# N160MC: 2010 Cessna LC41-550FG

- Status: Valid registration
- Airframe: [Cessna LC41-550FG](https://openairdocs.org/model/cessna-lc41-550fg) (registry code 2073320, 4 seats)
- Engine: [Continental TSIO-550-C](https://openairdocs.org/engine/continental-tsio-550-c) (registry code 17246)
- Data sheets: [TCDS A00003SE](https://openairdocs.org/tcds/A00003SE) (Textron Aviation Inc.), [TCDS E5SO](https://openairdocs.org/tcds/E5SO) (Continental Aerospace Technologies, Inc.) (OpenAirDocs)
- Serial number: 411160
- Year built: 2010
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, utility
- Airworthiness date: May 20, 2010
- Certificate issued: September 5, 2018
- Expires: September 30, 2028
- Mode S code: A0F2C4
- Registered owner: [Haiasi LLC](https://openairdocs.org/faa-owner/HAIASI%20LLC)
- Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)
- Owner type: LLC
- Owner's area on the map: 39.7236° N, 75.5412° W: Placed by OpenAirDocs at the center of ZIP code 19801, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=160MC
- Page: https://openairdocs.org/aircraft/N160MC

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): 24 in force

### Matched by airframe (Cessna LC41-550FG)

- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2013-11-10](https://openairdocs.org/ad/2013-11-10): Fuselage Structure (General) · Cessna LC40-550FG, LC41-550FG and LC42-550FG. Effective Jul 26, 2013
- [AD 2011-03-04](https://openairdocs.org/ad/2011-03-04): Stabilizers · Cessna LC40-550FG, LC41-550FG and LC42-550FG. Effective Mar 14, 2011
- [AD 2010-26-54](https://openairdocs.org/ad/2010-26-54): Wings · Cessna LC41-550FG and LC42-550FG. Effective Jan 10, 2011
- [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2007-07-06 R1](https://openairdocs.org/ad/2007-07-06-R1): Aileron and elevator control systems · Cessna LC40-550FG, LC41-550FG and LC42-550FG. Effective Dec 5, 2008
- [AD 2008-02-06](https://openairdocs.org/ad/2008-02-06): GSM 85 servo gearbox units · Cessna 182T, 206H, LC40-550FG and 11 more. Effective Feb 26, 2008
- [AD 2006-25-08](https://openairdocs.org/ad/2006-25-08): Deice system · Cessna LC41-550FG and LC42-550FG with STC SA02260CH. Effective Dec 21, 2006
- [AD 2005-12-20](https://openairdocs.org/ad/2005-12-20): Elevator torque tube assembly · Cessna LC41-550FG. Effective Jun 21, 2005

### Matched by engine (Continental TSIO-550-C)

- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2023-02-12](https://openairdocs.org/ad/2023-02-12): Engine Air Intake System · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Feb 17, 2023
- [AD 2020-16-11](https://openairdocs.org/ad/2020-16-11): SUMMARY: Reciprocating Cylinder Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 23 more. Effective Sep 21, 2020
- [AD 2016-21-04](https://openairdocs.org/ad/2016-21-04): Oil cooler cross fitting assembly · Continental Motors TSIO-550-C, TSIO-550-K, TSIO-550-N and 2 more. Effective Nov 18, 2016
- [AD 2016-16-12](https://openairdocs.org/ad/2016-16-12): Cylinder assemblies · Continental Motors LTSIO-520-AE, TSIO-520-A, TSIO-520-AE and 89 more. Effective Sep 15, 2016
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2007-16-10](https://openairdocs.org/ad/2007-16-10): Kelly Aerospace Power Systems turbochargers · Turbonormalizing system (Engine Technologies STC SE10589SC or SA10588SC). Effective Aug 23, 2007
- [AD 2004-08-10](https://openairdocs.org/ad/2004-08-10): Serial-numbered (SN) cylinders · Modify Teledyne Continental TSIO-520-NB engine (RAM Aircraft Limited Partnership STC SE09104SC or 4 others). Effective May 5, 2004
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993

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

- [AD 2010-26-53](https://openairdocs.org/ad/2010-26-53) (historical): Wings · Cessna LC41-550FG and LC42-550FG
- [AD 2009-09-09](https://openairdocs.org/ad/2009-09-09) (historical): Rudder hinge brackets · Cessna LC40-550FG, LC41-550FG and LC42-550FG. Effective May 11, 2009
- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 2007-07-06](https://openairdocs.org/ad/2007-07-06) (historical): Aileron and the elevator linear bearings and control rods · Cessna LC40-550FG, LC41-550FG and LC42-550FG. Effective Apr 9, 2007
- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

