# N811AA: 1968 Dassault/Sud FAN JET FALCON SER D, registration cancelled 2026-04-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 8, 2026
- Status when cancelled: Valid registration
- Airframe: [Dassault/Sud FAN JET FALCON SER D](https://openairdocs.org/model/dassault-sud-fan-jet-falcon-ser-d) (registry code 2720304)
- Engine: [GE CF700 series](https://openairdocs.org/engine/ge-cf700-series) (registry code 30010)
- Data sheets: [TCDS E7EA](https://openairdocs.org/tcds/E7EA) (OpenAirDocs)
- Serial number: 187
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 15, 1969
- Certificate issued: February 26, 1997
- Last registry action: August 18, 2023
- Mode S code: AB0D14
- Owner when cancelled: [USA Jet Airlines Inc](https://openairdocs.org/faa-owner/USA%20JET%20AIRLINES%20INC)
- Location: [Belleville, MI](https://openairdocs.org/faa-place/MI/Belleville)
- Owner type: Corporation
- Owner's area on the map: 42.1832° N, 83.4890° W: Placed by OpenAirDocs at the center of ZIP code 48111, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N811AA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=811AA
- Page: https://openairdocs.org/deregistered/N811AA-2026-04-08

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Dassault/Sud FAN JET FALCON SER D: https://openairdocs.org/model/dassault-sud-fan-jet-falcon-ser-d.md

