# Lancair LC41-550FG

- Type: Aircraft model (FAA registry)
- Registry code: 5150001
- Manufacturer (registry): LANCAIR COMPANY
- Model: LC41-550FG
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 4
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A00003SE](https://openairdocs.org/tcds/A00003SE) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 122
- Page: https://openairdocs.org/model/lancair-lc41-550fg

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [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

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

## Information bulletins (advisory) (2)

- [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

## Registered aircraft (122, first 50)

- [N1024Z](https://openairdocs.org/aircraft/N1024Z): [Aqua Men Service LLC](https://openairdocs.org/faa-owner/AQUA%20MEN%20SERVICE%20LLC), [Temple, GA](https://openairdocs.org/faa-place/GA/Temple), built 2005, S/N 41097
- [N104PP](https://openairdocs.org/aircraft/N104PP): [Toledo Public Schools](https://openairdocs.org/faa-owner/TOLEDO%20PUBLIC%20SCHOOLS), [Swanton, OH](https://openairdocs.org/faa-place/OH/Swanton), S/N 41086
- [N131MW](https://openairdocs.org/aircraft/N131MW): [Farina George](https://openairdocs.org/faa-owner/FARINA%20GEORGE), [Killen, AL](https://openairdocs.org/faa-place/AL/Killen), built 2004, S/N 41021
- [N139DC](https://openairdocs.org/aircraft/N139DC): [Legacy Air LLC](https://openairdocs.org/faa-owner/LEGACY%20AIR%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 2005, S/N 41056
- [N144LC](https://openairdocs.org/aircraft/N144LC): [Pruetts Food Inc](https://openairdocs.org/faa-owner/PRUETTS%20FOOD%20INC), [Broken Bow, OK](https://openairdocs.org/faa-place/OK/Broken%20Bow), built 2004, S/N 41019
- [N150LC](https://openairdocs.org/aircraft/N150LC): [Lipoff Jay I](https://openairdocs.org/faa-owner/LIPOFF%20JAY%20I), [Sarasota, FL](https://openairdocs.org/faa-place/FL/Sarasota), built 2005, S/N 41501
- [N169HT](https://openairdocs.org/aircraft/N169HT): [Aerie Leisure Inc](https://openairdocs.org/faa-owner/AERIE%20LEISURE%20INC), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), built 2005, S/N 41054
- [N169PJ](https://openairdocs.org/aircraft/N169PJ): [Bernard Douglas A](https://openairdocs.org/faa-owner/BERNARD%20DOUGLAS%20A), [New Iberia, LA](https://openairdocs.org/faa-place/LA/New%20Iberia), built 2005, S/N 41065
- [N209DW](https://openairdocs.org/aircraft/N209DW): [White Columbia Inc Trustee](https://openairdocs.org/faa-owner/WHITE%20COLUMBIA%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2005, S/N 41504
- [N212TJ](https://openairdocs.org/aircraft/N212TJ): [212tj LLC](https://openairdocs.org/faa-owner/212TJ%20LLC), [Monterey, CA](https://openairdocs.org/faa-place/CA/Monterey), built 2004, S/N 41038
- [N221WB](https://openairdocs.org/aircraft/N221WB): [Otter Rock Aero LLC](https://openairdocs.org/faa-owner/OTTER%20ROCK%20AERO%20LLC), [Newport, OR](https://openairdocs.org/faa-place/OR/Newport), built 2005, S/N 41091
- [N222BY](https://openairdocs.org/aircraft/N222BY): [Rda Solutions LLC](https://openairdocs.org/faa-owner/RDA%20SOLUTIONS%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 2004, S/N 41022
- [N227SM](https://openairdocs.org/aircraft/N227SM): [Ipme Management Corp](https://openairdocs.org/faa-owner/IPME%20MANAGEMENT%20CORP), [Jefferson, GA](https://openairdocs.org/faa-place/GA/Jefferson), built 2004, S/N 41011
- [N230SX](https://openairdocs.org/aircraft/N230SX): [2z West LLC](https://openairdocs.org/faa-owner/2Z%20WEST%20LLC), [Alpine, WY](https://openairdocs.org/faa-place/WY/Alpine), built 2004, S/N 41045
- [N234KT](https://openairdocs.org/aircraft/N234KT): [Cessna 182 LLC](https://openairdocs.org/faa-owner/CESSNA%20182%20LLC), [Kitty Hawk, NC](https://openairdocs.org/faa-place/NC/Kitty%20Hawk), built 2004, S/N 41023
- [N236RS](https://openairdocs.org/aircraft/N236RS): [Schoombee Clinton John](https://openairdocs.org/faa-owner/SCHOOMBEE%20CLINTON%20JOHN), [Murrieta, CA](https://openairdocs.org/faa-place/CA/Murrieta), built 2004, S/N 41003
- [N23KP](https://openairdocs.org/aircraft/N23KP): [Sp Aviation Inc](https://openairdocs.org/faa-owner/SP%20AVIATION%20INC), [Hayward, CA](https://openairdocs.org/faa-place/CA/Hayward), built 2004, S/N 41004
- [N240AF](https://openairdocs.org/aircraft/N240AF): [Columbia Av8ors Inc](https://openairdocs.org/faa-owner/COLUMBIA%20AV8ORS%20INC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 2005, S/N 41525
- [N244D](https://openairdocs.org/aircraft/N244D): [Olympia Hangars LLC](https://openairdocs.org/faa-owner/OLYMPIA%20HANGARS%20LLC), [Tumwater, WA](https://openairdocs.org/faa-place/WA/Tumwater), built 2005, S/N 41096
- [N245DB](https://openairdocs.org/aircraft/N245DB): [Vangundy R Eric](https://openairdocs.org/faa-owner/VANGUNDY%20R%20ERIC), [Chapin, IL](https://openairdocs.org/faa-place/IL/Chapin), built 2005, S/N 41102
- [N247DM](https://openairdocs.org/aircraft/N247DM): [Grimmett Lester](https://openairdocs.org/faa-owner/GRIMMETT%20LESTER), [Clinton, MS](https://openairdocs.org/faa-place/MS/Clinton), built 2005, S/N 41506
- [N2500T](https://openairdocs.org/aircraft/N2500T): [J & C Holdings Inc](https://openairdocs.org/faa-owner/J%20%26%20C%20HOLDINGS%20INC), [Laguna Beach, CA](https://openairdocs.org/faa-place/CA/Laguna%20Beach), built 2004, S/N 41026
- [N2507L](https://openairdocs.org/aircraft/N2507L): [Simply Southern N2507l LLC](https://openairdocs.org/faa-owner/SIMPLY%20SOUTHERN%20N2507L%20LLC), [Fayetteville, GA](https://openairdocs.org/faa-place/GA/Fayetteville), built 2005, S/N 41106
