# Service difficulty reports: Dassault-Breguet FALCON 20

A list on [Dassault-Breguet FALCON 20](https://openairdocs.org/model/dassault-breguet-falcon-20.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 208 reports

- [SDR KC8A20250418002](https://openairdocs.org/sdr/KC8A20250418002.md): Cowl Door · inflt separation · Apr 15, 2025 · N229CK · Amd FALCON20 · Nacelle/Pylon, Main Frame
  > DURING CRUISE, RIGHT ENGINE UPPER AND LOWER RIGHT COWLING DEPARTED AIRCRAFT. 'THIS IS A RE-SUBMISSION DUE TO MISSING REGISTRATION NUMBER NOT LISTED IN 1. (C).
- [SDR KC8A20250418001](https://openairdocs.org/sdr/KC8A20250418001.md): Cowl Door · inflt separation · Apr 15, 2025 · N200MV · Amd FALCON20 · Nacelle/Pylon, Main Frame
  > DURING CRUISE. RIGHT ENGINE UPPER AND LOWER RIGHT COWLING DEPARTED AIRCRAFT.
- [SDR KC8A2023122677](https://openairdocs.org/sdr/KC8A2023122677.md): Terminal · shorted · Dec 21, 2023 · N229CK · Amd FALCON20 · Light System Wiring
  > PILOT EXPERIENCED SMOKE IN COCKPIT DURING APPROACH INTO KBKV AIRPORT, DECLARED AN EMERGENCY AND LANDED SAFELY. SOURCE OF SMOKE WAS COMING FROM OVERHEAD PANEL ABOVE CAPTAIN'S SEAT. NO CAUSE OR CORRECTIVE ACTION AT THIS TIME, MECHANIC DISPATCHED TO LOCATION FOR
- [SDR 2023FA0000749](https://openairdocs.org/sdr/2023FA0000749.md): Position Switch · false indication · Nov 8, 2023 · N285TW · Amd FALCON20 · Indicating/Recording System
  > ON DECENT IN TO ELP THE LANDING GEAR WAS EXTENDED, THE RH M/L/G DOWN AND LOCKED GREEN LIGHT DID NOT ILLUMINATE. THE ALTERNATE LANDING GEAR EXTENSION SYSTEM WAS USED WITH THE GREEN LIGHT STILL WAS NOT ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND FLEW BY THE
- [SDR Y2PA2023100523050](https://openairdocs.org/sdr/Y2PA2023100523050.md): Actuator · leaking · Sep 30, 2023 · N811AA · Amd FALCON20 · Landing Gear Actuator
  > 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 SUCCESSFULLY, GEAR EXTENDED. THEY DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. FOUND THE RH MAI
- [SDR 2023F00260](https://openairdocs.org/sdr/2023F00260.md): Fcu · abnormal · Aug 29, 2023 · N699TW · Amd FALCON20 · Fuel Control/Turbine Engines
  > AIRCRAFT DEPARTED CHS, SHORTLY AFTER TAKEOFF THE RH ENGINE ROLLED BACK ON POWER. CREW CONTACTED ATC AND RETURNED TO CHS.
