# N86RF: 1985 Cessna 208A - Status: Valid registration - Airframe: [Cessna 208A](https://openairdocs.org/model/cessna-208a) (registry code 2073703, 2 seats) - Engine: [Pratt & Whitney Canada PT6A-114A](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-114a) (registry code 52257) - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) (Textron Aviation Inc.), [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 20800033 - Year built: 1985 - Type: Fixed wing single engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: August 25, 2006 - Certificate issued: August 8, 2017 - Expires: August 31, 2027 - Mode S code: ABCDFB - 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=86RF - Page: https://openairdocs.org/aircraft/N86RF 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): 9 in force ### Matched by airframe (Cessna 208A) - [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 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 (Pratt & Whitney Canada PT6A-114A) - [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022 - [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015 - [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012 - [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001 - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 ### Historical (superseded or no longer in force) - [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014 ## Information bulletins (advisory) (2 in force) - [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011 - [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010 ## NTSB investigations None matched to N86RF. ## FAA accident and incident reports None matched to N86RF. ## 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) (81, 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 208A) - [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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [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 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 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 SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc - [STC SA2526CE](https://openairdocs.org/stc/SA2526CE): Installation of a seat for a third occupant. Remove cargo barrier and close-out nets. Remove partition nets (2 each). Install aft single seat assembly. Textron Aviation Inc - [STC SA2135CE](https://openairdocs.org/stc/SA2135CE): Increase seating capacity to five places. (208 WITH CARGOMASTER OPTION). Textron Aviation Inc - [STC SA02547AT](https://openairdocs.org/stc/SA02547AT): Installation of a Voice Alert System. Aircraft Components Inc - [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). Icarus Avionics, LLC - [STC SA02042SE](https://openairdocs.org/stc/SA02042SE): Fabrication of AeroAcoustics Aircraft Systems (AASI) Aircraft Payload Extender STOL system. AeroAcoustics Aircraft Systems Inc - [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated - [STC SA02293AK](https://openairdocs.org/stc/SA02293AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Chelton Flight Systems Inc - [STC SA02359AK-D](https://openairdocs.org/stc/SA02359AK-D): Fabrication and installation of F. Atlee dodge Aircraft Services, Cessna Tie-Down clamp. F. Atlee Dodge Aircraft Services, LLC - [STC SA01834CH](https://openairdocs.org/stc/SA01834CH): Installation of the High Intensity Discharge Light Assembly Kit. Knots 2U Ltd - [STC SA00518NY](https://openairdocs.org/stc/SA00518NY): Installation of modified McCauley Model 3GFR34C703 propeller incorporating a zero latch system. Western Propeller Company - [STC SA02146LA](https://openairdocs.org/stc/SA02146LA): Installation of a Ballistic Protection System (BPS). Lifeport, Inc - [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc - [STC SA02519NY](https://openairdocs.org/stc/SA02519NY): Guardian Mobility Skytrax (Asset Tracking) System to be installed. GMC Guardian Mobility Corporation - [STC SA01205WI-D](https://openairdocs.org/stc/SA01205WI-D): Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. Honeywell International Inc - [STC SA00196BO](https://openairdocs.org/stc/SA00196BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit. Pratt & Whitney Engine Services Inc - [STC SA00020NY](https://openairdocs.org/stc/SA00020NY): Installation of power analyzer and recorder Part No. SL17067. Aerosonic Corporation - [STC SA00692NY](https://openairdocs.org/stc/SA00692NY): Installation of Avionics Specialties, Inc. Power Analyzer and Recorder (PAR) Part No. SL17082. Aerosonic Corporation - [STC SA628NE](https://openairdocs.org/stc/SA628NE): Installation