# Service difficulty reports: Buckeye FALCON

A list on [Buckeye FALCON](https://openairdocs.org/model/buckeye-falcon.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 215 reports

- [SDR EBVR2023021301](https://openairdocs.org/sdr/EBVR2023021301.md): Cable · failed · Feb 10, 2023 · N522EE · Amd FALCON · Powerplant System
  > WHILE LOWERING THE #2 (CENTER) ENGINE FOR ACCESS, THE HOISTING WINCH CABLE SNAPPED CAUSING THE ENGINE TO FALL TO THE GROUND SERIOUSLY ENDANGERING THE TECHNICIANS WORKING TO REMOVE THE ENGINE.
- [SDR Y2PA201812184048](https://openairdocs.org/sdr/Y2PA201812184048.md): Unknown · malfunctioned · Dec 14, 2018 · N827AA · Amd FALCON · Cabin Pressure Control System
  > CREW REPORTED – AIRCRAFT DECOMPRESSED AND LOST ALL CABIN PRESSURE. CREW ON O2. CABIN ALTITUDE CLIMBED TO 15,000 FEET. DECLARED EMERGENCY/RETURNED TO KYIP. USA JET MAINTENANCE AT KYIP PRESSURIZED AIRCRAFT I/A/W DA-20 MM 21-30-05. OPS CHECK WAS GOOD. NO DEF
- [SDR Y2PA2017032200004](https://openairdocs.org/sdr/Y2PA2017032200004.md): Skin · corroded · Mar 22, 2017 · N822AA · Amd FALCON · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON SKIN AT FRAMES 14 AND 15, STRINGER 19R. REPAIRED THE SKIN IAW SRM 51-71-02 AND EA 96-51-02 R1.
- [SDR Y2PA2017032200003](https://openairdocs.org/sdr/Y2PA2017032200003.md): Access Panel · corroded · Mar 22, 2017 · N822AA · Amd FALCON · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON THE MAIN TANK PANEL. REPAIRED IAW DRAWING 57-16146-1.
- [SDR Y2PA2017032200002](https://openairdocs.org/sdr/Y2PA2017032200002.md): Skin · corroded · Mar 22, 2017 · N822AA · Amd FALCON · Fuselage Main, Plate/Skin
  > DURING C-CHECK, FOUND CORROSION ON SKIN AT FRAME 17 BETWEEN STRINGERS 17-19L. REPAIRED THE FRAME IAW DRAWING 53-16157-1.
- [SDR 2012FA0000829](https://openairdocs.org/sdr/2012FA0000829.md): Thrust Washer · misinstalled · Dec 20, 2012 · Amd FALCON · Wheel/Ski/Float
  > ALL MLG WHEEL ASSEMBLIES LOOSE. FOUND THRUST WASHER INSTALLED INCORRECTLY. MLG WHEEL ASSEMBLIES AND BEARINGS WERE REPLACED. THRUST WASHER.
- [SDR Y2PA20120417013](https://openairdocs.org/sdr/Y2PA20120417013.md): Turbine Case · ruptured · Apr 17, 2012 · N811AA · Amd FALCON · Turbine Section
  > AT 14000 FT, NR 1 ENGINE FIRE INDICATION AND HORN ACTUATED. REDUCED THRUST IAW EMERGENCY CHECKLIST, LIGHT EXTINGUISHED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INSPECTION DISCOVERED A HOLE ON PYLON SIDE OF THE ENGINE TURBINE CASING, CAUSING FIRE IND
- [SDR 2012FA0000006](https://openairdocs.org/sdr/2012FA0000006.md): Connector · shorted · Dec 13, 2011 · N111HZ · Amd FALCON · Light System Wiring
  > LIGHT ASSY, UNIT SUPPLIES 28VDC AISLE MARKER LIGHTING AND 6VDC AISLE PATH EMERGENCY LIGHTING. THE LIGHT ASSY ON THIS ACFT WAS MOUNTED AT THE INBD BOTTOM CUT OUT OF THE AFT RT DIVAN ARM REST. THE ARM REST HAD 2 MARKED AREAS, 1 ON FWD FACE OF ARM REST NEAR LIG
- [SDR CA110907004](https://openairdocs.org/sdr/CA110907004.md): Valve · unserviceable · Aug 28, 2011 · Amd FALCON · Pressure Regulator/Outflow Valve
  > (CAN) THE CREW NOTICED AN UNCONTROLABLE OVER PRESSURIZATION IN CRUISE. THEY SET THE SYS TO MANUAL MODE TO CONTROL BUT MANUAL MODE DID NOT WORK ALSO. THEY BEGAN TO DESCEND AND HAD TO SHUTOFF ALL ENGINE BLEED AIR WHICH WOULD ALLOW THE CABIN TO START TO DESCEND
- [SDR CA100921007](https://openairdocs.org/sdr/CA100921007.md): Window · damaged · Sep 9, 2010 · Amd FALCON · Flight Compartment Windows
  > (CAN) WE HAVE REMOVED THE LT COCKPIT WINDOW BECAUSE IT WAS OUT OF TOLERANCE. A DETAILED INSPECTION OF THE PRIMARY STRUCTURE WAS CARRIED OUT AND FOUND CORROSION.
