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 CA140103013Sensor · corroded(CAN) ON DEPARTURE ACFT WAS UNABLE TO RETRACT FLAPS. IN CONSULT WITH MOC AND BEING ADVISED THIS IS A REOCCURRING ISSUE A DIVERSION BACK WAS REQUIRED. CREW AND DISPATCH DETERMINED FLIGHT WOULD BE BETWEEN 3500-4000KGS OVER LANDING ON RWY. CREW ASKED FOR TRUCKSJan 1, 2014 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating SystemSDR CA140103011Sensor · failed(CAN) ON APPROACH, HAD SLAT FAILURE, INITIATED GO-AROUND AND RETURNED FOR A NORMAL LANDING ON RWY. REPLACED LT OTBD SLAT SKEW SENSOR S3/4 IAW AMM 27-83-01. ELECTRICAL RIGGING OF SLAT CONTROL SYSTEM CARRIED OUT IAW AMM 27-80-00-TASK 27-80-00-820-802A. SYSTEM FDec 31, 2013 · Emb ERJ190100IGW · Trailing Flap Position Indicating SystemSDR CA131223004Pressure Valve · failed(CAN) CREW REPORTED A FUEL SPILL OF APPROXIMATELY 20 FT X 20 FT, APPROXIMATELY 300-400K. FUEL SHEET CALLED FOR 11,600K AND FUELLER COULD NOT GET MORE THAN 11,000K ON THE ACFT. NO PASSENGERS ON BOARD. FIM TASK 28-25-12-00 CARRIED OUT. WING TANKS PRESSURE REDec 22, 2013 · Emb ERJ190100IGW · Aircraft Fuel Distribution SystemSDR CA131218021Unknown · odor(CAN) ON DEPARTURE, A FUME ODOR WAS DETECTED IN THE FLIGHT DECK. CREW WAITED A COUPLE OF MINUTES FOR THE FUME TO DISSIPATE IAW A BULLETIN. WHEN FUMES DID NOT DISSIPATE THE CREW DECLARED A PAN PAN AND RETURNED TO DEPARTURE, WHERE AN UNEVENTFUL OVERWEIGHT LANDDec 18, 2013 · Emb ERJ190100IGW · Air Distribution SystemSDR CA131219006Blade · cracked(CAN) AT REMOVAL OF BLADE, SHIMS, RETAINER AND SPACER, TECH FOUND IMPRESSIVE QTY OF PARTS WORN CRACKED. THIS AIRCRAFT IS FLYING WITH NEW SPINNER, SPINNER SUPPORT AND BLADE RETAINER FROM SBCF-10E-SB72-0242-00.Dec 17, 2013 · Emb ERJ190100IGW · Turbine Engine Compressor SectionSDR CA131217001Pump · failed(CAN) APPROXIMATELY 1HR SOUTH HYDRAULIC QUANTITY LEVEL ON NR 1 BEGAN TO DROP. A PATCH WAS DONE THROUGH SFO AND MOC THRU DISPATCH. THE LEVEL CONTINUED TO DROP TILL IT WENT INTO THE BLUE LEVEL. NR 1 EDP FAILED. CREW DECLARED A PAN PAN ABOUT 15 MINS OUT. CFRDec 16, 2013 · Emb ERJ190100IGW · Hydraulic Pump (Electric/Engine), MainSDR CA131212009Apu · overtemp(CAN) APU IS GOING INTO AMBER TEMP APPROXIMATELY 740 DEGRESS DURING START OF THE NR 1 ENG ONLY. APU REPLACED.Dec 5, 2013 · Emb ERJ190100IGW · APU Core EngineSDR CA131205004Bearing · corroded(CAN) BEARING STOP, DISCOVERED CRACKED DURING STIFF AILERON INVESTIGATION. REPLACED BEARING.Dec 4, 2013 · Emb ERJ190100IGW · Aileron Control SystemSDR CA131129008Wire Harness · failed(CAN) JUST AFTER TAKEOFF CREW RECEIVED A WING A/ICE 1 LEAK EICAS. QRH DIRECTED CREW TO EXIT/AVOID ICING CONDITIONS. AFTER CONSULTATION WITH SOC/DISPATCH, CREW