# N950RF: 1989 Cessna 208

- Status: Valid registration
- Airframe: [Cessna 208](https://openairdocs.org/model/cessna-208) (registry code 2073702, 10 seats)
- Engine: [Honeywell TPE331-12JR](https://openairdocs.org/engine/honeywell-tpe331-12jr) (registry code 33806)
- Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) (Textron Aviation Inc.), [TCDS E4WE](https://openairdocs.org/tcds/E4WE) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 20800150
- Year built: 1989
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Multiple
- Airworthiness date: July 13, 2023
- Certificate issued: July 7, 2020
- Expires: July 31, 2027
- Mode S code: AD3624
- Registered owner: [Randigo LLC](https://openairdocs.org/faa-owner/RANDIGO%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: LLC
- Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, 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=950RF
- Page: https://openairdocs.org/aircraft/N950RF

From the FAA registry file of October 22, 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): 32 in force

### Matched by airframe (Cessna 208)

- [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 2021-04-10](https://openairdocs.org/ad/2021-04-10): Elevator Structure · Textron 208 and 208B. Effective Apr 12, 2021
- [AD 2009-15-05](https://openairdocs.org/ad/2009-15-05): Yaw bridle cable tension · Cessna 208 and 208B. Effective Jul 27, 2009
- [AD 2009-05-12](https://openairdocs.org/ad/2009-05-12): Aileron control system · Cessna 208 and 208B. Effective Apr 15, 2009
- [AD 2008-26-10](https://openairdocs.org/ad/2008-26-10): Alternate static air source selector valve · Cessna 172, 172A, 172B and 179 more. Effective Jan 5, 2009
- [AD 2008-13-06](https://openairdocs.org/ad/2008-13-06): Right wing wire bundles · Cessna 208 and 208B. Effective Jul 30, 2008
- [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 2008-10-02](https://openairdocs.org/ad/2008-10-02): Part number identification placard · Cessna 172, 172R, 172RG and 64 more. Effective May 12, 2008
- [AD 2007-10-15](https://openairdocs.org/ad/2007-10-15): S1 Known Icing Equipment AFM supplements · Cessna 208 and 208B. Effective Jun 21, 2007
- [AD 2006-01-11 R1](https://openairdocs.org/ad/2006-01-11-R1): Cargo pod and landing gear fairings · Cessna 208 and 208B. Effective Feb 22, 2006
- [AD 2005-25-08](https://openairdocs.org/ad/2005-25-08): Electronic Flight Information System (EFIS) · B-N Group BN-2A, 172, 180 and 22 more. Effective Jan 23, 2006
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 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 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2004-17-01](https://openairdocs.org/ad/2004-17-01): Flap bellcranks · Cessna 208 and 208B. Effective Sep 26, 2004
- [AD 2004-08-17](https://openairdocs.org/ad/2004-08-17): Upper and Lower Wing Strut Attach Fitting Nut · Cessna 208 and 208B. Effective May 17, 2004
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 2001
- [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 97-25-04](https://openairdocs.org/ad/97-25-04): Airplane Flight Manual (AFM) - Limitations - Power Levers · Cessna 208, 208A, 208B and 2 more. Effective Jan 21, 1998
- [AD 97-01-13](https://openairdocs.org/ad/97-01-13): Fuel, Oil and Hydraulic Hoses · Cessna 150, 150A, 150B and 232 more. Effective Feb 3, 1997
- [AD 96-09-15](https://openairdocs.org/ad/96-09-15): Airplane Flight Manual - Icing Conditions · Cessna 208 and 208B. Effective Jun 11, 1996
- [AD 90-05-04](https://openairdocs.org/ad/90-05-04): Engine Mount Ring · Cessna 208, 208A and 208B. Effective Mar 23, 1990
- [AD 90-05-01](https://openairdocs.org/ad/90-05-01): Bellcrank Assembly · Cessna 208, 208A and 208B. Effective Mar 5, 1990
- [AD 86-22-06](https://openairdocs.org/ad/86-22-06): Wing Fuel Tank Selectors · Cessna 208 and 208A. Effective Nov 7, 1986