- [SDR Y2PA200909110003](https://openairdocs.org/sdr/Y2PA200909110003.md): Lamp · inoperative · Sep 9, 2009 · N827AA · Amd FALCON · Landing Gear Position and Warning
  > DURING LANDING APPROACH, CREW NOTED RT MLG GREEN DOWN-LOCKED LIGHT NOT ILLUMINATED. EXECUTED MISSED APPROACH, FOLLOWED CHECK PROCEDURE AND DIVERTED. DECLARED EMERGENCY AND LANDED SAFELY WITHOUT INCIDENT. MX IDENTIFIED (2) BURNED OUT LIGHT BULBS FOR RT GEAR
- [SDR 2009FA0000231](https://openairdocs.org/sdr/2009FA0000231.md): Feeder Cable · shorted · Mar 16, 2009 · N273JC · Amd FALCON · Electrical Power System Wiring
  > ON ACFT, ACCOMPLISHING SB 7X-106 DRAFT 1 TITLED "ELECTRICAL POWER-PRIMARY DC GENERATION SYS INSP OF THE RT MAIN FEEDER GENERATOR 2 INCH. THE BLACK BOOT WHICH SURROUNDS THE FWD FEEDER CABLE FEED THROUGH CONNECTION AT FR46LH SIDE WAS FOUND SLIGHTLY MELTED ON THE
- [SDR 2009FA0000097](https://openairdocs.org/sdr/2009FA0000097.md): Power Supply · defective · Feb 18, 2009 · Amd FALCON · Exterior Lighting
  > WRONG PARTS INSIDE STROBE POWER SUPPLY PN 39-44-31: C3, C6, C9 (CAPACITORS), Q5 (TRANSISTOR) AND WIRE COLOR. NO SN ON UNIT; SN ON CUSTOMER PAPERWORK IS 1024088873.
- [SDR 2009FA0000066](https://openairdocs.org/sdr/2009FA0000066.md): Terminal · arced · Jan 10, 2009 · N907SB · Amd FALCON · Electrical Power System Wiring
  > IMPROPER OEM TORQUE OF THE NR2 GENERATOR FEEDER CABLE AT THE FRAME 46 BULKHEAD TERMINAL RESULTED IN ARCING AND DAMAGE TO THE FEEDER CABLE.