- [SDR Y2PA2023082223044](https://openairdocs.org/sdr/Y2PA2023082223044.md): Transfer Pump · low pressure · Aug 19, 2023 · N962AA · Amd FALCON20 · Fuel Storage
  > CREW REPORTED THAT PREFLIGHT-TAXI-TAKEOFF-CLIMB-THROUGH CRUISE CHECK AT FL320 ALL FUEL INDICATIONS WERE NORMAL. 30 MINUTES LATER FO NOTICED THAT THERE WERE LESS THAN 500 LBS. INDICATING ON THE R/H FUEL GAUGE AND THE L/H FUEL GAUGE SHOWED 3500 LBS. THE CAPTAIN
- [SDR Y2PA2023082223045](https://openairdocs.org/sdr/Y2PA2023082223045.md): Valve · binding · Aug 14, 2023 · N811AA · Amd FALCON20 · Air Conditioning System
  > 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 NOT REDUCE CABIN ALTITUDE WITH AUTO OR MANUAL SYSTEMS. THEY EXECUTED EMERGENCY DESCENT. THEY EXECUTED
- [SDR Y2PA2023081423044](https://openairdocs.org/sdr/Y2PA2023081423044.md): Seal · failed · Aug 10, 2023 · N962AA · Amd FALCON20 · Detection System
  > DISCREPANCY: THE CREW REPORTED ON DEPARTURE, CLIMBING THROUGH 8,000 FEET THE ENGINE #2 FIRE WARNING WENT OFF. THE CREW LEVELED THE AIRPLANE AT 9,000 FEET TO RUN THE RED BOARDER CHECKLIST PROCEDURE. DURING STEP 1 OF THE CHECKLIST PROCEDURE (THRUST LEVER-VERIFY
- [SDR 2023F00063](https://openairdocs.org/sdr/2023F00063.md): None · none · Feb 21, 2023 · N148TW · Amd FALCON20 · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED KGKY FOR KELP, WHILE IN CRUISE THE CREW EXPERIENCED ICING CONDITIONS AT FL280 AND WHEN SELECTING THE AIRFRAME AND ENGINE ANTI-ICE SYSTEMS ON THE LH ENGINE HAD A FLAMEOUT DUE TO THE HIGH DEMAND PUT ON THE BLEED AIR SYSTEM. CREW NOTIFIED ATC TH
- [SDR Y2PA2022090622048](https://openairdocs.org/sdr/Y2PA2022090622048.md): Engine · flamed out · Aug 31, 2022 · N811AA · Amd FALCON20 · Powerplant System
  > 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 WITH CLEVELAND CENTER TO OBTAIN LOWER ALTITUDE, THEY DESCENDED AND PERFORMED A SUCCESSFUL RELIGHT AT
- [SDR 2021F00393](https://openairdocs.org/sdr/2021F00393.md): Powerplant · fod · Dec 17, 2021 · N158TW · Amd FALCON20 · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED LRD AND AT 800' THE RH ENGINE LOST POWER, A RESTART ATTEMPT WAS UNSUCCESSFUL AND THE TOWER WAS INFORMED OF THE SITUATION AND THE AIRCRAFT RETURNED TO LRD FOR AN UNEVENTFUL LANDING. POST FLIGHT INSPECTION REVEALED THE RH ENGINE COMPRESSOR AND
- [SDR 2021F00388](https://openairdocs.org/sdr/2021F00388.md): None · none · Nov 20, 2021 · N226CK · Amd FALCON20 · Aircraft Fuel System
  > CREW SUSPECTED FUEL LEAK FROM RIGHT SIDE. PRECAUTIONARY RIGHT ENGINE SHUT DOWN PERFORMED. INSPECTED AIRCRAFT FOR FUEL LEAKS, NONE NOTED. REMOVED LOWER ACCESS PANELS TO INSPECT FUEL TRANSFER AND CONTROL SYSTEM FOR LEAKS, NONE NOTED. PERFORMED ENGINE RUNS AND LE
- [SDR Y2PA2021092021047](https://openairdocs.org/sdr/Y2PA2021092021047.md): Engine · power loss · Sep 15, 2021 · N822AA · Amd FALCON20 · Engine (Turbine/Turboprop)
  > DISCREPANCY: CREW REPORTED THAT EN-ROUTE DPA-HQA FL 350 HEARD NOISE AND FELT LOW RUMBLING THEN CHECKED ENGINE PARAMETERS. SAW OIL PRESSURE LOW ON GAUGE JUST AT RED LINE WITHOUT ASSOCIATED WARNING LIGHT. HEADING STARTED TO DRIFT TO THE LEFT WITH AN ASSOCIATED R