- [N2509W](https://openairdocs.org/aircraft/N2509W): [Double D'S LLC](https://openairdocs.org/faa-owner/DOUBLE%20D'S%20LLC), [Massillon, OH](https://openairdocs.org/faa-place/OH/Massillon), built 2005, S/N 41061
- [N2511G](https://openairdocs.org/aircraft/N2511G): [Van Bortel Aircraft Inc](https://openairdocs.org/faa-owner/VAN%20BORTEL%20AIRCRAFT%20INC), [Arlington, TX](https://openairdocs.org/faa-place/TX/Arlington), built 2005, S/N 41101
- [N2511Y](https://openairdocs.org/aircraft/N2511Y): [Prieur Philip](https://openairdocs.org/faa-owner/PRIEUR%20PHILIP), [Suwanee, GA](https://openairdocs.org/faa-place/GA/Suwanee), built 2005, S/N 41060
- [N2514F](https://openairdocs.org/aircraft/N2514F): [Van Bortel Aircraft Inc](https://openairdocs.org/faa-owner/VAN%20BORTEL%20AIRCRAFT%20INC), [Arlington, TX](https://openairdocs.org/faa-place/TX/Arlington), built 2005, S/N 41093
- [N2515B](https://openairdocs.org/aircraft/N2515B): [Independent Columbia Aviators LLC](https://openairdocs.org/faa-owner/INDEPENDENT%20COLUMBIA%20AVIATORS%20LLC), [Katonah, NY](https://openairdocs.org/faa-place/NY/Katonah), built 2004, S/N 41040
- [N2518H](https://openairdocs.org/aircraft/N2518H): [Hakan Michael](https://openairdocs.org/faa-owner/HAKAN%20MICHAEL), [Carpinteria, CA](https://openairdocs.org/faa-place/CA/Carpinteria), built 2005, S/N 41079
- [N251DX](https://openairdocs.org/aircraft/N251DX): [Flight Advantage Inc](https://openairdocs.org/faa-owner/FLIGHT%20ADVANTAGE%20INC), [Hot Springs, AR](https://openairdocs.org/faa-place/AR/Hot%20Springs), built 2005, S/N 41068
- [N2520C](https://openairdocs.org/aircraft/N2520C): [Krause Douglas R](https://openairdocs.org/faa-owner/KRAUSE%20DOUGLAS%20R), [Hinckley, OH](https://openairdocs.org/faa-place/OH/Hinckley), built 2005, S/N 41516
- [N2520S](https://openairdocs.org/aircraft/N2520S): [Peregrine Air LLC](https://openairdocs.org/faa-owner/PEREGRINE%20AIR%20LLC), [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs), built 2005, S/N 41073
- [N2521W](https://openairdocs.org/aircraft/N2521W): [Pc Enterprise Holdings LLC](https://openairdocs.org/faa-owner/PC%20ENTERPRISE%20HOLDINGS%20LLC), [Penfield, NY](https://openairdocs.org/faa-place/NY/Penfield), built 2005, S/N 41514
- [N2522F](https://openairdocs.org/aircraft/N2522F): [Gentrius LLC](https://openairdocs.org/faa-owner/GENTRIUS%20LLC), [Austin, TX](https://openairdocs.org/faa-place/TX/Austin), S/N 41049
- [N2522S](https://openairdocs.org/aircraft/N2522S): [Eagleray Design LLC](https://openairdocs.org/faa-owner/EAGLERAY%20DESIGN%20LLC), [Burlington, VT](https://openairdocs.org/faa-place/VT/Burlington), S/N 41083
- [N2524G](https://openairdocs.org/aircraft/N2524G): [Tgc Aviation LLC](https://openairdocs.org/faa-owner/TGC%20AVIATION%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 2005, S/N 41515
- [N2526B](https://openairdocs.org/aircraft/N2526B): [Timd Group USA Inc](https://openairdocs.org/faa-owner/TIMD%20GROUP%20USA%20INC), [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne), built 2005, S/N 41105
- [N2526L](https://openairdocs.org/aircraft/N2526L): [Quest Aero LLC](https://openairdocs.org/faa-owner/QUEST%20AERO%20LLC), [Zeeland, MI](https://openairdocs.org/faa-place/MI/Zeeland), built 2004, S/N 41035
- [N2527Z](https://openairdocs.org/aircraft/N2527Z): [Qualitair LLC Trustee](https://openairdocs.org/faa-owner/QUALITAIR%20LLC%20TRUSTEE), Michelstadt, built 2005, S/N 41502
- [N25281](https://openairdocs.org/aircraft/N25281): [Relair LLC](https://openairdocs.org/faa-owner/RELAIR%20LLC), [Conesus, NY](https://openairdocs.org/faa-place/NY/Conesus), built 2005, S/N 41088
- [N2528D](https://openairdocs.org/aircraft/N2528D): [Olson Michael S](https://openairdocs.org/faa-owner/OLSON%20MICHAEL%20S), [Ellsworth, KS](https://openairdocs.org/faa-place/KS/Ellsworth), built 2005, S/N 41523
- [N2528T](https://openairdocs.org/aircraft/N2528T): [N2528t LLC](https://openairdocs.org/faa-owner/N2528T%20LLC), [Norcross, GA](https://openairdocs.org/faa-place/GA/Norcross), built 2004, S/N 41029
- [N2528Z](https://openairdocs.org/aircraft/N2528Z): [Rothermel Aviation LLC](https://openairdocs.org/faa-owner/ROTHERMEL%20AVIATION%20LLC), [Klingerstown, PA](https://openairdocs.org/faa-place/PA/Klingerstown), S/N 41055
- [N2529P](https://openairdocs.org/aircraft/N2529P): [Matera Management LLC](https://openairdocs.org/faa-owner/MATERA%20MANAGEMENT%20LLC), [Spanish Fork, UT](https://openairdocs.org/faa-place/UT/Spanish%20Fork), built 2005, S/N 41521
- [N2533K](https://openairdocs.org/aircraft/N2533K): [Domicile Capital LLC](https://openairdocs.org/faa-owner/DOMICILE%20CAPITAL%20LLC), [Monterey, CA](https://openairdocs.org/faa-place/CA/Monterey), built 2005, S/N 41531
- [N2535L](https://openairdocs.org/aircraft/N2535L): [K & L Adventures LLC](https://openairdocs.org/faa-owner/K%20%26%20L%20ADVENTURES%20LLC), [Moses Lake, WA](https://openairdocs.org/faa-place/WA/Moses%20Lake), built 2005, S/N 41082
- [N25367](https://openairdocs.org/aircraft/N25367): [Robinson Stephen C](https://openairdocs.org/faa-owner/ROBINSON%20STEPHEN%20C), [Garrison, ND](https://openairdocs.org/faa-place/ND/Garrison), built 2005, S/N 41503
- [N2538M](https://openairdocs.org/aircraft/N2538M): [Warren James Rent](https://openairdocs.org/faa-owner/WARREN%20JAMES%20RENT), [Rapid City, SD](https://openairdocs.org/faa-place/SD/Rapid%20City), built 2005, S/N 41081
- [N2540M](https://openairdocs.org/aircraft/N2540M): [Global Emergency Services LLC](https://openairdocs.org/faa-owner/GLOBAL%20EMERGENCY%20SERVICES%20LLC), [Beaumont, TX](https://openairdocs.org/faa-place/TX/Beaumont), S/N 41031
- [N2541A](https://openairdocs.org/aircraft/N2541A): [Energy307 LLC](https://openairdocs.org/faa-owner/ENERGY307%20LLC), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 2005, S/N 41085