DIVERTED. W513 HARNESS REPLACED AND OPS NORMAL. AMM 30-11-02.Nov 28, 2013 · Emb ERJ190100IGW · Flight Control System WiringSDR CA131128007Sensor · failed(CAN) UPON REACHING TOP OF CLIMB A SLAT FAIL EICAS CAUTION WAS GENERATED. FLIGHT CONTINUED AND LANDED IN A SLAT 0, FLAP 2, CONFIGURATION. REPLACED LT OTBD SLAT SKEW SENSOR .7500 AND RT OTBD SLAT SKEW SENSOR IAW AMM 27-83-01. ALSO REPLACED RT OTBD SLAT SKEW SNov 27, 2013 · Emb ERJ190100IGW · Leading Edge Slat Position Indicating SystemSDR CA131128004Vent Line · damaged(CAN) TAIL PIPE OIL LEAK AND THE CENTER VENT TUBE, CVT, FLATTENED ON THE NR 2 ENGINE. HERE IS THE EXPLANATION FROM MFG: ACCEPTED THEORY "CVT UNDERGOES BUCKLING DUE TO OVER-PRESSURIZATION CAUSED BY DEFLAGRATION, SUBSONIC COMBUSTION", "VAPORIZED OIL/AIR MIXTUNov 26, 2013 · Emb ERJ190100IGW · Engine (Turbine/Turboprop)SDR CA131125002Nut · loose(CAN) LT AND RT MLG SHIMMY DAMPERS BOTH FOUND WITH LOOSE JAM AND FLANGED NUTS. MPN 2225-0070 AND 2225-0069, RESPECTIVELY. REF IPC 32-11-03, FIG 01 ITEMS 60 AND 70. BOTH SHIMMY DAMPERS RETORQUED IAW AMM 32-11-03, SUBTASK 212-005-A.Nov 21, 2013 · Emb ERJ190100IGW · Shimmy DamperSDR CA131111019Actuator · failed(CAN) ON DESCENT, FLIGHT COULD NOT SELECT FLAP 1, SLAT 3 SELECTED. EMERGENCY WAS NOT DECLARED. REPLACED LT NR 2 FLAP ACTUATOR IAW AMM 27-51-01, PB 401 AS INTENTIFIED BY FC 27512014ACE AND TRIP WIRE.Nov 9, 2013 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA131111021Door · unsecure(CAN) AFTER DEPARTURE, FLIGHT RECEIVED LT PASSENGER EXIT DOOR INDICATION, ACCOMPANIED BY A WHISTLING SOUND. PRESSURIZATION TO A160 WAS NORMAL. INSTEAD OF CROSSING OVER THE ROCKIES, ELECTED TO RETURN TO DEPARTURE. FLIGHT WAS NOT OVERWEIGHT WHEN THEY LANDED, ANov 9, 2013 · Emb ERJ190100IGW · Emergency ExitsSDR CA131108002Tube · failed(CAN) DURING CRUISE, THE CREW RECEIVED A SYS 2 LOW HYDRAULIC FLUID INDICATION. THE LEAK CONTINUED FOR 30 MINUTES UNTIL THE SYS WAS EMPTY AND THE PUMP FAILED. THE QRH WAS CARRIED OUT AND A PAN WAS DECLARED WITH ATC. THE FLIGHT LANDED WITHOUT FURTHER EVENT WINov 7, 2013 · Emb ERJ190100IGW · Hydraulic System, MainSDR CA131108003Controller · failed(CAN) ENROUTE FLIGHT EXPERIENCED A "FLAP FAIL" ECAM MESSAGE. QRH WAS CARRIED OUT AND ATC WAS ADVISED WITH A PAN DECLARED. THE ACFT LANDED WITHOUT FURTHER INCIDENT. THE ACFT STOPPED ON THE RUNWAY FOR EMERGENCY RESPONSE SERVICES TO INSPECT THE ACFT BEFORE TAXINov 7, 2013 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA131106001Line · chafed(CAN) FOUND DURING B-03 CHECK BOTH LT AND RT FUEL FEED LINES FROM THE WING SPAR TO THE PYLON ARE CHAFING AGAINST THE CLAMP COUPLER. IPC 28-21-21-09, ITEM 160. REPLACEMENT OF THE SLEEVE CONNECTING FUEL