- [SDR Y2PA2019123019051](https://openairdocs.org/sdr/Y2PA2019123019051.md): Indicator · malfunctioned · Dec 22, 2019 · N811A · Amd FALCON20 · Landing Gear Position and Warning
  > ON BASE TO FINAL, GEAR DOWN, FLAPS 25°, FINAL ITEMS WAS CALLED FOR WHILE ON VISUAL. STARTING THE FINAL ITEMS CHECKLIST GEAR ONLY HAD LT MLG, AND NLG ILLUMINATED DOWN AND LOCKED, RT MLG HAD NO LIGHTS. WENT AROUND AND DECLARED AN EMERGENCY. FO FLEW WHILE CAP
- [SDR Y2PA2019121719050](https://openairdocs.org/sdr/Y2PA2019121719050.md): Switch · out of adjust · Dec 15, 2019 · N811AA · Amd FALCON20 · Landing Gear Position and Warning
  > DISCREPANCY: CREW REPORTED RIGHT GEAR “GREEN” DOWN AND LOCKED FAILED TO ILLUMINATE, LANDING GEAR WARNING HORN COULD NOT BE SILENCED, CREW PERFORMED LANDING GEAR EXTENSION EMERGENCY CHECKLIST “PROCEDURE A”, COMPLETED UNSUCCESSFULLY, “PROCEDURE C” ALSO UNSUCC
- [SDR Y2PA201911265046](https://openairdocs.org/sdr/Y2PA201911265046.md): Skin · cracked · Nov 25, 2019 · N811AA · Amd FALCON20 · Fuselage Main, Plate/Skin
  > 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 ACTION: PHOENIX RISING REPAIRED CRACK AT NOSE WHEEL WELL LF AFT CORNER FRAME 7 AT STRINGER 22 IAW
- [SDR Y2PA201911265045](https://openairdocs.org/sdr/Y2PA201911265045.md): Skin · corroded · Nov 25, 2019 · N811AA · Amd FALCON20 · Fuselage Main, Plate/Skin
  > 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 ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-
- [SDR Y2PA2019112600025](https://openairdocs.org/sdr/Y2PA2019112600025.md): Skin · corroded · Nov 25, 2019 · N811AA · Amd FALCON20 · Fuselage Main, Plate/Skin
  > 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 ACTION: PHOENIX RISING REPAIRED CORROSION AT LH FRAMES 16-18 AT STRINGERS 19-21 IAW DRAWING 19-
- [SDR Y2PA201911265044](https://openairdocs.org/sdr/Y2PA201911265044.md): Skin · corroded · Nov 25, 2019 · N811AA · Amd FALCON20 · Fuselage Main, Plate/Skin
  > 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 ARE LOCATED FROM FRAME 18 TO FRAME 19, BETWEEN STRINGER 10 TO STRINGER 13 CORRECTIVE ACTION: PH
- [SDR Y2PA201911265043](https://openairdocs.org/sdr/Y2PA201911265043.md): Skin · corroded · Nov 25, 2019 · N811AA · Amd FALCON20 · Fuselage Main, Plate/Skin
  > 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 ARE LOCATED FROM FRAME 5 TO FRAME 19, BETWEEN STRINGER 15 TO STRINGER 20 CORRECTIVE ACTION: PHOEN
- [SDR Y2PA201911265047](https://openairdocs.org/sdr/Y2PA201911265047.md): Selector Switch · defective · Nov 23, 2019 · N822AA · Amd FALCON20 · Landing Gear Retraction/Extension System
  > DISCREPANCY: CREW REPORTED LANDING GEAR WOULD NOT RETRACT, ATC DECLARED EMERGENCY. CREW STATED THEY HAD 3 GREEN LIGHTS, REFERENCED P.O.H. AND LANDED NORMALLY AT KYIP CORRECTIVE ACTION: USA JET MAINTENANCE AT KYIP REMOVED AND REPLACED NOSE LANDING GEAR DOOR
