# N571SC: Cessna 208

- Status: Valid registration
- Airframe: [Cessna 208](https://openairdocs.org/model/cessna-208) (registry code 2073702, 10 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: 20800571
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: May 29, 2015
- Certificate issued: June 7, 2021
- Expires: June 30, 2028
- Mode S code: A753B3
- Registered owner: [Gospel Ministries International Inc](https://openairdocs.org/faa-owner/GOSPEL%20MINISTRIES%20INTERNATIONAL%20INC)
- Location: [Mc Donald, TN](https://openairdocs.org/faa-place/TN/Mc%20Donald)
- Owner type: Corporation
- Owner's area on the map: 35.1229° N, 84.9855° W: Placed by OpenAirDocs at the center of ZIP code 37353, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=571SC
- Page: https://openairdocs.org/aircraft/N571SC

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): 30 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 (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 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 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) (5 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-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 N571SC.

## FAA accident and incident reports

None matched to N571SC.

## Reports on N571SC not matched to an aircraft (1)

They name N571SC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19970415015629I](https://openairdocs.org/incident/19970415015629I), Apr 15, 1997: Doug DC1010 (N571SC), Cleveland, OH. Narrative: on April 15, 1997, at approximately 0755 EDT, sun country 2121 crossed the runway 23L hold short line without cle-atct clearance. This required an…

