GE CF34-10E5A1

Service difficulty reports · 476

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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 = 'CF3410E5A1'
  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 CA100118005Windshield · cracked(CAN) INITIAL VERBAL REPORT. ACFT, ON PUSH BACK DURING ENGINE START CAPTS WINDSHIELD CRACKED. NO FURTHER REPORTS AT THIS TIME. WINDSHIELD HAS BEEN CHANGED. RECORDS SHOW THE WINDSHIELD HAS BEEN INSTALLED FOR 11497 HOURS.Jan 18, 2010 · Emb ERJ190100IGW · Flight Compartment WindowsSDR CA100111002Mechanism · frozen(CAN) ON ARRIVAL L2 DOOR ARM/DISARM AND EXTERNAL FLAPER LEVERS FROZEN. USING RAMP HTR, APPLIED HEAT FROM INSIDE ACFT TO THAW DOOR MECHANISM.Dec 30, 2009 · Emb ERJ190100IGW · Passenger/Crew DoorsSDR CA091223013Baffle · loose(CAN) INTERNAL VANE OF REFUEL NOZZLE BREAKING UP, RELEASING METAL FRAGMENTS INTO WING FUEL TANKS (TC NR 20091223013)Dec 16, 2009 · Emb ERJ190100IGW · Aircraft Fuel SystemSDR CA100111001Door · frozen(CAN) THE AIRCRAFT CAME IN WITH ALL CABIN DOORS FROZEN IN THE ARMED POSITION. A FEW MINUTES AFTER ARRIVAL, THE FLIGHT ATTENDANT WAS ABLE TO DISARM L1 AND OPEN THE DOOR, BUT IT WAS VERY HARD. L2, R2 & R1 WERE STILL FROZEN. ONCE ALL PAX DEPLANED, THE CAPTAIN Dec 14, 2009 · Emb ERJ190100IGW · Passenger/Crew DoorsSDR CA091210006Slat System · failed(CAN) ON APPROACH, FLAP AND SLAT FAIL, PAN PAN DECLARED, GO AROUND AND QRH COMPLETED. LANDED WITHOUT FURTHER INCIDENT. REPLACED SLAT 2-3 SKEW SENSOR HARNESS.Dec 8, 2009 · Emb ERJ190100IGW · Leading Edge Slat Control SystemSDR CA091202003Steering Sys · faulted(CAN) LANDING IN SFO CREW EXPERIENCED A NOSE GEAR STEERING FAULT. RESET ATTEMPTED NIL FIX. ALTERNATE BREAKING USED TO GET TO GATE. (TC NR 20091202003)Nov 30, 2009 · Emb ERJ190100IGW · Landing Gear Steering SystemSDR CA091202005Landing Gear · malfunctioned(CAN) ON APPROACH TO YYC LEFT MAIN LANDING GEAR DID NOT EXTEND. GO AROUND AND QRH COMPLETED. GEAR RESELECTED ALL INDICATIONS NORMAL. (TC NR 20091202005)Nov 27, 2009 · Emb ERJ190100IGW · Landing Gear Retraction/Extension SystemSDR CA091126004Slat System · malfunctioned(CAN) EN ROUTE, IN THE BEGINNING OF THE CRUISE STAGE, THE CREW EXPERIENCED A FLAP FAILURE. A DECISION TO RETURN WAS MADE IN CONSULTATION WITH MTC AND SOC. THE FLIGHT RETURNED, DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT AT THE ZERO FLAP SETTINGNov 26, 2009 · Emb ERJ190100IGW · Leading Edge Slat Control SystemSDR CA091202006Flap System · malfunctioned(CAN) YYC TO SEA START OF CRUISE FLAP FAILURE CREW RETURNED TO YYC. DECLARED EMERGENCY AND LANDED WITH FLAPS 0 WITHOUT INCIDENT. (TC NR 20091202006)Nov 