of a Teledyne Avionics Power Analyzer & Recorder No. SL17024. Aerosonic Corporation - [STC SA01439WI](https://openairdocs.org/stc/SA01439WI): Installation of MT-Propeller Model MTV-16-1-E-C-F-R(P)/CFR250-55 reversing and full feathering 4-blade constant speed propeller. MT- Propeller Entwicklung GmbH - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc - [STC SA01170NY](https://openairdocs.org/stc/SA01170NY): Installation of NPX138N-XXX FM Transceiver. Northern Airborne Technology Ltd - [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies - [STC SA83CH](https://openairdocs.org/stc/SA83CH): Installation of a Shadin engine trend monitor system. Shadin Avionics - [STC SA00171BO](https://openairdocs.org/stc/SA00171BO): Installation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010. Pratt & Whitney Engine Services Inc - [STC SA00812NY](https://openairdocs.org/stc/SA00812NY): Installation of Technisonic Industries Limited TFM-138, A, and B (does not include TFM-138, s/n 1540 and up, TFM-138B, s/n 1500 and up). Technisonic Industries Limited - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA02168CH](https://openairdocs.org/stc/SA02168CH): Installation of a McCauley Propeller Systems 4HFR34C775/96MGA-0 four-blade propeller. McCauley Propeller Systems - [STC SA01951NY-D](https://openairdocs.org/stc/SA01951NY-D): Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. Wulfsberg Electronics Division - [STC SA01128NY-D](https://openairdocs.org/stc/SA01128NY-D): Installation of Satellite Tracking Beacon. Optec Inc - [STC SA00161BO](https://openairdocs.org/stc/SA00161BO): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. Avidyne Corporation - [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA02655AT](https://openairdocs.org/stc/SA02655AT): Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. JAARS Inc - [STC SA01296SE](https://openairdocs.org/stc/SA01296SE): Installation of a fuel condition lever low-idle lock assembly in accordance with Callahan Aircraft Services Drawing 7610-04, Revision A, Sheets 1-7, dated September 19, 2003, or later FAA approved revision. Installation, operation, and maintenance must be in accordance with Empire Airlines STC Control Document 7610-1, Revision A, dated September 19, 2003, or later FAA approved revision. Empire Airlines Inc - [STC ST02547AT](https://openairdocs.org/stc/ST02547AT): Installation of a voice alert system. Aircraft Components Inc - [STC SA01159SE](https://openairdocs.org/stc/SA01159SE): Installation of Eros MF10-04-07 quick donning full face oxygen masks. Empire Airlines Inc - [STC SA00970CH](https://openairdocs.org/stc/SA00970CH): Installation of various SMR Technologies electrical propeller de-icer models. SMR Technologies - [STC SA02182AK](https://openairdocs.org/stc/SA02182AK): Installation of Honeywell KGP 560 Enhanced Ground Proximity Warning System (EGPWS). Aero Twin, Inc - [STC ST01117LA](https://openairdocs.org/stc/ST01117LA): Installation of Teledyne Battery Products Model G-6381ES sealed lead-acid aircraft storage battery. Teledyne Battery Products - [STC SA02165AK](https://openairdocs.org/stc/SA02165AK): Installation of ARNAV Systems, Inc., MFD 5200 CDU, p/n 453-2550; MFD 5115 RPU, P/N 453-2530-08, DR-100 Receiver, P/N 453-0160; and EMM 35 Engine Trend Monitor, P/N 453-5030. Arnav Systems Inc - [STC SA00649NY](https://openairdocs.org/stc/SA00649NY): Installation of Bendix/King CAS66A TCAS I. Kitchener Aero Avionics Ltd - [STC SA00704SE](https://openairdocs.org/stc/SA00704SE): Replacement of certain BF Goodrich pneumatic deicer boots. SMR Technologies - [STC SA01086NY](https://openairdocs.org/stc/SA01086NY): Installation of Kehler Model 6000 and 6100 Wheel Skis. Meler & Company Incorporated - [STC SA02126AK-D](https://openairdocs.org/stc/SA02126AK-D): Fabrication and installation of Aero Twin brake disk spacer kit. Aero Twin Inc All 81: https://openairdocs.org/aircraft/N86RF/stcs.md ## Earlier aircraft with N86RF The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N86RF before. - [Cancelled 2018-01-10](https://openairdocs.org/deregistered/N86RF-2018-01-10): Ficek VP-1, S/N 1-VP, built 1976. Registration expired, pending cancellation. Owner: [Ficek Rudolph S](https://openairdocs.org/faa-owner/FICEK%20RUDOLPH%20S), [Orland Park, IL](https://openairdocs.org/faa-place/IL/Orland%20Park) ## Related - Other Cessna 208A aircraft: https://openairdocs.org/model/cessna-208a/aircraft.md - The Pratt & Whitney Canada PT6A-114A engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-114a.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.