All 122: https://openairdocs.org/model/lancair-lc41-550fg/aircraft.md

## NTSB investigations (12)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN20WA142](https://openairdocs.org/ntsb/CEN20WA142), Mar 30, 2020: Lancair LC41 (N6504H), Gotha, Germany, substantial damage
- [NTSB CEN19LA159](https://openairdocs.org/ntsb/CEN19LA159), May 30, 2019: Lancair LC41 (N2514F), Cleburne, TX, substantial damage. Probable cause: A total loss of engine power due to oil starvation as the result of the oil pressure switch failure due to a manufacturing defect.
- [NTSB GAA17CA174](https://openairdocs.org/ntsb/GAA17CA174), Mar 5, 2017: Lancair Columbia 400 (N2516K), Henderson, NV, substantial damage. Probable cause: The pilot’s improper decision to land the airplane with a gusting crosswind, which resulted in a loss of airplane control.
- [NTSB GAA17CA078](https://openairdocs.org/ntsb/GAA17CA078), Nov 22, 2016: Lancair LC41 550FG (N169WT), Redding, CA, substantial damage. Probable cause: The pilot’s unstabilized approach and subsequent failure to attain the proper touchdown point, which resulted in a runway overrun.
- [NTSB CEN11LA577](https://openairdocs.org/ntsb/CEN11LA577), Aug 14, 2011: Cessna 400 (N2515G), Eastland, TX, substantial damage. Probable cause: A loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation. .
- [NTSB CEN11FA227](https://openairdocs.org/ntsb/CEN11FA227), Mar 11, 2011: Lancair LC41-550FG (N521RT), Carbondale, IL, substantial damage. Probable cause: The fatigue fracture and subsequent failure of the No. 2 cylinder exhaust valve during cruise flight, which resulted in a total loss of engine power.
- [NTSB LAX08LA217](https://openairdocs.org/ntsb/LAX08LA217), Jul 6, 2008: Lancair LC41-550FG (N2544W), Hailey, ID, substantial damage. Probable cause: The loss of directional control while taxiing due to the failure of the right brake.
- [NTSB SEA08FA078](https://openairdocs.org/ntsb/SEA08FA078), Feb 16, 2008: Lancair LC41 (N621ER), Portland, OR, destroyed, 1 fatal. Probable cause: The pilot's failure to follow the missed approach procedure. Contributing to the accident were the fog and below landing minimums visibility conditions.
- [NTSB SEA07FA247](https://openairdocs.org/ntsb/SEA07FA247), Sep 1, 2007: Lancair LC41-550FG (N2520P), Kernville, CA, destroyed, 6 fatal. Probable cause: The pilot's failure to maintain aircraft control while maneuvering in the traffic pattern for landing. Contributing to the accident was the pilot's failure to maintain an adequate airspeed.
- [NTSB NYC06FA072](https://openairdocs.org/ntsb/NYC06FA072), Feb 23, 2006: Lancair LC41-550FG (N400WX), Stafford, VA, destroyed, 4 fatal. Probable cause: The pilot's failure to execute the published missed approach. Factors included the night lighting conditions, low ceilings and fog.
- [NTSB LAX06FA014](https://openairdocs.org/ntsb/LAX06FA014), Oct 17, 2005: Lancair LC-41-550FG (N285JB), Warner Springs, CA, destroyed, 3 fatal. Probable cause: The flight crew's failure to maintain adequate terrain clearance and their decision to continue flight into known adverse weather conditions. Contributing to the accident was overcast conditions, and…
- [NTSB SEA03LA180](https://openairdocs.org/ntsb/SEA03LA180), Aug 27, 2003: Lancair LC41 (N166PD), Bend, OR, destroyed. Probable cause: The inadequate design of the drogue chute mechanical jettison system, which resulted in its failure to separate from the aircraft during in-flight spin recovery tests, and the incorrectly wired…