26, 2009 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA091126003Actuator · malfunctioned(CAN) DURING THE APPROACH, THE FLIGHT HAD A FLAPS FAILED MESSAGE. THE CREW EXECUTED A GO-AROUND, DECLARED AN EMERGENCY AND LANDED NORMALLY WITH THE FLAPS IN POSITION 1 (TC NR 20091126003)Nov 25, 2009 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA091202007Flap System · warning message(CAN) YYZ TO SEA ON APPROACH FLAP FAIL MESSAGE, GO AROUND CARRIED OUT AND EMERGENCY DECLARED. NORMAL LANDING FLAPS 1 (TC NR 20091202007)Nov 25, 2009 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA091119001Landing Gear · malfunctioned(CAN) ON APPROACH LANDING GEAR LEVER SELECTED DOWN. EICAS MESSAGE " BRK CTRL FAULT" FOLLOWED BY LT MLG SHOWED RED AND NOT DOWN AND LOCKED. GEAR RECYCLED SAME RESULT HOWEVER AFTER A FEW SECONDS EICAS MESSAGE WENT OUT AND GOT 3 GREEN GEAR DOWN LIGHTS. LANDING GNov 19, 2009 · Emb ERJ190100IGW · Landing Gear Retraction/Extension SystemSDR CA091118011Diffuser · fragmented(CAN) ACFT WAS RECENTLY IN FOR A B-01/N-01 MX VISIT. FRAGMENTS OF REFUEL DIFFUSER ASSY WERE FOUND IN THE RT WING FUEL TANK AS SHOWN IN THE ATTACHMENTS. FURTHERMORE, THIS ISN’T AN ISOLATED INCIDENT AS THE SAME FRAGMENTS WERE RECENTLY FOUND IN THE RT WING FUEL TNov 16, 2009 · Emb ERJ190100IGW · Fuel StorageSDR CA091116002Steering Unit · failed(CAN) 1000 FEET AGL FLIGHT CREW SELECTED GEAR DOWN AND RECIEVED A GEAR STEER FAIL MESH. LANDING NORMAL HOWEVER REQUIRED TOW OFF OF RUNWAY. MX CLEARED MAU NVM CONSIDERED OK FOR FURTHER FLIGHT.Nov 14, 2009 · Emb ERJ190100IGW · Landing Gear Steering SystemSDR CA091116005Actuator · failed(CAN) FLT CREW REPORTED FLAP SLAT FAILURE INBOUND. FLAPS 2, SLATS 0 NO EMERGENCY DECLARED. MX RT SLAT ACTUATOR REPLACED.Nov 14, 2009 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA091116003Actuator · failed(CAN) FLIGHT CREW. ON APPROACH, YYC SLATS FAILED AND ACFT LANDED WITH SALT 0 AND FLAP 2. MX NR 3 AND NR 5 RT SLAT ACTUATORS REPLACED, SYS SERVICABLE.Nov 8, 2009 · Emb ERJ190100IGW · Leading Edge Slat ActuatorSDR CA091116010Support Bracket · debonded(CAN) LT AND RT MLG BAY FIRE DETECTION LOOP SUPPORT BONDED BRACKETS HAVE BECOME DISBONDED. (REPORTED INTERNALLY FROM A LINE MECHANIC) PN NOT PROVIDED, UNABLE TO LOCATE IN IPC. SIMILAR CONDITIONS EXIST ON THE FOLLOWING ACFT. C-FLWH LH WHEEL WELL C-FHOS LT & RTNov 3, 2009 · Emb ERJ190100IGW · Fuselage Main, Attach FittingsSDR CA091028003Support · loose(CAN) LH AND RH MAIN GEARBAY FIRE DETECTION LOOP SUPPORT STRUCTURE ADRIFT FROM AIRFRAME ALL FOUR BONDED SUPPORT STRUCTURE BRACKETS HAVE DISBONDED FROM THE AIRFRAME. THE REMAINING 3 MECHANICALLY