C F E CFE-738-1-1B
Service difficulty reports · 158
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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 = 'CFE73811B' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'CFE73811B' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DXTA200702002Acm · odor5 MINUTES BEFORE LANDING CABIN SMELLED OF SMOKE AFTER LANDING, SWITCHED CAB PAC SWITCH TO OFF AND SMOKE DISAPPEARED. NO DIVERT. FOUND FWD ACM SEIZED. R & R FWD ACM, OPS CHECKS GOOD. I/A/W 750 MM 21-51-00.SDR DXTA200701990Adc · inoperativeMACH TRIM LIGHT ILLUMINATED ON PFD. DUPLICATED DISCREPANCY. CLEARED FADEC FAULTS I.A.W. THE FALCON 2000 M.M. 45-000. NR 1 ADC REMOVED AND REPLACED DUE TO PILOT REPORT OF LOSS OF AIRSPEED. SYSTEM OPS CHECKS NORMAL I/A/W THE FALCON 2000 M.M. 34-103.SDR DXTA200701945Adc · malfunctionedIN FLIGHT (AUTO SLATS) LIGHT ILLUMINATED ACCOMANIED BY LOSS OF NR 2 AIRSPEED INDICATOR. MANUALLY PULLED (ADC 2) CIRCUT BREAKER IAW CHECKLIST. DUPLICATED, FOUND NR 2 ADC TO BE DEFECTIVE. REMOVED NR 2 ADC INSTALLED CUSTOMER SUPPLIED OVERHAULED ADC IN NR 2 ADC PSDR DXTA200701918Unknown · odorAPPROX. 5 MIN AFTER DEPARTURE A STRONG ODOR, SIMILAR TO A HAIR DRYER BURNING, NOTICED IN COCKPIT. FLT ATTENDANT REPORTED SAME ODOR IN PAX CABIN AFTER NOTICED IN COCKPIT. ODOR LASTED APPROX 3 MIN. NOTICED AGAIN 4 MIN LATER, NO ODOR DETECTED AFTER LANDING. RAN ASDR DXTA200701916Unknown · unknownON TAKEOFF, MASTER WARNING T/O CONFIG CAME ON ALL CONFIG ITEMS CHECKED AND RESET T/O CONFIG LIGHT STILL COMES ON. ABORTED TAKEOFF. WITH BSCU NR 1 RESET, T/O WARNING SYSTEM OPS CHECK GOOD. BSCU BELIEVED TO BE THE CAUSE OF "T/O CONFIG" ANN. TAKE-OFF WARNING SDR DXTA200701910Unknown · odorDURING CLIMB OUT AROUND 7000 FT THE AIRPLANE FILLED WITH THE ODOR OF WHAT APPEARED TO BE AN ELECTRICAL FIRE. NO SMOKE WAS NOTICED BY ANYONE. THE SMELL DISSIPATED AFTER APPROXIMATELY 2 MINUTES THEN RETURNED INTERMITTENTLY. THE ODOR CAME BACK FAIRLY STRONG WHEN SDR 2007F00017Vane · crackedNR 2 ENG WITH HIGH EGT, BEING INSPECTED DEFECTS WERE FOUND ON THE LPT, SEVERAL CRACKS ON 1 STAGE OF LPT. 3 BOROSCOPES WERE PERFORMED AND NO CORRECTIVE ACTION DONE.SDR DXTA200701880Circuit Card · malfunctionedGEAR FAILED TO RETRACT ON TAKEOFF. WHEN GEAR HANDLE WAS RAISED, WE GOT TWO RED MAIN GEAR LIGHTS AND RT GREEN LIGHT. 