GE CF6-50 series

Service difficulty reports · 201

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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.

SDR FDEA201803080631Connector · loosePRIOR TO DESCENT, THE NR 1 ENGINE GAUGE WENT BLANK, FOLLOWED BY YELLOW X. WITHIN 10 SECONDS IT CAME BACK ON SHOWING AN EXCEEDANCE OF 955 DEGREES. THEN THE EGT WENT BACK TO NORMAL. FOLLOWED QRH, PULLED THROTTLE TO IDLE. ABOUT TWO MINUTES LATER RECEIVEMar 8, 2018 · N307FE · Doug MD1030F · Engine Indicating System WiringSDR FDEA201412284194Sensor · failedLEVEL 2 OIL TEMP HIGH. OIL TEMP 203 ABOVE RED LINE. NR 2 ENGINE SHUTDOWN. SPIKING AFTER SHUTDOWN AT GATE. TROUBLESHOT IAW FIM 79-32-00/201. REMOVED AND REPLACED THE NR 2 ENGINE OIL TEMP SENSOR IAW MM 79-32-01-2. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.Dec 28, 2014 · N303FE · Doug MD1030F · Engine Oil Temperature RegulatorSDR CA140605007Tube · mismanufactured(CAN) PART WAS BEING INSPECTED IN PREPARATION FOR REPAIRS FOR CUSTOMER WHEN IT WAS NOTICED THAT A NON-REPAIRABLE AREA DIAMETER "B" HAD BEEN MADE TO SIZE BY THE USE OF PLASMA SPRAY. IAW ENGINE MANUAL GEK50481, CHAPTER 72-57-10, SUBTASK 72-57-10-220-052.Jun 5, 2014 · Engine (Turbine/Turboprop)SDR FDEA201306071219Wire Harness · failedREJECT TAKEOFF, RNWY 36L AT APROX 60 KTS FOR NR 2 ENG EXCEEDANCE WITH EGT 1055. ACARS DATA SHOWS JUST AFTER REACHING TAKEOFF POWER A SUDDEN EGT INCREASE AT A RATE OF 150 DEG C PER SECOND WITH OTHER ENGINE PARAMETERS STEADY. PERFORMED #2 ENG EGT THERMOCOUPLE Jun 7, 2013 · N312FE · Doug MD1030F · Engine Indicating System WiringSDR FDEA201205171828Override Switch · inoperativeDURING TEST FLIGHT AT FL250, SHUTDOWN NR 1 ENGINE AND ATTEMPTED MULTIPILE RESTARTS WHICH FAILED, DESCENDED TO 14,000 FT AND ATTEMPTED RESTARTS NOT AVAIL. RETURNED TO DEPARTURE WITH NR 1 ENGINE INOPERATIVE. FOUND ENGINE IGNITION OVERRIDE SWITCH INOP, REPLACEMay 17, 2012 · N307FE · Doug MD1030F · Ignition Power SupplySDR Q2SA2012042876002Engine · damagedNUMBER FOUR ENGINE STALLED DURING CLIMB AND FLAP CLEAN UP. AT APPROXIMATELY 3000 FEET THE CREW PULLED THE THRUST LEVER BACK TO BREAK THE ENGINE STALL. THEY THEN CONTINUED TO CLEAN UP AND ACCELERATE TO VZ + 100 TILL 10,000 FEET. AFTER PASSING 10,000 FEET THEApr 28, 2012 · N760SA · Boeing 747230B · Engine (Turbine/Turboprop)SDR UIEA2011101900575Manifold · crackedUPON OPENING OF THE NR 1 ENGINE NACELLE, MX FOUND THE LOWER LPT COOLING MANIFOLD BROKEN AT SEVERAL LOCATIONS. REFER TO FIG 1 FOR DAMAGE LOCATION AND DETAILS. DUE TO PRESENCE OF CRACKS AROUND THE LPT COOLING MANIFOLD