- [SDR 2020F00028](https://openairdocs.org/sdr/2020F00028.md): Engine · fod · Oct 1, 2019 · N960AA · Amd FALCON20 · Engine (Turbine/Turboprop)
  > WHILE THE AIRCRAFT WAS ENROUTE AT FLIGHT LEVEL 27000, THE PILOT IN COMMAND NOTICED LIGHT ICE ACCUMULATION. THE PILOT IN COMMAND SELECTED ENGINE AND AIRFRAME DE-ICE SYSTEM ON. A FEW MINUTES AFTER THE DE-ICE SYSTEMS WERE TURNED ON THE LEFT ENGINE BEGAN TO STALL
- [SDR KC8A20190802004](https://openairdocs.org/sdr/KC8A20190802004.md): Frame · cracked · Aug 2, 2019 · N227CK · Amd FALCON20 · Fuselage Main, Frame
  > DURING AN EDDY CURRENT INSPECTION REQUIRED PER AD 2017-10-01, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33. BOTH CRACKS ARE LOCATED BETWEEN STRINGERS 5L AND 6L AND STRINGERS 5R AND 6R. CRAC
- [SDR KC8A20190711003](https://openairdocs.org/sdr/KC8A20190711003.md): Frame · cracked · Jul 11, 2019 · N226CK · Amd FALCON20 · Fuselage Main, Frame
  > DURING AN EDDY CURRENT INSPECTION REQUIRED PER FAA AD 2017-10-01, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33. BOTH CRACKS ARE LOCATED BETWEEN STRINGERS 5L AND 6L AND STRINGERS 5R AND 6R.
- [SDR KC8A20190410002](https://openairdocs.org/sdr/KC8A20190410002.md): Frame · cracked · Apr 10, 2019 · N192CK · Amd FALCON20 · Fuselage Main, Frame
  > DURING AN EDDY CURRENT INSPECTION REQUIRED PER AD 2017-10-01, A CRACK WAS FOUND IN THE BEND BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT SIDE OF FRAME 33. CRACK IS LOCATED BETWEEN STRINGERS 5L AND 6L AND IS APPROXIMATELY.75 INCHES LONG. CRACKS TO B
- [SDR DJSR2019050800001](https://openairdocs.org/sdr/DJSR2019050800001.md): Wire · shorted · Apr 6, 2019 · N481FL · Amd FALCON20 · Flight Control System Wiring
  > TRIM RUNAWAY NOSE DOWN. FOUND AND REPAIRED SHORTED WIRE ON 3A 21 TERMINAL STRIP.
- [SDR HAEA20190307003](https://openairdocs.org/sdr/HAEA20190307003.md): Warning System · activated · Mar 7, 2019 · N699TW · Amd FALCON20 · Fuel Transfer Valve
  > AIRCRAFT DEPARTED DPA FOR TCL DURING CRUISE THE LT WING FUEL TRANSFER PUMP PRESSURE LIGHT ILLUMINATED AND THE CREW ATTEMPTED TO BALANCE THE FUEL USING THE NORMAL AFM PROCEDURE FOR AN INOP FUEL TRANSFER PUMP BUT WAS UNSUCCESSFUL, UPON ARRIVAL AT TCL THEY WERE G
- [SDR HAEA20190305002](https://openairdocs.org/sdr/HAEA20190305002.md): Unknown · malfunctioned · Mar 5, 2019 · N285TW · Amd FALCON20 · Landing Gear Retraction/Extension System
  > ON APPROACH IN TO KYIP THE LANDING GEAR WAS SELECTED DOWN WITH ONLY 3 RED LIGHTS ILLUMINATED, PILOT REPORTED IT DID NOT SOUND LIKE THE GEAR HAD EXTENDED AND CONTACTED TOWER TO DO A FLYBY AND WAS TOLD THEY DID NOT SEE THE GEAR EXTENDED. LANDING GEAR EMER EXTENS
- [SDR DJSR20181227001](https://openairdocs.org/sdr/DJSR20181227001.md): Unknown · malfunctioned · Dec 27, 2018 · N481FL · Amd FALCON20 · Landing Gear Brake System
  > ON LANDING IN EAU RUNWAY 22 IN WET CONDITIONS WITH A CROSSWIND BLOWING FROM 140 DEGREES AT 14 KNOTS GUSTING TO 25 KNOTS. AFTER TOUCHDOWN, PILOT REPORTED INEFFECTIVE LEFT SIDE BRAKING AND EXITED SMOOTHLY OFF THE LEFTSIDE OF THE RUNWAY, WITH NO DAMAGE TO AIRCRAF