## Information bulletins (advisory) (11 in force)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-18-16](https://openairdocs.org/saib/NE-18-16): POWERPLANT  Alternator Drive Coupling. Issued Jun 20, 2018
- [SAIB NE-17-11](https://openairdocs.org/saib/NE-17-11): POWERPLANT  Engine damage as a result of kickback. Issued May 10, 2017
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-09-08](https://openairdocs.org/saib/NE-09-08): Reciprocating Engine Cylinder Section. Issued Jan 30, 2009
- [SAIB NE-02-41](https://openairdocs.org/saib/NE-02-41): . Issued Aug 8, 2002

## NTSB investigations

None matched to N160MC.

## FAA accident and incident reports

None matched to N160MC.

## Reports on N160MC not matched to an aircraft (3)

They name N160MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19980716021779I](https://openairdocs.org/incident/19980716021779I), Jul 16, 1998: Swrngn SA227AC (N160MC), Great Falls, MT. Aircraft failed pressurize on climb out. Returned. Cargo door not properly closed.
- [Incident 19980428012979I](https://openairdocs.org/incident/19980428012979I), Apr 28, 1998: Swrngn SA227AC (N160MC), Billings, MT. Narrative: on 04/28/98 at 2136 LCL, big sky airlines flight 1106 experienced a failure of the main landing gear retraction after take-off from Billings,…
- [Incident 19920819037179I](https://openairdocs.org/incident/19920819037179I), Aug 19, 1992: Swrngn SA227AC (N160MC), Washington, DC, Minor damage. Aborted takeoff because aircraft not accelerating fast enough. Departed end of runway.