### Matched by engine (Honeywell TPE331-12JR)

- [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 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 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 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 2002-12-09](https://openairdocs.org/ad/2002-12-09): Spectrometric Oil Analysis Program (SOAP) Sampling of Oil and Filter, Gearbox Components · Honeywell International TPE331-11U, TPE331-12B, TPE331-12JR and 3 more. Effective Jul 3, 2002
- [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

### Historical (superseded or no longer in force)

- [AD 2006-06-06](https://openairdocs.org/ad/2006-06-06) (historical): Airplane Flight Manual (AFM) · Cessna Aircraft Company, The 208 and 208B. Effective Mar 24, 2006
- [AD 2006-01-11](https://openairdocs.org/ad/2006-01-11) (historical): Pilot assist handle and deicing boots on the cargo pod · Cessna Aircraft Company, The 208 and 208B. Effective Feb 22, 2006
- [AD 2005-07-01](https://openairdocs.org/ad/2005-07-01) (historical): Airplane Flight Manual (AFM) · Cessna Aircraft Company, The 208 and 208B. Effective Mar 29, 2005
- [AD 2003-21-04](https://openairdocs.org/ad/2003-21-04) (historical): Right inboard forward flap bell crank · Cessna 208 and 208B. Effective Oct 21, 2003
- [AD 2002-22-17](https://openairdocs.org/ad/2002-22-17) (historical): Inboard forward flap bellcranks · Cessna 208 and 208B. Effective Dec 31, 2002
- [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 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) (4 in force)

- [SAIB CE-17-25](https://openairdocs.org/saib/CE-17-25): ELEVATOR TORQUE TUBE  Inspections for cracks and corrosion in elevator torque tubes. Issued Aug 25, 2017
- [SAIB CE-09-42](https://openairdocs.org/saib/CE-09-42): Lights - Landing Light, Beacon Light and Taxi Light Switch Applications. Issued Jul 24, 2009
- [SAIB CE-06-46R1](https://openairdocs.org/saib/CE-06-46R1): . Issued Sep 18, 2006
- [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever  Loss of Power Control. Issued Jul 11, 2016

## NTSB investigations

None matched to N950RF.

## FAA accident and incident reports

None matched to N950RF.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## STCs that may be installed (OpenAirDocs) (274, 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 (Cessna 208)