- [SDR HAEA200800205](https://openairdocs.org/sdr/HAEA200800205.md): Fire Loop · shorted · Jun 4, 2008 · N221TW · Amd FALCON · Fire Detection
  > AC DEPARTED AND CLIMBED TO 3000 FT MSL. NR1 ENG FIRE WARNING HORN AND LIGHT ACTIVATED. AC DECLARED EMERGENCY AND RETURNED TO DEPARTURE. MAINT FOUND NO EVIDENCE OF FIRE. DISCOVERED NR1 FIRE LOOP SHORTED OUT. REPOSITIONED AND TESTED FIRES SYS WARNING. OPS CHECK
- [SDR J1Q2008F00002](https://openairdocs.org/sdr/J1Q2008F00002.md): Outflow Valve · malfunctioned · Mar 29, 2008 · N724JC · Amd FALCON · Pressure Regulator/Outflow Valve
  > DURING ROUTINE SERVICING AND CLEANING OF OUTFLOW VALVES, (3) PNEUMATIC LINES WERE FOUND SEVERELY DAMAGED AN FLARES DUE TO OVERTIGHTENING. (2) OF THE LINES, PN MY20721-207 AND MY207212-218, ATTACH TO THE LT OUTFLOW VALVE. THE (3RD) LINE PN MY20721-219 ATTACHE
- [SDR DJSR20080226](https://openairdocs.org/sdr/DJSR20080226.md): Mechanism · iced · Feb 26, 2008 · N521FL · Amd FALCON · Landing Gear Door Retract Section
  > NOSE GEAR DOOR WOULD NOT CLOSE IN FLIGHT.
- [SDR J1Q2008F00000](https://openairdocs.org/sdr/J1Q2008F00000.md): Hose · disconnected · Feb 1, 2008 · N724JC · Amd FALCON · Airfoil Anti/De-ice System
  > UPON TROUBLESHOOTING, A PILOT SQUAWK (NO GREEN LIGHT, ON WING ANTI-ICE) IT WAS FOUND THAT THE RT IB DROOP LEADING EDGE ANTI-ICE HOSE HAD COME DISCONNECTED FROM THE IB CONNECTION. THIS RESULTED IN VISIBLE HEAT DAMAGE TO THE SMALL WIRE BUNDLE, DISCOLORATION TO
- [SDR Y2PA200800028](https://openairdocs.org/sdr/Y2PA200800028.md): B-Nut · loose · Jan 11, 2008 · N822AA · Amd FALCON · Engine (Turbine/Turboprop)
  > IN CRUISE NR 1 ENGINE SURGED THEN ROLLED BACK AND FLAMED OUT. CREW REQUESTED IMMEDIATE DESCENT FROM FL350 AND VECTORS TO NEAREST SUITABLE AIRPORT. CREW DECLARED AN EMERGENCY FOR THE NR 1 ENGINE WOULD NOT RELIGHT AND DIVERTED TO MLI. AIRCRAFT LANDED ON SINGL
- [SDR HAEA200700203](https://openairdocs.org/sdr/HAEA200700203.md): Engine · fod · Dec 7, 2007 · N977TW · Amd FALCON · Engine (Turbine/Turboprop)
  > DEPARTED BIS CLIMBING THROUGH 3000 FT, RT ENGINE LOST POWER. CREW REQUESTED VECTOR TO RETURN TO BLOCKS. ON DECENT RT ENGINE POWER WAS AVAILABLE. AIRCRAFT LANDED WITH OUT INCIDENT. RT ENGINE FOD'D DUE TO ICE INGESTION AND REQUIRES ENGINE CHANGE. [CLOSED]
- [SDR HAEA200700201](https://openairdocs.org/sdr/HAEA200700201.md): Frame · corroded · Jul 19, 2007 · N221TW · Amd FALCON · Fuselage Main, Frame
  > DURING MCI INSPECTION FRAME 7 ON THE LT SIDE, DIRECTLY BEHIND AFT EDGE OF PILOTS SIDE WINDOW WAS FOUND TO BE CORRODED IN THE UPPER TUB. ENGINEERING EVALUATED THE CORROSION AND DETERMINED THAT REPAIR WAS NEEDED AND ISSUED AN ENGINEERING INSTRUCTION FOR THE REPA
- [SDR KC82007F00000](https://openairdocs.org/sdr/KC82007F00000.md): Transmitter · malfunctioned · Jul 16, 2007 · N995CK · Amd FALCON · Fuel Indicating System
  > THE LT FUEL TRANSFER PUMP STOPPED TRANSFERING FUEL TO THE LT FEEDER FUEL TANK ON THE PREVIOUS LEG. THE TRANSFER PUMP WAS DEFERRED IAW THE APPROVED MEL. DURING THE NEXT LEG, THE FEEDER FUEL TANK QUANTITY SENDING UNIT STUCK AT THE HIGH INDICATED POSITION. EVE
- [SDR Y2PA200700023](https://openairdocs.org/sdr/Y2PA200700023.md): Cooling Fan · seized · Jun 22, 2007 · N827AA · Amd FALCON · Air Distribution Fan
  > AS AIRCRAFT APPROACHING DESTINATION AIRPORT AND ENTERING RIGHT DOWN WIND FOR RUNWAY 23L, CREW SAW AND SMELLED ELECTRICAL SMOKE COMING FROM TOP OF PANEL ON F/O'S SIDE. CREW DECLARED EMERGENCY AND LANDED ASAP, TAXIED AIRCRAFT OFF RUN WAY, SHUT DOWN AND EVACUATE
- [SDR 042507N220CA](https://openairdocs.org/sdr/042507N220CA.md): Engine · stalled · Apr 25, 2007 · N220CA · Amd FALCON · Engine (Turbine/Turboprop)
  > ON CLIMB-OUT FROM ADS AT FL250, THE NR 2 ENGINE STALLED. THE A/C RETURNED TO ADS. AFTER EXTENSIVE TROUBLESHOOTING THE CAUSE OF PROBLEM WAS NOT FOUND. THE ENGINE WAS RETURNED TO COMPANY THAT WAS LEASED FROM.
