N520AW1981 Dassault MYSTERE-FALCON 20-F5
Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Gg Flight LLC
- Owner type
- LLC
- City, state
- Findlay, OH
- Certificate issued
- Sep 27, 2021
- Expires
- Sep 30, 2028
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 22, 2008
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Dassault
- Model
- MYSTERE-FALCON 20-F5
- Year
- 1981
- Serial number
- 453
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 2
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A68903
Engine
- Make and model
- Honeywell Tfe731-5br-2c
- Type
- Turbo-fan
- Power
- 4,750 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2021 – nowGg Flight LLCFindlay, OH · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (9)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2023-20-05 | Dassault Aviation Airplanes | Nov 8, 2023 | Airframe (MYSTERE-FALCON 20-F5)Only with: Applies only to airplanes on which the Supplemental Structural Inspection Program (SSIP) (Dassault Service Bulletin 730) has been embodied into the existing maintenance or inspection program. |
| 2020-03-19 | Time Limits/ Maintenance Checks | Apr 2, 2020 | Airframe (MYSTERE-FALCON 20-F5)Only with: Except airplanes on which the Supplemental Structural Inspection Program (SSIP) (Dassault Service Bulletin 730) has been embodied into the existing maintenance or inspection program. |
| 2017-10-01 | Fuselage | Jun 13, 2017 | Airframe (MYSTERE-FALCON 20-F5) |
| 2015-20-08 | Fire protection | Nov 12, 2015 | Airframe (MYSTERE-FALCON 20-F5) |
| 2013-22-10 | Fire Protection | Dec 19, 2013 | Airframe (MYSTERE-FALCON 20-F5) |
Show all 9 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2012-17-05 | Honeywell International Inc. Turbofan Engines | Oct 2, 2012 | Engine (TFE731-5BR-2C)Only with: Applies only with specific first stage low-pressure turbine (LPT1) rotor assembly P/Ns installed: TFE731-5 with P/N 3075184-2, -3, or -4; TFE731-5AR/-5BR with P/N 3075447-1, -2, -4, 3075713-1, -2, -3, or 3074748-5; TFE731-4, -4R, -5AR, -5BR, -5R with P/N 3074748-4, -5, 3075447-1, -2, -4, 3075713-1, -2, or -3. |
| 2009-14-07 | Dassault Model Mystere-Falcon 20-C5, 20-D5, 20-E5, and 20-F5 Airplanes | Aug 12, 2009 | Airframe (MYSTERE-FALCON 20-F5)Only with: Airplanes without Dassault Service Bulletin F20-766 implemented. |
| 2008-19-12 | Honeywell International Inc. TFE731-4, -4R, -5, -5AR, -5BR, and -5R Series Turbofan… | Oct 27, 2008 | Engine (TFE731-5BR-2C)Only with: Interstage turbine transition (ITT) duct P/N 3075292-1, 3075292-3, 3074766-1, 3077063-1, 3075655-1, 3075655-2, 3075699-1, or 3075699-3 installed. |
| 2004-19-02 | Dassault Model Fan Jet Falcon Series Airplanes and Model Mystere-Falcon 20 Series… | Oct 25, 2004 | Airframe (MYSTERE-FALCON 20-F5) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Electrical power · bearing · failedNov 27, 2002
ON 11/27/02, THE AIRCRAFT EXPERIENCED VIBRATION WHILE ENROUTE. THE CREW FELT IT WAS A STARTER/GENERATOR AND DIVERTED. WHILE ON APPROACH, THE RT STARTER/GENERATOR FAILED. AFTER AN UNEVENTFUL LANDING THE STARTER/GENERATOR WAS REPLACED AND ALL WAS NORMAL. ON TEARDOWN THE FRONT BEARING WAS FOUND TO BE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine indicating · indicator · failedJul 17, 1999
IN CRUISE FLIGHT, THE ENGINE INDICATOR CB 1E2 POPPED OUT. THE N1, N2, ITT, OIL PRESSURE, AND OIL TEMPERATURE INDICATORS LOST POWER. THE CREW DIVERTED TO A MAINTENANCE FACILITY WHERE THEY FOUND THE N2 GAUGE SHORTED INTERNALLY. (THIS FAILURE ALSO CAUSED THE DEEC BATTERY CB 92E2 TO OPEN. REPLACED N2…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026