/ACE-96-15): . Issued Dec 20, 1996 - [SAIB NE-16-19](https://openairdocs.org/saib/NE-16-19): Turbine Engine Compressor Section Stator Nozzle Distress. Issued Jul 22, 2016 - [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever Loss of Power Control. Issued Jul 11, 2016 - [SAIB CE-03-43](https://openairdocs.org/saib/CE-03-43) (historical): . Issued Jun 27, 2003 - [SAIB CE-02-11](https://openairdocs.org/saib/CE-02-11) (historical): . Issued Jan 4, 2002 ## NTSB investigations None matched to N392CA. ## FAA accident and incident reports None matched to N392CA. ## Reports on N392CA not matched to an aircraft (1) They name N392CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 19810715057329I](https://openairdocs.org/incident/19810715057329I), Jul 15, 1981: Beech B90 (N392CA), Broomfield, CO, Minor damage. Aircraft landed then veered off runway. Right landing. Gear failed. ## Service difficulty reports (32) 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 8EKA20140801](https://openairdocs.org/sdr/8EKA20140801), Feb 13, 2014: PANEL. CORRODED. DURING INSPECTION FOUND CORROSION IN AFT CARGO DOOR. REMOVED CORROSION DAMAGED PANELS. FABRICATED & INSTALLED TWO REPAIR PANELS. ALL REPAIRS PERFORMED IAW SRM. - [SDR 8EKA201402060002](https://openairdocs.org/sdr/8EKA201402060002), Jan 30, 2014: PROFILE. CRACKED. DURING 1200 HR FALSE SPAR RECURRING AD INSPECTION, IAW AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE LT WING. REMOVED LT WING AUXILIARY - [SDR 8EKA2014020600001](https://openairdocs.org/sdr/8EKA2014020600001), Jan 30, 2014: PROFILE. CRACKED. DURING 1200 HR FALSE SPAR RECURRING INSPECTION, & AD INSPECTION AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE RT WING. REMOVED RT WING A - [SDR EHAA20130412004](https://openairdocs.org/sdr/EHAA20130412004), Apr 12, 2013: TERMINAL BLOCK. BURNED. DURING FLIGHT LT WINDOW HEAT SHORTED. - [SDR KGBR20110411357](https://openairdocs.org/sdr/KGBR20110411357), Apr 11, 2011: ATTACH FITTING. CORRODED. HORIZONTAL STABILIZER LEFT (STAB SIDE) FWD ATTACH FITTING HAS LEVEL 3 CORROSION. - [SDR KGBR20110411356](https://openairdocs.org/sdr/KGBR20110411356), Apr 11, 2011: FITTING. CORRODED. VERTICAL STABILIZER AFT FITTING (VERT STAB SIDE) HAS LEVEL 3 CORROSION ON THE AFT LEFT SIDE OF THE FITTING. - [SDR KGBR20110411355](https://openairdocs.org/sdr/KGBR20110411355), Apr 11, 2011: ATTACH FITTING. CORRODED. HORIZONTAL STABILIZER RIGHT ATTACH FITTINGS (HSS SIDE) FWD AND AFT FITTINGS HAVE LEVEL 2 CORROSION. - [SDR KGBR20110411354](https://openairdocs.org/sdr/KGBR20110411354), Apr 11, 2011: FITTING. CORRODED. HORIZONTAL STABILIZER RIGHT LOWER FITTING (FUSE SIDE) AT FS 13268 HAS LEVEL 1 CORROSION. - [SDR KGBR20110411353](https://openairdocs.org/sdr/KGBR20110411353), Apr 11, 2011: FITTING. CORRODED. HORIZONTAL STABILIZER LEFT AFT UPPER (FUSE SIDE) AT FS 13845 HAS LEVEL 3 CORROSION. - [SDR KGBR20110411352](https://openairdocs.org/sdr/KGBR20110411352), Apr 11, 2011: FITTING. CORRODED. VERTICAL STABILIZER LEFT FWD FITTING (FUSE SIDE) AT FS 13268 HAS LEVEL 3 CORROSION. - [SDR KGBR20110411351](https://openairdocs.org/sdr/KGBR20110411351), Apr 11, 2011: FITTING. CORRODED. VERTICAL STABILIZER LEFT AFT FITTING (FUSE SIDE) AT FS 13845 HAS LEVEL 3 CORROSION. - [SDR KGBR20110411350](https://openairdocs.org/sdr/KGBR20110411350), Apr 11, 2011: FITTING. CORRODED. VERTICAL STABILIZER RIGHT FITTING (FUSE SIDE) AT FS 13845 HAS LEVEL 2 CORROSION. - [SDR