# Service difficulty reports: GE CF700 series

A list on [GE CF700 series](https://openairdocs.org/engine/ge-cf700-series.md).

Newest first. General aviation reporting is voluntary.

- [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 KC8AN998CK](https://openairdocs.org/sdr/KC8AN998CK.md): Door Frame · cracked · Nov 6, 2009 · N998CK · Amd FALCON20 · Cargo/Baggage Doors
  > DURING THE AIRCRAFT SCHEDULED INSPECTION, THE VISUAL INSPECTION OF THE CARGO DOOR STRUCTURE REVEALED CRACKS IN THE LOWER FORMERS AT FRAMES 11, 12 AND 13. THE CRACKED FORMERS AND ATTACH CLIPS WHERE REPLACED. FAA FORM 337 COMPLETED FOR THIS REPAIR.
- [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 Y2PA080015](https://openairdocs.org/sdr/Y2PA080015.md): Engine · flamed out · Jun 4, 2008 · N823AA · Amd FALCOND · Engine (Turbine/Turboprop)
  > CREW REPORTED, DIVERTED AROUND WEATHER AT FL350 WITH ENGINE ANTI-ICE ON. WHEN ACFT CLEARED WEATHER STILL AT FL360 CRUISING M.68 TEMP ON RAT -25, TURNED NR2 ENG ANTI-ICE OFF AND NR 2 ENG FLAMED OUT. ACFT BEGAN DESCENT TO FL220, WHEN IN RELIGHT ENVELOPE TRIED
- [SDR SIMA200802105](https://openairdocs.org/sdr/SIMA200802105.md): Blades · damaged · Jan 19, 2008 · N511AE · Cndair CL6002C10 · Turbine Engine Compressor Section
  > ON FLIGHT 3714, CREW REPORTED IN CRUISE FLT ENGINE 1 N1 VIB IND STARTED TO CLIMB AND THEN WENT INTO AMBER AT 1.9 CREW REDUCED POWER AND AT FIRST VIB IND WENT DOWN. IT THEN STARTED TO CLIMB AGAIN AND COULD BE FELT IN MAIN CABIN. CREW THEN DECLARED AN EMERGENC
- [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 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 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 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 2005FA0001280](https://openairdocs.org/sdr/2005FA0001280.md): Shutoff Valve · intermittent · Aug 29, 2005 · N312K · Amd FALCONF · Air Distribution System
  > INSTALLED O/H VALVE. PERFORMED LEAK CHECKS OF VALVE WITH NO DEFECTS NOTED. AC NOTED LOW AIRFLOW ON GROUND. OPS CHECKED PRESSURIZATION ON GROUND AND FOUND THAT AC WOULD NOT PRESSURIZE. TROUBLESHOT VALVE AND DETERMINED THAT THE VALVE INSTALLED WAS MALFUNCTIO
- [SDR 2006FA0000178](https://openairdocs.org/sdr/2006FA0000178.md): Line · chafed · Jan 24, 2005 · N20NY · Amd FALCON · Hydraulic System, Main
  > WHILE COMPLAYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICKNESS LINES REPLACED. (K)
- [SDR 2006FA0000179](https://openairdocs.org/sdr/2006FA0000179.md): Line · chafed · Jan 24, 2005 · N20NY · Amd FALCON · Hydraulic System, Main
  > WHILE COMPLYING WITH SB, FOUND 2 HYDRAULIC LINES PN MY20751107 AND MY20751207 CHAFED 20 PERCENT OF WALL THICHNESS LINES REPLACED. (K)
- [SDR KC82005F00005](https://openairdocs.org/sdr/KC82005F00005.md): Control Panel · stuck · Nov 12, 2004 · N192CK · Amd FALCON20 · Aileron Tab Control System
  > WHEN PILOT ACTIVATED THE AILERON TRIM, THE TRIM CONTROL STUCK AND RAN TOWARDS FULL TRAVEL AND POPED CIRCUIT BREAKER. FOUND AILERON TRIM CONTROL STUCK ON IN THE TRIM CONTROL PANEL. REPLACED TRIM CONTROL PANEL WITH SERVICEABLE TRIM CONTROL PANEL. ALL WORK PER
