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 BQVA2009031600001Regulator · malfunctionedNR 2 ENGINE OIL PRESSURE AT BOTTOM OF GREEN ARC ON GAUGE, 60 PSI.SDR 2008FA0000597Support · crackedTHE NR 4 BEARING SUPPORT, PN 305086010, CRACKED CAUSING THE ENGINE TO SEIZE. AT OPERATING TEMPERATURES, THE NR 4 BEARING SUPPORT AND INVESTMENT
CAST MANIFOLD MAY HAVE BECAME LOOSE, PERMITTING RELATIVE MOVEMENT BETWEEN THE PARTS. SB CEF738-72-8060 REPLACES THE SDR DXTA200807253199Indicator · inoperativeON TAKEOFF ROLL NO AIRSPEED INDICATED ON F/O'S INDICATOR. AIRSPEED ON CAPT'S & STBY AIRSPEED CHECKED GOOD. TAKEOFF ABORTED AT 70KTS WITH STILL NO INDICATION ON F/O'S SIDE. TROUBLESHOT TO A FAILED NR 2 ADC. REMOVED FAILED UNIT & INSTALLED OVERHAULED UNIT. ACSDR DXTA200803068Yaw Damper · inoperativeDURING LEVEL FLIGHT, ACCELERATING THROUGH 250KT AT 10,000 FT, THE AC EXPERIENCED A SUDDEN YAW TO THE RT WITH THE TRIM INDICATOR AT ZERO. INSTALLED A NEW YAW DAMPER SVL-86A OPS CHECKED GOOD. ALL WORK DONE IAW F-2000 MM 22-105 22-104SDR DXTA200803023Line · disconnectedUNCOMMANDED SHUTDOWN OF NR 2 ENGINE BY FADEC AFTER STARTUP. TROUBLESHOT TO A DISCONNECTED PS AIR LINE AT THE H2B FADEC. CONNECTED LINE PERFORMED NUMEROUS ENGINE STARTS AND RUNS NO DISCREPANCIES NOTED. ENGINE OPERATIONAL CHECK GOOD. ALL WORK IAW MM 71-002 AND SDR DXTA200803008Actuator · inoperativeNORMAL TRIM SYS FAILED INFLIGHT AND WOULD NOT RE-ENGAGE, (ELEVATOR). REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR WITH A REPAIRED/MODIFIED ASSEMBLY PER MM W/C 27-406, 27-404.SDR DXTA200802995Shroud · contaminatedSTRONG ODOR OF HOT OIL DURING DESCENT. EVALUATED AND FOUND BURNED OIL IN APU BLEED AIR SHROUD. REMOVED APU P/N 3800548-2 S/N P-295 AND INSTALLED REPAIRED UNIT P/N 3800548-2 S/N P-358 (T.T. 3165, CYCLES 3212). RUN UP, LEAK CHECK, AND OPERATIONAL CHECK GOOD. SDR DXTA20082980Trim System · malfunctionedDURING DESCENT AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER (E).SDR DXTA200802980Unknown · multiple failDURING DESCENT, AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER CAS MESSAGE. REPLACED STAB CONTROL RELAYS- 504CH, 505CH, 506CH & 507CH. REPLACED STAB CONTROL PCB'S 502CH & 503CH. OPS CHECKED STAB CONTROL RELAY BOX DUE TO RELAY AND PCB REPLACEMENT. INSPECSDR DXTA20082919Cooling Fan · malfunctionedUPON LANDING, RED TEMP FOR CAPTIANS MFD DISPLAYED. IN ADDITION A SLIGHT SMELL OF ELECTRICAL SMOKE WAS EVIDENT UPON SHUTDOWN OF AVIONICS. T/S FOUND PILOTS MFD COOLING FAN INOP. REMOVED INOP FAM AND INSTALLED A NEW FAN. OPS CHECK GOOD I/A/W DA2000 MM 34-001.