## 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 N160MC not matched to an aircraft (28)

They name N160MC, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 2003F00628](https://openairdocs.org/sdr/2003F00628), Jun 30, 2003: WATER INJECTION. MALFUNCTIONED. CAWI DID NOT FIRE. INSUFFICIENT AWI FLOW, HOT WEATHER OPS, OAT WAS APPROXIMATELY 100 DEGREES FARENHEIT. ADJUSTED CAWI FLOW VALVE OUT ONE FULL TURN. GROUND RUN C
- [SDR BSA2002F00001](https://openairdocs.org/sdr/BSA2002F00001), Sep 10, 2002: HANDLE. OUT OF ADJUST. DURING CRUISE THE ANNUNCIATOR PANEL WARNING LIGHT CAME ON. CREW FOLLOWED EMERGENCY PROCEDURES, DEPRESSURIZED THE A/C AND CONTINUED TO DESTINATION AT A LOWER ALT
- [SDR 2002F00335](https://openairdocs.org/sdr/2002F00335), Feb 24, 2002: LATCH. MISINSTALLED. MWH - FLT 6006 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE FLIGHT. WHEN AIRCRAFT WAS DEPRESSURIZED THE LIGHT WENT OUT. CREW CONTINUED TO NEXT STATION AS IT
- [SDR 2002F00521](https://openairdocs.org/sdr/2002F00521), Jan 24, 2002: WARNING SYSTEM. FALSE ACTIVATION. MSO - FLT 2583 - CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB 20 MILES NORTH OF THE STATION. CREW RETURNED TO THE STATION. NO APPARENT PROBLEM WAS FOUND. CARGO
- [SDR 2002F00354](https://openairdocs.org/sdr/2002F00354), Jan 22, 2002: LINE. RUPTURED. THE RT HYD PRESS LIGHT CAME ON DURING CRUISE AND THE LT HYD PRESS LIGHT CAME ON DURING DESCENT. THE FLAPS EXTENDED SLOWLY, CREW DECLARED EMERGENCY, USED THE GEA
- [SDR 2002F00357](https://openairdocs.org/sdr/2002F00357), Dec 16, 2001: SEAL. DAMAGED. FLT 2588 - HLN - DURING CLIMB-OUT, CABIN PRESSURE WAS LOST. CREW AND PASSENGERS UTILIZED OXYGEN MASKS AND FLIGHT CONTINUED TO DESTINATION. CABIN DOOR SEAL HAD A
- [SDR 20010515SG001](https://openairdocs.org/sdr/20010515SG001), Apr 6, 2001: HANDLE. OUT OF POSITION. DURING CLIMB-OUT, CREW FOUND AIRCRAFT WOULDN''T PRESSURIZE IN EITHER MAN OR AUTO MODE. SUCTION GAUGE SHOWED IN NORMAL RANGE. RECYCLED CARGO DOOR HANDLE, PRESSUR
- [SDR 2002F00520](https://openairdocs.org/sdr/2002F00520), Jan 21, 2001: MECHANISM. DAMAGED. BIL - FLT 1315 - CARGO DOOR WARNING LIGHT CAME ON DURING CRUISE AT FL190. THE CREW DECREASED CABIN PRESSURE AS THEY RETURNED TO STATION. THE WARNING LIGHT WENT 
- [SDR 20010206SG004](https://openairdocs.org/sdr/20010206SG004), Nov 30, 2000: WARNING LIGHT. ILLUMINATED. HOB - FLT 1331 - LEFT WING OVERHEAT LIGHT CAME STEADY ON DURING CRUISE. CREW FOLLOWED CHECKLIST PROCEDURES, EXTENDED GEAR AND TURNED OFF LEFT BLEED. LIGHT WENT 
- [SDR 20000810SH010](https://openairdocs.org/sdr/20000810SH010), Jul 6, 2000: CONNECTOR. DAMAGED. DFW - FLT 1325 - BATTERY OVERHEAT LIGHTS CAME ON IN-FLIGHT. WHEN BATTERY WAS SHUT OFF BY CREW USING EMERGENCY CHECKLIST PROCEDURES, LIGHTS WENT OFF AND BATTERY 
- [SDR 20001005AP030](https://openairdocs.org/sdr/20001005AP030), May 24, 2000: LINE. LEAKING. FLT 1321 - DFW - DURING CRUISE FLIGHT, THE CREW NOTICED THE HYD PRESS LOW LIGHTS CAME ON . HYDRAULIC PRESSURE GAGES WERE CHEKED AND THE LACK OF HYD PRESS WAS CO
- [SDR 20000816AP005](https://openairdocs.org/sdr/20000816AP005), May 24, 2000: LINE. BROKEN. DFW - FLT 1321 - DURING CRUISE FLIGHT, THE CREW NOTICED THE HYD PRESSURE LOW LIGHTS CAME ON. HYDRAULIC PRESSURE GAUGES WERE CHECKED AND THE LACK OF HYD PRESSURE
- [SDR MALA975388](https://openairdocs.org/sdr/MALA975388), May 4, 1997: RADAR. FAILED. DURING CRUISE FLIGHT, CREW REPORTED WEATHER RADAR INOP. AIR TURN BACK TO MSP. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR. OPS CHECK GOOD. (M)
- [SDR MALA965209](https://openairdocs.org/sdr/MALA965209), Nov 21, 1996: SWITCH. FAILED. FLT 3365 - ON APROACH TO DTW, THE GEAR HAD TO BE CYCLED TWO TIMES BEFORE A NOSE GEAR DOWN INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE DOWN AND LOCKED SWIT
- [SDR MALA965079](https://openairdocs.org/sdr/MALA965079), Jul 22, 1996: SWITCHES. LACK OF LUBE. FLT 3397 - ON APPROACH TO DTW, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR AND THE LIGHT ILLUMINATED AFTER 15 SECONDS. MAINTENANCE 
- [SDR MALA965001](https://openairdocs.org/sdr/MALA965001), May 20, 1996: CONNECTOR. WATER CONTAM. FLT NR 3467 - ON CLIMB-OUT FROM YXU, THE LEFT BATTERY AMBER AND RED LIGHTS ILLUMINATED AND THE BATTERY TEMP INDICATION WAS HIGH. THE CREW TURNED OFF THE BATTERY
- [SDR MALA954695](https://openairdocs.org/sdr/MALA954695), Nov 8, 1995: STARTER/GEN. FAILED. DURING A TRAINING FLIGHT IN FAR, THE LEFT ESSENTIAL BUS AND LEFT GENERATOR FAILED. THE AIRCRAFT RETUREND TO FAR WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED
- [SDR MALA954663](https://openairdocs.org/sdr/MALA954663), Oct 12, 1995: RIB. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, THE LEFT FLAP INBOARD ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING DOUBLER IAW FAC SRM 51-00
- [SDR MALA954612](https://openairdocs.org/sdr/MALA954612), Aug 29, 1995: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 438.060 TO BE CRACKED AT THE MOUNT POST HOLE. REPAIRS WERE COMPL
- [SDR MALA954611](https://openairdocs.org/sdr/MALA954611), Aug 29, 1995: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE CARGO DOOR AFT FUSELAGE FRAME AT FS 491 TO BE CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE
- [SDR MALA954438](https://openairdocs.org/sdr/MALA954438), May 2, 1995: STIFFENER. CRACKED. DURING BLOCK CHECK IN MSP, MAINTENANCE FOUND CENTER STIFFENER ASSY P/N 27-31110 AT BL 0.00 AND FS 254.52 CRACKED. REPAIRED BY REPLACING CENTER STIFFENER ASSY WI
- [SDR MALA954437](https://openairdocs.org/sdr/MALA954437), May 2, 1995: FRAME. CRACKED. DURING BLOCK CHECK INSPECTION MSP, MAINTENANCE FOUND A CRACK IN LOWER RT BELT FRAME RELIEF RADIUS AT FS 144.24 AND WL 80.39 RIGHT BELOW STRINGER NR 11A. REPAIRS
- [SDR MALA954414](https://openairdocs.org/sdr/MALA954414), Apr 16, 1995: BLEED AIR. ODOR. MSP - FLT 3235 - EN ROUTE, CREW NOTED A HOT SMELL FROM THE RIGHT BLEED SYSTEM. THE CREW SHUT OFF THE RIGHT BLEED SYSTEM AND THE SMELL DISSIPATED. THE AIRCRAFT C
- [SDR MALA954402](https://openairdocs.org/sdr/MALA954402), Apr 7, 1995: ANGLE. CRACKED. DURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT WING TO NACELLE UPPER INBOARD ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY STOP DRILLING THE C
- [SDR MALA954395](https://openairdocs.org/sdr/MALA954395), Apr 4, 1995: DNLOCK SPRING. BROKEN. FLT NR 3074 - ON APPROACH TO MSP, THE NOSE GEAR REMAINED UP AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE NOSE GEAR EXTENDED NORMALLY. THE
- [SDR MALA954387](https://openairdocs.org/sdr/MALA954387), Mar 25, 1995: HSI. FAILED. FLT 3211 - ON CLIMB-OUT FROM MSP, THE CAPTAINS HSI FAILED. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 1 HSI. SYSTEM OPERATED SATISFACTORILY. (W)
- [SDR MALA954384](https://openairdocs.org/sdr/MALA954384), Mar 23, 1995: FRAME. CRACKED. MSP - DURING ROUTINE MAINTENANCE, LEFT FUSELAGE CONSTANT SECTION LOWER BELT FRAME AT FS 174.06 WAS FOUND CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INST
- [SDR MALA954250](https://openairdocs.org/sdr/MALA954250), Jan 19, 1995: TORQUE TUBE. BENT. MSP - DURING SCHEDULED INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE BENT. REPAIRS COMPLETED BY REPLACING TORQUE TUBE IAW FAC 27-20-20, 27-00-00, AND SRM 51-