- [SDR HAEA200700199](https://openairdocs.org/sdr/HAEA200700199.md): Wire · shorted · Mar 13, 2007 · N232TW · Amd FALCON · Window System Wiring
  > ON TAXI OUT, COPILOTS WINDSHIELD HEAT PRODUCED SMOKE. MAINTENANCE REMOVED WINDOW FACIA AND DISCOVERED SHORTED WIRES. REPAIRED WIRES AND TESTED SYSTEM. OPERATIONS NORMAL. [CLOSED]
- [SDR Y2PA200700022](https://openairdocs.org/sdr/Y2PA200700022.md): Inlet · damaged · Feb 22, 2007 · N827AA · Amd FALCON · Engine Air Intake System
  > WEATHER CLEAR - VFR - CLIMBING THROUGH 8000' CREW HEARD A LOUD NOISE FROM REAR AND FELT AN IMPACT. CREW NOTICED LEFT ENGINE EPR CLIMB AND OIL PRESSURE DECREASING. AFTER CREW CONFIRMED SECONDARY INDICATIONS AN ENGINE SHUTDOWN WAS INITIATED USING APPROVED USA
- [SDR 01172007N220C](https://openairdocs.org/sdr/01172007N220C.md): Engine · malfunctioned · Jan 17, 2007 · N220CA · Amd FALCON · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF AND CLIMBOUT TO FL210 FROM KDAY, THE CREW NOTICED THE OIL PRESSURE INDICATION WAS ERRATIC. CREW NOTIFIED ATC OF SHUT DOWN RIGHT HAND ENGINE AS A PRECAUTIONARY MEASURE. CREW PROCEEDED TO CHANGE DESTINATION TO KTOL. LANDED WITHOUT FURTHER INCIDE
- [SDR HAEA200600197](https://openairdocs.org/sdr/HAEA200600197.md): Anti-Skid Sys · failed · Dec 14, 2006 · N158TW · Amd FALCON · Brake Anti-Skid Section
  > UPON LANDING AT SHV, AIRCRAFT STARTED TO GENTLY VEER LEFT OF CENTERLINE. THE CREW RELEASED THE BRAKES AND TURNED ANTI-SKID OFF. AIRCRAFT CAME TO AN UNEVENTFUL STOP ON THE RUNWAY. INSPECTION REVEALED BOTH LH AND RH MAIN TIRES BLOWN. ANTI-SKID TESTED NORMALLY ON
- [SDR HAEA200600196](https://openairdocs.org/sdr/HAEA200600196.md): Latch · faulty · Dec 6, 2006 · N240TW · Amd FALCON · Landing Gear Position and Warning
  > FALSE LANDING GEAR INDICATION (IN TRANSIT) IN MIDFLIGHT. MAINTENANCE REPLACED DOOR LATCH. PERFORMED GEAR RETRACTION SEVERAL TIMES, OPS CHECK GOOD. [CLOSED]
- [SDR 2007FA0000756](https://openairdocs.org/sdr/2007FA0000756.md): Life Raft · partial inflate · Nov 12, 2006 · N191MC · Amd FALCON · Escape Slide
  > THE LIFE RAFT VACUUM BAG INFLATED DUE TO CYLINDER LEAKAGE BETWEEN THE CYLINDER HEAD AND LIFE RAFT CYLINDER. THE AC WAS CRUISING AT 40,000 FT WHEN THE PILOT HEAR A LOUD POP. UPON INVESTIGATION, THE PILOT HAD DISCOVERED THE LIFE RAFT HAD AN UNCOMMANDED INFLATI
- [SDR HAEA200600195](https://openairdocs.org/sdr/HAEA200600195.md): Relay · inoperative · Sep 28, 2006 · N148TW · Amd FALCON · Engine Starter
  > AFTER NR 1 ENGINE FAILED TO START, CREW REPORTED ELECTRICAL ODOR IN THE REAR COMPARTMENT. MAINTENANCE EN ROUTE. MAINTENANCE FOUND THE START RELAY 6K1 BAD. REPLACED 6K1 RELAY. OPERATIONAL CHECK GOOD.