## FAA accident and incident reports (19)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20250909012539I](https://openairdocs.org/incident/20250909012539I), Sep 9, 2025: Lancair Company LC41-550FG (N2518H), Santa Barbara, CA, Minor damage. While sitting in airplane with engine running at approximately 900TO1000 RPM, airplane rolled forward into a hanger door damaging the spinner and the propellor.
- [Incident 20250127002529I](https://openairdocs.org/incident/20250127002529I), Jan 27, 2025: Lancair Company LC41-550FG (N2533K), Monterey, CA, No damage. After landing on runway 28L at Monterey Regional Airport, controller inquired about parking location. Pilot responded "northwest ramp." Monterey tower provided…
- [Incident 20230919016649I](https://openairdocs.org/incident/20230919016649I), Sep 19, 2023: Lancair Company LC41-550FG (N2520S), Atlanta, GA, No damage. After landing on runway 3R the pilot was instructed to turn off at taxiway golf and cross runway 3L. The pilot turned off into the grass instead of golf and…
- [Incident 20200424002609I](https://openairdocs.org/incident/20200424002609I), Apr 24, 2020: Lancair Company LC41-550FG (N576BS), Huntsville, AL, Minor damage. Aircraft was taxiing to the active runway when the pilot noticed he had no brake pressure on the right brake. As the aircraft was taxiing back to the ramp, the…
- [Accident 20190530017719A](https://openairdocs.org/incident/20190530017719A), May 30, 2019: Lancair Company LC41-550FG (N2514F), Cleburn, TX, Substantial damage. The pilot was making a maintenance check flight due to maintenance change of a number 5 engine cylinder. The pilot did not participate in a post maintenance…
- [Incident 20180729018319I](https://openairdocs.org/incident/20180729018319I), Jul 29, 2018: Lancair Company LC41-550FG (N25367), Mohall, ND, Minor damage. The pilot had a hard landing and stated "on landing the nose wheel broke from the strut, the prop struck the ground and the aircraft rolled to a stop. "
- [Accident 20170305006119A](https://openairdocs.org/incident/20170305006119A), Mar 5, 2017: Lancair Company LC41-550FG (N2516K), Henderson, NV, Substantial damage. On March 5, 2017, about 1759 pacific standard time, a Lancair LC41-550FG, N2516K, impacted the terrain during an attempted visual flight rules (VFR) go-around…
- [Accident 20161122018689A](https://openairdocs.org/incident/20161122018689A), Nov 22, 2016: Lancair Company LC41-550FG (N169WT), Redding, CA, Substantial damage. Pilot landed too fast and proceeded to roll past end of runway into ditch.
- [Accident 20110813016479A](https://openairdocs.org/incident/20110813016479A), Aug 13, 2011: Lancair Company LC41-550FG (N2515G), Eastland, TX, Substantial damage. On August 13, 2011, the aircraft departed Eastland municipal airport with the pilot and one passenger aboard. During takeoff, the aircraft annunciators…
- [Accident 20110311004259A](https://openairdocs.org/incident/20110311004259A), Mar 11, 2011: Lancair Company LC41-550FG (N521RT), Carbondale, IL, Substantial damage. While in cruise flight, the engine lost power. The propeller eventually stopped and an off airport landing was performed. The aircraft contacted a telephone…
- [Incident 20101113053699I](https://openairdocs.org/incident/20101113053699I), Nov 13, 2010: Lancair Com LC41-550FG (N2540M), Sturgeon Bay, WI, Minor damage. Pilot emerged from IMC approach on autopilot at minimums on GPS appraoch at night for runway 20AT minimums, pilot cancelled auto pilot and descended for…
- [Incident 20090113000079I](https://openairdocs.org/incident/20090113000079I), Jan 13, 2009: Lancar LC41550FG (N504JL), Hailey, ID, Minor damage. The pilot of N504JL, a Lancair model LC-41 taxiied to the self serve fuel pump at sun. Because of an injured leg the passenger got out of the aircraft and…
- [Incident 20081111851719I](https://openairdocs.org/incident/20081111851719I), Nov 11, 2008: Lancar LC41550FG (N2518H), Palm Springs, CA, Minor damage. (-23) During landing at rwy 17, the wheel and nose gear assembly (wnga) separated from the nose landing gear oleo strut. Post incident investigation revealed…
- [Accident 20080706840019A](https://openairdocs.org/incident/20080706840019A), Jul 6, 2008: Lancar LC41550FG (N2544W), Hailey, ID, Substantial damage. (-23) The pilot stated while taxiing north on taxiway bravo for a runway 13 departure, the aircraft began to drift to the left. The pilot stated he attempted…
- [Accident 20080216011079A](https://openairdocs.org/incident/20080216011079A), Feb 16, 2008: Lancar LC41550FG (N621ER), Portland, OR, Destroyed, 1 fatal. (-23) Aircraft impacted ground approximately 2500 feet south of runway 10R. One person on board, the pilot, sustained fatal injuries. Appears to have been a…
- [Accident 20070831020979A](https://openairdocs.org/incident/20070831020979A), Aug 31, 2007: Lancar LC41550FG (N2520P), Kernville, CA, Destroyed, 6 fatal. (-23) Information received from Kern county sheriff's department witness statements report the aircraft entering the airport traffic area and appeared to begin…
- [Accident 20060222007519A](https://openairdocs.org/incident/20060222007519A), Feb 22, 2006: Amtr LC41550FG (N400WX), Stafford, VA, Destroyed, 4 fatal. (-23) The aircraft, a Lancair columbia 400, departed winston-salem airport, NC (int) enroute to shannon airport, fredericksburg, VA (ezf) on February 22, 2006.…
- [Accident 20051017028409A](https://openairdocs.org/incident/20051017028409A), Oct 17, 2005: Amtr LC41550FG (N285JB), Warner Springs, CA, Destroyed, 3 fatal. (-23) On October 17, 2005, at approximately 1032 PDT, a Lancair LC41-550G, N285JB, collided with mountainous terrain six miles north of Warner Springs,…
- [Accident 20030827022449A](https://openairdocs.org/incident/20030827022449A), Aug 27, 2003: Amtr LC41550FG (N166PD), Millcan, OR, Destroyed. (-23) According to PIC, while conducting spin flight testing at 14000', on the prototype Lancair columbia 400AIRCRAFT, the PIC was unable to recover from the…