- [SDR HAEA20180102001](https://openairdocs.org/sdr/HAEA20180102001.md): Line · cracked · Dec 5, 2018 · N221TW · Amd FALCON20 · Pressure Regulator/Outflow Valve
  > SUPPLEMENTAL INFORMATION. AIRCRAFT DEPARTED KFNT-KSHV AND WAS @ FL280 WHEN THE CABIN ALT WARNING HORN AND LIGHT ACTIVATED THE CREW STARTED THE CHECKLIST AND SELECTED CABIN PRESSURIZATION MANUAL MODE AND ATTEMPTED TO LOWER THE CABIN ALTITUDE WITH NO SUCCESS, AN
- [SDR KC8A201808282718](https://openairdocs.org/sdr/KC8A201808282718.md): Relay · inoperative · Aug 27, 2018 · N229CK · Amd FALCON20 · AC Generation System
  > LOSS OF AUX BUSS ELECTRICAL POWER. LANDING GEAR EXTENDED USING EMERGENCY PROCEDURES. FOUND AUX BUSS RELAY, 9-P, FAILED OPEN RESULTING IN AUX BUSS POWER LOSS. REPLACED THE RELAY, PERFORMED RETRACTION AND SYSTEMS CHECKS IAW THE MAINTENANCE MANUAL.
- [SDR KC8A20180221001](https://openairdocs.org/sdr/KC8A20180221001.md): Frame · cracked · Feb 21, 2018 · N808CK · Amd FALCON20 · Fuselage Main, Frame
  > DURING EDDY CURRENT INSPECTION, CRACKS WHERE FOUND IN THE BENDS BETWEEN THE VERTICAL FRAME AND FRAME FLANGE ON THE LEFT AND RIGHT SIDES OF FRAME 33.
- [SDR DJSR20180208001](https://openairdocs.org/sdr/DJSR20180208001.md): Control Box · malfunctioned · Feb 8, 2018 · N481FL · Amd FALCON20 · Aileron Tab Control System
  > APPROXIMATELY 20 MINUTES INTO THE FLIGHT, COPILOT NOTICED THE AILERON TRIM RUN AWAY. HELD THE OPPOSITE TRIM DIRECTION AND NOTICED THE ROLL CIRCUIT BREAKER TRIPPED. AFTER VERIFYING ALL CHECKLISTS COMPLETED, THE CAPTAIN DIVERTED WITH A VISUAL APPROACH. MECHAN
- [SDR DJSR20180207001](https://openairdocs.org/sdr/DJSR20180207001.md): Trim System · malfunctioned · Feb 7, 2018 · N481FL · Amd FALCON20 · Rudder Tab Control System
  > RUDDER TRIM RAN AWAY TO THE LT SIDE, CIRCUIT BREAKER TRIPPED.
- [SDR KC8A20171213007](https://openairdocs.org/sdr/KC8A20171213007.md): Door Frame · cracked · Dec 13, 2017 · N229CK · Amd FALCON20 · Fuselage Main, Structure
  > CRACKS FOUND IN CARGO DOOR LOWER FORWARD AND AFT FORMERS AT FRAME 11. THE FOLLOWING DAMAGED FORMERS REPLACED WITH NEW: P/N 17219-5105-1 FORMER 1-EA. P/N 17219-5105-2 FORMER 1-EA. ALL WORK DONE IN ACCORDANCE WITH AVCON INDUSTRIES INC. CARGO DOOR MAINTENA
- [SDR 2017FA0000468](https://openairdocs.org/sdr/2017FA0000468.md): Engine · power loss · Aug 28, 2017 · N158TW · Amd FALCON20 · Engine (Turbine/Turboprop)
  > AFTER DEPARTING LIT ICING CONDITIONS DEVELOPED AT FL270 THE ENGINE ANTI-ICE WAS ACTIVATED FOLLOWED BY THE AIRFRAME ANTI ICE SYSTEM, SHORTLY AFTER THAT THE NR 1 AND NR 2 ENGINES STARTING LOSING RPM. THE CREW SWITCHED TO AIR START AND AT FL255-250 BOTH ENGINES R
- [SDR KC8A20170516002](https://openairdocs.org/sdr/KC8A20170516002.md): Frame · cracked · May 16, 2017 · N998CK · Amd FALCON20 · Fuselage Main, Frame
  > DURING EDDY CURRENT INSPECTION, A CRACK WAS FOUND IN THE BEND BETWEEN THE VERTICAL FRAME WEB AND FRAME FLANGE ON OF FRAME 33, APPROXIMATELY 20 MM BELOW STRINGER 5L, APPROXIMATELY 21 MM LONG AND OVER 1.3 MM IN DEPTH. CRACK TO BE REPAIRED.
