# N162CA: 2007 Columbia Aircraft Mfg LC41-550FG

- Status: Valid registration
- Airframe: [Columbia Aircraft Mfg LC41-550FG](https://openairdocs.org/model/columbia-aircraft-mfg-lc41-550fg) (registry code 5150011, 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: 41772
- Year built: 2007
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, utility
- Airworthiness date: July 28, 2007
- Certificate issued: April 18, 2023
- Expires: April 30, 2030
- Mode S code: A0F94F
- Registered owner: [Wdf Montana LLC](https://openairdocs.org/faa-owner/WDF%20MONTANA%20LLC)
- Location: [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell)
- Owner type: LLC
- Owner's area on the map: 48.2306° N, 114.4033° W: Placed by OpenAirDocs at the center of ZIP code 59901, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=162CA
- Page: https://openairdocs.org/aircraft/N162CA

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 (Columbia Aircraft Mfg 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 N162CA.

## FAA accident and incident reports

None matched to N162CA.

## 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 N162CA not matched to an aircraft (43)

They name N162CA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SWIA200110068](https://openairdocs.org/sdr/SWIA200110068), Jul 26, 2001: SWITCH. FAILED. ON TAXI, FLAPS SELECTED 15 DEGREES. FLAP INDICATOR GOES FROM 15 DEGREES TO 0 DEGREES EVERY MINUTE. GREEN BARS DISAPPEAR WHEN FLAPS ARE AT 0 DEGREES. THEY REAPPE
- [SDR SWIA200110067](https://openairdocs.org/sdr/SWIA200110067), Jul 24, 2001: WARNING SYSTEM. ACTIVATED. ABORTED TAKEOFF - TRIPLE CHIME - AURAL WARNING - BRAKES, FLAPS, AUTO FEATHER OCCURRED DURING TAKEOFF ROLL. REPLACED AND SECURED AURAL WARNING UNIT. PERFORMED OP
- [SDR SWIA200110066](https://openairdocs.org/sdr/SWIA200110066), Jul 17, 2001: CONTROL UNIT. FAILED. DURING CRUISE, ASWS & FLAP LIGHTS ON MAP & ASYMMETRY DISSAGREEMENT, CONTROL FAULT LIGHTS ON OVERHEAD. PANEL FLAP INDICATOR FLUCTUATING 0 DEGREES - 45 DEGREES SE
- [SDR SWIA972628](https://openairdocs.org/sdr/SWIA972628), Jun 11, 2001: ACTUATOR. FAILED. CONTROL FAULT WHEN SELECTING FLAPS 15, RESET AS PER QRH. CONTROL FAULT AGAIN WHEN SELECTING FLAPS 25. PERFORMED ACTUATOR TEST ON BOTH OUTBOARD ACTUATORS. FOUND 
- [SDR SWIA972550](https://openairdocs.org/sdr/SWIA972550), May 4, 2001: SEQUENCE VALVE. DEFECTIVE. EN ROUTE A SYSTEM GREEN LIGHT ON FOR RIGHT MAIN GEAR AFTER LOWERING GEAR HANDLE. ALL SIX DISAGREEMENT LIGHTS ON AND NO ADDITIONAL GREEN LIGHTS. AFTER APPROXIMAT
- [SDR SWIA972549](https://openairdocs.org/sdr/SWIA972549), May 4, 2001: ACTUATOR. FAILED. LANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED GEAR EXTENSION BY ELECTRIC OVERRIDE CHECK LIST IN QRH. ALL EXTENDED NORMALLY. REPLACED MAIN ACTUATING CYLINDER