10 SECS LATER WE HAD 2 RED MAIN GEAR DOOR LIGHTS, A FLASHING GEAR HANDLE AND 2 MAIN GEAR GREEN LIGHTS. FOLLOWED CHECKLIST AND LOWERED GEAR. THESDR DXTA200601793Hmu · fluctuatesENROUTE FROM EGE TO SNA THE (FUEL 2) LIGHT ILLUMINATED. THE LOW BOOSTER PUMP PRESSURE CHECKLIST WAS APPLIED THE LIGHT REMAINED ILLUMINATED. DUE TO NO INDICATION OF A FUEL LEAKS AND NO CHECKLIST REQUIREMENT TO LAND IMMEDIATELY THE FLIGHT WAS CONTINUED. APPROXIMSDR DXTA200601762Radar · intermittentWEATHER RADAR INTERMITTENT; WX FAULT MESSAGE APPEARS ON BOTH MFD'S AFTER SEVERAL MINUTES OF OF CONITINIOUS OPERATION , TILT CONTROLS APPEARED NOT TO WORK, DISPLAYS SHOWED WHAT APPEARED TO BE GROUND CLUTTER REGARDLESS OF TILT ANGLE SELECTED. T/S TO REMOVED AND SDR DXTA200601721Proximity Sensor · inoperativeDURING GEAR RETRACTION LDG GEAR WOULD NOT RETRACT HEARD LOUD BANGING NOISES GEAR TRIED TO CYCLE ITSELF TO THE UP POSITION APPROXIMATELY 10 TIMES AND EVENTUALLY RETRACTED. 3 RED AND NO GREEN LIGHTS WERE ON DURING RETRACTION ATTEMPTS. EXTENDED LANDING GEAR NORMSDR DXTA200601716Video Monitor · burned outSMOKE COMING FROM THE OVERHEAD LOCATION NEAR SEAT NR1 IN THE CABIN. SMOKE SMELLED LIKE ELECTRICAL BURNING . FOUND FWD MONITOR CIRCUIT BREAKER POPPED IN BAGGAGE COMPARTMENT. NO EMERGENCY DECLARED. CONFIRMED DISCREPANCY. RESET CIRCUIT BREAKER AND OPERATING MONISDR DXTA200601703Unknown · odorSTRONG BURNING ODOR IN COCKPIT, SMELLED ELECTRICALLY FOLLOWED BY LOSS OF NR 2 FMS. LOUDER THAN NORMAL FAN TYPE SOUND IN COCKPIT. RAN APU AND AVIONICS SYSTEM FOR ABOUT 45 MINS TO 1 HR. NO SMELL IN COCKPIT NOTED. 1 FAN SEEMS SLIGHTLY LOUDER. RAN WINDSHIELD HSDR DXTA200601704Proximity Sensor · failedDURING GEAR RETRACTION, RT MAIN GEAR WOULD NOT RETRACT, INDICATED GREEN DOWN WITH RED DOOR LIGHT. THEN LT MAIN GEAR HAD SAME INDICATIONS. 20 SECONDS LATER GEAR HANDLE FLASHED. NOSE GEAR AND DOOR APPARENTLY BEHAVED PROPERLY. LOWERED ALL LDG GEAR IAW ABNORMASDR DXTA200601692Antenna · failedWEATHER RADAR FAILED IN FLIGHT. REMOVED AND INSTALLED AN OVERHAULED RECEIVER/TRANSMITTER ANTENNA AND PERFORMED SATISFACTORY OPS CHECK. REF MM CH. 34-41-00 FOR WORK COMPLETED.SDR DXTA200601697Warning Light · false activationAFTER TAKEOFF, FOLLOWING GEAR RETRACTION. NOSE GEAR DOOR LIGHT (RED), ILLUMINATED, EXTENDED THE GEAR AND RETURNED FOR NORMAL LANDING, NORMAL INDICATIONS UPON GEAR EXTENSION. (3 GREEN NO RED). JACKED AIRCRAFT. GAINED ACCESS TO NOSE LANDING GEAR PROXIMITY SENSOSDR DXTA200601659Engine · fireUPON STARTING THE RT ENGINE, HAD A HUNG START AND ABORTED PER THE CHECKLIST. AT THAT POINT, GROUND CALLED, STATED FLAMES SHOOTING OUT THE BACK OF THE PLANE. ON THE GROUND, THERE WAS A LARGE PUDDLE OF FUEL AND THE BOTTOM RT SIDE OF THE ELEVATOR WAS BLACKENED SDR DXTA200601639Circuit Card · malfunctionedAFTER STARTING BOTH ENGINES AND COMPLETING THE AFTER START CHECKLIST. THE DOORS LIGHT ILLUMINATED. SHORTLY