# N206FS: 2019 Iai GULFSTREAM G280 - Status: Valid registration - Airframe: [Iai GULFSTREAM G280](https://openairdocs.org/model/iai-gulfstream-g280) (registry code 3980218, 21 seats) - Engine: [Honeywell AS907-2-1G](https://openairdocs.org/engine/honeywell-as907-2-1g) (registry code 33400) - Data sheets: [TCDS A61NM](https://openairdocs.org/tcds/A61NM) (Gulfstream Aerospace LP), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs) - Serial number: 2198 - Year built: 2019 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 26, 2019 - Certificate issued: July 30, 2020 - Expires: July 31, 2027 - Mode S code: A1A8DB - Registered owner: [Commerce Bank](https://openairdocs.org/faa-owner/COMMERCE%20BANK) - Location: [Saint Louis, MO](https://openairdocs.org/faa-place/MO/Saint%20Louis) - Owner type: Corporation - Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=206FS - Page: https://openairdocs.org/aircraft/N206FS From the FAA registry file of October 21, 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): 10 in force ### Matched by airframe (Iai GULFSTREAM G280) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2026-09-04](https://openairdocs.org/ad/2026-09-04): Flight Controls · Gulfstream Aerospace LP Gulfstream G280. Effective Jun 12, 2026 - [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 2023-04-02](https://openairdocs.org/ad/2023-04-02): Navigation · Gulfstream Aerospace LP Gulfstream G280. Effective Apr 7, 2023 - [AD 2021-17-14](https://openairdocs.org/ad/2021-17-14): Wings · Gulfstream Aerospace LP Gulfstream G280. Effective Oct 14, 2021 - [AD 2020-26-12](https://openairdocs.org/ad/2020-26-12): Flight controls · Gulfstream Aerospace LP Gulfstream G280. Effective Feb 1, 2021 - [AD 2020-15-02](https://openairdocs.org/ad/2020-15-02): Fuselage · Gulfstream Aerospace LP Gulfstream G280. Effective Aug 27, 2020 - [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017 ### Matched by engine (Honeywell AS907-2-1G) - [AD 2023-24-04](https://openairdocs.org/ad/2023-24-04): Engine Fuel and Control · Honeywell International AS907-1-1A and AS907-2-1G. Effective Jan 10, 2024 - [AD 2018-04-13](https://openairdocs.org/ad/2018-04-13): Engine Controls Section · Honeywell International AS907-1-1A, AS907-2-1A, AS907-2-1G and 1 more. Effective Apr 12, 2018 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N206FS. ## FAA accident and incident reports None matched to N206FS. ## Reports on N206FS not matched to an aircraft (2) They name N206FS, but no registry record covers the event date, or the aircraft registered then was built later. - [Incident 19981028043809I](https://openairdocs.org/incident/19981028043809I), Oct 28, 1998: Bell 206L3 (N206FS), Fourchon, LA, Minor damage. (-5)During cruise flight the pilot heard a loud bang as if something had hit the aircraft. The pilot made a precautionary landing at the nearest suitable… - [Incident 19950607029489I](https://openairdocs.org/incident/19950607029489I), Jun 7, 1995: Bell 206L3 (N206FS), Galveston, TX, Minor damage. Sliding passenger vent window depared inflight. Flown to shore base. Window replaced. ## Service difficulty reports (43) As reported by operators and repair stations. - [SDR W6JA20210907048](https://openairdocs.org/sdr/W6JA20210907048), Sep 7, 2021: WINDSHIELD. CRACKED. FLIGHT THAT DEPARTED KLUK TO KJAX. CREW REPORTED AT FL450 THAT PILOT WINDSHIELD CRACKED/SPLINTERED. CREW THEN FOLLOWED AIRCRAFT QRH AND DESCENDED TO FL150. RETU - [SDR HEEA20111108456](https://openairdocs.org/sdr/HEEA20111108456), Nov 8, 2011: FRAME. CORRODED. AFT LOWER FRAME ASSY WAS FOUND TO BE CORRODED. THE AFT LOWER FRAME WILL THEN BE REPAIRED IAW THE FAA-APPROVED REPAIR DATA. - [SDR HEEA20110830002](https://openairdocs.org/sdr/HEEA20110830002), Aug 30, 2011: DIFFUSER. SEPARATED. ENGINE WAS REMOVED DUE TO CYCLED WHEELS. COMPRESSOR DISASSEMBLED DUE TO CRACKED SCROLL. DIFFUSER FOUND TO HAVE SEPARATED PLATE. REPLACED DIFFUSER. - [SDR HEEA126111](https://openairdocs.org/sdr/HEEA126111), Sep 16, 2009: CONTROL TUBE. CRACKED. CORROSION AND CRACKS ON CONTROL TUBE, NEXT TO END AT FIXED CLEVIS. SCRAPPED CONTROL TUBE. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09. - [SDR HEEA126112](https://openairdocs.org/sdr/HEEA126112), Sep 16, 2009: STRUCTURE. CORRODED. EXCESSIVE CORROSION ON TOP CENTER SURFACE OF HORIZONTAL STABILIZER ASSY. SENT TO VENDOR FOR REPAIR. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09. - [SDR HEEA126113](https://openairdocs.org/sdr/HEEA126113), Sep 16, 2009: STRUCTURE. CORRODED. CORROSION AND CRACKS ON LT STABILIZER SPAR TUBE. SENT TO VENDOR FOR REPAIR. NOTE: PREVIOUSLY SUBMITTED ON 10/6/09. - [SDR HEEA085068](https://openairdocs.org/sdr/HEEA085068), Feb 28, 2003: BATTERY. DISCHARGED. MAIN BATTERY, NO VOLTS. - [SDR HEEA084280](https://openairdocs.org/sdr/HEEA084280), Feb 11, 2003: BEARING. WORN. MAIN ROTOR BELLCRANK HAS WORN BEARINGS. REPLACED 2 BEARINGS 206001053005. REPAIRED. - [SDR HEEA083411](https://openairdocs.org/sdr/HEEA083411), Jan 9, 2003: BATTERY. WEAK. MAIN BATTERY WEAK. - [SDR HEEA083319](https://openairdocs.org/sdr/HEEA083319), Jan 9, 2003: SHAFT. SHEARED. STARTER GENERATOR HAS A SHEARED SHAFT. - [SDR HEEA083316](https://openairdocs.org/sdr/HEEA083316), Jan 9, 2003: CHECK VALVE. SMOKE. TURBINE OIL PRESSURE CHECK VALVE SMOKING ON SHUTDOWN. REPAIRED. - [SDR HEEA083299](https://openairdocs.org/sdr/HEEA083299), Jan 9, 2003: SEAT BELT. MISMANUFACTURED. SEAT BELT RESTRAINT TOO SHORT. - [SDR HEEA083273](https://openairdocs.org/sdr/HEEA083273), Jan 8, 2003: SPLINE ADAPTER. WORN. TACH GENERATOR HAS A WORN DRIVE SPLINE. - [SDR HEEA079580](https://openairdocs.org/sdr/HEEA079580), May 30, 2002: GPS. INOPERATIVE. GPS RECEIVER INOPERATIVE. - [SDR HEEA079477](https://openairdocs.org/sdr/HEEA079477), May 28, 2002: CROSSTUBE. CORRODED. CROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. - [SDR HEEA079213](https://openairdocs.org/sdr/HEEA079213), May 24, 2002: SKID. CORRODED. SKID TUBE CRACKED DUE TO CORROSION EXFOLIATING FROM TUBE AT FORWARD END NEAR HOLD DOWN RING. - [SDR HEEA073634](https://openairdocs.org/sdr/HEEA073634), Jun 18, 2001: SKID. CORRODED. CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. - [SDR HEEA073633](https://openairdocs.org/sdr/HEEA073633), Jun 18, 2001: SKID. CORRODED. CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. - [SDR HEEA073629](https://openairdocs.org/sdr/HEEA073629), Jun 18, 2001: CROSSTUBE. CORRODED. CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. - [SDR HEEA073627](https://openairdocs.org/sdr/HEEA073627), Jun 18, 2001: CROSSTUBE. CORRODED. CORROSION PITS BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE. - [SDR HEEA073570](https://openairdocs.org/sdr/HEEA073570), Jun 18, 2001: RESTRAINT. WEAK. SPRINGS WEAK AND STICKING ARMS. REPLACED WITH SERVICEABLE ASSY. - [SDR HEEA072611](https://openairdocs.org/sdr/HEEA072611), Apr 16, 2001: SERVO. LEAKING. CAUSING EXCESSIVE INTERNAL LEAKAGE. FOUND DEFECTIVE LAPPING. SENT TO FORTNER ACCESSORY SERVICE CORP. FOR WARRANTY REPAIR. - [SDR HEEA072499](https://openairdocs.org/sdr/HEEA072499), Apr 11, 2001: VALVE. DAMAGED. THREADS DAMAGED THAT GO INTO COMBUSTION CASE. REPLACED WITH SERVICEABLE PART. - [SDR HEEA072149](https://openairdocs.org/sdr/HEEA072149), Apr 6, 2001: WEB. WORN. OUTBOARD FORWARD SERVO MOUNT LUGS ARE BEING WORN BY THE SERVO FORWARD