GE CF6-50 series
Service difficulty reports · 201
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 = 'CF650' 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 = 'CF650' 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 CNM2008F00002Compressor · stalledDURING CRUISE AT FL 300 NR 3 ENG COMPRESSOR STALLED N1 DROPPED TO APPROXIMATELY 70 PERCENT VIBRATION FELT IN NR 3 THROTTLE/ FUEL LEVEL/ FIRE HANDLE AS WELL AS AIRFRAME. (K)SDR UIE2008F00036None · noneATB. BOTH AUTOPILOTS A AND B WILL NOT ENGAGE (BOTH TESTED OK ON GROUND). A/P A AND B PITCH AND ROLL COMPUTERS, ASTU AND M AND LU BITE CHECK ALL OK. FLT CTL HYD POWER SHUT OFF SWITCHES ALL CHECKED IN ON POSITION. A/P ACCESS BOXES INSTALLATION SECURED. MSP ELECSDR ARW2008F00000Indicator · failedF/O ALTIMETER FAILED IN TAKEOFF; WORKED OK IN CLIMB AND CRUISE. REMOVED AND REPLACED ALTIMETER INDICATOR IAW MM 34-02-01; PERFORMED OPS CHECK IAW M34-12-00; FOUND NORMAL. (K)SDR P5CA0701523Filter · cloggedON TAKEOFF, NR 2 ENGINE FLAMED OUT. ENGINE HAD SUCCESSFUL RESTART. INLET AND EXHAUST FEELING AND COMPRESSOR CHECKED SATIS NR 2 FUEL TANK WAS SUMPED THEN REPLACED NR 2 ENGINE FUEL FILTER. NO FURTHER PROBLEMS.SDR CNMA20070008Drive Assy · malfunctionedAT 10,000 MSL AIRCRAFT SLOWED TO 250 KTS, AP OUT OF TRIM LIGHT ILLUMINATED GREATER THAN 5 SECONDS. AUTOPILOT DECOUPLED AND AC PITCHED NOSE DOWN EXCESSIVELY. TRIM SWITCHES FROM BOTH CONTROL COLUMNS DID MOVE LONG TRIM HANDLES BUT STAB INDICATOR REMAINED FIXED SDR 0406200701Unknown · unknownON TAKEOFF ROLL, TAKEOFF WARNING HORN SOUNDED. LARGE SHUTTER CAUSED BY ROUGH RUNWAY OCCURRED. COULD NOT DUPLICATE WITH AIRCRAFT STOPPED. RETURNED TO RAMP. ACCOMPLISH TO AURAL WARNING TEST IAW MM 31-26-00. ALL OPS NORMAL, COULD NOT DUPLICATE. ACCOMPLISHED SDR UIEA200700203Skin · delaminatedRT WING O/B MID FLAP UPPER SURFACE LEADING EDGE AT WING STA 1000.00 TO WING STA 995.00 IS DELAMINATED 2.5IN WIDE 4.5IN LONG. REPAIRED RT WING O/B MID FLAP UPPER SURFACE DELAMINATION IAW SRM 51-10-01 EO4757A353.SDR 0312200701Hose · wornAFTER TAKEOFF, WITH LG RETRACTED, OBSERVED HYDRAULIC SYSTEM NR 4 LOOSE WITH BOTH NR 4 EDP, ADR LOW PRESSURE ON. AOM 2-2-55 AND 2-2-59 FOLLOWED, RETURNED TO DEPARTURE.FOUND LT WING GEAR DOOR ACTUATOR HYDRAULIC LINE WORN. REMOVED AND REPLACED HYDRAULIC LINE, SDR 2007FA0000228Sensor · malfunctionedDURING TAKEOFF, THE LANDING GEAR HANDLE WILL NOT GO TO UP OR RETRACT POSITION. AIRCRAFT RETURNED TO BASE. PERFORMED TROUBLESHOOTING ON THE LANDING GEAR SYSTEM AND FOUND THAT LT WING GEAR TRUCK ROTATION SENSOR AT FAULT. ADJUSTED THE LT WING GEAR TRUCK ROTATISDR UIEA200700130Strap · crackedCRACKS FOUND ON BS 800 LT STRAP AND INNER CHORD AT NR 2 MAIN ENTRY DOOR. REPAIRED ACCOMPLISHED IAW SR ID NR 1-289052431 AND FAA FORM 8100-9.SDR 2006FA0001184Spring · brokenCOMPRESSOR DISCHARGE PRESSURE RESTORING SPRING P/N 3018-248 HAS FRACTURED CLOSE TO THE SPRING SEAT 