## Service difficulty reports (41)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2025FA0000764](https://openairdocs.org/sdr/2025FA0000764), Nov 18, 2025: BRAKE DISC. SHEARED. PILOT REPORTED THAT AFTER LANDING AND EXITING THE RUNWAY, HE ATTEMPTED TO MAKE A LEFT TURN ON A TAXIWAY USING DIFFERENTIAL BRAKING. HE STATED HE HEARD A POPPING
- [SDR 2025FA0000068](https://openairdocs.org/sdr/2025FA0000068), Jan 29, 2025: ACCESS PANEL. DAMAGED. LOWER RIGHT WING ACCESS PANEL, ORIGINAL P/N LB57650007-1 REV- HAS A NACA AIR SCOOP AIR DUCT THAT CONNECTS TO FUEL SYSTEM VENT SYSTEM. THIS PANEL RECEIVED A MINO
- [SDR 2023FA0000569](https://openairdocs.org/sdr/2023FA0000569), Sep 26, 2023: BRAKE DISC. BROKEN. DURING THE ANNUAL INSPECTION, MAINTENANCE FOUND THE LH BRAKE DISC BROKEN APPROXIMATELY 4.5 INCHES IN LENGTH AND APPROXIMATELY 1/4 INCH IN WIDTH AROUND FLANGE WH
- [SDR BIER2022011301](https://openairdocs.org/sdr/BIER2022011301), Jan 13, 2022: MANIFOLD. CHAFED. INDUCTION MANIFOLD P/N 655607 WAS REMOVED FROM CURRENT ENGINE MODEL TSIO-550C(11) DUE TO CHAFE DAMAGE. WHEN NEW REPLACEMENT MANIFOLD P/N 646440 WAS RECEIVED AND
- [SDR 2020FA0000001](https://openairdocs.org/sdr/2020FA0000001), Jan 3, 2020: BOLT. SHEARED. DURING OVERHAUL OF THE NLG FOUND THE BOLT WHICH HOLDS THE CENTERING CAMSHAFT TO THE NLG STRUT SHEARED AT THE THREADS. THE HEAD, SHANK AND THREADS OF THE BOLT RE
- [SDR BIER20180918001](https://openairdocs.org/sdr/BIER20180918001), Sep 12, 2018: STRUCTURE. CRACKED. FUSELAGE AFT FOOTWELL RECESS LOWER CORNERS (FS 127.5) (LT & RT) HAVE DELAMINATIONS WITH LT AFT CORNER HAVING A CRACK 1.375 INCHES LONG.
- [SDR 2018FA0000196](https://openairdocs.org/sdr/2018FA0000196), Jun 25, 2018: CYLINDER HEAD. DAMAGED. APPROXIMATELY 8 HOURS AFTER THE NR 5 CYLINDER WAS REPLACED WITH A NEW FACTORY CYLINDER KIT, THE PILOT NOTIFIED US THAT THE NR 5 CYLINDER WOULD NOT "WARM UP" AND
- [SDR 2018FA0000101](https://openairdocs.org/sdr/2018FA0000101), Mar 13, 2018: CABLE. DAMAGED. ALTERNATE AIR CONTROL CABLE IS ROUTED NEAR THE EXHAUST. OVER TIME DUE TO HEAT DAMAGE THE CABLE BECOMES STUCK AND NOT USABLE. HISTORY WITH AFT AIR CABLE. 5-1-14 
- [SDR BIER20160517001](https://openairdocs.org/sdr/BIER20160517001), May 17, 2016: VALVE. LEAKING. DURING THE PROCESS TO ACCOMPLISHING INSPECTION AND TESTING FOR CFR PART 91.411 AND \ 91.413, FOUND THE ALTERNATE STATIC VALVE CAUSING A LEAK THAT EXCEEDS LIMITS
- [SDR BIER2016031500001](https://openairdocs.org/sdr/BIER2016031500001), Mar 14, 2016: CASE. CRACKED. CUSTOMER ARRIVED AT REPAIR STATION STATING HE HAD AN OIL LEAK. ENGINE COWLING WAS REMOVED TO DETERMINE SOURCE OF LEAK. INITIAL INSPECTION AND REPAIR WAS ON LEAK
- [SDR 2016FA0000084](https://openairdocs.org/sdr/2016FA0000084), Dec 8, 2015: MAGNETO. FAILED. DUEL MAG FAILURE. RT MAGNETO HAD A STRIPPED GEAR. LT MAG TIMING WAS AS PER THE DATA PLATE. BOTH MAGS WERE PICKED UP BY THE NTSB.
- [SDR NF2R201812190001](https://openairdocs.org/sdr/NF2R201812190001), Sep 12, 2014: LIFTER. GALLED. INSPECTION OF ALL 6 CYLINDERS FOUND 5 OUT OF LIMITS AND ALL CYLINDERS HAD BAD EXHAUST AND INTAKE GUIDES AND VALVES. FOUND LIFTERS ARE PITTED AND STARTING TO CHI