- [SDR KC82006F00003](https://openairdocs.org/sdr/KC82006F00003.md): Valve · stuck · Jun 13, 2006 · N240CK · Amd FALCON · Cabin Cooling System
  > CABIN WOULD NOT PRESSURIZE AFTER TAKEOFF. FOUND CABIN AIR CONDITIONING VALVE TO BE STUCK IN THE CLOSED POSITION. VALVE WAS SET INT THE OPEN POSITION AND DEFERRED, APPROVED MEL. VALVE WILL BE REPLACED UPON PROCUREMENT OF SERVICEABLE PART. (K)
- [SDR DAT2006F00004](https://openairdocs.org/sdr/DAT2006F00004.md): Engine · leaking · May 5, 2006 · N385AC · Amd FALCON · Engine (Turbine/Turboprop)
  > DURING THE FLIGHT, THE FLIGHT CREW SAW A LOW OIL PRESSURE LIGHT. THE FLIGHT CREW CHECKED THE ENGINE GAUGES AND CONFIRMED IT BY THE LOW OIL PRESSURE GAUGE. THE FLIGHT CREW WENT THROUGH THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE RT ENGINE. THE FLIGHT CREW
- [SDR 5092006N209CA](https://openairdocs.org/sdr/5092006N209CA.md): Engine · shutdown · May 5, 2006 · N209CA · Amd FALCON · Engine (Turbine/Turboprop)
  > A/C DEPARTED TUL BOUND FOR OLS, WHILE CLIMBING THROUGH 22,000 FT, A/C WAS STRUCK BY LIGHTNING. THE NR 1 ENGINE ROLLED BACK AND QUIT. THE NR 1 ENGINE WAS RESTARTED AND THE A/C DIVERTED TO OKC. MX INSPECTED A/C AND FOUND LIGHTNING STRIKE ON WING BELOW NR 1 EN
- [SDR HAEA200600189](https://openairdocs.org/sdr/HAEA200600189.md): Engine · unknown · Apr 24, 2006 · N148TW · Amd FALCON · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED MCI, CLIMBING THROUGH FL200 RT OIL PRESSURE LIGHT ILLUMINATED AND RT OIL PRESSURE READ ZERO. RT ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO COU. LANDED WITHOUT EVENT. MAINTENANCE INSPECTED ENGINE AND FOUND BEE NUT LOOSE ON OIL LINE. TIGHTENED O
- [SDR HAEA200600188](https://openairdocs.org/sdr/HAEA200600188.md): Seal · failed · Mar 20, 2006 · N240TW · Amd FALCON · Turbine Engine Oil System
  > APPROX 50 MINS INTO FLT (FL280) HEARD A LOW RUMBLING NOISE. INSTRUMENTS NORMAL EXCEPT NR 1 ENG OIL PRESSURE DROPPED 50 PSI TO 10 PSI. CONTINUED NORMALLY 30 SEC, THEN RPM BEGIN TO FLUCTUATE BETWEEN 80 & 90%, WITH CONTINUOUS RUMBLING NOISE. RETARDED THROTTLE
- [SDR Y2PA200600007](https://openairdocs.org/sdr/Y2PA200600007.md): Valve · malfunctioned · Mar 3, 2006 · N822AA · Amd FALCON · Fuel Storage
  > DURING CLIMB CREW ENCOUNTERED FUEL ODORS IN COCKPIT THEN AT 1000 FT AGL FUEL MIST DEVELOPED WHEN AIRCRAFT PRESSURIZED. CREW CLOSED ENGINE BLEED AIR, INCREASING CABIN ALTITUDE. CREW DECLARED EMERGENCY WITH TOL TOWER AND ENTERED BASE LEG FOR UNEVENTFUL LANDING