- [SDR Y2PA2017032100004](https://openairdocs.org/sdr/Y2PA2017032100004.md): Oil System · low pressure · Mar 21, 2017 · N827AA · Amd FALCON20 · Engine Oil Pressure
  > CREW REPORTED AN OIL PRESSURE LIGHT IN FLIGHT. RAN PROCEDURE. ZERO OIL PRESSURE ON TRI-PLEX GAUGE. PERFORMED PRECAUTIONARY SHUTDOWN, DECLARED AN EMERGENCY WITH ATC AND LANDED. MAINTENANCE REPLACED NR 2 ENGINE DUE TO OIL LOSS. REASON FOR LOSS OF OIL IS UND
- [SDR 2017FA0000074](https://openairdocs.org/sdr/2017FA0000074.md): Line · chafed · Feb 17, 2017 · N960AA · Amd FALCON20 · Engine Fuel Distribution
  > DURING CRUISE THE FLIGHT CREW NOTED THAT THE NR 2 ENGINE ROLLED BACK AND SHUT DOWN IN FLIGHT. DECLAIRED AN EMERGENCY AND DIVERTED. FOUND A FUEL LINE HAD CHAFED TRHOUGH. REPLACED THE LINE AND RETURNED THE AIRCRAFT TO SERVICE.
- [SDR KC8A20170206001](https://openairdocs.org/sdr/KC8A20170206001.md): Skin · corroded · Feb 6, 2017 · N227CK · Amd FALCON20 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON THE INSIDE OF THE SKIN ALONG THE SPOT WELDS ON THE RIGHT SIDE OF THE FORWARD FUSELAGE BETWEEN FUSELAGE FRAMES 7 AND 9, AND BETWEEN STRINGERS 20R-22R DURING ROUTINE INSPECTION. CORRODED MATERIAL REMOVED AND AN EXTERNAL SKIN PATCH INSTALLED PE
- [SDR KC8A20161215005](https://openairdocs.org/sdr/KC8A20161215005.md): Skin · corroded · Dec 15, 2016 · N229CK · Amd FALCON20 · Fuselage Main, Plate/Skin
  > SKIN CORROSION FOUND ON THE RIGHT SIDE OF THE FORWARD FUSELAGE BETWEEN FUSELAGE FRAMES 7 AND 9, AND BETWEEN STRINGERS 19 - 22R DURING ROUTINE INSPECTION. CORRODE MATERIAL REMOVED AND AN EXTERNAL SKIN PATCH INSTALLED RD 16-09 REV. A.
- [SDR Y2PA2016102300025](https://openairdocs.org/sdr/Y2PA2016102300025.md): Motor · intermittent · Oct 23, 2016 · Amd FALCON20 · Stabilizer Control System
  > DURING DESCENT, PILOTS PRIMARY TRIM WAS FOUND TO BE INOPERATIVE. THE COPILOTS TRIM WAS ALSO INEFFECTIVE. ALTERNATE TRIM WAS SELECTED AND WAS INEFFECTIVE. THE PROCEDURES IN THE POH WERE REVIEWED AND CHECKED. DECLARED AN EMERGENCY, AN UNEVENTFUL LANDING WAS
- [SDR HAEA201607150001](https://openairdocs.org/sdr/HAEA201607150001.md): Transducer · failed · Jul 15, 2016 · N232TW · Amd FALCON20 · Stall Warning System
  > DURING CRUISE FLIGHT, THE STALL HORN SOUNDED WITH ALL FLIGHT INSTRUMENTS NORMAL AND NOTICED AN ELECTRICAL ODOR, PERFORMED AN UNSCHEDULED LANDING. THE STALL VANE TRANSDUCER FAILED AND CAUSED THE ELECTRICAL ODOR, UNIT WAS REPLACED.