WAS OVER LIMITS WITH AMM 75-24-00, SUBMITTEOct 13, 2011 · N524MC · Boeing 7472D7B · Engine Cooling SystemSDR UIEA2011080400416Nozzle · crackedDURING AN ENGINE CHANGE AT AN A-CHECK, MX FOUND 3 EA CRACKS ON THE NR 4 ENGINE FIXED COWL EXHAUST NOZZLE FOWARD FLANGE CORE COWL SUPPORT ASSY (REF FIGURE 1). REPAIRED IAW EO 4778A148.Aug 4, 2011 · N524MC · Boeing 7472D7B · Engine Collector/Tailpipe/NozzleSDR UIEA2011072700440Frame · crackedFRAME AT BS 760 BETWEEN S-5R AND S-7R FOUND CRACKED AND WAS FOUND DURING THE SECTION 42 UPPER LOBE INSPECTION ACCOMPLISHED IAW EO 4753A165, REV C (SB 747-53-2349 REV 3, AD 2009-18-07). THE CRACK WAS LOCAL ONLY TO THE FRAME PN AND WAS LOCATED AT S-6R. THE CRACKJul 27, 2011 · N524MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2011060700300Bulkhead Web · crackedDURING C-CHECK, A CRACK WAS FOUND IN THE PRESSURE WEB. THE CRACK WAS LOCATED AT THE 11 O'CLOCK POSITION, EXTENDING THROUGH TWO (2) FASTENER HOLES OTBD OF THE RT 2ND INTERMEDIATE STIFFENER FROM THE TOP. THE CRACK EXTENDED 0.1875 IN INBD AND 0.125 IN OTBD AS SJun 7, 2011 · N522MC · Boeing 7472D7B · Fuselage Main, BulkheadSDR UIEA2011053000268Sleeve · damagedDURING WALK AROUND CHECK, MX FOUND A HOLE 0.5" WIDE ON THE OUTER SLEEVE OF THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 2 ENGINE. THE HOLE IS 6.0" FROM THE EXHAUST SLEEVE T/E AT THE 11:00 O' CLOCK POSITION. (DISPOSITION WAS MADE TO REMOVE ANY BURRS UMay 30, 2011 · N523MC · Boeing 7472D7B · Engine Collector/Tailpipe/NozzleSDR FDEA201104221590Engine · malfunctionedREJECTED T/O 18R, ENG FAIL LIGHT ON BETWEEN 80 & 90KTS. REJECTED BY 100 KTS. TO GW 377,000. N1 NR2 MORE THAN 11 PERCENT HIGHER THAN NR 3. IAW JRH DECREASED PART POWER TRIM SCREW ON NR 2 ENGINE APPROX .6250 TURN, COUNTERCLOCK WISE DIRECTION JRH SECTION 7, Apr 22, 2011 · N316FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR UIEA2011032800159Unknown · unknownTAKEOFF REJECTED AT 90 KNOTS, WHEN YAW TO THE LT WAS FELT. INSPECTED NR 1 AND NR 2 ENGINES, NO DEFECTS NOTED, PERFORMED HIGH ENERGY STOP INSP, NO DEFECTS NOTED. PERFORMED CHECK OF BRAKES ON LT HAND BODY GEAR, AND LOCKED OUT NR 7 BRAKE DUE TO OVERHEAT CONDITIOMar 28, 2011 · N523MC · Boeing 7472D7B · Landing Gear SystemSDR UIEA2011032200155Accumulator · leakingCREW REPORTED HYD LEAK ON THE NR 4 SYS (FOUND BRAKE ACCUMULATOR LEAKING. R & R ACCUMULATOR, SERVICED SYSTEM, PERFORMED OPERATIONAL AND LEAK CHECKS, ALL; OK.)Mar 22, 2011 · N523MC · Boeing 7472D7B · Hydraulic System, MainSDR UIEA2011031100149Check Valve · failedBLOCK TURN BACK DUE NR 4 ENGINE FAILED