- [STC SA12517WI](https://openairdocs.org/stc/SA12517WI): Installation of a Single Point Pressure Refueling System. AO Aviation LLC
- [STC SA12388AK](https://openairdocs.org/stc/SA12388AK): Removal of engine fire detection system. Randigo LLC
- [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01975WI](https://openairdocs.org/stc/SA01975WI): Installation of Fuselage Camera Ports with or without Mission Power System. Avcon Industries Inc
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA8954SW](https://openairdocs.org/stc/SA8954SW): Installation of Hartzell HC-B3TN-3Z/ T10282N(K)+4 or HC-B3TN-3Z/ T10282N+4 propeller. John Wentzell Downs Jr
- [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 SA02812SE](https://openairdocs.org/stc/SA02812SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC SA12011DE](https://openairdocs.org/stc/SA12011DE): Installation of Mission Equipment, including consoles and turret mounts. Southeast Aerospace
- [STC SA09625AC](https://openairdocs.org/stc/SA09625AC): Installation of Dual Camera Ports and Navigation Sight Ports. Metrea Special Aerospace ISR Inc
- [STC SA01516WI](https://openairdocs.org/stc/SA01516WI): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA11933IB](https://openairdocs.org/stc/SA11933IB): Manufacturing and Installation of the Camera Mount. Icarus Aero Inc
- [STC SA00892WI](https://openairdocs.org/stc/SA00892WI): TKS Ice Protection System Installation approving aircraft for flight into known icing conditions. CAV Ice Protection Limited
- [STC SA02549SE](https://openairdocs.org/stc/SA02549SE): Installation of new structural components in certain fuselage bulkheads. Metal Innovations Inc. dba MII Aero
- [STC SA01657CH](https://openairdocs.org/stc/SA01657CH): Installation of Honeywell Bendix/King KGP 560 Enhanced Ground Proximity Warning System, KMD 850 Multi-Function Display, and KLN 94 GPS Navigator. Amphenol Cable and Interconnect Technologies Inc
- [STC SA04746NY](https://openairdocs.org/stc/SA04746NY): Installation of Outlook Aero LLC ISR Payload Mount System. Outlook Aero LLC
- [STC SA01330LA](https://openairdocs.org/stc/SA01330LA): Installation of alternate avionics support assembly. Radiorax Aviation Systems LLC
- [STC SA01871NY](https://openairdocs.org/stc/SA01871NY): Installation of Hawker Sealed Lead-Acid Battery. Securaplane Technologies Inc
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [STC SA09948AC](https://openairdocs.org/stc/SA09948AC): Incorporation of engine indications, fuel quantity indications, and electrical system indications into the display units of the Garmin G600 TXi system. Xtreme Avonics LLC
- [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 SA00301BO](https://openairdocs.org/stc/SA00301BO): Installation of Light Emitting Diode (LED) based Position, Anticollision, Taxi, and Landing Light Systems with Single Mode (visible) or Dual Mode (visible plus infrared) options. ATI Engineering Services LLC
- [STC SA04646CH](https://openairdocs.org/stc/SA04646CH): Installation of Hartzell Model HC-E4N-3KTV( )/GC11114( )-2 propeller. Wipaire Inc
- [STC SA04639CH](https://openairdocs.org/stc/SA04639CH): Incorporation of an Avcon External Belly Mounted Radar Pod in accordance with FAA approved Master Data List 07801000 Revision (IR), dated 06/26/2024, or later FAA or ODA Approved Revision. AVCON INDUSTRIES INC
- [STC SA7687SW](https://openairdocs.org/stc/SA7687SW): Modification of the lower fuselage skin to include provisions for a scanner or camera and navigation sight port. Randingo LLC
- [STC SA03817NY](https://openairdocs.org/stc/SA03817NY): Installation of the Parachute Kit. airplus engineering GmbH
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02917NY-D](https://openairdocs.org/stc/SA02917NY-D): Installation of Camera Ports. MAG Aerospace
- [STC SA01105DE](https://openairdocs.org/stc/SA01105DE): Installation of the Persistent Systems MPU5 Wave Radio System. Persistent Systems
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA4940NM](https://openairdocs.org/stc/SA4940NM): Install engine fluids collection tank. Raisbeck Engineering Inc
- [STC SA03681AT](https://openairdocs.org/stc/SA03681AT): Installation of Honeywell KTA 870 Traffic Advisory System (TAS) on all Cessna 208 series aircraft. LB Aircraft Engineering LLC
- [STC SA00389AT](https://openairdocs.org/stc/SA00389AT): Installation of Burns Aerospace seats in passenger interior. Summit Aviation Inc
- [STC SA01044AT](https://openairdocs.org/stc/SA01044AT): Installation of main landing gear fairings. Summit Aviation Inc
- [STC SA01239AT](https://openairdocs.org/stc/SA01239AT): Installation of an additional anti-collision light. Summit Aviation Inc
- [STC SA01678AT-D](https://openairdocs.org/stc/SA01678AT-D): Installation of an Electrically Driven Standby Vacuum System. Summit Aviation Inc
- [STC SA01973AT-D](https://openairdocs.org/stc/SA01973AT-D): Installation of a Composite Support Flange for the Inertial Separator Duct. Summit Aviation Inc
- [STC SA2549SO](https://openairdocs.org/stc/SA2549SO): Installation of Teledyne System No. 112-9200 Normalized Angle of Attack System. Summit Aviation Inc
- [STC SA04559AT](https://openairdocs.org/stc/SA04559AT): Installation of a up to three 28 VDC mission power busses provisions. MAG Aerospace
- [STC SA01542SE](https://openairdocs.org/stc/SA01542SE): The manufacture of a Crew Door Restraint System. DV Aviation Inc
- [STC SA11220SC](https://openairdocs.org/stc/SA11220SC): Installation of a Pratt & Whitney flight data acquisition, storage, and transmission system (FAST). Pratt & Whitney Engine Services Inc
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics

All 274: https://openairdocs.org/aircraft/N950RF/stcs.md

## Related

- Other Cessna 208 aircraft: https://openairdocs.org/model/cessna-208/aircraft.md
- The Honeywell TPE331-12JR engine: https://openairdocs.org/engine/honeywell-tpe331-12jr.md

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