- [SDR SWIA972353](https://openairdocs.org/sdr/SWIA972353), Feb 12, 2001: RCCB. FAILED. RIGHT PROPELLER HEAT CONTINUES TO FAIL IN FLIGHT. EN ROUTE LAX DIVERTED TO PSP. INSPECTED LEFT AND RIGHT PROPELLER DEICE LEADS, LOOKED OK. CHECKED RIGHT PROPELL
- [SDR SWIA972302](https://openairdocs.org/sdr/SWIA972302), Jan 26, 2001: SENSOR. FAILED. LANDING GEAR WOULD NOT EXTEND NORMALLY. CYCLED TWICE, NO EFFECT. PERFORMED QRH GEAR EXTENSION BY ELECTRICAL OVERRIDE TO EXTEND GEAR. REPLACED RIGHT MAIN A DOWNL
- [SDR SWIA972258](https://openairdocs.org/sdr/SWIA972258), Jan 8, 2001: ACTUATOR. MALFUNCTIONED. CONTROL FAULT ON FLAP DURING RETRACTION ON GROUND. PRESS RESET AS PER QRH, FAULT CLEARED BUT REOCCURS WHEN RESELECTING FLAPS TO 15 DEGREES. INSTALLED SERVICEABL
- [SDR SWIA972255](https://openairdocs.org/sdr/SWIA972255), Jan 6, 2001: ACTUATOR. FAILED. AFTER SELECTING FLAPS 45 DEGREES DISAGREEMENT ILLUMINATED OUTBOARD PAIRS WERE AFFECTED WITH 4 LIGHT PAIRS NOT ILLUMINATED. DID NOT FIX ITSELF. REMOVED AND REPLA
- [SDR SWIA972209](https://openairdocs.org/sdr/SWIA972209), Dec 23, 2000: WARNING SYSTEM. ACTIVATED. ''TAKEOFF TRIM'' WARNING SOUNDS ON POWER LEVER ADVANCEMENT WITH TRIM INDEX WELL WITHIN GREEN ARC. INSPECTED OUT OF TRIM PROX SENSORS. BOTH FOUND GOOD. PERFORMED
- [SDR SWIA972205](https://openairdocs.org/sdr/SWIA972205), Dec 21, 2000: WIRE. BROKEN. ON TAKEOFF AURAL WARNING ''TAKE OFF'' CAME ON. ABORTED TAKEOFF. TRIM WAS IN THE GREEN BAND. UPON RETURN TO GATE, WARNING PERSISTED REGARDLESS OF TRIM WHEEL POSI
- [SDR SWIA971524](https://openairdocs.org/sdr/SWIA971524), Jul 3, 1999: MASK. MALFUNCTIONED. ROW 7 OXYGEN MASKS FELL DOWN. RETURNED TO SEA. SECURED OXYGEN MASK. EXAMINED LATCHING DEVICE AND FOUND NO DEFECTS. OPS CHECKS GOOD.
- [SDR SWIA971508](https://openairdocs.org/sdr/SWIA971508), Jun 4, 1999: CIRCUIT BREAKER. TRIPPED. LANDING GEAR WOULD NOT RETRACT. RETURNED TO PDX. RESET UP/DOWN CONTROL AND DOWN CONTROL OVERRIDE CIRCUIT BREAKERS.
- [SDR SWIA971298](https://openairdocs.org/sdr/SWIA971298), Nov 1, 1998: LINE. FAILED. RIGHT ENGINE LOST OIL PRESSURE ON DESCENT. PRESSURE DROPPED BELOW 40 PSI AND ENGINE HAD TO BE SHUT DOWN. REPLACED OIL COOLER CROSS FLOW LINE. RAN ENGINE, LEAK A
- [SDR COMA9810054](https://openairdocs.org/sdr/COMA9810054), Mar 4, 1998: SIGN. BROKEN. EMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA9810038](https://openairdocs.org/sdr/COMA9810038), Feb 6, 1998: TQ INDICATOR. MALFUNCTION. DURING TAKEOFF, THE RIGHT HAND TORQUE INDICATION WAS 195 PERCENT. REPLACED THE TORQUE INDICATOR.