- [SDR Y2PA04021](https://openairdocs.org/sdr/Y2PA04021.md): Garlock Seal · leaking · Aug 28, 2004 · N822AA · Amd FALCON · Turbine Engine Oil System
  > NR 2 ENGNE OIL PRESSURE BECAME ERRATIC ALL OTHER GAUGED INDICATED NORMAL. OIL PRESSURE GAUGE THEN DROPPED FOLLOWED BY 'OIL P' LIGHT. SHUTDOWN NR 2 ENGINE IMMEDIATELY, REFERRED TO EMERGENCY CHECKLIST PG E2. DECLARED EMERGENCY AND DIVERTED TO RDU. AIRCRAFT LA
- [SDR HAEA200400156](https://openairdocs.org/sdr/HAEA200400156.md): Indicator · sluggish · Jul 13, 2004 · N314TW · Amd FALCON20 · Airspeed/Mach Indicator
  > ON DEPARTURE FROM ADS CAPTAINS AIRSPEED INDICATOR HAS 30-45 KNOT SPLIT FROM CO-PILOTS AIRSPEED INDICATOR. AIRCRAFT RETURNED TO ADS FOR MAINTENANCE. MAINTENANCE REPLACED CAPTAINS AIRSPEED INDICATOR. OPS TESTS GOOD. (CLOSED)
- [SDR HAEA151](https://openairdocs.org/sdr/HAEA151.md): Arm · binding · Jun 29, 2004 · N295TW · Amd FALCON · Landing Gear Door Retract Section
  > ON DEPARTURE, GEAR DOORS FAILED TO RETRACT AFTER GEAR RETRACTION. AIRCRAFT DIVERTED FOR MAINTENANCE. CLEANED AND LUBRICATED EXTENSION ARM, GEAR SWING. OPS CHECK GOOD.
- [SDR HAEA150](https://openairdocs.org/sdr/HAEA150.md): Tire · blew out · Jun 27, 2004 · N221TW · Amd FALCON · Tire
  > AIRCRAFT RT IB MAIN TIRE BLEW OUT ON TAKEOFF. AIRCRAFT DIVERTED. AIRCRAFT LANDED, NO INCIDENT.
- [SDR 00139](https://openairdocs.org/sdr/00139.md): Squat Switch · out of rig · May 13, 2004 · N204TW · Amd FALCON · Landing Gear Position and Warning
  > PILOT REPORTED CABIN WOULD NOT PRESSURIZE. CABIN LIGHT CAME ON, RETURN TO DEPARTURE AIRPORT ADS FOR MAINTENANCE. MAINTENANCE FOUND SQUAT SWITCH ON RT MLG OUT OF RIG, ADJUSTED AND PERFORMED OP CHECKS, AIRCRAFT RETURNED TO SERVICE. (CLOSED)
- [SDR KC82004F00001](https://openairdocs.org/sdr/KC82004F00001.md): Windshield · cracked · Apr 26, 2004 · N70CK · Amd FALCON20 · Flight Compartment Windows
  > CAPTAINS SIDE WINDSHIELD INNER LAMINATE CRACKED DUE TO INNER HEATING ELEMENTS SHORTING. WINDSHIELD WAS REPLACED WITH NEW WINDSHIELD IAW MM.
- [SDR Y2PA04008](https://openairdocs.org/sdr/Y2PA04008.md): Wheel · vibration · Apr 5, 2004 · N811AA · Amd FALCOND · Wheel/Ski/Float
  > 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 FACILITIES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. EMERGENCY WAS CANCELLED BY
- [SDR 00118](https://openairdocs.org/sdr/00118.md): Wire · chafed · Oct 17, 2003 · N232TW · Amd FALCON · Electrical Power System Wiring
  > PILOT REPORTED AFTER DEPARTURE FROM AMA BOTH GENERATORS WENT OFF LINE AND SMOKE IN COCKPIT, RETURNED TO AMA UNEVENTFUL LANDING. MAINTENANCE FOUND POWER WIRE TO LT RAIN REPELLENT SWITCH CHAFING AIRFRAME, REPOSITION AND INSULATE WIRE AT CONNECTOR, AIRCRAFT RAN A
- [SDR GXP2003F00000](https://openairdocs.org/sdr/GXP2003F00000.md): Uplock Switch · dirty · May 5, 2003 · N174GA · Amd FALCON · Landing Gear Position and Warning
  > AIRCRAFT RETURNED TO AIRPORT, AFTER TAKEOFF LANDING GEAR DOOR WILL NOT CLOSE AFTER GEARS WERE RETRACTED. CLEANED ALL LANDING GEAR UPLOCK SWITCHES, 3G SWITCH AND RESEATED 6G RELAY. OPS CHECKED LANDING GEAR WITH HYD MULE. NO DEFECTS NOTED OPS CHECKED GOOD.