- [SDR 2013FA0000643](https://openairdocs.org/sdr/2013FA0000643), Nov 18, 2013: CONTROL ROD. WORN. RT FLAP CONTROL ROD HAS EXCESSIVE PLAY CAUSED BY THE URETHANE INSULATOR THAT IS MOUNTED BETWEEN 2 METAL CONTROL ROD SECTIONS AND HELD TOGETHER BY MS27039-1-23 S
- [SDR 2013FA0000642](https://openairdocs.org/sdr/2013FA0000642), Nov 18, 2013: CONTROL ROD. WORN. RIGHT FLAP CONTROL ROD HAS EXCESSIVE PLAY. THE ROD ASSY IS PN LA57266102 WHICH IS CONSTRUCTED BY PN'S 286102-8 FOR THE URETHANE INSULATOR AND PN'S 2562102-3 AND
- [SDR VNFR20130624001](https://openairdocs.org/sdr/VNFR20130624001), Jun 24, 2013: WINDOW. CRACKED. DURING FLIGHT, THE PILOT REPORTED A POP ON PERFORMING A NORMAL LANDING, PILOT NOTED THE RT REAR PASSENGER WINDOW HAD A LARGE CRACK THAT EXTENDED IN A CRESCENT S
- [SDR VNFR20130618001](https://openairdocs.org/sdr/VNFR20130618001), Jun 18, 2013: SPARK PLUG. CRACKED. CRACKED CERAMIC ON NR 5 LOWER SPARK PLUG.
- [SDR 2013FA0000328](https://openairdocs.org/sdr/2013FA0000328), May 17, 2013: FAN. FAILED. DURING CRUISE FLIGHT, HEARD A BANG AND THEN SAW A METAL OBJECT COME THROUGH HIS TOP ENGINE COWLING. LANDED AT THE NEAREST AVAILABLE AIRPORT. COOLING FAN ASSY, A
- [SDR 2012FA0000793](https://openairdocs.org/sdr/2012FA0000793), Dec 4, 2012: EXHAUST PIPE. CRACKED. DURING A 50 HOUR INSPECTION, A LARGE CRACK WAS FOUND THAT NEARLY CIRCLED THE ENTIRE TRANSITION. LOWER HALF OF TURBO TRANSITION WAS VERY CLOSE TO SEPARATING FROM
- [SDR 2012FA0000231](https://openairdocs.org/sdr/2012FA0000231), Apr 20, 2012: SHAFT. SHEARED. PILOT REPORTED LOSS OF RIGHT HAND ALTERNATOR ON FINAL APPROACH TO THE AIRPORT. DURING TAXI OPERATIONS TO THE RAMP THE PILOT REPORTED HEARING A "NOISE" FROM THE 
- [SDR 2012FA0000103](https://openairdocs.org/sdr/2012FA0000103), Feb 9, 2012: SPARK PLUG. CRACKED. RT B32S SPARK PLUGS HAVE CRACKED PORCELAIN, QTY 6 OUT OF 12, FOUND DURING ANNUAL INSPECTION.
- [SDR 2011FA0000184](https://openairdocs.org/sdr/2011FA0000184), Mar 18, 2011: TORQUE TUBE. CORRODED. ELEVATOR TORQUE TUBE HAS INTERNAL CORROSION INSIDE TORQUE TUBE WITH RUST CONCENTRATION AROUND WELDED AREAS. AMM CHAP 27-30-00, PAGE 3 ITEM 2(C)(3) STATES TO INS
- [SDR YWYR201209158126](https://openairdocs.org/sdr/YWYR201209158126), Oct 26, 2010: SPARK PLUG. CRACKED. DURING ANNUAL INSPECTION, 5 OF THE 12 ACFT SPARK PLUGS WERE FOUND TO HAVE CRACKS IN THE ELECTRODE INSULATORS. ENGINE CYLINDERS WERE INSPECTED USING BORESCOPE AN
- [SDR YWYR201209158048](https://openairdocs.org/sdr/YWYR201209158048), Sep 13, 2010: SPARK PLUG. CRACKED. DURING AN ANNUAL INSPECTION, ONE OF TWELVE SPARK PLUGS WERE FOUND TO HAVE A CRACKED ELECTRODE INSULATOR. SPARK PLUG WAS REPLACED WITH NEW PART.
- [SDR 2010FA0000251](https://openairdocs.org/sdr/2010FA0000251), Mar 10, 2010: MOUNT FLANGE. CRACKED. OIL COOLER MOUNTING FLANGE IS CRACKED AT RADIUS. THIS IS A RECURRING ISSUE WITH THESE COOLERS. THIS COOLER IS HAS 254.0 HRS SINCE LAST CHANGE DUE TO THE SAME RE
- [SDR T9ZR725YWO4459](https://openairdocs.org/sdr/T9ZR725YWO4459), Feb 26, 2010: STARTER. OUT OF TOLERANCE. DURING REMOVAL OF THE STARTER AND THE O/H OF THE STARTER DRIVE ADAPTER IT WAS FOUND THAT THE NEWLY INSTALLED STARTER IS .015 SMALLER AT THE HOUSING FLANGE THAN 
- [SDR 2010FA0000189](https://openairdocs.org/sdr/2010FA0000189), Jan 4, 2010: SPARK PLUG. BROKEN. ONE SPARK PLUG CERAMIC WAS FOUND BROKEN. OTHERS WERE FOUND CRACKED. THESE SPARK PLUGS WERE MIS-FIRING DURING HIGH POWER OPERATION. NO DEFECT WAS NOTED DURING NO