SDR DXTA20082910Switch · out of adjustRED DOOR LIGHT CAME ON DURING T/O ROLL, APPROXIMATELY 100 YRDS AFTER BRAKE RELEASE AND FULL POWER. INSPECTED CONDITION AND ADJUSTMENT OF ALL DOOR SWITCHES AND PROX SENSORS, FOUND BAGGAGE BAY FWD SWITCH (43MV) OUT OF ADJUSTMENT AND STICKING. ADJUSTED AND CLEANSDR DXTA20082881Bulb · burned outWHEN PUTTING THE LANDING GEAR CONTROL HANDLE DOWN, THE LT MAIN (2) GREEN DOWN INDICATORS FAIL TO BOTH LIGHT. THE BOTTOM LT WILL NOT LIGHT CONSISTENTLY AT GEAR EXTENSION UNLESS YOU WIGGLE THE LIGHT. REMOVED AND REPLACED BOTH BULBS OPS CHECKED GOOD. REF: MM SECSDR 2008FA0000071Lanyard · missingACCESS COVER FOR THE EMERGENCY WINDOW HANDLE DOES NOT HAVE A LANYARD WHEN IT IS REMOVED. THE COVER HANGS BY THE WIRING THAT ILLUMINATES IT PUTTING STRESS ON THE SOLDERED CONNECTIONS TO BREAK CAUSING EITHER AN INOPERATIVE EMERGENCY LIGHT OR A SHORT CAUSING MORSDR DXTA200802827Pressure Switch · malfunctionedWHEN MAIN BRAKES ARE RELEASED BRAKE PRESSURE ANNUNICATOR ILLUMINATES, CHECKED LT AND RT SIDE, ONLY ILLUMINATES FOR LT SIDE. LT BRAKE MINELCO RED + RT AILERON MINELCO RED. (M-2B) REMOVED PRESSURE SWITCH ON THE LT SIDE P/N 7G1042 S/N 723. INSTALLED A NEW SWISDR DXTA200802811Pcb · inoperativeINTERCEPTED ILS LOCALIZER WITH AUTOPILOT ENGAGED ABOUT 3 MILES BEFORE GLIDESLOPE INTERCEPT AUTOPILOT ABRUPTLY PITCHED DOWN 4 TO 5 DEGREES THEN UP A FEW DEGREES WITH A SMALL AMOUNT OF BANK. REPLACED 2B10C CARD AND CHECKED IAW A/C SYS MANUAL, COMPLETED IAW MM 22SDR DXTA200802795Circuit Board · damagedBRAKES DO NOT WORK PROGRESSIVELY. THEY GRAB OR RELEASE SUDDENLY WHEN PRESSED OR RELEASED. INSPECTED ALL GEAR UPLOCK SWITCHES WIRING, NO DEFECTS NOTED. CHECKED UPLOCK SWITCHES ADJUSTMENTS AND GEAR UPLOCK LINKAGE, NO DEFECTS NOTED. REPLACED LANDING GEAR CONTROLSDR DXTA200802766Uplock Switch · malfunctionedGEAR SELECTED UP, GEAR RETRACTED NORMALLY, 3 RED DOOR LIGHTS REMAINED ON WITH RED GEAR UNSAFE LIGHT FLASKING. FOUND NLG UPLOCK WITH BROKEN INTERNAL SPRING. R & R NLG UPLOCK WITH MODIFIED UNIT. LEAK, OPS, AND ADJUSTMENT TEST GOOD I/A/W FALCON 2000 MM 32-300SDR DXTA200802763Proximity Sensor · malfunctionedAFTER TAKEOFF AND GEAR HANDLE SELECTED TO THE GEAR RETRACTION POSITION. NOSE GEAR RETRACTION MOVEMENT WAS FELT AND HEARD. 2 RED MAIN GEAR LIGHTS (NO NOSE LIGHT) ALONG WITH A RED FLASHING HANDLE LIGHT OCCURRED. REMOVED AND REPLACED LT & RT MLG PROX SWITCHES SDR DXTA200802752Adc · malfunctionedDURING TAKEOFF, TEN SECONDS AFTER FULL POWER WAS SET (AUTO SLATS) MESSAGE APPEARED. REPLACED ADC-850C AIR DATA COMPUTER NR 1 WITH AN OVERHAULED UNIT PER F2000 MM 34-103. COMPLETED LEAK CHECKS PER F2000 MM 34-100 & FAR 91.411 WITH NO LEAKS NOTED. OPS CHECKEDSDR DXTA200702729Probe · inoperativeRT AUTO SLAT LIGHT AT ROTATION ALONG WITH STALL EYEBROW. NO OTHER ABNORMAL INDICATIONS. STALL EYEBROW INDICATION UNTIL 200 KTS. AUTO SLAT LIGHT WENT OUT 15 MIN INTO FLIGHT. REMOVED LT AOA PROBE AND INSTALLED A MODIFIED AOA PROBE IAW FALCON 2000 AMM 27-813.SDR DXTA200702716Terminal Block · damagedUPON POWER APPLICATION FOR TAKEOFF, TAKEOFF CONFIGURATION