## 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.

## Service difficulty reports on N571SC not matched to an aircraft (81, newest 50)

They name N571SC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 99ZZZM734](https://openairdocs.org/sdr/99ZZZM734), Oct 7, 1999: ENGINE. FAILED. FLT 102 - LAX - NR 1 ENGINE EXHAUST GAS TEMPERATURE CAUTION LIGHT CAME ON EARLY ON CLIMB-OUT, NR 1 THRUST HAD TO BE REDUCED TO MAINTAIN EXHAUST GAS TEMPERATURE 
- [SDR 99ZZZM649](https://openairdocs.org/sdr/99ZZZM649), Aug 5, 1999: LIGHT. INOPERATIVE. FLT 9001 - SFO - FORWARD RIGHT PORTION OF ZONE 'A' EMERGENCY LIGHTS FLOOR AISLE INOPERATIVE. ISOLATED SHORT CIRCUIT EMERGENCY (FLOOR AISLE) LIGHTS OPERATION CHE
- [SDR 99ZZZM712](https://openairdocs.org/sdr/99ZZZM712), Jul 14, 1999: SLIDE. DEPLOYED. FLT 9154 - SLC, LEFT NR 1 DOOR SLIDE DEPLOYED INADVERTENTLY. DEFERRED IN SLC CLEARED IN LAX. REPLACED ESCAPE SLIDE/RAFT PACK. (M)
- [SDR 99ZZZM648](https://openairdocs.org/sdr/99ZZZM648), Apr 26, 1999: POWER SUPPLY. INOPERATIVE. FLT 007 - SFO - ON PREFLIGHT CHECK NUMEROUS EMERGENCY LIGHTS FAILED TO TEST IN FORWARD CABIN. RIGHT FLOOR LIGHTS AND SEVERAL DOOR AND FORWARD BULKHEAD LIGHTS. R
- [SDR 99ZZZM214](https://openairdocs.org/sdr/99ZZZM214), Feb 2, 1999: LIGHT. LOOSE. FLT 008 IN SFO, EMERGENCY FLOOR LIGHT STRIP UNDER SEAT 23C IS LOOSE. REINSERT EMERGENCY FLOOR LIGHT STRIPS, OPERATIONAL CHECK NORMAL. (M)
- [SDR SCNA98053](https://openairdocs.org/sdr/SCNA98053), Jun 4, 1998: SLIDE. FAILED. DURING DEPLOYMENT OF THE R4 DOOR SLIDE FOR TRAINING PURPOSES THE SLIDE FAILED TO INFLATE FULLY.
- [SDR SCNA98051](https://openairdocs.org/sdr/SCNA98051), May 30, 1998: WIRE. FAILED. A SMOKE SMELL AT ROW 22ABC. FOUND WIRES BURNT UNDER SEAT 22E TRACK. TAPED AND INSULATED INDIVIDUAL WIRES AND UNPLUGGED UNDERSEAT BURNT DECODER HARNESSES. PLACED
- [SDR SCNA98039](https://openairdocs.org/sdr/SCNA98039), May 6, 1998: PACK. SMOKING. THE NUMBER THREE PACK APPEARS TO CAUSE LIGHT SMOKE WHEN ON IN THE AFT PORTION OF THE AIRCRAFT. RAN NUMBER THREE PACK OFF AND ON SETTING. INSPECTED DUCT, FOUND N
- [SDR SCNA98017](https://openairdocs.org/sdr/SCNA98017), Dec 11, 1997: EGT HARNESS. INOPERATIVE. AFTER DEPARTURE FROM HNL AT FLIGHT LEVEL 320, NUMBER 1 EGT BEGAN FLUCTUATING. RETURNED TO HNL. REMOVED AND REPLACED LOWER LT THERMOCOUPLE HARNESS. FUNCTIONALLY 
- [SDR SCNA98015](https://openairdocs.org/sdr/SCNA98015), Nov 4, 1997: LAMP HOLDERS. SHORTED. AFTER TAKEOFF, A GLOWING EMBER WAS OBSERVED FALLING FROM THE AREA OF THE CEILING LIGHT IN THE FORWARD GALLEY. REPLACED BOTH LAMP HOLDERS ON FORWARD GALLEY LIGHT
- [SDR SCNA97313](https://openairdocs.org/sdr/SCNA97313), Sep 13, 1997: WIRE. FAILED. EMERGENCY FLOOR TRACK LIGHTING WAS FOUND INOP AT LEFT AISLE FROM ROW 36 TO ROW 43. FOUND WIRE PULLED AT SPLICE AND REPAIRED SPLICE. FUNCTIONALLY TESTED NORMAL.
- [SDR SCNA97290](https://openairdocs.org/sdr/SCNA97290), Jul 4, 1997: FIRE CONTL BOX. FAILED. DURING DESCENT INTO DTW, THE NR 3 ENGINE FIRE WARNING SOUNDED, SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE BOTTLES. POST FLIGHT INSPECTION REVEALED NO SIGNS OF FIR
- [SDR SCNA97026](https://openairdocs.org/sdr/SCNA97026), Feb 1, 1997: MEGAPHONE. INOPERATIVE. MEGAPHONE AT L2 WOULD NOT SELF TEST. REMOVED AND REPLACED MEGAPHONE.
- [SDR SCNA97007](https://openairdocs.org/sdr/SCNA97007), Jan 6, 1997: DOOR SLIDE. INOPERATIVE. DOOR SLIDE LIGHT AT L3 DOOR DOES NOT PUSH TO TEST. REMOVED AND REPLACED WIRE HARNESS AND LIGHT ASSEMBLY. DOOR SLIDE LIGHT CHECKS GOOD IN ACCORDANCE WITH MM 25-6
- [SDR SCNA96439](https://openairdocs.org/sdr/SCNA96439), Dec 13, 1996: POWER SUPPLY. INOPERATIVE. AFT EMERGENCY POWER SUPPLY FAILED SELF TEST. REMOVED AND REPLACED AFT EMERGENCY EXIT POWER SUPPLY AND OPS CHECKED GOOD.
- [SDR SCNA96432](https://openairdocs.org/sdr/SCNA96432), Dec 6, 1996: SMOKE DETECTOR. INOPERATIVE. LAV 7 SMOKE DETECTOR LIGHT INOP. RESECURED WIRES TO LIGHT SOCKET AND OPS TESTED NORMAL.
- [SDR SCNA96388](https://openairdocs.org/sdr/SCNA96388), Nov 24, 1996: POWER SUPPLY. INOPERATIVE. THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAILED TO TEST. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECKED NORMAL.
- [SDR SCNA96383](https://openairdocs.org/sdr/SCNA96383), Nov 15, 1996: PIGTAIL. SHORTED. THE LEFT FORWARD EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. FOUND THE EMERGENCY LIGHT PIGTAIL SHORTED AT THE SECOND MODULE FROM THE LEFT, AFT SIDE OF
- [SDR SCNA96375](https://openairdocs.org/sdr/SCNA96375), Nov 4, 1996: SKIN. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON CENTER WING BOX UPPER SKIN FRM RBL 30 TO RBL 80 AT BS 1361, AT AFT SPAR. OPENED ACCESS TO CENTER WING BOX, REMOVED 
- [SDR SCNA96374](https://openairdocs.org/sdr/SCNA96374), Nov 3, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON OVERHEAD GILL LINER SUPPORT AT BS 1997, RBL 18. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE 
- [SDR SCNA96347](https://openairdocs.org/sdr/SCNA96347), Nov 1, 1996: STRINGER. CRACKED. DURING HEAVY MAINTENANCE, FOUND STRINGER 48L CRACKED BETWEEN BS 1099 AND BS 1119. STOP DRILLED 1 INCH CRACK, FABRICATED AND INSTALLED A REPAIR DOUBLER IN ACCORD
- [SDR SCNA96346](https://openairdocs.org/sdr/SCNA96346), Oct 27, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND FLOOR SUPPORT DAMAGED AT BS 1964, RBL 48. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WITH SRM
- [SDR SCNA96345](https://openairdocs.org/sdr/SCNA96345), Oct 24, 1996: BRACKET. CORRODED. DURING HEAVY MAINTENANCE, FOUND MOUNTING BRACKET CORRODED AT BS 435 CENTER TIE DOWN FITTING. REMOVED AND REPLACED MOUNTING BRACKET IN ACCORDANCE WITH SRM 51-30-
- [SDR SCNA96342](https://openairdocs.org/sdr/SCNA96342), Oct 24, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON TOP FLANGE OF THE LEFT HAND INBOARD SEAT TRACK AT BS 791 TO 840. REMOVED CORROSION, FABRICATED AND INSTALLED A REPA