ROD END BEARING DUE TO ROCKING MOTION OF THE SERVO. REPLACED WITH SERVICEABLE PART. - [SDR HEEA065056](https://openairdocs.org/sdr/HEEA065056), Nov 11, 1999: INDICATOR. READS HIGH. INDICATOR READS 4 PSI HIGH. - [SDR HEEA061569](https://openairdocs.org/sdr/HEEA061569), Apr 2, 1999: FILTER. MALFUNCTIONED. FILTER WILL NOT BYPASS. - [SDR HEEA060797](https://openairdocs.org/sdr/HEEA060797), Feb 22, 1999: FLOAT. LEAKING. FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS. - [SDR HEEA060796](https://openairdocs.org/sdr/HEEA060796), Feb 22, 1999: FLOAT. LEAKING. FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS. - [SDR HEEA060226](https://openairdocs.org/sdr/HEEA060226), Jan 22, 1999: SHAFT. CORRODED. CORROSION BEYOND LIMITS ON SEAL RIDE. REPLACED WITH SERVICEABLE SHAFT. - [SDR HEEA060222](https://openairdocs.org/sdr/HEEA060222), Jan 22, 1999: BEARING SEAT. WORN. BEARING SEAT WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE CARRIER ASSY. - [SDR HEEA060161](https://openairdocs.org/sdr/HEEA060161), Jan 22, 1999: RECEIVER. MALFUNCTIONED. RIGHT INSIDE KNOB STEM POWER OUT WITH KNOB ON LORAN. - [SDR HEEA0015563](https://openairdocs.org/sdr/HEEA0015563), Aug 14, 1998: TORQUEMETER. STICKING. TORQUE NEEDLE STICKS AT 14 PERCENT WHEN DECREASING PRESSURE. - [SDR HAIHEEA9953](https://openairdocs.org/sdr/HAIHEEA9953), May 28, 1997: INDICATOR. STICKS. TOT INDICATOR INTERMITTENTLY STICKS AT ZERO. - [SDR HEEA979014](https://openairdocs.org/sdr/HEEA979014), Feb 10, 1997: PROBE. FAILED. PROBE PEGS OUT FUEL QUANTITY INDICATOR HIGH SIDE. - [SDR HEEA968298](https://openairdocs.org/sdr/HEEA968298), Oct 14, 1996: INDICATOR. FAILED. NO TOT INDICATIONS. - [SDR HEEA968210](https://openairdocs.org/sdr/HEEA968210), Oct 10, 1996: TORQUEMETER. DEFECTIVE. ENGINE TORQUE GAUGE FLUCTUATES. - [SDR HEEA966864](https://openairdocs.org/sdr/HEEA966864), Mar 20, 1996: GRIP. WORN. ASSEMBLY LEAKING GREASE, DUE TO RETAINER SPINNING INSIDE OF GRIP. PRO SEAL UNBONDED. WORN AREA IN GRIP. MIN .007 MAX. .012 DEPTH. REPLACED WITH SERVICEABLE PART - [SDR HEEA956224](https://openairdocs.org/sdr/HEEA956224), Dec 12, 1995: SPLINE ADAPTER. MIS MFG. RECEIVING INSPECTION OF NEW, NEVER INSTALLED SPLINE ADAPTER INDICATED I.D. MANUFACTURED .0005" OVER MAX B.P. SPECS OF .6565". ADAPTER MEASURES .657. INSTALLED N - [SDR HEEA955985](https://openairdocs.org/sdr/HEEA955985), Nov 8, 1995: TRANSCEIVER. DEFECTIVE. SECOND KNOB WILL NOT TURN INTERNAL NUMBER. REPLACED ONE KNOB SHAFT FROM SPARE. ALSO REPLACED V101 CAVITY OSCILLATOR THAT WAS WEAK. REPAIRED PROBLEM. BENCH CHECK - [SDR HEEA955621](https://openairdocs.org/sdr/HEEA955621), Aug 25, 1995: CELL. DEFECTIVE. TIME. INSPECTED BY ACCESSORY SHOP AND FOUND CELL #14 VOLTAGE READING ZERO AS RECEIVED. CELL REPLACED WITH ONE GIVEN ON CONSIGNMENT. - [SDR HEEA955351](https://openairdocs.org/sdr/HEEA955351), Jul 11, 1995: TRANSCEIVER. MALFUNCTION. SWITCHES CHANNELS BY ITSELF AND HARD TO CHANGE FREQUENCY. - [SDR HEEA954838](https://openairdocs.org/sdr/HEEA954838), Apr 21, 1995: BEARING. CRACKED. BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES P/N 206-010-733-003. BEARINGS SCRAPPED LOCALLY. SEE MMIR'S # 4831 THROUGH # 4844 FOR ADDITIONAL BEARINGS. - [SDR HEEA954766](https://openairdocs.org/sdr/HEEA954766), Apr 11, 1995: SHAFT. CORRODED. CORROSION BEYOND LIMITS ON SEAL RIDE. ## Related - Other Iai GULFSTREAM G280 aircraft: https://openairdocs.org/model/iai-gulfstream-g280/aircraft.md - STCs for the Iai GULFSTREAM G280: https://openairdocs.org/model/iai-gulfstream-g280/stcs.md - The Honeywell AS907-2-1G engine: https://openairdocs.org/engine/honeywell-as907-2-1g.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.