AFTER THAT A STRONG ELECTRICAL ODOR WAS DETECTED IN COCKPIT AND GALLEY. AIRCRAFT WAS SHUTDOWN. UPON FURTHER INSPECTION WARN LT/ESS/B CB WAS TRIPPED. INSPSDR FAA1101001O-Ring · cutWHILE IN CRUISE FLT AT FL 340, NOTICED OIL PRESSURE ON RT ENGINE DROP INTO YELLOW. IT CONTINUED TO DROP 1 PSI EVERY 2 TO 4 MINUTES AND EVENTUALLY ENDED UP IN THE RED AT 17 PSI BEFORE SHUTTING ENGINE DOWN ON THE GROUND. OIL TEMP WAS 67* C, OIL QUANTITY WAS 1 QTSDR 917133O-Ring · cutWHILE IN CRUISE FLT AT FL 340, NOTICED OIL PRESSURE ON RT ENGINE DROP INTO YELLOW. IT CONTINUED TO DROP 1 PSI EVERY 2 TO 4 MINUTES AND EVENTUALLY ENDED UP IN THE RED AT 17 PSI BEFORE SHUTTING ENGINE DOWN ON THE GROUND. OIL TEMP WAS 67 DEGREES C, OIL QUANTITY SDR DXTA200601469Transmitter · faultedAFTER FLAP RETRACTION LOW FUEL ONE AND TWO LIGHTS CAME ON. FOLLOWED BY APU FAULT LIGHT (APU MASTER WAS OFF). CABIN LOST PRESSURE. LOW FUEL LIGHTS WERE INTERMITTENT. DURING OUR DESCENT BACK INTO BTV, OIL PRESSURE GAUGE ON LEFT ENGINE ROLLED DOWN TO 14 PSI. OSDR DXTA200601444Fuel Filter · unknownTAXIING IN, RT ENG SHUTDOWN & RECEIVED FOLLOWING EIED MESSAGE -F2B T2 RANGE FAULT-. DOWNLOADED FADEC'S & SENT TO MCC. PERFORMED 2 STARTS ON NR 2 ENG, BOTH START NORM. RAN ENG AT LOW PWR 5 MINS, OPS CHECKS NORM. GAINED ACCESS TO RT TZ SENSOR, FOUND EXCESSIVSDR DXTA200601422Carbon Seal · failedAPPROX. 1.5 HOURS INTO FLIGHT LT ENGINE OIL PRESSURE GAUGE STARTED SHOWING INTERMITTENT. ON DESCENT OUT OF FL370 OIL PRESSURE STARTED DROPPING SLOWLY, CONTINUED TO MONITOR THEN OIL PRESSURE WENT <30 PSI MASTER CAUTION. REMOVED STARTER CARBON SEAL P/N 3056647SDR DXTA200500721Fadec · malfunctionedDURING NR 2 ENGINE START - INITIALLY EXPERIENCED SURGING NOISE WHICH EVOLVED INTO EXTREMELY VIOLENT VIBRATION RESULTING IN SHAKING ENTIRE A/C AND THEN IT IMMEDIATELY BEGAN RAPID RISE TO YELLOW ARC PRIOR TO MANUAL SHUTDOWN. REPLACED NR 2 B FADEC IAW FALCON 200SDR DXTA200400483Engine · malfunctionedIN FLIGHT AT FL370- NOTICABLE VIBRATION (INTERMITTENTLY), NO WARNING LIGHTS OR INDICATIONS. RIGHT ENGINE ROLLED BACK, NO ABNORMAL INDICATION, IGNITION LIGHT MOMENTARY ILLUMINATION ONLY RIGHT THROTTLE NOT RESPONSIVE DISCENDING THRU APPROX 29000 FT. ITT EXCEEDSDR 2005FA0000238Clamp · looseCLIMBING THROUGH 27,000 FT THE RT GENERATOR WENT OFFLINE, SHORTLY AFTERWARDS, LT GENERATOR WENT OFFLINE, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITH NO FURTHER INCIDENT, INVESTIGATION FOUND A LOOSE CLAMP CONNECTING A BLEED AIR DUCT TO THE CABIN COLD TEMPESDR DXTA200400407Odor · detectedELECTRICAL SMOKE SMELL IN COCKPIT WITH ELECTRICAL POWER ON, WHEN CIRCUIT