ANNUNICATOR ILLUMINATED ACCOMPANIED BY ORAL WARNING. CONFIRMED DISCREPANCY. T/S PROBLEM TO INTERMITTENT GROUND AT JUNCTION BLOCK 4JM. RESEALED ALL PINS. PERFORMED FUNCTIONAL TEST OF TAKE-OFF SAFETIESDR DXTA200702683Engine · failedHAD AN UNCOMMANDED NR 2 ENGINE FAILURE AT FL430. WE OBSERVED A FADEC 2 MWP LIGHT AND THEN AN UNCOMMANDED SHUTDOWN OF THE ENGINE. REPLACED A FAILED RT ENGINE PER THE MM 54-010, 54-104, 54-106, 54-107, 71-000, 71-015 AND THE ENGINE LMM 72-00-00, 72-00-08, 72-70SDR DXTA200702645Landing Gear · malfunctionedGEAR WOULD NOT EXTEND NORMALLY, WITH GEAR HANDLE DOWN, ONLY MAIN GEAR DOORS OPENED. 2 CYCLES SAME RESULT. GEAR CAME DOWN WITH EMERGENCY GEAR HANDLE PULLED. INSP, FAULT CODE 435 PRESENT DURING GEAR SWING. REMOVED LANDING GEAR SELECT HANDLE P/N 307-39. S/N 212SDR DXTA200702632Hydraulic System · reads lowNR 1 HYDRAULIC SYSTEM QUANTITY INDICATED IN THE RED ZONE FOR QUANTITY DURING TAKEOFF RUN. ABORTED TAKEOFF ENSUED AS A RESULT OF LOW HYDRAULIC QUANTITY. SERVICED HYD SYSTEM IAW MM CH 29-112.SDR DXTA200702571Condesor · odorAFTER LANDING AND APU START, VERY STRONG ODOR OF RAW JET FUEL IS COCKPIT AND CABIN. RAN APU. NOTED MUSTY ODOR COMING FROM VENTS. AFTER 2 MINUTES ODOR BEGAN TO DISIPATE. REMOVED AND INSPECTED THE WATER SEPERATOR AND THE WATER SEPERATOR FILTER. NO DISCREPANSDR DXTA200702556Accumulator · leakingDURING CLIMBOUT THE NR 1 HYDRAULIC SYSTEM INDICATION DROPPED TO 10 PERCENT ON QUANTITY AND PRESSURE DROPPED AS WELL. NOTED LEAK FROM LT T/R ACCUMULATOR TO FILTER ASSY. REPAIRED LEAK AND SERVICED SYSTEM 1 RESERVOIR. PERFORMED SYSTEM 1 HYDRAULIC OPERATION TEST WSDR DXTA200702475Unknown · odorBURNING RUBBER ODOR ENTERS COCKPIT DURING CLIMB 17000 TO 19000 FT AND LASTS FOR 30-40 SECONDS THEN DISAPPEARS. NO SMOKE VISIBLE, SEEMS TO ORIGINATE FROM LT SIDE OF COCKPIT IN THE AUDIO PANEL AREA. 09-28-07 VISUALLY INSPECTED DV WINDOW ELECTRICAL CONTACTS, SDR DXTA200702410Computer · malfunctionedAP TRIM FAIL ILLUMINATED WITH (E) DISPLAYED ON PFD. OCCURRED IN CLIMB THROUGH FL400. REPLACED LEFT AND RIGHT FCC-4002 FLIGHT CTRL COMPUTERS I/A/W F2000 MM 34-003. PERFORMED A/P FUNCTIONAL TEST W/ NO DISCREPANCIES NOTED, I/A/W F2000 MM 22-100.SDR DXTA200702351Oven · odorWHITE ODORLESS SMOKE POURS OUT OF THE GALLEY CONVECTIVE OVEN WHEN OPERATING. CLEANED OUT INSIDE OF OVEN. OPERATED AT HIGHEST TEMPERATURE SETTING FOR 15 MINUTES. VERY MINIMAL SMOKE NOTED AFTER CLEANING. IAW F2000 M/M 20-314SDR DXTA200702343Coffeemaker · smokeBURNING SMELL AND SMOKE COMING FROM THE COFFEE POT. ISOLATED COFFEE POT AREA FROM WALL AND CONTINUED WITHOUT FURTHER INSTANCE. REMOVED AND REPLACED WIRE TERMINALS TO COFFEE POT- CHECK WIRES WITH METER WIRES CHECK GOOD AT THIS TIME- INSTALLED SAME COFFEE POT- SDR DXTA200702334Brake · malfunctionedWHEN MAIN A/C BRAKES ARE APPLIED BRAKES WILL