TO ACCELERATE PAST 40 PERCENT N1, WITH HIGH EGT AND 4 COMPRESSOR STALLS WERE EXPERIENCED. (REPLACED 8TH STAGE CHECK VALVE AND PERFORMED ENGINE RUNUP. ALL OPERATES NORMAL. DUE TO COMPRESSOR STALL, BOROSCOPE INSPECTION ACCMar 11, 2011 · N524MC · Boeing 7472D7B · Engine (Turbine/Turboprop)SDR UIEA2011020500092Duct · damagedENGINE NR 2 OUTBOARD T/R HALF HI BYPASS "C" DUCT INTERNAL WALL WITH DELAMINATION AND MISSING SKIN MATERIAL(REMOVED SECTION OF DAMAGED SKIN AND PREPARED AREA FABRICATED DOUBLER FROM 2024-T3 0.063 PO 10024219 LOCATED, TRIMMED, DRILLED, PRIMED AND INSTALLED AND SFeb 5, 2011 · N523MC · Boeing 7472D7B · Engine (Turbine/Turboprop)SDR UIEA2010122900248Latch · brokenDURING MX WALKAROUND OF ACFT, REVEALED NR 1 ENGINE THRUST REVERSER LOWER AFT ACCESS DOOR AND BLOWOUT DOOR WERE FOUND OPENED. UPON FURTHER INSP, MX FOUND THE AFT TENSION LATCH BROKEN. (DISPOSITION IS TO ACCOMPLISH A TIME LIMITED REPAIR BY INSPECTING THE 2 OTHDec 29, 2010 · N540MC · Boeing 747243B · Engine Thrust ReverserSDR CNMA20100034Smoke Detector · false activationONE SMOKE DETECTOR LIGHT ON AND APPLICABLE CARGO FIRE LIGHT ON (FWD CARGO FIRE LIGHT ON DISCHARGED FIRE BOTTLES). REPLACED FWD CARGO NR3 SMOKE DETECTOR IAW AMN 26-14 AND TESTED GOOD. REPLACED AUX MWACS (MASTER WARNING CONTROL UNIT) IAW AMM 33-15 REPLACED TESTNov 28, 2010 · N270AX · Doug DC1030 · Smoke DetectionSDR UIEA2010111000177Nacelle · crackedTHE PURPOSE OF THIS EO 4771A096 & NBSP; IS TO DOCUMENT A MAJOR REPAIR. DURING WALK-AROUND INSPECTION AT RMS, MX FOUND THE NR 1 RT FAN COWL WITH DAMAGE; CRACK MEASURING 6.0 IN. LONG (REF FIG 1). THE DAMAGE IS BEYOND THE ALLOWABLE DAMAGE LIMITS IAW SRM 51-40-06,Nov 10, 2010 · N522MC · Boeing 7472D7B · Nacelle/Pylon, Main FrameSDR CNMA20100032Support Fitting · corrodedCTR LANDING GEAR LT AND RT TRUNNION SUPPORT FITTING CORRODED ON TOP AROUND BOLT HOLES. CLEANED CORROSION IAW EO 5310E0973 ROTARY PEEN REWORK AREA IAW DPS 4.999-2. PERFORMED HFEC INSP IAW NDT MANUAL, PART 6 TO VERIFIY NO CORROSION REMAINS. REPLACED HARDWARE WINov 4, 2010 · N270AX · Doug DC1030 · Fuselage, Landing Gear Attach FittingsSDR UIEA201000235Conduit · damagedDURING WALKAROUND INSP, MX FOUND THE ELECTRICAL CONDUIT AND CONNECTOR MOUNT HOUSING AT THE NOSE GEAR DAMAGED (REF FIG 1). DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPEAT INSPECTIONS AT EVERY 5 FLIGOct 22, 2010 · N522MC · Boeing 7472D7B · Flight Control System WiringSDR Q2SA761005Valve · crackedNR 1 ENGINE FAILED IN FLIGHT 85% N1, 60% N2, 600 DEG EGT, FF 4600, ROLL BACK - NO RESPONSE, NO RESTART. DURING