BREAKER PANEL PUSH TO LIGHT BUTTON WAS USED THE OVERHEAD CIRCUIT BREAKER ON ESSENTIAL BUSS POPPED, STRONGEST SMELL ON LT SIDE. ITEM IS UNDER INVESTIGATION.SDR DXTA200400380Light · inoperativeON APPROACH GEAR SELECTED DOWN LT GEAR INDICATOR INOP, TESTED GEAR LIGHTS AND LT GEAR LIGHTS FAILED TO TEST. ACCOMPLISHED GEAR NOT DOWN CHECKLIST IAW PILOT EMERGENCY PROCEDURES, USED ALTERNATE GEAR EXTENSION CHECKLIST TO LOWER INSURE GEAR DOWN. REPLACED BOTHSDR DXTA200400372Warning Horn · activatedDURING T/O ROLL WITH POWER LEVERS IN T/O FOR APPROXIMATLEY 10-15 SECONDS AND AT APPROXIMATELY 40KNTS (NO TAKE OFF) CONFIG WARNING ACTIVATED REASON FOR WARNING CANNOT BE DETERMINED, CONFIGURATION WAS NORMAL FOR ALL SYSTEMS.- ITEM IS UNDER INVESTIGATION.SDR Y292004F00000Elt · activatedON GOING PROBLEMS WITH OUR ELT COMING ON IN FLIGHT FOR NO APPARENT REASON. THE PILOTS ARE USUALLY ABLE TO RESET FROM COCKPIT. REPLACED THE ELT UNIT 3 TIMES. TROUBLESHOT AND INSPECTED REST OF SYSTEM WITH NO FAULTS FOUND. WOULD LIKE TO KNOW IF THIS IS A PROBSDR DXTA220400317Light · inoperativeON APPROACH LOWERED GEAR HANDLE AND DID NOT RECEIVE GREEN LIGHT, PERFORMED EMERGENCY GEAR EXTENSION AND DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR SWING, FOUND BOTH RT GREEN LIGHTS BURNED OUT, REPLACED BULBS AND SYSDR DXTA200400314Engine · malfunctionedAT FL370 NR 1 ENGINE OIL PRESSURE DROPPED BELOW 25 PSI. PRECAUTIONARY SHUT DOWN NR 1 ENGINE AND DIVERTED TO IA, AIRCRAFT LANDED SAFELY. ITEM IS UNDER INVESTIGATION.SDR 2003FA0001041Door · crackedON POSTFLIGHT INSPECTION A CRACK WAS FOUND ON AUX GEAR DOOR NEAR UPPER RT BOLT HOLE. THERE IS NO EVIDENCE OF IMPACT BY A FOREIGN OBJECT.SDR CW12003F00000Line · crackedWHILE PERFORMING A ROUTINE ENGINE INSPECTION A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FORSDR CW12003F00001Pressure Switch · crackedWHILE PERFORMING A ROUTINE ENGINE INSPECTION A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FORSDR CW12003F00002Pipe · crackedWHILE PERFORMING A ROUTINE ENGINE INSPECTION, A BLEED AIR TAP FOR NACELLE ANTI-ICE PRESSURE SWITCHES WAS FOUND TO BE CRACKED AT THE WELD LOCATION. PROBABLE CAUSE WAS VIBRATION. THIS COULD BE PREVENTED BY INSTALLING SUPPORT BRACKET AND NOTING SPECIFIC AREA FOSDR BTV2002F00000Latch · failedREFUELING DOOR CAME OFF IN FLIGHT, STRIKING RIGHT HORIZONTAL STABILIZER. DOOR LATCH FAILURE.SDR CW12002F00000Air Duct · collapsedCREW REPORTED CABIN COULD NOT WARM UP IN AUTOMATIC MODE, INSPITE OF TEMPERATURE INCREASE ON POTENTIOMETER. UPON EXAMINATION INSIDE OF DUCT PN 721-407 WAS FOUND TO HAVE INSULATION AND INTERIOR MESH COLLASPED