- [SDR 2016F00120](https://openairdocs.org/sdr/2016F00120.md): Unknown · malfunctioned · Apr 27, 2016 · N314TW · Amd FALCON20 · Landing Gear Retraction/Extension System
  > ON APPROACH, THE LT MLG WOULD NOT EXTEND, USING THE ALTERNATE GEAR EXTENSION PROCEDURES THE GEAR WOULD NOT EXTEND. ACFT LANDED WITH THE LT MAIN GEAR RETRACTED, MX LIFTED THE WING & EXTENDED THE GEAR & TOWED THE PLANE TO THE MX HANGAR. ACFT IS STILL IN WORK.
- [SDR Y2PA20160412013](https://openairdocs.org/sdr/Y2PA20160412013.md): Warning Light · false activation · Apr 12, 2016 · N822AA · Amd FALCON20 · Door Warning System
  > CREW REPORTED NORMAL TAKEOFF AND DEPARTURE OF DAY, VFR FLIGHT. PASSING 17000 FT ± CARGO DOOR WARNING LIGHT CAME ON. CANCELED HORN, PERFORMED THE CHECKLIST, DECLARED EMERGENCY, RETURNED TO DEPARTURE. LIGHT EXTINGUISHED PASSING 15000 FT ON DESCENT. MAINTENAN
- [SDR DJSR20160305001](https://openairdocs.org/sdr/DJSR20160305001.md): Circuit Breaker · tripped · Mar 5, 2016 · N481FL · Amd FALCON20 · Aileron Control System
  > AILERON TRIM, FULL RT DEFLECTION, TRIPPED, TRIM ROLL, CIRCUIT BREAKER.
- [SDR Y2PA2016022200002](https://openairdocs.org/sdr/Y2PA2016022200002.md): Cabin Pressure · malfunctioned · Feb 17, 2016 · N822AA · Amd FALCON20 · Cabin Pressure Control System
  > CREW RECOGNIZED A PRESSURIZATION PROBLEM EARLY, CALLED FOR CHECKLIST FOR CABIN PRESSURE TO HIGH. INITIATED DESCENT, DECLARED EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE WAS SENT TO WORK THE PROBLEM. PERFORMED A VISUAL INSP
- [SDR DJSR20160216001](https://openairdocs.org/sdr/DJSR20160216001.md): Actuator · defective · Feb 16, 2016 · N481FL · Amd FALCON20 · Landing Gear Actuator
  > NR 1 MLG WOULD NOT INDICATE DOWN. PERFORMED EXTENTION PROCEDURE "B". STILL NO DOWNLOCK INDICATION, LANDED WITHOUT INCIDENT.
- [SDR DJSR20160210](https://openairdocs.org/sdr/DJSR20160210.md): Unknown · odor · Feb 10, 2016 · N481FL · Amd FALCON20 · Air Distribution System
  > DURING CLIMB OUT, SMELLED A SUSPICIOUS ODOR AND THERE WAS A LIGHT HAZE. PERFORMED FULL FUNCTIONAL TESTS PF AIRCRAFT'S LIGHTING SYSTEMS, AVIONICS AND INTERIOR ELECTRICAL SYSTEMS. RAN ENGINES WHILE TESTING PRESSURIZATION, HEATING ENVIROMENTAL OPERATION. NO FO

Next page: https://openairdocs.org/model/dassault-breguet-falcon-20/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'FALCON20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/dassault-breguet-falcon-20/reports

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