FASTENED BRACKETS AFIX THE ENTIRE FIRE DETECTION LOOP SUPPORT ASSOct 10, 2009 · Emb ERJ190100IGW · Fuselage Miscellaneous StructureSDR CA091028002Support · loose(CAN) LT AND RT MAIN GEARBAY FIRE DETECTION LOOP SUPPORT STRUCTURE ADRIFT FROM AIRFRAME THREE OUT OF FOUR BONDED STRUCTURE BRACKETS HAVE DISBONDED FROM THE STRUCTURE. THE REMAINING THREE MECHANICALLY FASTENED BRACKETS AFIX THE ENTIRE FIRE DETECTION LOOP SUPPOOct 4, 2009 · Emb ERJ190100IGW · Fuselage Miscellaneous StructureSDR CA090916002Attach Fitting · failed(CAN) AFTER REMOVING THE LANDING GEAR IN ORDER TO REPLACE THE FWD SPAR PINTLE PIN BEARING, CORROSION/PITTING WAS FOUND ON THE BORE FACE WHERE THE RETRACT ACTUATOR ATTACHES TO THE MLG SHOCK STRUT. WHEN THE PIN WAS REMOVED FROM THE RETRACT ACTUATOR LUG, WHITE POSep 13, 2009 · Emb ERJ190100IGW · Main Landing Gear Attach SectionSDR CA090921003Attach Fitting · corroded(CAN) DURING REMOVAL OF THE RT MLG, PITTING CORROSION WAS FOUND ON RETRACT ACTUATOR ATTACHMENT POINT, AFT LUG AFT FACE. ATTACHMENT PIN WAS FOUND CORRODED ALSO.Sep 13, 2009 · Emb ERJ190100IGW · Fuselage Main, Attach FittingsSDR CA090910009Connector · disconnectedHEATED PLASTIC ODOR CAME FROM UNDER SEAT 18AC. AFTER SCREENS 19AC AND 20AC WENT BLANK. 19A AND 20AC CAME BACK BUT NOT 19C. ODOR DISAPPEARED. CONNECTOR UNDER 18A RECONNECTED. 19C SVDU REPLACED. IP SEQUENCE AND SOFTWARE DOWNLOADED. AUDIO/VIDEO WORKS. NO BURNINGSep 9, 2009 · Emb ERJ190100IGW · Entertainment SystemSDR CA090904005Slat System · malfunctionedON APPROACH TO LAND, FLIGHT HAD SLAT FAILURE. EMERGENCY EQUIPMENT WAS CALLED OUT TO RUNWAY. SLAT BREAKERS RESET. OPS CHECK CARRIED OUT, UNABLE TO DUPLICATE. NIL REPEAT.Aug 24, 2009 · Emb ERJ190100IGW · Leading Edge Slat Control SystemSDR CA090904004Actuator · failedDURING APPROACH, FLIGHT CREW RECEIVED A `SLAT FAIL` MESSAGE. THE CREW CARRIED OUT THE QRH AND LANDED UNEVENTFULLY. FAULT WAS "SLAT SLOW RATE". PREVIOUS "SLAT FAIL" FAULTS NON-VOLATILE MEMORY (NVM) NOT CLEARED. AFTER MEMORY CLEARED, DID NOT REPEAT. NOTE: PRAug 22, 2009 · Emb ERJ190100IGW · Leading Edge Slat ActuatorSDR CA090904003Flap System · malfunctionedON APPROACH, CREW RECEIVED A FLAP FAIL MSG. A GO AROUND WAS CONDUCTED AND THE CHECK LIST FOLLOWED. FLAP SYS RETURNED TO NORMAL AND AN APPROACH AND LANDING WAS CARRIED OUT. FIM CARRIED OUT, NO FAULT FOUND. NIL HISTORY, NIL REPEAT.Aug 20, 2009 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA090904002Actuator · failedON APPROACH, THE CREW EXPERIENCED A FLAP/SLAT FAILURE WITH FLAPS AT POSITION 2, AND SLATS AT POSITION 0. AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS CARRIED OUT. LT NR 