# N603AE: Raytheon G36

- Status: Valid registration
- Airframe: [Raytheon G36](https://openairdocs.org/model/raytheon-g36) (registry code 7150061, 6 seats)
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: E-3735
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Certificate issued: September 11, 2021
- Expires: September 30, 2028
- Mode S code: A7D269
- Registered owner: [Pinch Aviation LLC](https://openairdocs.org/faa-owner/PINCH%20AVIATION%20LLC)
- Location: [Monticello, IN](https://openairdocs.org/faa-place/IN/Monticello)
- Owner type: LLC
- Owner's area on the map: 40.7883° N, 86.7520° W: Placed by OpenAirDocs at the center of ZIP code 47960, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=603AE
- Page: https://openairdocs.org/aircraft/N603AE

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): 5 in force

### Matched by airframe (Raytheon G36)

- [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 2009-15-01](https://openairdocs.org/ad/2009-15-01): Wire harness/connector(s) · Textron G36. Effective Jul 27, 2009
- [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 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

## Information bulletins (advisory) (5 in force)

- [SAIB CE-15-22](https://openairdocs.org/saib/CE-15-22): Wing Leading Edge Hinge-Pin Corrosion. Issued Sep 15, 2015
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB CE-12-18](https://openairdocs.org/saib/CE-12-18): Flight Controls: Elevator Control Cable Condition. Issued Feb 7, 2012
- [SAIB CE-11-21](https://openairdocs.org/saib/CE-11-21): Flight Controls: Trailing Edge Flaps; Flap Nose Rib Cracking. Issued Feb 16, 2011
- [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

## NTSB investigations

None matched to N603AE.

## FAA accident and incident reports

None matched to N603AE.

## Reports on N603AE not matched to an aircraft (1)

They name N603AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20000329001679I](https://openairdocs.org/incident/20000329001679I), Mar 29, 2000: Emb EMB145LR (N603AE), Covington/Cinci, KY. (-23) Captain dyk complained of a general weakness during inbound flight to cvg (after initial desent.) An emergency was declared @ 2050L. Fo lande d ac on rwy…