- [SDR 2009FA0000723](https://openairdocs.org/sdr/2009FA0000723), Aug 4, 2009: GUARD. BROKEN. THE AIR CONDITIONER BELT GUARD FAILED IN FLIGHT. INSP REVEALED 2 SMALL CRACKS AT THE LT SIDE WELDED NUT. THIS FAILURE CAUSED A 2 INCH X 2 INCH STEEL PIECE OF TH
- [SDR YWYR201209157151](https://openairdocs.org/sdr/YWYR201209157151), May 21, 2009: SPARK PLUG. CRACKED. DURING ANNUAL INSPECTION, 1 OF THE 12 ENGINE SPARK PLUGS WAS FOUND TO HAVE A CRACKED ELECTRODE INSULATOR.
- [SDR MDR40120009004](https://openairdocs.org/sdr/MDR40120009004), Apr 1, 2009: TUBE. CHAFED. THE OIL FILLER TUBES ARE BEING CHAFED BEYOND MFG LIMIT OF .010 DUE TO CONTACT WITH THE CYLINDER BAFFLING BETWEEN CYLINDERS NR 2 AND 4. SHOULD THE TUBE CHAFE COM
- [SDR 2008FA0000269](https://openairdocs.org/sdr/2008FA0000269), Apr 1, 2008: TRANSITION DUCT. CRACKED. DURING ANNUAL INSPECTION FOUND TURBO TRANSITION PART OF EXHAUST CRACKED ALL THE WAY THRU FRONT RADIUS OF THE PIPE. (K)
- [SDR 2008FA0000225](https://openairdocs.org/sdr/2008FA0000225), Apr 1, 2008: TRANSITION DUCT. CRACKED. DURING ANNUAL INSP FOUND TURBO TRANSITION PART OF EXHAUST CRACKED ALL THE WAY THRU FRONT RADIUS OF THE PIPE. (K)
- [SDR 2008FA0000211](https://openairdocs.org/sdr/2008FA0000211), Mar 12, 2008: DUCT. CRACKED. RT TURBO TRANSITION DUCT CRACKED. (NOTE: THIS IS THE SECOND TIME WE HAVE SEEN THIS)
- [SDR 2007FA0000028](https://openairdocs.org/sdr/2007FA0000028), Dec 29, 2006: DIPSTICK. SEPARATED. THE OIL GAGE ASSEMBLY (DIPSTICK) SEPARATED AT THE UPPER SWEDGED JOINT. (K)
- [SDR 2006FA0000889](https://openairdocs.org/sdr/2006FA0000889), Aug 29, 2006: UNION. CRACKED. THE AN911-1J UNION THAT SUPPLIES OIL TO THE OIL PRESSURE TRANSDUCER, THE HOBBS PRESSURE SWITCH, AND THE OIL FEED LINE, AT THE BASE OF THE OIL COOLER, ON THE BAC
- [SDR 2006FA0000829](https://openairdocs.org/sdr/2006FA0000829), Aug 9, 2006: POINTS. BROKEN. MAGNETO FAILURE, ON ECR ON INSP RT MAGNETO POINT HAD BROKEN IN HALF. (K)
- [SDR 2006FA0000752](https://openairdocs.org/sdr/2006FA0000752), Jul 20, 2006: SAFETY WIRE. MISINSTALLED. ALL 4 ENGINE VIBRATION ISOLATOR MOUNT BOLTS WERE SAFETY WIRED BACKWARDS. NO EVIDENCE OF DAMAGE. (K)
- [SDR 2006FA0000343](https://openairdocs.org/sdr/2006FA0000343), Apr 1, 2006: POINTS. BROKEN. ON ENGINE GROUND RUN PRIOR TO FLIGHT MAGNETO CHECK FOUND RT MAGNETO HAD FAILED INSPECTION FOUND POINTS BROKEN PICTURE INCLOSED. (K)
- [SDR AU510001912](https://openairdocs.org/sdr/AU510001912), Dec 12, 2005: TIRE. DISINTEGRATED. (AUS) NOSE WHEEL TYRE DISINTEGRATED CIRCUMFERENTIALLY. INVESTIGATION FOUND EXCESSIVELY LONG NOSEWHEEL SPAT ATTACHMENT SCREWS WHICH CUT INTO THE TYRE AS IT ROTAT
- [SDR AU510001765](https://openairdocs.org/sdr/AU510001765), Apr 8, 2005: PUMP. FAILED. (AUS) VACUUM PUMPS FAILED. (OTHER CAUSE: MATERIAL - DEBRIS REMAINING AFTER FAILURE ) (CASA NR 510001765)
- [SDR AU510001680](https://openairdocs.org/sdr/AU510001680), Apr 8, 2005: PUMP. FAILED. EXCESSIVE AMOUNT OF VACUUM PUMPS FAILING EITHER ON FITMENT OR SHORTLY AFTER. THESE PUMPS ARE PURCHASED FROM AERO ACCESSORIES INC.
- [SDR AU510002168](https://openairdocs.org/sdr/AU510002168), Feb 11, 2005: BEARING. MISMANUFACTURED. NEW WHEEL BEARING HAD TWO ROLLERS MISSING. FAULTY MFG.