TROUBLESHOOTING, FOUND FUEL PRESSURIZING AND DRAIN VALVE HOUSING CRACKED. REMOVED AND REPLACED P AND D VALVE IAW AMM 73-11-03, OPS AND LEAK CHECK OKOct 21, 2010 · N761SA · Boeing 7472F6B · Engine (Turbine/Turboprop)SDR UIEA201000232Doubler · crackedDURING MX WALKAROUND, MX FOUND THE MAIN DECK - MDSCD AREA - BS1910 ROLL OUT GUIDE - DOUBLER CRACKED (REF FIG 1). THE DAMAGE EXCEEDS THE ALLOWABLE LIMITS IAW AMM 25-58-00. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUOct 17, 2010 · N540MC · Boeing 747243B · Fuselage Main, Plate/SkinSDR UIEA2010092700166Sleeve · crackedDURING MX WALK AROUND, MX FOUND 2 EA CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, NR1 STARTING AT APPROX THE 7 O'CLOCK POSITION. THE CIRCUMFERENTIAL CRACK IS APPROX 3.0 IN LONG, THE NR2 CRACK IS LOCATED AT INBD SIDE AND AFT OF EXHAUST CONE AREA MEASURING 0.750 ISep 27, 2010 · N540MC · Boeing 747243B · Engine Collector/Tailpipe/NozzleSDR UIEA2010091100155Tire · failedMLG WHEELS NR 2, 4, 6, 8 HAD THERMAL DISCHARGE AT GATE. (REPLACED NR 2, 4, 6, 8 WHEELS. SPIN AND LEAK CHECK OK. ANTI SKID TEST AND CHAPTER 5-51-26 INSP ACCOMPLISHED AND ALL NORMAL.)Sep 11, 2010 · N540MC · Boeing 747243B · Tire TubeSDR UIEA2010082600147Mount · damagedTHE PURPOSE OF EO 4725A284 IS TO DOCUMENT A MAJOR REPAIR. DURING WALKAROUND INSP, MX FOUND THE ELECTRICAL CONDUIT AND CONNECTOR MOUNT HSG AT THE NLG DAMAGED. REPAIRED IAW EO 4725A284&NBSP.Aug 26, 2010 · N523MC · Boeing 7472D7B · Fuselage Miscellaneous StructureSDR FDEA201008122965Valve · out of adjustWITH MAX T/O POWER NR3 SLOW TO ACCELERATE. ENGAGED A/T AND 1 & 2 DROVE TO T/O SETTING, NR3 STOPPED .1875" SHY OF TARGET N1 WITH 1" KNOB SPLIT BETWEEN 1 & 2 MATCHED AND NR 3. ATTEMPTED MANUAL ADJUSTMENT OF NR 3 TO T/O SETTING. NR3 WAS AT MECHANICAL STOP, Aug 12, 2010 · N307FE · Doug MD1030F · Power LeverSDR UIEA2010080900148Actuator · brokenBODY GEAR UNLOCKED LIGHT ILLUMINATED IN BOTH PRIMARY AND ALTERNATE POSITIONS WHEN LINED UP FOR TAKEOFF (FOUND RT BODY GEAR STEERING ACTUATOR BROKEN. R & R BODY GEAR STEERING ACTUATOR IAW MM 32-53-11, OPS CHECK OK)Aug 9, 2010 · N523MC · Boeing 7472D7B · Landing Gear Steering SystemSDR UIEA2010080500132Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE NR 2 ENG INLET COWL OUTER BARREL SKIN CRACK/DAMAGE (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AND PERMAug 5, 2010 · N523MC · Boeing 7472D7B · Engine Air Intake SystemSDR UIEA2010080200127Actuator · damagedUPON ARRIVAL, THE NR2 RT THRUST REVERSER, MX FOUND THE T/R NOT COMPLETELY STOWED. AFTER INSP, MX FOUND THE CTR BALLSCREW SHEARED