## 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 N603AE not matched to an aircraft (30)

They name N603AE, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR SIMA200209501](https://openairdocs.org/sdr/SIMA200209501), Apr 3, 2002: PITCH CONTROL. MALFUNCTIONED. ORD - FLT 4023 - AT APPROX 800-1000 FT F/O MAIN AND STANDBY PITCH TRIM BECAME INOPERATIVE CAPTAIN MAIN AND STANDBY PITCH. ALSO, INOPERATIVE CHECKLIST FOLLOWED A
- [SDR SIMA200207304](https://openairdocs.org/sdr/SIMA200207304), Mar 11, 2002: FLOOR SUPPORT. CORRODED. ABI - DURING INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY FLOOR SUPPORT AT FRAME 20 AND 23, BEYOND LIMITS. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW EMB1
- [SDR SIMA200207208](https://openairdocs.org/sdr/SIMA200207208), Mar 9, 2002: STRUCTURE. CORRODED. ABI - DURING INSPECTION OF AIRCRAFT, FOUND THE FORWARD DIGITAL CORRODED. REMOVED CORROSION BY CUT OUT. FABRICATED A REPLACEMENT STRAP 16.5 INCH BY 21.5 INC, TWO
- [SDR SIMA200207007](https://openairdocs.org/sdr/SIMA200207007), Mar 8, 2002: STRINGER. GOUGED. DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND EXTERNAL STRINGER 19R UNDER AFT BELLY PANEL GOUGED. BLENDED GOUGE. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO 
- [SDR SIMA200207006](https://openairdocs.org/sdr/SIMA200207006), Mar 7, 2002: SILL. CORRODED. ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON SERVICE DOOR CENTER SILL. REMOVED CORROSION BY BLENDING OUT. PERFORMED AN NDT INSPECTION OF THE 
- [SDR SIMA200207005](https://openairdocs.org/sdr/SIMA200207005), Mar 6, 2002: SILL. CORRODED. ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND LOWER CARGO DOOR CENTER SILL BEAM CORRODED. REMOVED CORRODED SILL BEAM. INSTALLED SILL BEAM IN CARGO DOOR IAW
- [SDR SIMA200207004](https://openairdocs.org/sdr/SIMA200207004), Mar 5, 2002: BEAM. CHAFED. ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, FOUND LEFT BEAM CHAFED BETWEEN FRAMES 20 AND 24. BLENDED CHAFE. PERFORMED AN NDT INSPECTION OF THE AREA WITH NO REJ
- [SDR SIMA200207002](https://openairdocs.org/sdr/SIMA200207002), Mar 1, 2002: DOUBLER. CORRODED. ABI - DURING AN IMBV INSPECTION OF AIRCRAFT, THE PREVIOUS REPAIR AND THE LEFT OMEGA BEAM AT FRAME 20 WERE FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED PREV R
- [SDR SIMA200207809](https://openairdocs.org/sdr/SIMA200207809), Feb 27, 2002: SILL. CORRODED. ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL IS CORRODED BETWEEN FRAMES 26-27. BLENDED CORROSION, NDT AND RETREATED AREA IAW EMB145 GST 0714/02. (M)
- [SDR SIMA200207810](https://openairdocs.org/sdr/SIMA200207810), Feb 27, 2002: FLOORBEAM. CORRODED. THIS IS A LEVEL 2 FINDING. LEFT FLOORBEAM CORRODED AT FRAME 26. REMOVED CORROSION, NDT AND RETREATED IAW EMB 145 GST-0714/02. (M)
- [SDR SIMA200207801](https://openairdocs.org/sdr/SIMA200207801), Feb 27, 2002: SILL. CORRODED. ABI - THIS IS A LEVEL 2 FINDING. RIGHT SILL IS CORRODED BETWEEN FRAMES 23-25. REMOVED CORROSION, NDT TREATED IAW EMB145 GST-0714/02. (M)
- [SDR SIMA200207803](https://openairdocs.org/sdr/SIMA200207803), Feb 25, 2002: SILL. CORRODED. ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL IS CORRODED BETWEEN FRAMES 37-39. BLENDED AREA IAW EMB GST-0714/02 AND RETREATED FOR CORROSION IAW EMB 145 CPM 51-21-
- [SDR SIMA200207802](https://openairdocs.org/sdr/SIMA200207802), Feb 25, 2002: SILL. CORRODED. ABI - THIS IS A LEVEL 2 FINDING, LEFT SILL IS CORRODED BETWEEN FRAMES 19 AND 21. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. (M)
- [SDR SIMA200207806](https://openairdocs.org/sdr/SIMA200207806), Feb 25, 2002: SILL. CORRODED. ABI - THIS IS A LEVEL 2 FINDING. LEFT SILL CORRODED BETWEEN FRAMES 19 AND 21. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. RETREATED AREA 
- [SDR SIMA200207808](https://openairdocs.org/sdr/SIMA200207808), Feb 25, 2002: FRAME. CORRODED. ABI - THIS IS A LEVEL 2 FINDING. RIGHT PROFILE AT FRAME 18 IS CORRODED. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. (M)