- [SDR SCNA96341](https://openairdocs.org/sdr/SCNA96341), Oct 23, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 1960, LBL 78. REMOVED DAMGED SEAT TRACK SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCORDA
- [SDR SCNA96373](https://openairdocs.org/sdr/SCNA96373), Oct 22, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK AT BS 420, LBL 53. REMOVED CORROSION, FABRICATED AND INSTALLED A REPAIR IN ACCORDANCE WITH ENGINEERING A
- [SDR SCNA96368](https://openairdocs.org/sdr/SCNA96368), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1909, RBL 53 TO RBL 85. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT 
- [SDR SCNA96367](https://openairdocs.org/sdr/SCNA96367), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE FOUND CORROSION ON FLOOR SUPPORT AT BS 1887, BL ZERO TO RBL 90. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT 
- [SDR SCNA96366](https://openairdocs.org/sdr/SCNA96366), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1835 TO BS 1887, LBL 40. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT
- [SDR SCNA96365](https://openairdocs.org/sdr/SCNA96365), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1901, LBL 53 TO LBL 86. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT 
- [SDR SCNA96364](https://openairdocs.org/sdr/SCNA96364), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921 TO BS 1964, LBL 18. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT
- [SDR SCNA96363](https://openairdocs.org/sdr/SCNA96363), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1871 RBL 64 TO RBL 90. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT I
- [SDR SCNA96344](https://openairdocs.org/sdr/SCNA96344), Oct 22, 1996: BRACKET. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON G4 GALLEY ATTACH BRACKET. FABRICATED AND INSTALLED A NEW ATTACH BRACKET IN ACCORDANCE WITH SRM 51-21-01.
- [SDR SCNA96343](https://openairdocs.org/sdr/SCNA96343), Oct 22, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK UNDER L1 DOOR THRESHOLD. REMOVED CORRODED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION IN
- [SDR SCNA96340](https://openairdocs.org/sdr/SCNA96340), Oct 22, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1835 LBL 65 TO BS 1887, LBL 60. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED 
- [SDR SCNA96339](https://openairdocs.org/sdr/SCNA96339), Oct 22, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK FROM BS 1800, RBL 67 TO BS 1887, RBL 59. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INSTALLED
- [SDR SCNA96338](https://openairdocs.org/sdr/SCNA96338), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1887 TO BS 1920, BL 0. REMOVED CORRODED SECTION OF SUPPORT, FABRICATED AND INSTALLED A NEW SECT
- [SDR SCNA96337](https://openairdocs.org/sdr/SCNA96337), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 13. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SECTION OF FLOOR SUPPORT
- [SDR SCNA96336](https://openairdocs.org/sdr/SCNA96336), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1923, LBL 13 TO RBL 13. REMOVED CORRODED SECTION OF SUPPORT, FABRICATED AND INSTALLED A NEW SEC
- [SDR SCNA96335](https://openairdocs.org/sdr/SCNA96335), Oct 22, 1996: SEAT TRACK. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON SEAT TRACK BETWEEN BS 1887 AND BS 1964, RBL 88 TO RBL 78. REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED AND INS
- [SDR SCNA96334](https://openairdocs.org/sdr/SCNA96334), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1900 TO 1921, LBL 13. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A NEW SECTION IN ACCOR
- [SDR SCNA96333](https://openairdocs.org/sdr/SCNA96333), Oct 22, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1921, RBL 20 TO RBL 49. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN 
- [SDR SCNA96372](https://openairdocs.org/sdr/SCNA96372), Oct 21, 1996: FLOOR SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON THE FLOOR SUPPORT AT BS 1964, RBL 39. REMOVED CORRODED FLOOR SUPPORT, FABRICATED, AND INSTALLED A NEW FLOOR SUPPORT
- [SDR SCNA96362](https://openairdocs.org/sdr/SCNA96362), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1835 - BS 1837, RBL 39. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN 
- [SDR SCNA96361](https://openairdocs.org/sdr/SCNA96361), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964 RBL 46. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WIT
- [SDR SCNA96360](https://openairdocs.org/sdr/SCNA96360), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1887 LBL 75. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WIT
- [SDR SCNA96359](https://openairdocs.org/sdr/SCNA96359), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 39. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WI
- [SDR SCNA96358](https://openairdocs.org/sdr/SCNA96358), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, LBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WI
- [SDR SCNA96357](https://openairdocs.org/sdr/SCNA96357), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT BS 1964, RBL 29. REMOVED FLOOR SUPPORT, FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IN ACCORDANCE WI
- [SDR SCNA96356](https://openairdocs.org/sdr/SCNA96356), Oct 21, 1996: SUPPORT. CORRODED. DURING HEAVY MAINTENANCE, FOUND CORROSION ON FLOOR SUPPORT AT BS 1964 RBL 64. REMOVED CORRODED SUPPORT, FABRICATED AND INSTALLED A NEW SUPPORT IN ACCORDANCE WIT

All 81: https://openairdocs.org/aircraft/N571SC/unmatched-reports.md

## STCs that may be installed (OpenAirDocs) (278, 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 278: https://openairdocs.org/aircraft/N571SC/stcs.md

## Related

- Other Cessna 208 aircraft: https://openairdocs.org/model/cessna-208/aircraft.md
- The Pratt & Whitney Canada PT6A-114A engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-114a.md

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