AND THE UPPER BALLSCREW ACTUATOR SUPPORT BRACKET DAMAGED. (DISPOSITION IS TO REPLACE THE CTR BALLSCREW WITH A SERVICEABLE UNIT, REAug 2, 2010 · N522MC · Boeing 7472D7B · Engine Thrust ReverserSDR FDEA201008012755Engine · malfunctionedDURING TAKEOFF ROLL, WITH AUTOTHROTTLES ENGAGED AT 85 TO 90 KTS A LEVEL 1 ENG 3 EXCEDEANCES ANNUNCIATED. ABORTED TAKEOFF. COMPLIED WITH QRH. N2 NR 3, 109.6 INSPECTED ENGINE EXHAUST FOUND NO PARTICLES PRESENT. NR3 ENGINE, N2 EXCEEDANCE 109.6 REQUIRES BORESCOPAug 1, 2010 · N316FE · Doug MD1030F · Engine (Turbine/Turboprop)SDR WGFY2010FA0751008Former · crackedSTRUT NR 4 NS270.00 LT SIDE UPPER FORMER WAS CRACK.Jul 24, 2010 · N751SA · Boeing 747228F · Nacelle/Pylon, Frame/Spar/RibSDR WGFY2010FA0751009Former · crackedSTRUT NR 4 NAC 270.00 RT SIDE UPPER FORMER WAS CRACK.Jul 24, 2010 · N751SA · Boeing 747228F · Nacelle/Pylon, Frame/Spar/RibSDR CNMA20100028Panel · corrodedEXFOLIATED CORROSION ON RT WING LOWER PLATE BELOW ACCESS PANEL 616BB AT XQRS 346. REMOVED DAMAGED SECTION OF LOWER WING SKIN, ACCOMPLISHED SURFACE SCAN AND OPEN HOLE HFEC INSP, ROTO PEENED AFFECTED AREA. FABRICATED ALL REPAIR PARTS. INSTALLED ALL REPAIR PARTSJul 24, 2010 · N522AX · Doug DC1030 · Wing, Plate/SkinSDR WGFY2010FA0751006Stiffener · corrodedAFT WHEEL WELL BULKHEAD STIFFENERS CORROSION AT BS 1480, WL 166.Jul 22, 2010 · N751SA · Boeing 747228F · Fuselage Main, BulkheadSDR FDEA201007212632Door Frame · crackedMAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB AT STA 1251 REPAIRED IAW SRM 53-50-00 FIG 19, SH 1, VOL 1.Jul 21, 2010 · N320FE · Doug DC1030F · Fuselage Main, StructureSDR WGFY2010FA0751002Strap · crackedPYLON NR1, STA 248.00 STRAP WAS CRACKED.Jul 19, 2010 · N751SA · Boeing 747228F · Nacelle/Pylon Miscellaneous StructureSDR WGFY2010FA0751003Stiffener · crackedPYLON NR 2 STIFFENER NR 3 AND STRAP, STA 248 WAS CRACKED.Jul 19, 2010 · N751SA · Boeing 747228F · Nacelle/Pylon Miscellaneous StructureSDR WGFY2010FA0751004Stiffener · crackedPYLON NR2 STRAP STA 250 BETWEEN STIFFENER NR 2 & STIFFENER NR 3 WAS CRACKED.Jul 19, 2010 · N751SA · Boeing 747228F · Nacelle/Pylon Miscellaneous StructureSDR UIEA2010070400089Skin · corrodedNRC 0740 (RA4174), "MAIN DECK" FOUND CORROSION ON THE WING CTR SECTION BOX UPPER SURFACE SKIN AT STA 1241, RBL 75 TO 80, WL 149 (THE WORK ACCOMPLISHED IAW REA: MF0068720008 AND RF7A: 00687-0008).Jul 4, 2010 · N523MC · Boeing 7472D7B · Wing, Plate/SkinSDR UIEA2010070200079Skin · corrodedNRC 041 LOWER FUSELAGE SKIN SUSPECT TO CORROSION ON LAP JOINT AT STR 46 BETWEEN STA 2070 TO 2180 LT SIDE. (THE