- [SDR CED2006F00012](https://openairdocs.org/sdr/CED2006F00012.md): Engine · fod · Dec 2, 2005 · N207CA · Amd FALCON · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF, THE NR 1 ENGINE STALLED. THE FLIGHT CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT THE NR 1 ENGINE HAD ICE FOD. (K)
- [SDR ZN3R030M](https://openairdocs.org/sdr/ZN3R030M.md): Oil Cooler · misrepaired · Nov 22, 2005 · Amd FALCON · Engine Oil Cooler
  > OIL COOLER 160156-2, SN 23-610C SERIES 2 HAS POSSIBLE UNAPPROVED REPAIR CONSISTING OF A PLUG WELD IN THE MIDDLE OF THE OIL COOLER FINS AND WALL COMPLETELY THRU. CHIEF INSPECTOR NOTIFIED AT REPAIR STATION AND REQUESTED SUP TO BE COMPLETED ON 11/22/05.
- [SDR CED2006F00002](https://openairdocs.org/sdr/CED2006F00002.md): Controller · defective · Nov 2, 2005 · N207CA · Amd FALCON · Cabin Pressure Controller
  > WHEN ENROUTE, THE AIRCRAFT CABIN PRESSURIZATION WARNING LIGHT AND HORN CAME ON. THE FLIGHT CREW RETURNED, WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE PRESSURIZATION SYSTEM AND FOUND THE PRESSURIZATION CONTROLLER TO BE MALFUNCTIONING AND REPLACED THE
- [SDR CED2006F00024](https://openairdocs.org/sdr/CED2006F00024.md): Uplock Switch · inoperative · Sep 1, 2005 · N385AC · Amd FALCON · Landing Gear Position and Warning
  > ON APPROACH THE LANDING GEAR HAD TO BE LOWERED USING PROCEDURE A (EMERGENCY PROCEDURES). MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR2 LANDING GEAR UPLOCK SWITCH INOPERATIVE. REMOVED AND REPLACED UPLOCK SWITCH WITH SERVICEABLE PART. OPS CHECK GOOD.
- [SDR HAEA200500181](https://openairdocs.org/sdr/HAEA200500181.md): Gcu · failed · Aug 14, 2005 · N158TW · Amd FALCON · AC Generation System
  > ENROUTE, AT FL280, BATTERY BUS ANNUNCIATOR LIGHT ILLUMINATED. RESET BUS IAW CHECKLIST AND REDUCED ELECTRICAL LOAD. PROBLEM CORRECTED FOR A FEW MINUTES FOLLOWED BY LOSS OF NR 1 GEN LIGHT. ATTEMPTED RESET OF NR 1 GEN UNSUCCESSFUL. NR 1 GEN WAS SHUT OFF AND E
- [SDR 7272005N234CA](https://openairdocs.org/sdr/7272005N234CA.md): Engine · bird ingestion · Jul 27, 2005 · N234CA · Amd FALCON · Engine (Turbine/Turboprop)
  > ON TAKEOFF FROM NR 1 ENGINE INGESTED A BIRD. THIS OCCURRED AFTER V1. JUST AFTER ROTATION THE NR1 ENGINE QUIT. IT WAS RESTARTED AND THE AIRCRAFT CLIMBED TO THE ASSIGNED ALTITUDE. THE CREW NOTIFIED THE TOWER AND RETURNED TO DEPARTURE. (K)
- [SDR CED2006F00001](https://openairdocs.org/sdr/CED2006F00001.md): Squat Switch · out of adjust · Jun 18, 2005 · N209CA · Amd FALCON · Landing Gear Position and Warning
  > AFTER INITIATING TAKEOFF ROLL THE FLIGHT CREW RECEIVED A CABIN PRESSURIZATION WARNING HORN, THE FLIGHT CREW ABORTED TAKEOFF WITHOUT INCIDENT. MAINTENANCE FOUND A LANDING GEAR SQUAT SWITCH OUT OF ADJUSTMENT. (K)