GRAB THEN RELEASE, THEN GRAB WHILE BRAKES ARE APPLIED SMOOTHLY. [07-23-07] PERFORMED BRAKE PRESSURE CHECKS AND FOUND NO ABNORMAL PRESSURES. IAW F2000 MM 32-412. FOUND FAULT CODES FOR BSCU NR 1 AND 2 AND FOUND SDR DXTA200702311Circuit Board · inoperativeIN FLIGHT AT FL 430, MASTER CAUTION LIGHT ILLUMINATED, ACCOMPANIED BY AUDIBLE GONG. (FLAP ASYSTEMMETRY) CAUTION LIGHT ILLUMINATED (5) SECONDS LATER FLAP CONTROL CIRCUIT BREAKER IN OVERHEAD C/B PANEL POPPED. LANDED NO FLAP. REPLACED PCB CARD (50WW) WITH A NEW SDR DXTA200702294Unknown · odorINTERMITTENT BURNING ODOR FROM COCKPIT AIR ON GROUND AND DURING CLIMB. [07-12-07] INSPECTED COOLING SYSTEM. NO DEFECTS NOTED. INSPECTED APU INLET. FOUND NUMEROUS CUCADA INSECTS COVERING THE INLET SCREEN. CLEANED APU INLET. RAN COOLING SYSTEM NO FURTHER ODORSDR DXTA200702288Flap System · inoperativeFLAPS DID NOT EXTEND WHEN COMMANDED. TRIED 10, 20, AND 40 DEGREES AND THE FLAPS NEVER MOVED. THE SLATS EXTENDED NORMALLY. [07-12-07] PERFORMED FUNCTION TEST OF SLAT POSITION DETECTORS AND FLAP POSITION MICRO SWITCHES IAW FALCON 2000 M.M. CHAPT 27-802, ALL RSDR DXTA200702250Dau · inoperativeWE GOT THE NO TAKE-OFF AURAL WARNING WITH NO TAKEOFF ANNUCIATE LIGHT ON TAKE OFF. REMOVED AND REPLACED DATA AQUISITION UNIT (DAU-4000) WITH OVERHAULED UNIT. PERFORMED OPS CHECK OF DAV AND TAKEOFF WARNING SYSTEM. OPS CHECK GOOD. WORKSDR DXTA200702230Transducer · malfunctionedWHEN BRAKING AT LOW TAXI SPEEDS THE LT BRAKE RELEASES AND THE AIRCRAFT WILL PULL TO THE RT. PERFORMED FUNCTIONAL CHECK OF ANTI-SKID SYSTEM, BOTH CHANNELS AND BOTH SYSTEMS ARE WORKING IAW M/M 32-414 CHECKED WIRING FROM BOTH BSCU'S TO ALL TRANDUCERS AND SERVO VSDR DXTA200702220Proximity Sensor · inoperativeLANDING GEAR WAS EXTENDED USING ABNORMAL GEAR EXTENSION CHECKLIST BECAUSE, UPON TAKEOFF AT GEAR RETRACTION NEITHER MAIN GEAR CAME UP. REMOVED LT GEAR DOOR PROX SWITCH PN 803682, SN1408 INSTALLED PN 84799031 SN 2047. REMOVED RT GEAR DOOR PROX SWITCH PN 803682SDR DXTA200702216Proximity Sensor · inoperativeRED NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. SELECTED GEAR DOWN AND GEAR EXTENDED NORMALLY. ALL INDICATIONS NORMAL.REMOVED INOP NOSE GEAR UPLOCK DETECTOR AND INSTALLED A NEW UNIT IAW CH 32-600 OF THE MM OPS CHECK GOOD.SDR DXTA200702209Control Unit · intermittentWHEN BRAKING THE AIRCRAFT TO A FULL STOP AT LOW TAXI SPEEDS, LT BRAKE RELEASED AS PRESSURE ON THE BRAKE PEDALS IS LESSENED TO PREVENT NOSE DIP. IS MOST PRONOUNCED WHEN PARKING OR HOLDING SHORT. REMOVED OLD NR 2 BSCU AND REPLACED WITH REPAIRED UNIT. OPERATIONALSDR DXTA200702204Landing Gear · malfunctionedWHEN GEAR HANDLE WAS PUT IN THE DOWN POSITION, NOTHING HAPPENED. (M2B) - PERFORMED FUNCTIONAL TEST OF EXTENSION AND RETRACTION OF LANDING GEARS AND DOORS, LANDING SAFETIES, AND MAIN DOOR PROX SWITCHES AND GEAR