KGBR20110411349](https://openairdocs.org/sdr/KGBR20110411349), Apr 11, 2011: FITTING. CORRODED. LEVEL 1 CORROSION ON THE LEFT AFT HSS LOWER FITTING (FUSE SIDE) IN FWD RIGHT AFT RADIUS OF THE FITTING AT FS 13845. - [SDR KGBR20110411347](https://openairdocs.org/sdr/KGBR20110411347), Apr 11, 2011: FITTING. CORRODED. LEVEL 1 CORROSION ON THE HSS LEFT FWD LOWER (FUSE SIDE) FITTING AROUND THE BUSHINGS. - [SDR KGBR20110411346](https://openairdocs.org/sdr/KGBR20110411346), Apr 11, 2011: FITTING. CORRODED. LEVEL 1 CORROSION ON LEFT AFT HSS FWD UPPER (FUSE SIDE) UNDER BUSHINGS AT FS 13268. - [SDR KGBR20110411345](https://openairdocs.org/sdr/KGBR20110411345), Apr 11, 2011: FITTING. CORRODED. RIGHT AFT HSS HAS LEVEL 3 CORROSION ON FITTING AT FS 13845. - [SDR KGBR20110411344](https://openairdocs.org/sdr/KGBR20110411344), Apr 11, 2011: FITTING. CORRODED. RIGHT FWD UPPER HSS (FUSE SIDE) HAS LEVEL 3 CORROSION ON FITTING AT FS 13268. - [SDR KGBR20110411343](https://openairdocs.org/sdr/KGBR20110411343), Apr 11, 2011: BLOCK. CORRODED. LEFT AND RIGHT RUDDER SERVO CABLE QUADRANT BLOCKS MOUNTED ON LOWER SURFACE RUDDER CABLE QUADRANT HAVE CORROSION. - [SDR KGBR20110411342](https://openairdocs.org/sdr/KGBR20110411342), Apr 11, 2011: SKIN PANEL. CORRODED. CORROSION ON RIGHT ELEVATOR TOP SKIN PANEL AT THE SKIN PANEL JOINTS LOCATED 44 INCHES I/B FROM O/B EDGE. - [SDR KGBR20110411341](https://openairdocs.org/sdr/KGBR20110411341), Apr 11, 2011: MOUNT FITTING. DELAMINATED. LEFT WING UPPER OUTBOARD ENGINE MOUNT FITTING HAS START OF DELAMINATION, FWD SIDE OF FRONT SPAR. - [SDR KGBR20110411340](https://openairdocs.org/sdr/KGBR20110411340), Apr 11, 2011: MOUNT. DELAMINATED. LEFT WING, UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATED - [SDR KGBR20110411339](https://openairdocs.org/sdr/KGBR20110411339), Apr 11, 2011: MOUNT. DELAMINATED. RIGHT WING UPPER INBOARD ENGINE MOUNT ON FWD SIDE OF FRONT SPAR IS DELAMINATED - [SDR KGBR20110411338](https://openairdocs.org/sdr/KGBR20110411338), Apr 11, 2011: SUPPORT. CORRODED. RIGHT OUTER FLAP INBOARD ACTUATOR BELLCRANK BOTTOM SUPPORT IS CORRODED ON INBOARD FWD CORNER. - [SDR KGBR110411338A](https://openairdocs.org/sdr/KGBR110411338A), Apr 11, 2011: SPAR. CORRODED. RIGHT WING, REAR SPAR WEB HAS CORROSION, WS 5940 AFT SIDE AT BOTTOM SPAR CAP (MARKED). - [SDR KGBR20110411337](https://openairdocs.org/sdr/KGBR20110411337), Apr 11, 2011: STRUCTURE. CORRODED. LEFT WING, CENTER SECTION, AREAS OF TRAILING EDGE OVER FLAP REMOVED, WS 1963-2200 AND WS 3296-3497, SAME AREAS HAVE SEVERE CORROSION (LEVEL 2). - [SDR KGBR20110411336](https://openairdocs.org/sdr/KGBR20110411336), Apr 11, 2011: SUPPORT. CORRODED. LEFT WING OUTBOARD FLAP, AND INBOARD ACTUATOR BELL CRANK BOTTOM SUPPORT ARE CORRODED (OUTBOARD SIDE OF BEARING CUP)(LEVEL 2). - [SDR KGBR20110411333](https://openairdocs.org/sdr/KGBR20110411333), Apr 11, 2011: SUPPORT FITTING. CORRODED. LEVEL 2 CORROSION ON MAIN LEFT LANDING GEAR FWD INTERIOR SUPPORT FITTING AT FS 5744.3 BELOW FLOOR. - [SDR KGBR20110411656](https://openairdocs.org/sdr/KGBR20110411656), Apr 11, 2011: PLATE. CORRODED. LEVEL 3 CORROSION ON CHINE PLATE LEFT SIDE BETWEEN FS 5390 AND FS 5744.3. - [SDR KGBR201104112332](https://openairdocs.org/sdr/KGBR201104112332), Apr 11, 2011: SEAT TRACK. CORRODED. RIGHT FLOOR SEAT TRACK IS CORRODED FROM FS 3950 TO FS 7332. - [SDR KGBR20110408321](https://openairdocs.org/sdr/KGBR20110408321), Apr 8, 2011: CONTROL QUADRANT. CORRODED. CORROSION ON UPPER