FEED LINE.Nov 5, 2013 · Emb ERJ190100IGW · Aircraft Fuel Distribution SystemSDR CA131106002Line · chafed(CAN) PERFORMING SB190-57-0016-01 MRO DICOVERED THE FUEL FEEL LINE IS CHAFING AGAINST THE CLAMP COUPLER. REPLACED SLEEVE CONNECTING FUEL FEED LINE.Nov 5, 2013 · Emb ERJ190100IGW · Aircraft Fuel Distribution SystemSDR CA131104001Windshield · failed(CAN) THE ACFT ENCOUNTERED A CRACKED RT OUTER WINDSHIELD DURING CRUISE. THE FLIGHT CREW FOLLOWED THE QRH AND OPERATED OTHERWISE NORMALLY INTO STATION, WHERE THEY WERE MET BY MAINTENENCE. NEW CO-PILOT WINDSHELD INSTALLED IAW AMM 56-11-00-400-801/801/A.Nov 1, 2013 · Emb ERJ190100IGW · Flight Compartment WindowsSDR CA131031006Line · damaged(CAN) FOUND ACFT WITH FUEL FEED LINGE FLANGE GROOVED BY THE ATTACHING CLAMP.Oct 30, 2013 · Emb ERJ190100IGW · Aircraft Fuel Distribution SystemSDR CA131030001Oven · fod(CAN) AFTER PUSHBACK THE CABIN CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE AFT GALLEY. THE FLIGHT RETURNED TO THE GATE FOR INVESTIGATION. OVEN NOTED TO BE CONTAMINATED WITH FOOD DEPOSITS. OVEN CLEANED, C/B RESET, FUNCTION CHECKED, NO RECURRENCE OF ODOR Oct 29, 2013 · Emb ERJ190100IGW · Buffet/GalleysSDR CA131031007Line · damaged(CAN) RT WING FUEL FEED FLANGE ASSY FOR ENGINE 2 FUEL LINE THROUGH/FRONT SPAR IS GROOVED. RT WING FUEL FEED FLANGE ASSY FOR ENG 2 FUEL LINE THROUGH/FRONT SPAR REPLACED IAW AMM 28-21-21. RIGHT PYLON MAIN FUEL FEED LINE RECONNECTED AT PYLON FIREWALL IAW AMM28Oct 11, 2013 · Emb ERJ190100IGW · Aircraft Fuel Distribution SystemSDR CA131010003Control Module · failed(CAN) AFTER TAKEOFF, AUTO-THRUST FAILED WITH AIRSPEED LOSS. FLIGHT RETURNED T/O FOR MAINTENANCE, DID NOT DECLARE EMERGENCY. APPROXIMATE LANDING WEIGHT 42,000 KGS. IAW CMC FC- 22110019FA2 AND 22310019TA1 IAW TASK- 22-11-00-811-875-A. FAULT ISOLATION PROCEDOct 9, 2013 · Emb ERJ190100IGW · Central ComputersSDR CA131010004Throttle · failed(CAN) REJECTED T/O AT 76 KNOTS OFF DUE AUTO THROTTLE FAILING TO HOLD BOTH ENGINES AND THE LT AUTO-THROTTLE FAILED. MOC ADVISED, FLIGHT RETURNED TO GATE. TCQ REPLACED AND TESTED IAW AMM 76-11-01, ENGINE RUNS CARRIED OUT AND OPS NORMAL.Oct 9, 2013 · Emb ERJ190100IGW · Power LeverSDR CA131007022Circuit Board · overheated(CAN) BURNING ELECTRICAL ODOR. SUSPECT IFE. SHUTDOWN IFE SYSTEM. ODOR DISSIPATED. ALL PSU PCB BOARD REPLACED IAW CMM 25-28-66 AND TESTED SERVICEABLE IAW AMM 33-24-00-710-801A AND AMM 33-25-00-710-801-A.Oct 5, 2013 · Emb ERJ190100IGW · Equipment/Furnishings WiringSDR CA131001009Slat System · failed(CAN) SLAT FAIL MESSAGE ON INITIAL APPROACH. FOLLOWED QRH PROCEDURE, FAULT CLEARED. NO OTHER DETAILS PROVIDED.Sep 30, 2013 · Emb ERJ190100IGW · Leading Edge Slat Control SystemSDR