5 SLAT ACT CHANGED DUE TO TORQUE LIMITER IND TRIPPED.Aug 18, 2009 · Emb ERJ190100IGW · Leading Edge Slat ActuatorSDR CA090826001Bearing · wornWHILE RUDDER WAS REMOVED FOR REPLACEMENT ON AC 306 IT WAS DISCOVERED THAT THERE WAS WEAR. AXIAL PLAY INTERNALLY OF THE RUDDER ATTACH BEARINGS - APRROX .025IN ON 4 OF THE 5 ATTACH BEARING (1 THROUGH 4) ON THE VERT STABLIZER. BEARINGS WHERE REPLACED AND END PLAAug 17, 2009 · Emb ERJ190100IGW · Rudder StructureSDR CA090813005Seal · missing(CAN) LT MLG AFT PINTAL BEARING DUST SEAL LOOSE AND RT IS MISSING. (TC# 20090813005)Aug 10, 2009 · Emb ERJ190100IGW · Main Landing GearSDR CA090813003Actuator · malfunctioned(CAN) SLAT FAIL CAUTION ON APPROACH. QRH CARRIED OUT, AND MSG PERSISTS. FIM ACCOMPLISHED, FOUND SLAT ACTUATORS NR 5 AND 8 TRIPPED TORQUE LIMITER INDICATORS. RE-SET PER AMM. NR 8: P/N 1703911, S/N 0320, MFR: HAMILTON SUNDSTRAND (TC# 20090813003)Aug 8, 2009 · Emb ERJ190100IGW · Leading Edge Slat ActuatorSDR CA090813002Landing Gear · malfunctioned(CAN) LANDING GEAR DISAGREE MASTER WARNING FOLLOWING GEAR EXT ON APPROACH. RT MAIN GEAR SHOWED UP. MISSED APR CARRIED OUT. ON SUBSEQUENT EXTENSION, RH GEAR REMAINED UP (YAW FELT). CYCLED PER QRH, THEN SHOWED ALL 3 DOWN AND LOCKED. BLED BOTH THE RT AND LT UPLAug 5, 2009 · Emb ERJ190100IGW · Landing Gear Retraction/Extension SystemSDR CA090813001Landing Gear · lack of lube(CAN) LG LEVER DISAGREE EICAS MSG WITH GEAR SELECTED DOWN. RT MAIN SHOWING UP. MANUAL EXTENSION REQUIRED. FOUND RT MLG VERY CLEAN (NO GREASE). ALL 3 GEARS LUBED PER AMM. (TC# 20090813001)Aug 4, 2009 · Emb ERJ190100IGW · Landing Gear Retraction/Extension SystemSDR CA090813012Structure · corrodedFWD CARGO LWR CTR SEAL REST, UPPER FWD AND AFT SILL DOUBLER PLATES, SCUFF PLATE SUPPORTS, AND ATTACHMENT HARDWARE HAVE CORROSION. THIS IS THE 2ND ACFT TO HAVE THIS PROBLEM FOUND AFTER SILL SCUFF PLATES REMOVED. BELIEVE THE CAUSE MAY BE DUE TO LACK OF CORROSIOJul 23, 2009 · Emb ERJ190100IGW · Fuselage Miscellaneous StructureSDR CA091112001Rod · bent(CAN) DURING ACCOMPLISHMENT OF SCHEDULED JC 3-327N, IT WAS FOUND THAT BOTH LT & RT AFT FLAPS FWD/LWR OPERATIING RODS WERE BENT. BOTH ROD ASSY WERE REPLACED. THIS IS A KNOWN PROBLEM WITH THE FLEET (WORLD WIDE). IT IS SUSPECTED THE ICE AND OTHER FOREIGN MATTERJun 25, 2009 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA090629002Counterbalance · corroded(CAN) PAINT PEELING AND VISIBLE CORROSION ON RUDDER COUNTERBALANCE WEIGHT. A ROUTINE VISUAL INSP OF RUDDER UNCOVERED AN INDICATION OF PAINT PEELING FROM THE RUDDER COUNTERBALANCE WEIGHT. FURTHER INVESTIGATION SHOWED VISIBLE SIGNS OF CORROSION ON COUNTERBALANJun 