## Service difficulty reports (21)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR Y2PA2023100523050](https://openairdocs.org/sdr/Y2PA2023100523050), Sep 30, 2023: ACTUATOR. LEAKING. CREW STATED THAT WHILE ON FINAL FOR RUNWAY 19L, THE GEAR DID NOT COME DOWN. THEY REQUESTED DELAY VECTORS TO RUN PROCEDURE. THEY PERFORMED PROCEDURE A SUCCESSFUL
- [SDR Y2PA2023082223045](https://openairdocs.org/sdr/Y2PA2023082223045), Aug 14, 2023: VALVE. BINDING. DISCREPANCY: CREW REPORTED THAT THE CABIN ALTITUDE LIGHT AND HORN WENT OFF UPON REACHING CRUISE ALTITUDE. THEY DONNED MASKS AND RAN POH PROCEDURE. THEY COULD NO
- [SDR Y2PA2022090622048](https://openairdocs.org/sdr/Y2PA2022090622048), Aug 31, 2022: ENGINE. FLAMED OUT. DISCREPANCY: CREW REPORTED THAT WHILE CONDUCTING ENGINE ACCELERATION CHECKS ON THE #1 ENGINE, THE #1 ENGINE FLAMED OUT AT FL290. THE CREW DECLARED AN EMERGENCY 
- [SDR Y2PA2019121719050](https://openairdocs.org/sdr/Y2PA2019121719050), Dec 15, 2019: SWITCH. OUT OF ADJUST. DISCREPANCY: CREW REPORTED RIGHT GEAR “GREEN” DOWN AND LOCKED FAILED TO ILLUMINATE, LANDING GEAR WARNING HORN COULD NOT BE SILENCED, CREW PERFORMED LANDING GEAR
- [SDR Y2PA201911265046](https://openairdocs.org/sdr/Y2PA201911265046), Nov 25, 2019: SKIN. CRACKED. DISCREPANCY: DURING C-CHECK AT KBVO, CRACK WAS FOUND ON NLG SKIN AND DOUBLER AT AFT LH CORNER OF WHEEL WELL. CRACK DIMENSIONS HAVE BEEN SENT TO DFJ CORRECTIVE A
- [SDR Y2PA201911265045](https://openairdocs.org/sdr/Y2PA201911265045), Nov 25, 2019: SKIN. CORRODED. DISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON BOTH LH AND RH SIDES OF THE FUSELAGE CORRECTIVE 
- [SDR Y2PA2019112600025](https://openairdocs.org/sdr/Y2PA2019112600025), Nov 25, 2019: SKIN. CORRODED. DISCREPANCY:DURING C-CHECK AT KBVO, EXCESSIVE CORROSION FOUND AT SPOT WELDS AT FRAME 18, FROM STRINGER 19-22 ON BOTH LH AND RH SIDES OF THE FUSELAGE CORRECTIVE 
- [SDR Y2PA201911265044](https://openairdocs.org/sdr/Y2PA201911265044), Nov 25, 2019: SKIN. CORRODED. DISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON LH SIDE OF FUSELAGE DURING SPOT WELD NDT INSPECTION.2 SPOTS ARE OUT OF LIMITS, AREAS AR
- [SDR Y2PA201911265043](https://openairdocs.org/sdr/Y2PA201911265043), Nov 25, 2019: SKIN. CORRODED. DISCREPANCY: DURING C-CHECK AT KBVO MULTIPLE SPOTS OF CORROSION FOUND ON RH SIDE OF FUSELAGE DURING SPOT WELD NDT INSPECTION.12 SPOTS ARE OUT OF LIMITS, AREAS A
- [SDR Y2PA2018112170040](https://openairdocs.org/sdr/Y2PA2018112170040), Nov 17, 2018: BLADE. FAILED. CREW REPORTED – AT 34,000 FT LEFT ENGINE EXPERIENCED A LOUD BANG, LOST THRUST, EPR=1.2, EGT=695°, N1=70% AND DEVELOPED A LOUD WHIRRING SOUND. DECLARED EMERGENCY
- [SDR Y2PA2018100100034](https://openairdocs.org/sdr/Y2PA2018100100034), Sep 26, 2018: SELECTOR SWITCH. UNSERVICEABLE. CREW REPORTED – FO'S LEG. NORMAL TAKEOFF ROLL @V1 (122) JUST BEFORE ROTATION TWO (2) JACKRABBITS RAN IN FRONT OF THE AIRCRAFT. AT LEAST ONE WAS STRUCK BY THE LE
- [SDR Y2PA2018052960020](https://openairdocs.org/sdr/Y2PA2018052960020), May 26, 2018: PRESSURE SENSOR. FAILED. CREW REPORTED THEY WERE UNABLE TO EXTINGUISH NR 2 HYDRAULIC LIGHT ON STANDBY GAUGE. RAN CHECKLIST. NO GUIDANCE IN CHECKLIST FOR IF LIGHT DOES NOT EXTINGUISH. US
- [SDR Y2PA2015043000021](https://openairdocs.org/sdr/Y2PA2015043000021), Apr 30, 2015: CONTROL PANEL. SHORTED. CREW REPORTED LANDING GEAR EXTENSION FAILURE, E27. LT GEAR UNSAFE, NO GREEN LIGHT. CYCLED GEAR ONCE, NO GREEN LIGHT. PERFORMED MISSED APPROACH AND ENTERED LANDI
- [SDR Y2PA20130316015](https://openairdocs.org/sdr/Y2PA20130316015), Mar 16, 2013: TRIM PANEL. MALFUNCTIONED. CREW REPORTED, ON HAND FLOWN AT 2500' IN IMC, PILOT FLYING ENCOUNTERED AN UNCOMMANDED ROLL TO THE LEFT. PF IMMEDIATELY PULLED "ROLL" CIRCUIT BREAKER TO STOP RUN
- [SDR Y2PA20130120004](https://openairdocs.org/sdr/Y2PA20130120004), Jan 20, 2013: TURBINE BLADES. FOD. CREW REPORTED ENGINE FLAMEOUT AT FL346 AND REQUESTED DESCENT TO FL290. CREW DECLARED AN EMERGENCY AND WERE VECTORED. CREW RAN ENGINE FAILURE AND RELIGHT CHECKLI
- [SDR Y2PA20120618032](https://openairdocs.org/sdr/Y2PA20120618032), Jun 14, 2012: GOVERNOR. BYPASSING. IN CRUISE AT .66 MACH AND FL 350, ADJUSTED EPR FROM 1.44 TO 1.60, AFTER 30 SECONDS FURTHER INCREASED EPR TO 1.75. APPROX 1 MINUTE LATER THE NR 1 ENGINE FLAMED O
- [SDR Y2PA20120428021](https://openairdocs.org/sdr/Y2PA20120428021), Apr 28, 2012: GOVERNOR. BYPASSING. NR 1 ENGINE FLAMED OUT AT FL350, NO INDICATION FOR REASON WHY. INSPECTED FUEL FILTERS, BOROSCOPED AND VISUALLY INSPECTED ENGINE, NO DEFECTS FOUND. R & R FUEL PR
- [SDR Y2PA20120417013](https://openairdocs.org/sdr/Y2PA20120417013), Apr 17, 2012: TURBINE CASE. RUPTURED. AT 14000 FT, NR 1 ENGINE FIRE INDICATION AND HORN ACTUATED. REDUCED THRUST IAW EMERGENCY CHECKLIST, LIGHT EXTINGUISHED. DECLARED EMERGENCY AND LANDED WITHOUT IN
- [SDR Y2PA05008](https://openairdocs.org/sdr/Y2PA05008), Jun 10, 2005: PUMP. INTERMITTENT. DURING CLIMB OUT NR 1 ENG STARTED TO SURGE. NR 1 FUEL PRESSURE DROPPED TO ZERO. OPENED CROSSFEED THEN NR 2 ENG LOST 50 PERCENT POWER, FUEL PRESSURE DROPPED TO N
- [SDR Y2PA04008](https://openairdocs.org/sdr/Y2PA04008), Apr 5, 2004: WHEEL. VIBRATION. ON TAKEOFF, CREW DETECTED VIBRATION ON RT MAIN GEAR. CREW HAD TOWER INSPECT RUNWAY TO FIND TIRE CAP AS SUSPECTED. AC DIVERTED, TO BURN FUEL AND OBTAIN EMERGENCY
- [SDR Y2PA96050](https://openairdocs.org/sdr/Y2PA96050), Jul 19, 1996: JET PUMP. CLOGGED. ELP - WHEN FUEL WAS NOT ABLE TO TRANSFER PROPERLY FROM RIGHT TO LEFT WING, THE CREW RETURNED TO POINT OF DEPARTURE AT ELP. NO EMERGENCY PROCEDURES WERE REQUIRED

## FAA accident and incident reports (1)

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 20130316008229I](https://openairdocs.org/incident/20130316008229I), Mar 16, 2013: Dassault/Sud FAN JET FALCON SER D (N811AA), Belleville, MI, No damage. On final approach crew encountered an uncommanded roll to the left. They pulled roll circuit breakers maintained aircraft control and made a normal landing.…

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