CA130930004Oil System · low pressure(CAN) ACFT WAS IN CRUISE, WHEN THE CREW NOTICED THE NR 1 ENGINE OIL PRESSURE AND OIL LEVEL DROPPING RATHER QUICKLY. THE CAPT ELECTED TO TURN. QTY SHOWED 2.6 AT THAT POINT THE CREW ELECTED TO SHUTDOWN THE ENGINE. THE FLIGHT WAS MET AND CHECKED OVER ON THE RSep 29, 2013 · Emb ERJ190100IGW · Engine Oil PressureSDR CA130927009Transducer · failed(CAN) LANDED AND HAD A BRAKE LOCK UP. DECLARED EMERGENCY WITH ATC. LEFT THE RWY AND SHUTDOWN ON TAXIWAY A4 WHERE EMERGENCY VEHICLES CAME OUT TO COOL THE BRAKES. MOC ADVISED. BRAKE O/TEMP FIM TASK 32-40-00-810-801-A CARRIED OUT IAW STEP C, MAIN BRAKE PASSESep 26, 2013 · Emb ERJ190100IGW · Landing Gear Brake SystemSDR CA130919004Flap System · failed(CAN) WHILE ON APPROACH FOR RWY 18, CREW EXPERIENCE A FLAP/SLAT FAILURE AND DID A GO AROUND. NO FAULTS ON ARRIVAL CMC INTERIGATED FAULT MSGS TROUBLESHOOTING CARRIED OUT IAW FIM 27-36-00-810-877-A00 AND 27-36-00-810-860-A00 IS A TRANSITORY CONDITION OF THE COSep 18, 2013 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA130916004Pneumatic System · malfunctioned(CAN) THE FLIGHT DEPARTED WITH AN AIR CONDITIONING PACK ALREADY ON MEL. DURING CRUISE, THE ACFT ENCOUNTERED AN ENGINE BLEED LOSS, RENDERING THE OTHER AIR CONDITIONING PACK ALSO UNSERVICEABLE. IAW STANDARD PROCEDURE FOR THIS SITUATION, THE FLIGHT CREW DECLARESep 10, 2013 · Emb ERJ190100IGW · Pneumatic Distribution SystemSDR CA130916005Fadec · malfunctioned(CAN) DURING CRUISE, THE ACFT ENCOUNTERED A NR 2 ENGINE SHUTDOWN. AS A PRECAUTION, THE FLIGHT CREW DECLARED A PAN PAN FOR PRIORITY TO DESCEND. INTERROGATED CMC, ENGINE NR 2 NO DISPATCH EICAS MESSAGE AND FADEC NR 2 FAULT ADVISORY. FADEC NR 2 REPLACED IAW AMMSep 10, 2013 · Emb ERJ190100IGW · Fuel Controlling SystemSDR CA130918013Oxygen Mask · damaged(CAN) DURING EMERGENCY DECENT THE CAPTAIN USED THE OXYGEN MASK. DURING THE REMOVAL OF THE MASK FROM THE STOWED POSITION, THE HARNESS INFLATION CENTRAL VALVE & OXYGEN SUPPLY CONTROL KNOB SEPARATED FROM THE MASK. THIS LEFT THE MASK HARNESS CONTINUALLY INFLATESep 10, 2013 · Emb ERJ190100IGW · Crew Oxygen SystemSDR CA130913001Bleed Air Sys · contaminated(CAN) DIRTY SOCK ODOR REPORTED BY CABIN CREW JUST PRIOR TO APPROACH. COMPLAINED OF DIZZINESS & NAUSEA. ENGINE BLEED SYS, 1 INOPERATIVE, OPTION 1, RESOLUTION ENGINE 2 BOROSCOPE INSPECTION, C/O IAW 72-00-00-200-803, FWD OF HPC STG 1 -NFF. ENGINE 1 BOROSCOPE CSep 8, 2013 · Emb ERJ190100IGW · Engine Bleed Air SystemSDR CA130911011Actuator · failed(CAN) AFTER TAKEOFF, UPON FLAP 2, RETRACTION NOTICEABLE VIBRATION OCCURRED ON BOTH FLIGHT CONTROLS. VIBRATION PERSISTED AFTER FLAP 1 RETRACTION, AS SPEED INCREASED SO DID VIBRATION. RETURNED TO DEPARTURE