- [SDR COMA9710478](https://openairdocs.org/sdr/COMA9710478), Nov 13, 1997: UNSAFE LIGHT. MALFUNCTIONED. WHEN LANDING GEAR SELECTED DOWN, THE RIGHT HAND MLG INDICATED UNSAFE. LANDING GEAR CYCLED TWICE BEFORE GREEN INDICATION. COULD NOT DUPLICATE DISCREPANCY. SYSTEM
- [SDR COMA9710404](https://openairdocs.org/sdr/COMA9710404), Sep 11, 1997: NOZZLE. LEAKING. FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE ENGINE FUEL NOZZLES AND TRANSFER TUBES.
- [SDR COMA9710340](https://openairdocs.org/sdr/COMA9710340), Jul 29, 1997: RELAY. OVERHEATED. OVERHEATED ELECTRIC SMELL IN COCKPIT. REPLACED FEEDER PROTECTION RELAY K0152.
- [SDR COMA9710232](https://openairdocs.org/sdr/COMA9710232), May 1, 1997: BULB. FAILED. EMERGENCY LAMP OVER ENTRANCE DOOR IS INOP. REPLACED BULB.
- [SDR COMA9710224](https://openairdocs.org/sdr/COMA9710224), Apr 22, 1997: ROLLERS. WORN. FLAP DISAGREE WARNING WHEN FLAPS SELECTED UP AFTER TAKEOFF. REPLACED RIGHT HAND OUTBOARD FLAP ROLLERS.
- [SDR COMA9710173](https://openairdocs.org/sdr/COMA9710173), Mar 15, 1997: TRIM TAB SENSOR. DEFECTIVE. TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.
- [SDR COMA9710129](https://openairdocs.org/sdr/COMA9710129), Feb 11, 1997: WIRE. DAMAGED. WHEN FLAPS SELECTED TO 15 DEGREES, CONTROL FAULT WARNING ON. REPAIRED DAMAGED WIRING CONNECTION AT RT OUTBOARD FLAP ACTUATOR.
- [SDR COMA9710027](https://openairdocs.org/sdr/COMA9710027), Jan 11, 1997: CONTROL UNIT. INOPERATIVE. ON LANDING, AIRCRAFT YAWED SHARPLY AFTER CLEARING RUNWAY NWS DID NOT RESPOND WITH INPUTS FROM TILLER OR PEDALS. REPLACED STEERING ECU, TAXI CHECK GOOD.
- [SDR COMA9610299](https://openairdocs.org/sdr/COMA9610299), Oct 9, 1996: BUTT STRAP. CORRODED. FOUND FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER REPORT NR 1671-1, REV. IR, DATED 10-22
- [SDR COMA9610290](https://openairdocs.org/sdr/COMA9610290), Sep 30, 1996: ACTUATOR. LEAKING. RT OUTBD MAIN GEAR DOOR ACTUATOR LEAKING. REPLACED GEAR DOOR ACTUATOR.
- [SDR COMA9610247](https://openairdocs.org/sdr/COMA9610247), Aug 16, 1996: SWITCH. OUT OF ADJUST. SERVICE DOOR WARNING LIGHT ILLUMINATED DURING FLIGHT. ADJUSTED THE AVIONICS DOOR MICROSWITCH.
- [SDR COMA9610196](https://openairdocs.org/sdr/COMA9610196), Jun 30, 1996: FLAP WARNING. ACTIVATED. FLAP CONTROL FAULT WARNING AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND WITH FLAP SYSTEM.
- [SDR COMA9610197](https://openairdocs.org/sdr/COMA9610197), Jun 27, 1996: SEALS. LEAKING. FUEL DRIPPING FROM RT ENGINE NACELLE. REPLACED THE O-RING SEALS ON THE ENGINE FUEL NOZZLES.
- [SDR COMA9610124](https://openairdocs.org/sdr/COMA9610124), Apr 5, 1996: SKIN. DENTED. DURING ROUTINE MAINTENANCE, A LARGE DENT WAS FOUND ON THE FUSELAGE AFT RIGHT LOWER SKIN JUST FORWARD OF FRAME 45 BETWEEN STRINGERS 19R AND 20R. THE DAMGE WAS RE