- [SDR SIMA200207807](https://openairdocs.org/sdr/SIMA200207807), Feb 25, 2002: SILL. CORRODED. ABI - THIS IS LEVEL 2 FINDING. RIGHT SILL CORRODED BETWEEN FRAMES 15 AND 16. BLENDED CORROSION, FOUND TO BE ACCEPTED AS IS IAW EMB GST-0714/02. (M)
- [SDR SIMA200110203](https://openairdocs.org/sdr/SIMA200110203), Apr 12, 2001: WARNING SYSTEM. MALFUNCTIONED. ORD - FLT 4027 - DURING TAKEOFF, CREW NOTED SPS 1 INOPERATIVE IND FOLLOWED BY AN AOA FAIL CAUTION. CREW ABORTED TAKEOFF. RETURNED TO GATE SAFELY AND IND DID DIS
- [SDR 20010112SG049](https://openairdocs.org/sdr/20010112SG049), Nov 3, 2000: SLEEVE. DAMAGED. DSM - FLT 4034 - ON CLIMB-OUT, HAD BLEED ONE LEAK WARNING AND A SMELL IN CABIN, THEN CARGO SMOKE WARNING INDICATION. CREW DISCHARGED BOTTLES IN CARGO AND RETURN
- [SDR 20010112SG048](https://openairdocs.org/sdr/20010112SG048), Nov 3, 2000: O-RING. WORN. DSM - FLT 4034 - ON CLIMB-OUT, HAD BLEED ONE LEAK WARNING AND A SMELL IN CABIN, THEN CARGO SMOKE WARNING INDICATION. CREW DISCHARGED BOTTLES IN CARGO AND RETURN
- [SDR SIMA3084](https://openairdocs.org/sdr/SIMA3084), Nov 3, 2000: O-RING. WORN. DSM - FLT 4034 - ON CLIMB-OUT, HAD BLEED ONE LEAK WARNING AND A SMELL IN CABIN, THEN CARGO SMOKE WARNING INDICATION. CREW DISCHARGED BOTTLES IN CARGO AND RETURN
- [SDR SIMA2921](https://openairdocs.org/sdr/SIMA2921), Oct 18, 2000: POWER SUPPLY. BURNED OUT. DFW - DURING PS-2 CHECK, MAINTENANCE NOTED RIGHT WING STROBE INOPERATIVE. MAINTENANCE FOUND POWER SUPPLY SLIGHTLY BURNED. POWER SUPPLY REMOVED AND REPLACED. OPE
- [SDR SIMA2917](https://openairdocs.org/sdr/SIMA2917), Oct 18, 2000: POWER SUPPLY. BURNED OUT. DFW - DURING PS-2 CHECK, MAINTENANCE NOTED RIGHT WING STROBE INOPERATIVE. MAINTENANCE FOUND POWER SUPPLY SLIGHTLY BURNED. POWER SUPPLY REMOVED AND REPLACED. OPE
- [SDR SIMA1931](https://openairdocs.org/sdr/SIMA1931), Jul 11, 2000: SEAL. LOOSE. ORD - FLT 4135 - THE FLIGHT CREW REPORTS A LOUD WHISTLE AROUND THE CABIN DOOR WHEN IN FLIGHT AND A/C IS PRESSURIZED. RESECURED PAX DOOR SEAL. OPS CHECK GOOD. (M
- [SDR SIMA1012](https://openairdocs.org/sdr/SIMA1012), Apr 10, 2000: POWER SUPPLY. INOPERATIVE. FLT 3653 - XNA - FORWARD EMERGENCY LIGHTS ILLUMINATE WHEN EMERGENCY LIGHTS ARE ARMED. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY POWER SUPPLY. OPS CHECK GOOD. 
- [SDR SIMA992372](https://openairdocs.org/sdr/SIMA992372), Aug 25, 1999: PRESSURE SWITCH. FAILED. ORD - FLT 4390 - NR 2 HYDRAULIC SYSTEM FAILED, HAD HIGH TEMP AND LOW QTY WARNING ON EICAS. DECLARED EMERGENCY, LANDED SAFELY. REMOVED AND REPLACED NR 2 SYSTEM E
- [SDR SIMA992301](https://openairdocs.org/sdr/SIMA992301), Aug 19, 1999: POWER SUPPLY. INOPERATIVE. ORD - FLT 4095 - TWO EMERGENCY EXIT SIGNS ON THE FORWARD CABIN BULKHEAD DO NOT ILLUMINATE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOO
- [SDR SIMA982931](https://openairdocs.org/sdr/SIMA982931), Oct 20, 1998: ENGINE. FAILED. ORD - FLT 4318 - NR 2 ENGINE FLAMED OUT DUE TO LOW N1. RESTARTED ENGINE SUCCESSFULLY. REMOVED AND REPLACED NR 2 ENGINE. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR SIMA982803](https://openairdocs.org/sdr/SIMA982803), Oct 7, 1998: SMOKE DETECTOR. MALFUNCTIONED. ORD - FLT 2600 - FOUND BAGGAGE SMOKE WARNING LIGHT CAME ON. DISCHARGED BOTH FIRE BOTTLES. LANDED SAFELY. PERFORMED VISUAL INSPECTION OF BAGGAGE COMPARTMENT WITH
- [SDR 98ZZZM923](https://openairdocs.org/sdr/98ZZZM923), Oct 7, 1998: SMOKE DETECTOR. MALFUNCTIONED. ORD - FLT 2600 - FOUND BAGGAGE SMOKE WARNING LIGHT CAME ON. DISCHARGED BOTH FIRE BOTTLES. LANDED SAFELY. PERFORMED VISUAL INSPECTION OF BAGGAGE COMPARTMENT WITH
- [SDR SIMA981653](https://openairdocs.org/sdr/SIMA981653), Jun 14, 1998: FADEC. OVERHEATED. IND - FLT 4209 - RECEIVED SIMULTANEOUS EICAS (ENGINE INDICATING AND CREW ALERTING SYSTEM), MESSAGES, E1 CTL A FAIL, E2 CTL B FAIL. FLIGHT CREW NOTICED SLIGHT SM