AND AUTOPILOT WAS SELECTED OFF WITH VIBRATION PRESENT Sep 6, 2013 · Emb ERJ190100IGW · Elevator Control SystemSDR CA130905011Flap System · failed(CAN) THE FLIGHT CREW HAD A FLAP FAILURE ON APPROACH. THE FLIGHT PERFORMED A MISSED APPROACH AND WAS ABLE TO SELECT THE FLAPS SUCCESSFULLY ON THE SECOND TRY LANDING RUNWAY 35R. QRH PROC CARRIED OUT AND FLAPS RESET SUCCESSFULLY.Aug 31, 2013 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA130830012Engine · failed(CAN) NR 2 ENGINE FAILED ON TAXI OUT TO RUNWAY. NR 2 ENGINE FAILED ON EICAS.Aug 30, 2013 · Emb ERJ190100IGW · Engine (Turbine/Turboprop)SDR CA130829001Adc · malfunctioned(CAN) CREW REPORTED THAT DURING CRUISE THEY EXPERIENCED UNRELIABLE AIRSPEED INDICATIONS, ERRATIC INSTRUMENT INDICATIONS, A FAILED AUTOPILOT AND AN APPROXIMATE 400FT ALTITUDE DEVIATION. UNRELIABLE AIRSPEED/ALTITUDE WITH AP/AT FAIL AFCS FAULT & ADS PROBE 1 FAILAug 27, 2013 · Emb ERJ190100IGW · Air Data ComputerSDR CA130827002Engine · fire(CAN) ON ARRIVAL AT THE GATE A RAMP CREW MEMBER NOTICED FLAMES IN THE TAILPIPE OF THE LT ENGINE AND THEN DISCHARGED A PORTABLE FIRE EXTINGUISHER THROUGH THE FRONT OF THE ENGINE. FLIGHT CREW WAS NOT AWARE OF ANY ISSUES UNTIL AFTER THE EVENT, ERS WAS NOT CALLEDAug 26, 2013 · Emb ERJ190100IGW · Engine (Turbine/Turboprop)SDR CA130823007Radio · failed(CAN) FLIGHT CREW ADVISED FLIGHT DISPATCH VIA ACARS MSG OF A TOTAL COMM FAILURE. THEY WERE BROADCASTING BLIND, AND SQUAWKING 7600. BECAUSE ACARS CONTINUED TO WORK, FLIGHT DISPATCH COORDINATED WITH THE APPROPRIATE ATC FACILITIES TO FACILITATE CONTINUING TO DEAug 22, 2013 · Emb ERJ190100IGW · Communications SystemSDR CA130823008Line · ruptured(CAN) ON THE TAXI IN, ENGINE NR 1 RUNNING, ENGINE NR 2 WAS OFF. LOW QTY INDICATION HYD 1. MAINTENANCE INVESTIGATION REVEALED THERE WAS A LEAK AND HYDRAULIC QUANTITY WAS ZERO. ACFT OFF-LINE FOR REPAIR. NR 1 ENGINE EDP HIGH PRESSURE LINE RUPTURED IN FWD PYLONAug 22, 2013 · Emb ERJ190100IGW · Hydraulic System, MainSDR CA130819017Spoiler Sys · failed(CAN) FLIGHT CONTROL SPOILER FAULT IN CRUISE. PAN PAN DECLARED WITH ATC. CFR WAS ON STANDBY FOR ARRIVAL. ACFT WAS INSPECTED, ACFT ON ARRIVAL AND TAXIED TO GATE. PASSENGERS WERE BRIEFED PRIOR TO ARRIVAL WITH NO ADVERSE REACTIONS FROM PASSENGERS. POWERED DOWN Aug 18, 2013 · Emb ERJ190100IGW · Drag Control SystemSDR CA130820001Actuator · failed(CAN) FLAP FAIL AT APPROXIMATELY 500 FT ABOVE ON SHORT FINAL WHEN SELECTING FINAL FLAP. GO-AROUND INITIATED, CARRIED OUT QRH PROCEDURE, CYCLED FLAPS AND ALL NORMAL. NO ADVERSE PASSENGER REACTION. NR 3 RT WING FLAP TRANSMISSION ACTUATOR REPLACED IAW AMM 27-51-Aug 10, 2013 · Emb ERJ190100IGW · Trailing Edge Flap ActuatorSDR CA130805016Anti-Skid