22, 2009 · Emb ERJ190100IGW · Rudder Miscellaneous StructureSDR CA090610004Link · misinstalled(CAN) UPON INSPECTION THE R/H NOSE LANDING GEAR FIXED DOOR LINKAGE WAS FOUND NOT IN SAFETY AT GEAR DOOR END. THE NUT, LOCKWIRE AND LOCKPLATES WERE LOOSE AND EASILY SPUN ON ROD END. A PIECE OF ALUMINUM CASTING WAS FOUND BROKEN ON THE LINK TOWARDS ROD END NEAR BJun 9, 2009 · Emb ERJ190100IGW · Landing Gear Door Retract SectionSDR CA090504004Slide · no test(CAN) DURING ESCAPE SLIDE FUNCTION CHECK ON RT SERVICE DOOR, SLIDE FAILED TO DEPLOY. ON SLIDE DEPLOYMENT DOOR PARTIALLY OPENED APPROX 6 INCHES-8 INCHES AWAY FROM FUSELAGE AND JAMMED. SLIDE WAS NOT FULLY UNLACED, FORCE WAS APPLIED TO HINGE ARM TO ASSIST DOOR OMay 1, 2009 · Emb ERJ190100IGW · Escape SlideSDR CA090428002Brake · damaged(CAN) DURING MX INSP FOLLOWING A PIECE OF BRAKE DISK FOUND ON THE APRON, ALL 4 BRAKE ASSEMBLIES ON THE ACFT WERE FOUND FAILED. 3 WERE FOUND WITH ROTORS AND STATORS BROKEN, REMAINING WAS FOUND HAVING THE CLIPS ON THE ROTORS LOOSE DUE TO WORN RIVETS/RIVET HOLES.Apr 27, 2009 · Emb ERJ190100IGW · Landing Gear Brake SystemSDR CA090417007Bearing · failedAFTER LANDING, FLIGHT CREW OBSERVED THAT THE NR 1 MW BRAKE TEMP WAS 300 DG WHILE THE OTHERS WERE AT 100 DG. MAINTENANCE FOUND BEARING ROLLERS INSIDE THE WHEEL/BRAKE ASSEMBLY. MAIN WHEEL WAS REMOVED FOR INVESTIGATION, BRAKE WAS SEIZED ON THE AXLE AND HAD TO BApr 15, 2009 · Emb ERJ190100IGW · Wheel/Ski/FloatSDR CA090326004Skin · deformed(CAN) LT AND RT LWR WING SKIN DEFORMATION FOUND IN AREA OF RIBS 21-22 AND STRINGER 23-25 BETWEEN NACA DUCT PANELS AND THE PRESSURE RELIEF PANEL.Mar 22, 2009 · Emb ERJ190100LR · Wing, Plate/SkinSDR CA090306002Floorbeam · corroded(CAN) AFT GALLEY FLOOR AREA WAS FOUND WITHOUT SEALANT BETWEEN THE FLOORBOARDS. WITH FLOORBOARDS REMOVED, CORROSION WAS DISCOVERED ON SEVERAL FLOORBEAMS, SEAT TRACKS AND SHEAR PLATES.Feb 27, 2009 · Emb ERJ190200LR · Fuselage Main, Floor BeamSDR CA090219003Connector · damaged(CAN) DURING GALLEY REMOVAL, ELECTRICAL CONNECTORS FOUND WITH DAMAGED/MISSING BACKSHELLS.Feb 18, 2009 · Emb ERJ190100IGW · Equipment/Furnishings WiringSDR CA090220002Control Tube · bent(CAN) ACFT, AFTER COMPLETING REF/A/B, MX NOTICED BOTH THE LT AND RT AILERON TORQUE TUBE ASSEMBLIES WERE BENT. CABLES FOUND LOOSE UPON ARRIVAL. ALL AILERON CABLES TIGHTENED ACCORDING TO REF/A/AND/B/AND. DUE TO CURVATURE OF TUBES, CABLES ARE NOW SITTING LOWFeb 17, 2009 · Emb ERJ190100LR · Aileron Control SystemSDR CA090204001Wheel · failedTHE RIGHT MAIN TIRE WAS BLOWN ON LANDING. THERE WAS TIRE DEBRIS FOUND ON RUNWAY. ENGINEERING BELIEVE THIS TO BE CAUSED BY A FROZEN