- [SDR CED2006F00015](https://openairdocs.org/sdr/CED2006F00015.md): Bulb · burned out · Jun 16, 2005 · N217CA · Amd FALCON · Landing Gear Position and Warning
  > ON DECENT, THE FLIGHT CREW DID NOT GET INDICATION THAT THE RT MAIN GEAR WAS DOWN AND LOCKED. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND DIVERTED. THEY HAD THE TOWER CONFIRM THAT THE GEAR WAS DOWN, THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CREW I
- [SDR 632005N217CA](https://openairdocs.org/sdr/632005N217CA.md): Rheostat · burned · Jun 3, 2005 · N217CA · Amd FALCON · Trailing Edge Flap Control System
  > ENROUTE, THE CREW OBSERVED SMOKE FROM CENTER CONSOLE, THE CREW REQUESTED AN EMERGENCY DESCENT AND LANDED. MAINTENANCE FOUND THE RHEOSTAT HAD BURNED INSIDE THE FLAP CONTROL BOX. (K)
- [SDR CED2006F00016](https://openairdocs.org/sdr/CED2006F00016.md): Squat Switch · intermittent · May 18, 2005 · N209CA · Amd FALCON · Landing Gear Position and Warning
  > ON TAKEOFF, THE GEAR HANDLE SAFETY SWITCH WOULD NOT RELEASE THE GEAR TO COME UP. MAINTENANCE CLEANED NOSE SQUAT SWITCH CONNECTOR. SYSTEM OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR FLIGHT. ON TAKEOFF, THE SAME PROBLEM REOCCURRED. AIRCRAFT RETURNED TO
- [SDR 592005N209CA](https://openairdocs.org/sdr/592005N209CA.md): Blade · broken · May 9, 2005 · N209CA · Amd FALCON · Engine (Turbine/Turboprop)
  > WHILE ENROUTE, AIRCRAFT DEVERTED, THE REASON WAS NR1 ENGINE ROLLED BACK. THE CREW USED THE CHECK LIST AND SHUTDOWN THE ENGINE. (K)
- [SDR 2005FA0000627](https://openairdocs.org/sdr/2005FA0000627.md): Line · cracked · Apr 22, 2005 · N200GT · Amd FALCON · Engine Oil Distribution (Airframe Furnished)
  > LOW OIL PRESS IN FLIGHT, PRECAUTIONARY SHUTDOWN PERFORMED. 23 PSI LOWEST READING ON OIL PRESS INDICATOR. OIL PRESS NEVER WENT TO -0- PSI. PRECAUTIONARY SHUTDOWN PERFORMED ON NR2 ENG. DECLARED EMERGENCY. ENG ROTATION WAS NORMAL AFTER SHUTDOWN. OIL QTY INDI
- [SDR 2005FA0000779](https://openairdocs.org/sdr/2005FA0000779.md): Engine · leaking · Apr 12, 2005 · N200GT · Amd FALCON · Engine (Turbine/Turboprop)
  > ENGINE EXPERIENCED LOW OIL PRESSURE IN FLIGHT. PRECAUTIONARY SHUTDOWN PERFORMED. 23 PSI LOWEST READING ON OIL PRESSURE INDICATOR. OIL PRESSURE NEVER WENT TO -0- PSI. NO ABNORMAL VIBRATION EXPERIENCED. PRECAUTIONARY SHUTDOWN PERFORMED ON NR 2 ENGINE. EMER

Next page: https://openairdocs.org/model/buckeye-falcon/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 = 'FALCON'
ORDER BY difficulty_date DESC
```

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

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