Sys · failed(CAN) ON SHORT FINAL TO LAND THE CREW RECEIVED A LT BRAKE FAULT INDICATION AND ELECTED TO GO AROUND. WHILE CARRYING OUT THE CHECKLIST THEY RECEIVED A RT BRAKE FAULT INDICATION. THE CREW DECLARED AN EMERGENCY, LANDING WAS CARRIED OUT WITH NO FURTHER COMPLICATAug 2, 2013 · Emb ERJ190100IGW · Brake Anti-Skid SectionSDR CA130729022Acm · failed(CAN) AIR RETURN DUE TO SMOKE ODOR IN THE COCKPIT AND CABIN REPORTED, PAN PAN DECLARED, ARFF CALLED OUT. OVERWEIGHT LANDING. NR 2 PACK ACM REPLACED IAW AMM 21-51-05-PB401. DUAL HEAT EXCHANGER CLEANED WITH STEAM CLEANER.Jul 29, 2013 · Emb ERJ190100IGW · Cabin Cooling SystemSDR CA131125004Duct · cracked(CAN) DURING THE PROCESS OF REPLACING NR 2 ENGINE PRECOOLER, PRECOOLER DUCT WAS REMOVED FOR SEAL CHANGE. DUCT WAS INSPECTED. CRACKS FOUND ON THE DUCT IN 3 LOCATIONS.Jul 3, 2013 · Emb ERJ190100IGW · Pneumatic Distribution SystemSDR CA130702004Module · failed(CAN) EMERGENCY DECLARED WITH ATC ACCOUNT OF BRIEF FIRE INDICATION. NO SMOKE VISIBLE IN ACFT BUT CABIN TEMPERATURE INCREASING. GENERIC O/O NR 3 REPLACED IAW AMM 31-41-06. CARGO HI-RATE BOTTLE REPLACED IAW AMM 26-23-01. CARRIED OUT WIRING CHECK IAW WDM 26-23Jun 30, 2013 · Emb ERJ190100IGW · Central ComputersSDR CA130625008Filter · dirty(CAN) EMERGENCY DECLARED DUE TO SMOKE IN THE COCKPIT AND PASSENGER CABIN DURING TAKEOFF ROLL, REJECTED T/O AT APPROXIMATELY 135 KTS. FIRE TRUCKS CALLED OUT. PASSENGER REACTION CALM. TROUBLESHOOTING C/O IAW 21-20-00-810-803A, NO FAULTS USING APU BLEED OR NR Jun 22, 2013 · Emb ERJ190100IGW · Air Distribution SystemSDR CA130625007Transmitter · malfunctioned(CAN) CAPTAIN SAW NR 1 ENGINE LOW OIL PRESSURE EICAS WARNING. CROSS CHECKED THE OIL PRESSURE WHICH WAS SHOWING ZERO, AND WENT THROUGH THE CHECK LIST IN THE QRH. THE NR 1 ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED WITH ATC AND THE FLIGHT DIVERTED. LANDINGJun 21, 2013 · Emb ERJ190100IGW · Engine Oil PressureSDR CA130620002Flap System · out of rig(CAN) LEFT INBD LOWER ROD ON NR 1 FLAP TRACK FOUND BENT ON ARRIVAL. AFTER MECHANICAL RIGGING COMPLETED FOUND INBD FLAP MECHANISM UPPER AND LOWER RODS AND FLAP MECHANISM NR 2 UPPER AND LOWER RODS NOT PROPERLY ADJUSTED. MECHANICAL RIGGING OF LT AFT FLAP, FLAP TRJun 18, 2013 · Emb ERJ190100IGW · Trailing Edge Flap Control SystemSDR CA130620007Rod · bent(CAN) FOUND LT INBD FLAP TRACK MECHANISM LOWER ROD BENT AND RT INBD FLAP TRACK NR 2 MECHANISM LOWER ROD BENT. FOUND BOTH INBD AFT FLAPS TO BE OUT OF RIG. MECHANICAL RIGGING OF LT AFT FLAP, FLAP TRACK 1 & 2, C/OUT IAW AMM 27-50-00-820-801-1. CHECKS SERVICEABJun 18, 2013 · Emb ERJ190100IGW · Trailing Edge Flap Control System
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