## STCs that may be installed (OpenAirDocs) (150, 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 (Raytheon G36)

- [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 SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [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 SA04505CH](https://openairdocs.org/stc/SA04505CH): Installation of Hartzell Propeller model HC-C3YF-1N/NM8410-4 or HC-C3YF-1N/NM8410K-4. Hartzell Propeller Inc
- [STC SA12416IB](https://openairdocs.org/stc/SA12416IB): Installation of Main wheel, Nose wheel, brake assembly, axle, master cylinder and brake lines. BERINGER AERO
- [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies
- [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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC
- [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC. Lists 36 Series
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02024WI](https://openairdocs.org/stc/SA02024WI): Installation of the Aft Auxiliary Heating System (AAHS). Peregrine
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04537CH](https://openairdocs.org/stc/SA04537CH): Installation of wingtip position/anti-collision light support bracket. Gallagher Aviation LLC
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA02535CH](https://openairdocs.org/stc/SA02535CH): Installation of M-T Propeller, Inc model MTV-9-D/205-58 or MTV-9-D/210-58 propeller. McFarlane Aviation LLC
- [STC SA01830WI](https://openairdocs.org/stc/SA01830WI): G1000 Integrated Avionics System hardware and software updates including optional Flight Stream 510. Textron Aviation Inc
- [STC SA01422AT-D](https://openairdocs.org/stc/SA01422AT-D): Installation of Lower Cabin Door Stiffener. Summit Aviation Inc. Lists 36 Series
- [STC SA02314AT-D](https://openairdocs.org/stc/SA02314AT-D): Installation of a stainless steel exhaust system. Summit Aviation Inc
- [STC SA10145SC-D](https://openairdocs.org/stc/SA10145SC-D): Installation of a Teledyne Continental Motors Model IO-550-R engine. Summit Aviation Inc
- [STC SA00638WI](https://openairdocs.org/stc/SA00638WI): Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. Aero-Mach Wilco LLC
- [STC SA01904WI](https://openairdocs.org/stc/SA01904WI): Installation of LED Position and Recognition Lights. Whelen Aerospace Technologies
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA00469NY](https://openairdocs.org/stc/SA00469NY): Installation of Main Landing Gear Auxiliary Landing Lights. Gallagher Aviation LLC
- [STC SA00901NY](https://openairdocs.org/stc/SA00901NY): Installation of a wing tip recognition lights. Gallagher Aviation LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA04634NY](https://openairdocs.org/stc/SA04634NY): Modification of the Brake Master Cylinder. Marsh Brothers Aviation Inc
- [STC SA493CH](https://openairdocs.org/stc/SA493CH): Increase in maximum gross weight from 3600 lbs. to 3700 lbs. with installation of Continental I0-550-B engine in accordance with D'Shannon Products Installation Instruction 71-20-00, dated 10/20/88, or later FAA-approved revision; and installation of Cooling Air Baffles in accordance with D'Shannon Products Installation Instruction DSP1M95-2, dated 6/1/95, FAA-approved 6/21/95 or later FAA Approved revisions. D'Shannon Products Ltd
- [STC SA4180WE](https://openairdocs.org/stc/SA4180WE): Installation of inflatable door seal. TALCO Aviation Corp
- [STC SA01945WI](https://openairdocs.org/stc/SA01945WI): Hardware and software update for the Garmin G1000 Integrated Avionics System. Garmin International Inc
- [STC SA00257BO](https://openairdocs.org/stc/SA00257BO): Installation of air conditioning system. A/C Systems LLC
- [STC SA10004SC](https://openairdocs.org/stc/SA10004SC): Installation of Hartzell PHC-C3YF-1RF/F8068 propeller. General Aviation Modifications Inc
- [STC SA03122CH](https://openairdocs.org/stc/SA03122CH): Increase Maximum Gross weight to 4011 pounds for Normal Category operations. General Aviation Modifications Inc
- [STC SA4-1629](https://openairdocs.org/stc/SA4-1629): Installation of wing tip fuel tanks. General Aviation Modifications Inc
- [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 SA01925WI](https://openairdocs.org/stc/SA01925WI): Installation of Garmin G1000 Software Update. Textron Aviation 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

All 150: https://openairdocs.org/aircraft/N603AE/stcs.md

## Related

- Other Raytheon G36 aircraft: https://openairdocs.org/model/raytheon-g36/aircraft.md

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