- [SDR GXP2003F00001](https://openairdocs.org/sdr/GXP2003F00001.md): Controller · malfunctioned · Apr 24, 2003 · N618GA · Amd FALCOND · Cabin Pressure Controller
  > AIRCRAFT RETURNED BACK TO JVY (IN) AFTER TAKEOFF DUE TO PRESSURIZATION, INOPERATIVE. AIRCRAFT DOWN DUE TO PARTS ON ORDER.
- [SDR 00081](https://openairdocs.org/sdr/00081.md): Landing Gear · inoperative · Feb 26, 2003 · N204TW · Amd FALCON · Main Landing Gear
  > PILOT REPORTED GEAR WOULD NOT COME UP AFTER TAKE-OFF FROM, RETURNED TO DEPARTURE AIRPORT FOR MAINTENANCE. WILL UPDATE AFTER MAINTENANCE.
- [SDR 00082](https://openairdocs.org/sdr/00082.md): Door · inoperative · Feb 24, 2003 · N158TW · Amd FALCON · Landing Gear Door Retract Section
  > AIRCRAFT DEPARTED, PILOT REPORTED GEAR DOORS DID NOT FULLY CLOSE, DIVERTED FOR MAINTENANCE. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS SYSTEM CHECKED GOOD.
- [SDR KC82003F00001](https://openairdocs.org/sdr/KC82003F00001.md): Connector · loose · Feb 10, 2003 · N980R · Amd FALCON20 · Directional Gyro and Indicating System
  > CREW REPORTED (NO PITCH FUNCTION ON CAPTAINS ADI). FOUND CONNECTOR ON THE PILOTS FLIGHT DIRECTOR INDICATOR LOOSE. CLEANED DEBRIS FROM THREADED END OF CONNECTOR AND RESECURED CONNECTOR. MANEUVERED VERTICAL GYRO FROM MOUNTED PLATFORM AND VERIFIED PITCH AND RO
- [SDR 00075](https://openairdocs.org/sdr/00075.md): Switch · inoperative · Jan 29, 2003 · N165TW · Amd FALCON · Landing Gear Position and Warning
  > PILOT REPORTED NO DOWN LOCK INDICATION FOR THE LEFT MAIN GEAR WHILE ON APPROACH, DECLARED EMERGENCY AND LANDED DTW WITHOUT INCIDENT. WILL UPDATE THIS REPORT AFTER MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LT MLG DOWN LOCK SWITCH. OPERATIONAL CHECK GOOD.
- [SDR 00074](https://openairdocs.org/sdr/00074.md): Switch · dirty · Jan 23, 2003 · N165TW · Amd FALCON · Door Warning System
  > PILOT REPORTED AFTER DEPARTURE FROM BHM CLIMBING THRU 5000 FT DOOR LIGHT WARNING CAME ON, LEVELED OFF AT 5000 FT REDUCED POWER LIGHT WENT OUT, RETURN TO DEPARTURE AIRPORT. MAINTENANCE CLEANED DOOR LIGHT SWITCH AND OPS CHECK GOOD. AIRCRAFT RETURN TO SERVICE.