## STCs that may be installed (OpenAirDocs) (78, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [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 78: https://openairdocs.org/model/lancair-lc41-550fg/stcs.md

## PMA parts (OpenAirDocs) (183, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [RAP164-02504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID191690382620260722154718.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-02504 · Jun 3, 2026
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195163166220231121213633.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184007482120231121213616.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183987935420231121213715.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181668694920231121213743.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180985549820231121213750.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177618033420231121213722.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175530717220231121213757.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165014162720231121213728.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139786447520231121213658.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139111226820231121213804.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126536442920231121213641.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118472319420231121213735.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118358198320231121213706.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117182341320231121213624.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107779885520231121213649.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198452104220231102131425.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Sep 25, 2023
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112847905220230707211400.0001): uAvionix Corporation · PMA PQ05445NM · Jun 28, 2023
- [APS66-06200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160415494220221020170232.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-06200 · Aug 10, 2022
- [APS177-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111785228520221020170335.0001): Pin. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 177-00300 · Aug 10, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150275305720220706160107.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [ALX-6526](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197879628620220916095403.0001): Alternator Assembly 12V 70A. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALX-6526 · May 3, 2022
- [ALU-6526](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115032903820220916095401.0001): Alternator Assembly (24V-60A). Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces ALU-6526 · May 3, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188968164920220525194425.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166121572720220525194543.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161543423120220525194312.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID784850468920210923143657.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [EA-23000-A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID762626194320210923143758.0001): EA-23000 Ignition/Starter Switch Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jul 28, 2021
- [700-00190-100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID441498625820210921142614.0001): SkyTrax 100B/200 ADS-B Receiver. Avidyne Corporation · PMA PQ4035CE · Replaces ModificationPart · Jul 28, 2021
- [A646463-300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID811723645020210617194235.0001): Exhaust Bypass Tube Assembly. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 654321 · Jun 3, 2021
- [A646463-184](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID447421172220210617194234.0001): Tee Assembly, Right Side. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 657010 · Jun 3, 2021
- [A646463-181](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID269899822320210617194233.0001): Tee Assembly, Left Side. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 657009 · Jun 3, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID677145279020210622142514.0001): AeroLEDs LLC · PMA PQ5259NM · Mar 11, 2021
- [409-00003-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID627285008820210702175245.0001): Internal Battery Pack, Refresh. Aspen Avionics · PMA PQ03868SW · Modification part · Jan 20, 2021
- [1049-4000-03-001C](https://drs.faa.gov/browse/excelExternalWindow/FB6A4D62429A217F86258633006145AB.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4201-20](https://drs.faa.gov/browse/excelExternalWindow/ED78E4F8D3C63347862586330061461D.0001): Annunciator Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-20](https://drs.faa.gov/browse/excelExternalWindow/CBC6239248334CCE86258633006145E5.0001): Connector Kit GDC31. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4200-50](https://drs.faa.gov/browse/excelExternalWindow/86CBD103649292948625863300614693.0001): Isolation Coupler Installation Kit. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4000-03-001B](https://drs.faa.gov/browse/excelExternalWindow/80F9B5EC9801FD16862586330061456E.0001): Roll Steering Converter. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [1049-4801-01](https://drs.faa.gov/browse/excelExternalWindow/39A0DF401545910A8625863300614652.0001): Isolation Coupler. DAC International · PMA PQ05446NM · Modification part · Nov 30, 2020
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/1A9437DB989160E2862586290049EF86.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Nov 4, 2020
- [TACH2](https://drs.faa.gov/browse/excelExternalWindow/29C3872705863D03862585E500683D52.0001): Tach2 Signal Converter. SureFly Partners Ltd · PMA PQ03861SW · Modification part · Sep 7, 2020
- [APS068-01100](https://drs.faa.gov/browse/excelExternalWindow/48A12ED2A35F49FE862585EC00452205.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Aug 26, 2020
- [18055-2A8](https://drs.faa.gov/browse/excelExternalWindow/0AD688838AAFE45086258593002D93D7.0001): Pump-Motor Assembly. Weldon Pump · PMA PQ2411CE · Replaces Dukes Inc. 5173-00-3 · Jan 28, 2020
- [9100-001-C](https://drs.faa.gov/browse/excelExternalWindow/DD343890DCD8BFDB86258569004013FB.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-D](https://drs.faa.gov/browse/excelExternalWindow/C7B6725B325949E98625856900401478.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-B](https://drs.faa.gov/browse/excelExternalWindow/BD58B0712CA0C6AA86258569004016AD.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-G](https://drs.faa.gov/browse/excelExternalWindow/ADE62C91D97E8B788625856900401557.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9100-001-E](https://drs.faa.gov/browse/excelExternalWindow/A37F050253EE808A86258569004014BA.0001): MaxDim Lamp Intensity Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019
- [9200-000-A](https://drs.faa.gov/browse/excelExternalWindow/8E10EF4D973C1D6D8625856900401662.0001): MaxPulse Landing Light Controller. Seaton Engineering Corporation · PMA PQ2574NM · Modification part · Sep 3, 2019

All of them: https://openairdocs.org/model/lancair-lc41-550fg/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Columbia Aircraft Mfg LC41-550FG](https://openairdocs.org/model/columbia-aircraft-mfg-lc41-550fg): 207 registered aircraft, registry code 5150011
- [Cessna LC41-550FG](https://openairdocs.org/model/cessna-lc41-550fg): 132 registered aircraft, registry code 2073320
- [Cessna LC41-550FG](https://openairdocs.org/model/cessna-lc41-550fg): 12 registered aircraft, registry code 2073323

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