- [SDR COMA9610099](https://openairdocs.org/sdr/COMA9610099), Mar 8, 1996: SWIVEL. LEAKING. HYDRAULIC FLUID LEAKAGE ON LEFT MLG STRUT. REPLACED BROKEN LINE SWIVEL FITTING.
- [SDR COMA9610089](https://openairdocs.org/sdr/COMA9610089), Feb 21, 1996: ACTUATOR. DEFECTIVE. LEFT INBD FLAP WILL NOT RETRACT. REPLACED THE LT INBD FLAP ACTUATOR.
- [SDR COMA9610082](https://openairdocs.org/sdr/COMA9610082), Feb 13, 1996: ACTUATOR. DEFECTIVE. FLAP CONTROL FAULT WARNING. REPLACED THE RT OUTBD FLAP ACTUATOR. PART TOTAL CYCLES, 2,517.
- [SDR COMA9610039](https://openairdocs.org/sdr/COMA9610039), Jan 25, 1996: SEAL. DEFECTIVE. RIGHT ENGINE NP FLUCTUATES. REPLACED PROPELLER TRANSFER TUBE SEALS.
- [SDR COMA9610028](https://openairdocs.org/sdr/COMA9610028), Jan 15, 1996: ANNUNICATOR PNL. MALFUNCTIONED. DURING TAKEOFF, RECEIVED FLAP CONTROL FAULT WARNING. REPLACED THE FLAP ANNUNCIATOR PANEL.
- [SDR COMA9512012](https://openairdocs.org/sdr/COMA9512012), Nov 24, 1995: AHRS COMPUTER. FAILED. NR 1 AHRS IS INOP. REPLACED THE NR 1 AHRS COMPUTER.
- [SDR COM11891](https://openairdocs.org/sdr/COM11891), May 15, 1995: SUPPORT. CRACKED. THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED, DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPAIRED IAW AERO 
- [SDR COM11822](https://openairdocs.org/sdr/COM11822), Mar 15, 1995: ROLLER. BINDING. FLAP DISAGREEMENT WARNING WHEN FLAPS SELECTED UP DURING CLIMB. REPLACED ROLLERS ON RT OUTBD FLAP.
- [SDR COM11817](https://openairdocs.org/sdr/COM11817), Mar 13, 1995: SKIN SUPPORT. CRACKED. FUEL WAS FOUND LEAKING FROM THE LEFT WING UPPER SKIN. TWO RIVET HEADS WERE FOUND BROKEN AT RIB NR 20 BETWEEN STRINGERS NR 2 AND NR 3. INTERNAL INSPECTION REVEAL
- [SDR COM11816](https://openairdocs.org/sdr/COM11816), Mar 12, 1995: ACTUATOR. DEFECTIVE. FLAP DISAGREEMENT WARNING, FLAPS WOULD NOT RETRACT. REPLACED THE RT OUTBD FLAP ACTUATOR.
- [SDR COM11815](https://openairdocs.org/sdr/COM11815), Mar 11, 1995: ROLLER. DEFECTIVE. FLAP DISAGREEMENT WARNING, FLAPS STUCK AT 15 DEGREES. REPLACED DEFECTIVE ROLLER ON LT OUTBD FLAP.
- [SDR COM11760](https://openairdocs.org/sdr/COM11760), Feb 6, 1995: ACTUATOR. DEFECTIVE. FLAP CONTROL FAULT WARNING WILL NOT RESET. REPLACED RT OUTBD FLAP ACTUATOR.

## 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 (Columbia Aircraft Mfg 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/N162CA/stcs.md

## Related

- Other Columbia Aircraft Mfg LC41-550FG aircraft: https://openairdocs.org/model/columbia-aircraft-mfg-lc41-550fg/aircraft.md
- The Continental TSIO-550-C engine: https://openairdocs.org/engine/continental-tsio-550-c.md

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