WORK ACCOMPLISHED IAW REA MF00687R0001 AND RFTA NO 00687-0001 AND J/C 00041-I-1 REF.)Jul 2, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010070100083Frame · crackedNRC 1111 "MAIN DECK" FOUND CRACK ON FRAME, STA 1860, RT SIDE BETWEEN STR 12 TO 13. (THE WORK ACCOMPLISHED IAW PEA NR MF00687R0009 AND RFTAIN0 :00687-0009).Jul 1, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2010070100084Frame · bentNRC: 1121 "FWD CGO" FRAME STA 700 (F/B) UPPER CHORD IS BENT BETWEEN RBL 17 - 21(THE WORK ACCOMPLISHED IAW REA NO MF00687-R0005 AND RFTA NR 00687-0005.)Jul 1, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2010070100085Frame · bentNRC 1122 "FWD CRACK" FRAME 720 (F/B) UPPER CHORD IS BENT BETWEEN RBL 14 TO 18. (THE WORK ACCOMPLISHED IAW REA NO MF00687R0006 AND RFTA NO 00687-0006).Jul 1, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2010070100086Frame · bentNRC 1123, FWD CARGO FRAME UPPER CHORD IS BENT STA 760 BETWEEN 28-29 (THE WORK PREPAIRED IAW REA NR HF00687R00007, REV A, RFTA NR 00687-007).Jul 1, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR UIEA2010070100088Frame · damagedNRC 1376 "MAIN DECK" DAMAGE WAS FOUND ON FRAME STA 1040, OTBD CHORD B/T SRT 15R-16R. (THE WORK ACCOMPLISHED IAW REA NR HF00687R0011 "A" AND RFTA NR 00687-004).Jul 1, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, FrameSDR WGFY2010FA0000488Skin · corrodedPYLON NR2 LT WING LOWER FRONT SPAR LOWER WING SKIN WBL 470 WAS CORRODED LEVEL 2,Jun 29, 2010 · N765SA · Boeing 7472F6B · Wing, Plate/SkinSDR UIEA2010062900078Skin · corrodedNRC 024 CORNER OF EXISTING REPAIR IS BULGED ON EXT FUSELAGE SKIN RT SIDE AT STA 400 AND STR 44 AREA. (BULGED) 2.0" X 1.5" X 0.061"(THE WORK ACCOMPLISHED IAW REA NR : HF00687R0002 AND NO 00687-0002 AND JC 0024-I-1.)Jun 29, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Plate/SkinSDR UIEA2010062800068Stringer · damagedNRC 0971: "LOWER DECK" JUST FWD OF STA 320 STR 37R ELONGAGED FASTENER HOLE ON STRINGER (DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC NRC 971 1/2 IAW SRM 53-01-03, FIG 3, FASTENERS INSTL IAW SRM 51-30-02).Jun 28, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/StringerSDR UIEA2010062800069Stringer · damagedNRC: 0972 "LOWER DECK" STA 320, STR 28.7, R. DOUBLE HOLE ON THE STRINGER. (DAMAGED AREA TRIMMED OUT. REINFORCED AREA WITH NEW SEGMENT AND REPAIR STRINGER PN N523MC, NRC 972 1/2 IAW SRM 53-10-03, FIG 3 & AMP; FASTENERS INSTL IAW SRM 51-30-02.)Jun 28, 2010 · N523MC · Boeing 7472D7B · Fuselage Main, Longeron/Stringer
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