BRAKE. OTHER P/N (O/B HALF WHEEL) IS 90002318, S/N IS JUL06-0529.Jan 29, 2009 · Emb ERJ190100IGW · Wheel/Ski/FloatSDR CA090115003Brake · damaged(CAN) ACFT BRAKE ROTATING DISCS HAVE DAMAGED AND MISSING ROTOR LUGS. WHEN REMOVING NR 1 MAIN WHEEL PARTS OF THE ROTATING DISCS FELL TO THE FLOOR. UPON FURTHER INVESTIGATION ADDITIONAL DAMAGED LUGS WERE NOTED. SB 90002340-32-02 RELATES TO THE INSPECTION OF TJan 14, 2009 · Emb ERJ190100IGW · Landing Gear Brake SystemSDR CA081201001Seat Back · loose(CAN) THE ATTACH SCREWS HOLDING SEAT BACK BRACKET TO SEAT ARM ARE LOOSE, THE BRACKET ATTACHES THE SEAT BACK TO THE ARM. THE SCREWS ARE 0.5 INCHES IN LENGTH, THE SWIVEL BRACKET ATTACH POINT WAS ALSO LOOSE. REF: 4/MM 41402003, IPL 25-22-90 PAGE 10044 FIGURE 7 ITNov 28, 2008 · Emb ERJ190100IGW · Flight Compartment EquipmentSDR CA081113004Duct · split(CAN) LT PRECOOLER INLET RUBBER DUCT SHOWS SIGNS WHERE THE SEAM HAS COME APART, AS A RESULT THE FAN AIR HAS FROM THE SPLIT SEAM HAS CAUSED DAMAGE TO THE THRUST REVERSER HEAT SHIELD. T/R FIRE BLANKET PN 104M1031-22, SN6011203-013 THIS HAS ALSO OCCURRED ON ACFT Nov 12, 2008 · Emb ERJ190100IGW · Engine Bleed Air SystemSDR CA081023003Wire Harness · damaged(CAN) ON FLAP RETRACTION AFTER T/O. SLAT FAIL EICAS MSG DISPLAYED. CARRIED OUT QRH FOR SLAT FAIL. DID NOT RECTIFY PROBLEM. ACFT RETURNED RT SLAT SKEW SENSOR HARNESS W611 REPLACED AS PER AMM 27-83-07 PB 401, RT SLAT 2/3 SKEW SENSOR REPLACED AS PER AMM 27-83-01Oct 19, 2008 · Emb ERJ190100IGW · Flight Control System WiringSDR CA081022002Control Module · failed(CAN) AFTER LANDING, DURING DECELERATION ON RUNWAY AT APPROX 80 KTS, LT AND RT BRAKE FAULT MSG APPEARED ON EICAS ACCOMPANIED BY COMPLETE LOSS OF BRAKING. AFTER APPROX 8 SECONDS BRAKING RETURNED TO NORMAL AND EICAS MSG DISAPPEARED. SERVICE NEWS LETTER SNL190-32Oct 14, 2008 · Emb ERJ190100IGW · Landing Gear Brake SystemSDR CA081023002Restrictor Valve · cracked(CAN) HYD LEAK 10 DPM ON SYS NR2 RETURN LINE AND UNION FREE FALL SELECTOR VALVE RT WW AREA. WRENCH CHECK NIL FIX. FOUND RESTRICTOR VALVE CRACKED ON EMERGENCY EXTENSION SELECTOR VALVE. RESTRICTOR VALVE REPLACED, BUT STILL HAD A LEAK. UPON CLOSE INSP, FOUND A VEOct 13, 2008 · Emb ERJ190100IGW · Hydraulic System, MainSDR CA081016009Wire Harness · defective(CAN) SLAT FAIL MESSAGE ON FLAP 5 SELECTION ON APPROACH. CREW CARRIED OUT A MISSED APPROACH, QRH WAS FOLLOWED AND LANDED UNEVENTFULLY ON SECOND TRY. SLAT HARNESS REPLACED, OPS TEST CARRIED OUT IAW AMM 27-80-00-710-801A, NO FAULTS NO EICAS MESSAGES.Oct 10, 2008 · Emb ERJ190100IGW · Flight Control System Wiring
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