9.SDR 2006FA0001185Spring · brokenCOMPRESSOR DISCHARGE PRESSURE RESTORING SPRING P/N 3018-248 HAS FRACTURED CLOSE TO THE SPRING SEAT 9.SDR 1030200604Unknown · smokeAFTER T/O - 10-25-06) + 20 MINUTES FL 250, CAPTAIN NOTICE SMOKE (LIGHT) AROUND CAPTAINS INSTRUMENT PANEL BELOW GLARE SHIELD. SMOKE DISSIPATED. FOUND THE FOLLOWING CB OPEN P4 PANEL, HEATER DRAIN MAST AIR, HEATER DRAIN MAST GRD. SERVICE. CONTINUE FLIGHT WITHOSDR EIA2006092Indication Sys · unknownRETURNED TO BLOCKS DUE TO NR 2 ENG LOSS OF N2 INDICATION INDICATOR AND TRANSMITTER CHANGED, NO HELP. PARTS SENT TO HKG FOR REPAIR.SDR CLC2006F00007Odor · detectedCREW EXPERIENCED A BOOM SOUND FROM LOWER EXE COMPT. IN CRUISE SHORTLY AFTER CREW BEGAN TO SMELL WHAT APPEARED TO BE EITHER FUMES OR A TRACE OF SMOKE IN COCKPIT. NO ABNORMAL ELECTRICAL CONDITION EXISTED AT THE F/E STATION, EMERGENCY PROCESS WAS FOLLOWED. BY SDR CLC2006F00004Duct · brokenON CLIMB OUT, NR 1 ENGINE FIRE DETECTOR ILLUMINATED. RETURNED TO DEPARTURE, INSPECTION OF AC ENGINE FOUND BLOWN DUCT. REMOVED AND REPLACED DUCT. (K)SDR 740002Engine · shutdownNR 2 ENGINE SHUTDOWN FOR UNKNOWN REASON, ACCOMPANIED BY A LOUD BANG. QRH CHECKLIST ACCOMPLISHED. AIRCRAFT RETURNED TO PANC.SDR CLC2006F00003O-Ring · leakingIN FLIGHT, JUST BEFORE DESCENT, NR 1 HYD QUANTITY DROPPED TO 1 GALLON. CREW PERFORMED IRREGULAR CHECKLIST PROCEDURES, NORMAL, IN CONTACT WITH FLIGHT CONTROL, IT WAS ADVISED FOR MAINTENANCE THAT A RETURN WAS CONSIDERED, CREW AWS FLIGHT CONTROL DECIDED BEST TO SDR UIEA200600017Fitting · shearedFOUND SHEARED HI-LOKS IN NR 4 PYLON AFT DIAGONAL BRACE FITTING.SDR UIEA200600016Panel · crackedNR 6 SPOILER HAS A SMALL CRACK AT OUTBOARD SIDE OF ACTUATOR HINGE FITTING ,1ST ROW, FWD HI-LOK, FROM DOUBLER EDGE TO HI-LOK. REMOVED AND REPLACED NR 6 SPOILER PANEL ASSY AS PER 747 MM 27-62-01.SDR UIEA200600008Panel · crackedL/W IB MIDFLAP COVE PANEL CRACKED AT PREVIOUS REPAIR- 4TH SUPPORT ARM FROM OB END.SDR CLC2006F00000Door · damagedWITH LANDING GEAR RETRACTION OUT. RT MAIN GEAR INDICATES STAYED RED. DIVERTED, INVESTIGATION FOUND SEQUENCE VALVE CABLE BROKEN, CAUSING RT MAIN GEAR DOOR DAMAGE, AND TIRE DAMAGE. (K)SDR 05FDEA03964Duct · chafedNR 1 ENG HIGH PRESSURE CONTROL VALVE CHAFING INTO 7TH STAGE AIR PRESSURE TURBINE CONTROL LINE. REMOVED 7TH STAGE COOLING TUBE, PER DC10-30 MM 75-22-00-02. REPAIRED DUCT PER EM 72-09-03. REINSTALLED DUCT AND HIGH PRESSURE VALVE. PERFORMED OPS AND LEAK CHECKSDR P5CA0501418Tire · blownON TAKEOFF ROLL, CREW HEARD 2 LOUD BANGS AND LOST NR1 HYDRAULIC SYSTEM. FOUND 8 BLOWN TIRES, REPLACED 12 TIRES AND 3 BRAKES IAW MM 32-45-01 AND 32-45-15, ACCOMPLISHED CONDITIONAL INSPECTIONS IAW MM 05-51-10 AND 05-51-09.SDR XN0A1273Igniter · failedENG NR 1 NO LIGHT OFF DURING START ON A-IGNITORS. STARTS ON B-IGNITORS. TRANSFERRED TO DMI NR 5833 IAW ENA MEL 74-00-01 CAT (C). PLACARDS INSTALLED. (ORIG/OPEN)SDR DHL2005365007Latch · lack of lubeCOCKPIT DOOR LATCH IS FAULTY AND DIFFICULT TO LOCK. LUBED CREW ENTRY DOOR TO COCKPIT SYS OPS CHECKED GOOD ON GROUND IAW A300 M/M 52-00-00.SDR 0501441243Cylinder · fracturedDURING PUSHBACK FOR DEPARTURE A LOUD BANG WAS HEARD AND THE CENTER GEAR STARTED TO RETRACT. THE TOP PORTION OF THE CLG OUTER CYLINDER FRACTURED AND LIBERATED FROM THE MAIN BODY OF THE OUTER CYLINDER. THE LIBERATED PORTION OF THE OUTER CYLINDER WAS FORCED UPWARSDR DHL2005367003Battery Pack · inoperativeL1 EMRG LT INOP. REMOVED AND REPLACED, L1 EMERG LT BATT PACK IAW 33-51-13.SDR CLC2005F00002Wire · burnedON TAXI OUT THE NR 2 AC BUSS CIRCUIT BREAKERS POPPED OUT. SMELLED SMOKE IN COCKPIT TAXIED BACK TO THE RAMP. FOUND BURNED WIRES AND FEEDER CABLES BELOW LAVATORY FLOOR FOR THE NR 2 GENERATOR, ALL 3 PHASES. GENERATOR FEEDER CABLES FOR NR 1 AND 3 GENERATORS ARESDR DHL2005363005Gcu · failedPOWER INTERUPTION B4 GEN 1 RESULTING IN RTO. DEFERRED NR 1 GEN IAW MEL 24-11-01 CONTROL NR 21499 ID NR 8742. PERFORMED AC GEN ADJ/TEST IAW MM 24-11-00 SYS OPS OK FOR SERVICE THIS CLEARS DMI NR 21499 REPLACED NR 1 GCU IAW MM 24-21-00. RAN ENG. IAW JRH 16.5SDR CLC2005F00000Slide · deployedDURING LINE MAINTENANCE THE R1 DOOR ESCAPE SLIDE WAS ACCIDENTALLY DEPLOYED BY MAINTENANCE. REPLACED ESCAPE SLIDE. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (K)SDR CLC2005F00001Slide · deployedDURING LINE MAINTENANCE THE R1 DOOR ESCAPE SLIDE WAS ACCIDENTLY DEPLOYED BY MAINTENANCE. REPLACED ESCAPE SLIDE. AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (K)SDR UIEA2005005Pump · leakingNR 1 HYD CONTENTS RAPIDLY DEPLETED DURING FLIGHT. APPROPRIATE DRILLS CARRIED OUT. REMOVED AND REPLACED NR 1 ENGINE EDP IAW MM. NO EVIDENCE OF LEAKS AFTERWARDS. SERVICED NR 1 HYD SYSTEM TO FULL. INSPECT PRESS AND CASE DRAIN FILTERS. SECURED ENGINE COWL ANSDR 04FDEA02866Engine · overtempNR 3 ENGINE OVERTEMP ON TAKEOFF AT 700 FT AGL. TEMP ROSE TO 984 DEG FOR 30 SECONDS. SHUT DOWN ENGINE. TRIED RETARDING THROTTLE TO COOL ENGINE BUT WHEN THROTTLE WAS INCREASED N1 AND N2 CONTINUED TO DETERIORATE. NR 3 ENG IS APPROVED FOR REMOVAL. DURING INSPSDR 04FDEA02711Bearing · migratedNR 3 ENGINE AFT MOUNT O/B VERTICAL LINK HAS BOTH BEARINGS MIGRATING. REMOVED UNSERVICABLE NR 3 AFT ENGINE MOUNT, INSTALLED SERVICEABLE NR 3 AFT ENGINE MOUNT ASSEMBLY IAW DC10-30 MM 71-20-01-03.SDR WRNA200400008Warning Light · illuminatedAFTER TAKE OFF, GEAR HANDLE UP, LT GEAR DOOR AMBER AND LT GEAR UNLOCK RED LIGHT STAYED ON, ON BOTH FWD AND F/E'S PANEL. AIRPLANE START TO VIBRATE ABOVE 230 KTS. FUEL JETTISON PROCEDURE WAS ACCOMPLISHED TO MAX. LANDING WEIGHT. AIRCRAFT LANDED NORMAL.SDR DHL2004362009Overheat Loop · inoperativeLT WING MANIFOLD OVERHEAT DETECT INOPERATIVE IN B-LOOP. DEFERRED IAW MEL 36-12-03. CONTROL NR 17394 ASSIGNED. SP C/W. 21864SDR DHL2004365002Windshield · crackedFO'S WINDSHIELD FRACTURED WHILE ENROUTE.SDR