- [SDR 00070](https://openairdocs.org/sdr/00070.md): Switch · failed · Jan 10, 2003 · N977TW · Amd FALCON · Landing Gear Position and Warning
  > PILOT REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER DEPARTURE, RETURNED FOR MAINTENANCE. MAINTENANCE ADJUSTED MICROSWITCH AND SWUNG GEAR CK GOOD. AIRCRAFT DEPARTED GEAR WOULD NOT RETRACT, RETURN TO DEPARTURE AIRPORT, MAINTENANCE R/R 17G1 MICROSWITCH PERF
- [SDR Y2PA02032](https://openairdocs.org/sdr/Y2PA02032.md): Boot · failed · Dec 20, 2002 · N821AA · Amd FALCOND · Humidity Control System
  > UNABLE TO MAINTAIN CABIN PRESS AT FL 290 W/O FLOOR HEAT AT MID RANGE, CABIN HEAT AT 75 PERCENT DEFLECTION AND N1 AT 93 PERCENT RPM. COPILOTS SIDE PANEL HOT TO TOUCH. COPILOT FLOOR HEAT, HOT AND METAL PARTS UNDER COPILOTS INSTR PNL HOT TO TOUCH. SMOKE TRACES
- [SDR A8J2003F00000](https://openairdocs.org/sdr/A8J2003F00000.md): Drive Shaft · failed · Dec 13, 2002 · N300CV · Amd FALCON · Starter-Generator
  > HAS SHEARED TWO SHAFTS ON TWO DIFFERENT ENGINES WITH APPROXIMATELY 30 HOURS WHEN OCCURENCE OCCURED. WE PURCHASED AN OX UNIT FROM THE SAME COMPANY THIS LAST TIME THE FAILURE OCCURED AND LOOKING AT THE PAPERWORK ON SN KK-81 (OX UNIT) IT SUBSEQUENTLY HAS SHEARED
- [SDR GXP2002F00004](https://openairdocs.org/sdr/GXP2002F00004.md): Packing · leaking · Jun 11, 2002 · N183GA · Amd FALCON20 · Hydraulic System, Main
  > LOSING HYDRAULIC FLUID FROM SYSTEM 2. REMOVED AND REPLACED PACKING ON NR 2 ENGINE HYDRAULIC PUMP. SAFETIED ALL CONNECTIONS AND FILLED HYDRAULIC SYSTEM RESERVOIR NR 1 AND NR 2. STARTED NR 2 ENGINE AND LET STABILIZE. HYDRAULIC PRESSURE GOOD AND RESERVOIR NR
- [SDR UVV2002F00000](https://openairdocs.org/sdr/UVV2002F00000.md): Panel · corroded · Apr 19, 2002 · N910BH · Rkwell NA26580 · Wing, Plate/Skin
  > FOUND OVER FLAP PANEL UNDERSIDE CORRODED COMPLETELY THROUGH SKIN TO HONEYCOMB SUBSTRUCTURE. AREA NOT READILY INSPECTABLE DUE TO VELCRO APPLIED OVER AREA TO ACT AS CHAFE STRIPS FOR FLAP UPPER SURFACE. RECOMMEND CLOSE VISUAL INSPECTION OF AREA DURING 150 HOUR
- [SDR HAEA0008](https://openairdocs.org/sdr/HAEA0008.md): Landing Gear · intermittent · Jan 3, 2002 · N204TW · Amd FALCON · Landing Gear Retraction/Extension System
  > GEAR DOOR WOULD NOT INDICATE UP. AIRCRAFT FERRIED TO ADS FOR MAINTENANCE. AIRCRAFT JACKED AND GEAR SWUNG COULD NOT DUPLICATE PROBLEM AIRCRAFT RETURNED TO SERVICE.
- [SDR 00004](https://openairdocs.org/sdr/00004.md): Engine · flamed out · Oct 16, 2001 · N232TW · Amd FALCON · Engine (Turbine/Turboprop)
  > DURING CRUISE, LT ENGINE FLAME-OUT AT FLT LEVEL 390. DESCENT TO FL 260, RELIGHT NORMAL & ALL INDICATIONS NORMAL. NO FURTHER PROBLEM.
- [SDR QY52001F00000](https://openairdocs.org/sdr/QY52001F00000.md): Switch · damaged · Sep 26, 2001 · N20NY · Amd FALCON · Landing Gear Door Actuator
  > 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 ACT
- [SDR GXPA0119](https://openairdocs.org/sdr/GXPA0119.md): Tube · faulty · Aug 31, 2001 · N619GA · Amd FALCOND · Engine (Turbine/Turboprop)
  > NR 1 ENGINE MAKING 1-44 EPR. MAXIMUM NEEDED 1-54 FOR TAKEOFF. EGT WAS 690 DEGREES. REPLACED SHORT TUBE ON ENGINE TO AIRFRAME. OPS CHECKED GOOD AT OUTSIDE TEMPERATURE 21 DEGREES. CALL FOR 1-54 EPR, MAKES 1-59 EPR.