RESTRICTING AIR FLOW. CAUSE OF COLLAPSE, UNKNOWN. SDR 20010413CW012Control Rod · separatedMETAL END OF CONTROL ROD IS SEPARATING FROM CARBON FIBER. A MOVEMENT OF .003 IN WAS OBSERVED DURING OPERATION OF SYSTEM DURING C INSPECTION PART SENT FOR EVALUATION.SDR 20001129SH010Seal · separatedLP FORWARD STATIC SEAL HAD INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND STAGE 2 HPT ROTOR DISC AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER SB CFE 738-A72-8041. (X)SDR 20001129SH011Seal · separatedLP FORWARD STATIC SEAL HAD INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND STAGE 2 HPT ROTOR DISC AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER SB CFE 738-A72-8041. (X)SDR 20001129SH012Seal · separatedLP FORWARD STATIC SEAL HAD INSUFFICCIENT CLEARANCE BETWEEN THE SEAL AND STAGE 2 HPT ROTOR DISC AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER SB CFE 738-A72-8041. (X)SDR 20001129SH013Seal · separatedLP FORWARD STATIC SEAL HAD INSUFFICCIENT CLEARANCE BETWEEN THE SEAL AND STAGE 2 HPT ROTOR DISC AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER SB CFE 738-A72-8041. (X)SDR 20000831SH022Seal · separatedLP FORWARD STATIC SEAL HAD INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER CFE FIELD ENGINEERING INSTRUCTION NR CFE 738-FESDR 20000831SH023Seal · separatedLP FWD STATIC SEAL HAD INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER CFE FIELD ENGINEERING INSTRUCTION NR CFE 738-FEI-00SDR 20000907SH027Seal · separatedLP FORWARD STATIC SEAL HAS INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE. INSPECTION PER DFE FIELD ENGINEERING INSTRUCTIONS NR CFE 738SDR 20000907SH028Seal · separatedLP FORWARD STATIC SEAL HAS INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE. INSPECTION PER DFE FIELD ENGINEERING INSTRUCTIONS NR CFE 738SDR 20000907SH029Seal · separatedLP FORWARD STATIC SEAL HAS INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER CFE FIELD ENGINEERING INSTRUCTIONS NR CFE 738-FSDR 20000907SH030Seal · separatedLP FORWARD STATIC SEAL HAS INSUFFICIENT CLEARANCE BETWEEN THE SEAL AND THE STAGE 2 HPT ROTOR DISK AFT FACE. POSSIBLE CAUSE IS THE SEPARATION OF THE 2-PIECE STATOR SEAL. PROBLEM FOUND BY BORESCOPE INSPECTION PER CFE FIELD ENGINEERING INSTRUCTIONS NR CFE 738-FSDR 20000717SH001Engine · failedFLL - AFTER TAKEOFF, CREW SELECTED GEAR UP. CREW HEARD A LOUD BANG AND THE RT ENGINE HAD AN UNCOMMANDED SHUT DOWN, CREW LANDED AIRCRAFT BACK AT FLL AND UPON POST-FLIGHT, DETERMINED ENGINE HAD AN UNCONTAINED FAILURE . FURTHER INVESTIGATION REVEALED ENGINE COR
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