N20NY1966 Dassault/Sud FAN JET FALCON
This N-number isn't registered right now. Below is its last known registration, canceled Oct 3, 2020.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply6 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Air Force Systems Command
- Owner type
- Government
- City, state
- Hanscom Afb, MA
- Certificate issued
- Mar 2, 1990
- Canceled
- Oct 3, 2020
- Airworthiness
- Experimental · Research and Development, Crew Training
- Airworthiness date
- May 12, 2016
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/Sud
- Model
- FAN JET FALCON
- Year
- 1966
- Serial number
- 61
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 12
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A190ED
Engine
- Make and model
- Ge Cf700-2d-2
- Type
- Turbo-fan
- Power
- 4,500 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- 1990 – 2020Air Force Systems CommandHanscom Afb, MA
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 (1)
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 |
|---|---|---|---|
| 2000-01-09 | GE Aircraft Engines CJ610 Series Turbojet Engines and CF700 Turbofan Engines | Feb 11, 2000 | Engine (CF700-2D-2)Serial numbers per Appendix 1 of the AD. Only with: Engines with rotating parts listed by P/N and SN in Appendix 1 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (6)
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.
- Hydraulic power · line · chafedJan 24, 2005
WHILE COMPLAYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICKNESS LINES REPLACED. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · line · chafedJan 24, 2005
WHILE COMPLYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICHNESS LINES REPLACED. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · switch · damagedSep 26, 2001
DURING SCHEDULED MAINTENANCE, A GEAR SWING WAS BEING ATTEMPTED BUT WAS UNABLE TO RETRACT GEAR. FOUND RIGHT, MAIN LANDING GEAR DOOR ACTUATOR SWITCH FAULTY, COULD NOT MAKE CONTACT ON A&B TERMINALS. REMOVED SWITCH FROM ACTUATOR AND FOUND INTERNAL DAMAGE IN ACTUATOR SWITCH RECEPTACLE. CAUSE OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reportsShow fewer reports
- Fuel · fitting · corrodedJun 29, 2001
LEFT FUEL DRAIN UNION WAS REMOVED FROM MAIN WING TANK TO SEAL LEAK. UNION WAS FOUND TO BE RUSTED AND PITTED ON INSIDE DIAMETER. PITTING ESTIMATED TO BE ONE THIRD OF WALL THICKNESS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · indicator · mismanufacturedNov 1, 1998
UNIT MANUFACTURED IN 1982 AND STILL IN SEALED PACKAGE WHEN RECEIVED. STABILIZER TRIM GAVE REVERSE INDICATION WHEN INSTALLED. ACTUAL TAIL PLANE POSITION 38 DEGREES/ZERO INDICATION. UNIT EXCHANGED FOR S/N 329 NEW INDICATOR (ALSO MFG 1982) WHICH OPERATED PROPERLY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Equipment and furnishings · seat frame · brokenJan 13, 1998
PILOT'S INBOARD ARM REST WAS NOTICED TO FLEX EXCESSIVELY. SEAT BACK UPHOLSTERY REMOVED TO INSPECT SEAT FRAME. FRAME TUBE FOUND COMPLETELY BROKEN THROUGH APPROXIMATELY 4 INCHES BELOW ARM REST ATTACH POINT. BREAK APPEARS TO ORIGINATE FROM A POP RIVET HOLE WHERE SHEET METAL ATTACHES TO TUBE AND TUBE…
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