WRNA200400007Sequence Valve · misalignedNOSE GEAR DID NOT RETRACT AFTER T/O RETURN TO AIRPORT. INSTALLED RIG PIN ON SEQUENCE VALVE AND RIGGED TO ZERO POSITION FOR REMOVED NLG DOOR. DOOR DEACTIVATED IAW CDL. FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.SDR WRNA200040000Switch · dirtyCARGO DOOR AND NOT LOCKED LIGHT ON, IN FLT. ALSO CARGO SWITCH FAULT LIGHT ON. DIVERTED TO GSO FOR REPAIR, 5200 GALS FUEL DUMPED FOR LANDING WT. REQUIREMENT. AIRCRAFT LANDED NORMAL. LUBED DOOR LOCK HANDLE SWITCH AND CLEANED STRIKER PLATES IAW SUP. MM 52-36-1SDR UIEA200400122Valve · erraticNR 4 ENGINE SHUTDOWN DURING DECENT: NR 4 ENGINE SHUTDOWN RUMBLE AND EGT RISING. AFTER RISING RELIGHT IS STARTED SURGING. SHUTDOWN AGAIN. NR 4 HIGH STAGE VALVE DEACTIVATED, CLOSE AND PERFORMED ENGINE RUN UP, CHECK NORMAL, ENGINE RUN BY FLT CREW AND NR 4 ENGSDR DHL2004364012Bulb · inoperativeNOSE GEAR INDICATOR ON PILOT'S LANDING GEAR PANEL DID NOT ILLUMINATE GREEN WHEN GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED THREE GREEN ON S/O PANEL. RELAMPED LANDING GEAR INDICATOR (P/N 3115) IAW M/M 33-13-00, OPS CHECKED GOOD.SDR DHL2004363006Fire Loop · will not testENG NR 2 FIRE LOOP "B" DOES NOT TEST. DEFERRED IAW MEL 26-12-01-1, ASSIGNED CONTROL NR 17142, PLACARD INSTALLED, SP/CW.SDR DHL2004364011Lever · malfunctionedEXIT DOOR 1R ESCAPE SLIDE DISARM LEVER DOES NOT REACH FULL DISARM POSITION. DEFERRED IAW MEL 52-61-01-2 DMI NR 17140 CAT (C) PLACARD INSTALLED.SDR P8UF200400001Valve · failedDURING CLIMB, FLIGHT CREW NOTICED HYDRAULIC LOSS ON SYSTEM NR 1, CAPTAIN DECIDED FLIGHT BACK TO POINT OF DEPARTURE.SDR 0401001225Fire Loop · malfunctionedON CLIMBOUT AT 31,000 FT, RECEIVED NR 2 ENGINE FIRE WARNING INDICATION. NR 2 ENGINE B-LOOP WAS PUT ON MEL. SHUT DOWN NR 2 ENGINE IAW COM PROCEDURE. DUMPED 90,000 LBS OF FUEL AND RETURNED TO NRT FOR AN UNEVENTFUL LANDING. WORK IN PROGRESS-SUPPLEMENTAL INFORMATSDR P5CA0401103Heater · odorF/O NR 1 WINDOW LOWER RIGHT CORNER OVERHEATING AND CAUSING BURNT WIRE SMELL. TURNED OFF AND C/B PULLED. DEFERRED R-1 WINDOW HEAT PER MEL 30-11-1.SDR UIEA200400106Door · crackedR-4 DOOR LOWER AFT CORNER HAS 2 CRACKS, ONE CRACK IS 4 INCHES AND THE OTHER CRACK IS 3 INCHES, STA 1715, W/L 199.8. CAUSE OF DAMAGE UNKNOWN. CRACKS FOUND DURING VISUAL INSPECTION. INSTALLED DOUBLER REPAIR IAW SRM.SDR UIEA200400100Channel · crackedCENTER CHANNEL CRACKED BEYOND PRIVOUS REPAIR IB HINGE ON NR 7 LE FLAP. FOUND DURING VISUAL INSPECTION. CAUSE IS UNKNOWN. LOCATION IS WING STA 944.5. CORRECTIVE ACTION REPLACED LE FLAP ASSY IAW MM.SDR UIEA200400098Brake · damagedGT9813/24 RME/JFK BRAKE TEMPERATURE OVERHEAT LIGHT: BRAKE TEMPERATURE OVERHEAT LIGHT ILLUMINATED DURING TAXI-IN. LEFT BODY, LEFT REAR BRAKE TEMPERATURE APPROXIMATELY INDICATING 7.40. FOUND NR 7 BRAKE DAMAGED, REMOVED AND REPLACED SAME IAW MM, LEAK CHECKS GO
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