ACTUATOR PROX SWITCHES, AND DOOR UP LOCK AND GEAR SDR DXTA200702198Landing Gear · malfunctionedLANDING GEAR WOULD NOT EXTEND AFTER SELECTING GEAR HANDLE DOWN. AFTER APPROXIMATELY 2-3 MIN, MAIN GEAR ANNUNCIATOR ILLUMINATED BUT NOSE GEAR DID NOT EXTEND. USED MANUAL GEAR EXTENSION TO EXTEND NOSE GEAR. CHECKED ALL PROX SWITCHES FOR GAP DIMENSIONS. ACCOMPLISSDR DXTA200702125Warning System · activatedAFTER T/O (3) RED LIGHTS NO GREEN ON GEAR, RED HANDLE FLASHING. PUT GEAR DOWN GOT (3) GREEN LIGHTS, NO RED LIGHTS NO FLASHING HANDLE. [4-27-07] TROUBLESHOT DISCREPANCY TO FAULTY NLG UPLOCK BOX PER CHECK IAW FALCON 2000 MM 32-320. REMOVED AND REPLACED NLG UPLSDR DXTA200702117Warning Light · illuminatedPITCH FELL CAUTION LIGHT ILLUMINATED DURING TAKEOFF AND STAYED ILLUMINATED FOR APPROXIMATELY 3 MINUTES. REPLACED PITCH VARIABLE BELLCRANK WITH A REPAIRED UNIT IN ACCORDANCE WITH F2000 MM 27-318. OPERATIONAL CHECKS GOOD.SDR DXTA200702075Apu · odorAPU GIVES OIL ODOR IN CABIN. NO DIVERSION. REMOVED AND REPLACED APU IAW FALCON 2000 MM 49-00, OPS CHECK APU GOOD.SDR CA070725002Drain Valve · damaged(CAN) THE AIRCRAFT POTABLE WATER SYSTEM WAS DAMAGED DUE TO HAVING THE WATER SYSTEM FULL OF WATER. THEN PARKING THE AIRCRAFT ON THE RAMP FOR 8 HRS AT -14 DEGREES C. WITH NO ADDITIONAL HEAT TO KEEP THE WATER SYSTEM FROM FREEZING. UPON ARRIVING, THE PILOTS REPORSDR DXTA200702012Landing Gear · noisyON TAKEOFF GEAR RETRACTION, LOUD NOISE HEARD FROM NOSE AREA LIKE GEAR DOOR NOT CATCHING OR BINDING SHOOK NOSE OF AIRPLANE. ON GEAR EXTENSION LOUD NOISE THIS TIME GRINDING SOUND LIKE WHEN TWO GEARS NOT MESHING TOGETHER RIGHT. POSITIONED AIRCRAFT IN HANGAR. INSPSDR DXTA200702010Unknown · unknownAFTER TAKEOFF, UPON GEAR RETRACTION, LT MAIN GEAR DOOR LIGHT REMAINED RED. NO NOISE OR VIBRATION TO INDICATE DOOR WAS NOT CLOSED. ALL OTHER GEAR LIGHTS NORMAL. RETURNED TO AIRPORT, LANDED AND RED LIGHT STAYED ON. REMOVED & REPLACED DEFECTIVE LMLG DOOR LATCH WSDR DXTA200702007Pressure Switch · out of toleranceBRAKE PRESS ANNUNCIATOR TRIGGERED T/O CONFIG DURING TAKEOFF BEFORE 50 KTS. TROUBLESHOT BRAKE SYSTEM TO NR 2 SYSTEM BRAKE PRESSUE SWITCH. REMOVED AND REPLACED NR 2 SYSTEM BRAKE PRESSURE SWITCH WITH A (NEW) UNIT IAW MM 32-42-00.SDR UG8A2007PA02OEngine · fodFOD DAMAGE TO LT ENGINE IN FLIGHT. COVER FOR FUEL CAP CAME OFF IN FLIGHT AND WAS INGESTED BY THE ENGINE. ENGINE OPERATION WAS REPORTED NORMAL. REMOVED DAMAGED ENGINE AND INSTALLED A RENTAL ENGINE. AIRCRAFT RETURNED TO SERVICE.SDR DXTA200702001Seal · wornLOUD GRINDING NOISE DURING GEAR DOWN CYCLE. DURING CYCLE, 20 SECOND WARNING LIGHT STARTED FLASHING. 3 GREEN/ NO RED WAS INDICATED APPROXIMATELY 10 SECONDS AFTER 20 SECOND WARNING FLASHER. INSPECTED MLG, MLG DOORS NOSE CONE. NO DEFECTS NOTED. PERFORMED MLG SWIN
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