SURFACE OF AILERON QUADRANT CONTROL RODS CENTER WING FS 6735. - [SDR KGBR20110408](https://openairdocs.org/sdr/KGBR20110408), Apr 8, 2011: CONTROL QUADRANT. CORRODED. RIGHT CENTER WING AILERON CONTROL QUADRANT IS CORRODED ON UPPER SURFACE FS 6735 (LEVEL 3). - [SDR KGBR2011040810010](https://openairdocs.org/sdr/KGBR2011040810010), Apr 8, 2011: SEAT TRACK. CORRODED. RIGHT SIDE SEAT TRACK RAIL IS CORRODED IN SEVERAL PLACES: FS 3950, FS 4310, AND FROM FS 5744 TO FS 8950. ## Service difficulty reports on N392CA not matched to an aircraft (2) They name N392CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR 20001025SH026](https://openairdocs.org/sdr/20001025SH026), Oct 2, 2000: MASTER CYLINDER. MALFUNCTIONED. RIGHT BRAKE DRAGGING AND LOCKING UP. THIS WOULD ONLY HAPPEN WHEN COPILOT RIGHT BRAKE WAS USED. WOULD NOT DRAG OR LOCK WHEN PILOT''S BRAKES WERE USED. AFTER TROU - [SDR 99ZZZX658](https://openairdocs.org/sdr/99ZZZX658), Oct 14, 1998: NOZZLE. DAMAGED. PRE-FLIGHT INSPECTION FOUND 5.50 INCH BY 4 INCH PIECE OF EXHAUST NOZZLE MISSING FROM AFT END OF NOZZLE. EXHAUST DUCT WAS DAMAGED AS PART DEPARTED AIRCRAFT. BOTH ## STCs that may be installed (OpenAirDocs) (317, 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 (CASA 300) - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA02658LA](https://openairdocs.org/stc/SA02658LA): Replacement of the original Pratt and Whitney PT6A-60A engines and propellers with Pratt and Whitney PT6A-67A engines and MT Propeller MTV-27-1-N-C-F-R(P)/CFR260-65b propellers. Blackhawk Modifications LLC - [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04221CH](https://openairdocs.org/stc/SA04221CH): Installation of Thermal Acoustic Kit. Skandia Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC - [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH - [STC SA03930NY](https://openairdocs.org/stc/SA03930NY): Installation of King Air Belly Payload Mount. Icarus Aero Inc - [STC SA02017WI](https://openairdocs.org/stc/SA02017WI): The Installation of the Parker-Meggitt iPRESS™ System. 3S Certification LLC - [STC ST04442CH](https://openairdocs.org/stc/ST04442CH): Installation of SmartSky LiTE System. Apcela IFC JV, LLC dba Apcela ATG - [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc - [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd - [STC SA01535WI-D](https://openairdocs.org/stc/SA01535WI-D): Installation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP). Garmin International Inc - [STC SA10941SC](https://openairdocs.org/stc/SA10941SC): Installation of a 3-Tube Rockwell Collins Pro Line 21 Avionics System with Rockwell Collins Integrated Flight Information System 5000, TCAS II, and Honeywell Enhanced Ground Proximity Warning System. BHE and Associates - [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd - [STC SA01868LA](https://openairdocs.org/stc/SA01868LA): Installation of a Wescam FLIR unit into an extended fuselage nose (STC SA00367SE). Metrea Special Aerospace ISR Inc - [STC SA2794NM](https://openairdocs.org/stc/SA2794NM): Installation of Flight Equipment and Engineer Corp. passenger seats. Metrea Special Aerospace ISR Inc - [STC SA4490NM](https://openairdocs.org/stc/SA4490NM): Installation of baggage compartment door. Metrea Special Aerospace ISR Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA156CH](https://openairdocs.org/stc/SA156CH): Installation of a TCAS I. Acron Aviation Inc - [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc - [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc - [STC SA11914IB](https://openairdocs.org/stc/SA11914IB): Installation of the MT-Propeller Entwicklung GmbH MTV-47-1-()-C-F-R(P)/CFR260-361(). MT-Propeller Entwicklung GmbH - [STC SA11855IB](https://openairdocs.org/stc/SA11855IB): Installation of the Flap Roller Bearing Assembly. Marsh Brothers Aviation Inc - [STC SA01848WI](https://openairdocs.org/stc/SA01848WI): Modification of a Rockwell Collins Global Positioning System (GPS). Rockwell Collins Inc - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC - [STC SA00335BO](https://openairdocs.org/stc/SA00335BO): Installation of a Night Vision Goggle (NVG) compatible Lighting System. ATI Engineering Services LLC - [STC SA00363BO](https://openairdocs.org/stc/SA00363BO): Installation of LED Position Lights. ATI Engineering Services LLC - [STC SA02033WI](https://openairdocs.org/stc/SA02033WI): Installation of the SmartSky LITE System. Aeronautix - [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC SA01615SE](https://openairdocs.org/stc/SA01615SE): Installation of winglets and related system changes. BLR Aerospace LLC - [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC - [STC ST02752SE](https://openairdocs.org/stc/ST02752SE): Installation of the Starlink Aviation System. AeroMech Incorporated - [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA00975CH](https://openairdocs.org/stc/SA00975CH): Installation of Butterfield Industries Oil Residue Collection System, kit Part Number BI 4020-1. Raisbeck Engineering - [STC SA00976CH](https://openairdocs.org/stc/SA00976CH): Installation of Butterfield Industries Air/Oil Separator System, kit Part Number BI 6001-3. Raisbeck Engineering Inc - [STC SA01111SE](https://openairdocs.org/stc/SA01111SE): Installation of engine plenum seal.`. Raisbeck Engineering - [STC SA02215SE](https://openairdocs.org/stc/SA02215SE): Fabrication of Inspection Panel Kit BI 9501-001. Raisbeck Engineering Inc - [STC SA02473SE](https://openairdocs.org/stc/SA02473SE): Installation of Raisbeck/Hartzell Swept Blade Turbofan Propellers. Raisbeck Engineering Inc - [STC SA02559SE](https://openairdocs.org/stc/SA02559SE): Installation of Raisbeck/Hartzell Five-Blade Swept Turbofan Propellers. Raisbeck Engineering Inc - [STC SA3683NM](https://openairdocs.org/stc/SA3683NM): Installation of exhaust stack fairings. Raisbeck Engineering Inc - [STC SA4733NM](https://openairdocs.org/stc/SA4733NM): Installation of lower aft fuselage strakes. Raisbeck Engineering Inc - [STC SA4734NM](https://openairdocs.org/stc/SA4734NM): Installation of nacelle overwing storage lockers and lower flap fairing. Raisbeck Engineering Inc - [STC SA04601CH](https://openairdocs.org/stc/SA04601CH): Installation of a McCauley Propeller Systems 4HFR34C780/1OSSTA-0 to -2 model propeller. MCCAULEY PROPELLER SYSTEMS - [STC SA02593AT](https://openairdocs.org/stc/SA02593AT): Installation of a Collins FDS-2000 Flight Display System. Summit Aviation Inc - [STC SA02570AT-D](https://openairdocs.org/stc/SA02570AT-D): Installation of a TCAS 4000 Traffic Alert and Collision Avoidance System. Summit Aviation Inc All 317: https://openairdocs.org/aircraft/N392CA/stcs.md ## Related - Other CASA 300 aircraft: https://openairdocs.org/model/casa-300/aircraft.md - The Honeywell TPE331-10R engine: https://openairdocs.org/engine/honeywell-tpe331-10r.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.