## STCs that may be installed (OpenAirDocs) (88, 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 LC41-550FG)

- [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 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 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 SA01134DE](https://openairdocs.org/stc/SA01134DE): Installation of EarthX ETX680-24-TSO Lithium Battery. EarthX Inc
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International 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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES 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 SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International 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
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA11188SC](https://openairdocs.org/stc/SA11188SC): Installation of a McCauley Propeller System. McCauley Propeller Systems
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA04067NY](https://openairdocs.org/stc/SA04067NY): Installation of MT-Propeller Entwicklung GmbH's Model# MTV-14-D/195-30b 4-Blade constant speed propeller and spinner on Textron Aviation Inc. Model LC41-550FG aircraft. MT- Propeller Entwicklung GmbH
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC ST03151CH](https://openairdocs.org/stc/ST03151CH): Installation of heat exchanger kit, Kelly Aerospace kit #KATS-11-006,. Kelly Aerospace Thermal Systems, LLC
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00353BO](https://openairdocs.org/stc/SA00353BO): Installation of an auto lean system. Flight Enhancements LLC
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts. Andrew D. Humphrey
- [STC SA11172SC](https://openairdocs.org/stc/SA11172SC): Installation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antenna. NavWorx Inc
- [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01435WI](https://openairdocs.org/stc/SA01435WI): Installation of TKS Ice Protection System Components, with placard stating, 'INTENTIONAL FLIGHT INTO KNOWN ICING IS PROHIBITED'. CAV Ice Protection Inc
- [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. Avidyne Corporation

All 88: https://openairdocs.org/aircraft/N160MC/stcs.md

## Related

- Other Cessna LC41-550FG aircraft: https://openairdocs.org/model/cessna-lc41-550fg/aircraft.md
- The Continental TSIO-550-C engine: https://openairdocs.org/engine/continental-tsio-550-c.md

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