- [SDR 2001F00283](https://openairdocs.org/sdr/2001F00283.md): Engine · malfunctioned · Aug 9, 2001 · N209CA · Amd FALCON · Engine (Turbine/Turboprop)
  > WHILE ON DESCENT TO KLRD FROM MMQT, WHILE PASSING FL180 A SMALL REDUCTION IN POWER WAS MADE. THE NR 1 ENGINE ROLLED BACK. AFTER 15-30 SECONDS THE NR 1 ENGINE SPOOLED BACK UP. THE AIRCRAFT CONTINUED ON TO KLRD WITH NO OTHER PROBLEMS AND MADE A NORMAL LANDING
- [SDR QY52001F00001](https://openairdocs.org/sdr/QY52001F00001.md): Fitting · corroded · Jun 29, 2001 · N20NY · Amd FALCON · Fuel Storage
  > 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.
- [SDR 20010514CW006](https://openairdocs.org/sdr/20010514CW006.md): Skin · corroded · Apr 27, 2001 · N731G · Amd FALCON20 · Fuselage Main, Plate/Skin
  > LEFT HAND NR 2 AND RIGHT HAND NR 1 CABIN WINDOW MOUNTING AREA AND INNER SKIN SHOWED CORROSION BEYOND SRM LIMITS. THE REMAINING WINDOW MOUNTING AREAS SHOWED CORROSION BUT WERE WITHIN LIMITS.
- [SDR GXPA0106](https://openairdocs.org/sdr/GXPA0106.md): Control Unit · malfunctioned · Mar 6, 2001 · N183GA · Amd FALCON20 · Cabin Pressure Control System
  > AIRCRAFT RETURNED TO AIRPORT DUE TO PRESSURIZATION PROBLEM. REMOVED AND REPLACED CABIN PRESSURE CONTROLER.
- [SDR GXPA0105](https://openairdocs.org/sdr/GXPA0105.md): Connector · dirty · Mar 1, 2001 · N613GA · Amd FALCON · Landing Gear Position and Warning
  > AIRCRAFT RETURNED TO AIRPORT DUE TO GEAR DOORS WOULD NOT CLOSE AFTER TAKE OFF. CORRECTIVE ACTION: CLEANED ALL LANDING GEAR SWITCH PLUGS AND PERFORMED RETRACTION TEST NUMEROUS TIMES.
- [SDR GXPA0103](https://openairdocs.org/sdr/GXPA0103.md): Control Unit · malfunctioned · Feb 20, 2001 · N613GA · Amd FALCON · Landing Gear Door Retract Section
  > AIRCRAFT MADE A RETURN LANDING, DUE TO GEAR DOORS WOULD NOT RETRACT AND CLOSE DURING LANDING GEAR RETRACTION. CORRECTIVE ACTION: EXTENDED AND RETRACTED GEAR DOOR, RECEIVED PROPER INDICATION FOR BOTH POSITIONS, VISUALLY INSPECTED ALL THREE GEAR AND SURROUNDIN
- [SDR GXPA0101](https://openairdocs.org/sdr/GXPA0101.md): Engine · stalled · Feb 2, 2001 · N613GA · Amd FALCON · Engine (Turbine/Turboprop)
  > AIRCRAFT DIVERTED DUE TO NR 2 ENGINE START COMPRESSOR STALLING AT 80 PERCENT N1. ICE AND FOD CAUSE. ENGINE REPLACED.
- [SDR 20010411CW015](https://openairdocs.org/sdr/20010411CW015.md): Battery · improper part · Jan 3, 2001 · N312K · Amd FALCON20 · Battery Overheat Warning System
  > IMPROPER TEMPERATURE PROBE INSTALLED FOR THIS PN BATTERY. TEMERATURE PROBES HAVE BEEN ROUTINELY INSTALLED WITHOUT SPECIFIC APPROVAL TO DO SO.

## 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 engine_model_key = 'CF700'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf700-series/reports

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