Embraer EMB-120ER

Service difficulty reports · 8,287

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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 aircraft_model_key = 'EMB120ER'
  ORDER BY difficulty_date DESC"

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SDR SWIA972369Indicator · failedON TAKEOFF AT 80 KTS, HIGH SPEED AURAL SOUNDED. ABORTED TAKEOFF. REMOVED AND REPLACED FIRST OFFICERS HIGH SPEED INDICATOR WITH SERVICEABLE. PERFORMED OPS CHECK WITH PITOT STATIC BOX. OPS CHECK GOOD. LEAK CHECK GOOD IAW MM 34-12-01. (S/N ON: 1795) (S/N OFeb 11, 2001 · N576SW · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA972362Engine · fluctuatesCLIMBING THROUGH 15,000 FT EXPERIENCED LARGE ENGINE FLUCTUATIONS (TORQUE DROPS OF 25 TO 45 PERCENT) POWER WAS REDUCED, RETURNED TO THE MFR APT. EECS DEF. CLEANED EEC CANNON PLUGS. OHMED EEC SYSTEM AND RAN EXTENSIVE GROUND CHECKS OF ALL PARAMETERS AND COULDFeb 11, 2001 · N234SW · Emb EMB120ER · Engine (Turbine/Turboprop)SDR SWIA972378Boot · tornENTIRE LEADING EDGE DEICE SYSTEM FAILED AT CRUISE. UPON INSPECTION FOUND A LARGE TEAR IN THE UPPER PORTION OF THE LEFT OUTBOARD BOOT. DIVERTED FROM RDM TO RDD. COMPLIED WITH REPLACEMENT OF LEFT OUTBOARD DEICE BOOT. OPS CHECK AND FUNCTIONAL CHECK GOOD OF LEFeb 10, 2001 · N578SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR C2XA01IA088Connector · looseIAH- DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY EXIT LIGHT AT SEAT 2A WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT ON MEL 33-51-01 CONTROL NUMBER 009385, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THEFeb 10, 2001 · N12715 · Emb EMB120ER · Emergency LightingSDR SWIA972359Actuator · seizedRUDDER TRIM FROZE IN ZERO POSITION IN FLIGHT. FLIGHT CONDITIONS VMC AT 7000 FEET. AFTER 10 MINUTES RUDDER TRIM WORKED FINE. INSPECTED RUDDER TRIMMING SYSTEM IAW EMB120 MM 27-23-00. WIPED MOISTURE FROM LINEAR ACTUATOR. RUDDER TRIM SYSTEM OPS CHECK GOOD.Feb 10, 2001 · N197SW · Emb EMB120ER · Rudder Tab Control SystemSDR C2XA01IA079Bulb · inoperativeIAH - FLIGHT 3534, DURING PRE-FLIGHT INSPECTION, ONE AISLE PATH EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE LIGHT ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND Feb 10, 2001 · N12715 · Emb EMB120ER · Emergency LightingSDR SWIA972364Light · inoperativeONE EMERGENCY LIGHT INOP AT ROW 7 FLOOR. REPLACED ONE EMERGENCY AISLE MONITOR UNIT AT ROW 7 FLOOR (P/N 10-1307-3). GROUND CHECK NORMAL.Feb 9, 2001 · N292UX · Emb EMB120ER · Emergency LightingSDR SWIA972349Connector · contaminatedFLAPS GET DISAGREEMENT WHEN RETRACTING FROM 15 DEGREES TO 0 DEGREES. CLEANED DEICE FLUID FROM BOTH OUTBOARD FLAP CONNECTOR PLUGS. OPS CHECK GOOD.Feb 9, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972347Handle · failedFLAP DISAGREEMENT AFTER TAKEOFF, WOULD NOT GO UP ABOVE 5 DEGREES TOTAL. OUTBOARD FLAP PAIR WOULD NOT GO ABOVE TWO LIGHT BARS ON FLAP PANEL. RETURNED TO SLC. REMOVED AND REPLACED FLAP SELECTOR HANDLE IAW MM 27-00-00. FAILED TEST FLIGHT. REMOVED AND REPLACEFeb 9, 2001 · N189SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972345Flight Dir · failedCAPTAINS COURSE SELECTOR NEEDLE TURNS ON ITS OWN INFLIGHT. UNABLE TO SELECT AND RETAIN A COURSE. RETURNED TO FAT. REPLACED CAPTAINS HCP AND CAPTAINS COURSE SELECTOR. OPS CHECKS GOOD IAW MM 34-21-00.Feb 9, 2001 · N221SW · Emb EMB120ER · Integrated Flight SystemSDR SWIA972340Actuator · malfunctionedFLAP DISAGREEMENT ON DEPARTURE, OUTBOARD FLAPS. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW EMB 120 MM 27-50-00. OPS CHECK AND LEAK CHECKED OK. P/N ON 320300-1007, S/N ON 0522, S/N OFF 0316.Feb 8, 2001 · N189SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972339Uplock Switch · malfunctionedLEFT GEAR DOOR INTERMITTENTLY WILL NOT RETRACT. (RED DISAGREEMENT LIGHT ON COLUMN A ON). ADJUSTED LEFT GEAR ACTUATOR IAW 32-30-00 AND UPLOCK PROX SWITCH ADJUSTED IAW 32-61-01. OPS CHECK GOOD.Feb 8, 2001 · N195SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972343Proximity Switch · out of adjON CLIMBOUT AFTER TAKEOFF RED B-RIGHT GEAR LIGHT CAME ON. CYCLED GEAR PER QRH ON GEAR RETRACTION RT MAIN DID NOT FULLY COME UP. EXTENDED GEAR AND GOT GOOD 3 GREEN INDICATION. RETURNED TO SLC. REPLACED TIGHT GEAR UPLOCK B-SYSTEM PROXIMITY SWITCH IAW 32-61-0Feb 7, 2001 · N190SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972337Actuator · failedOUTBOARD FLAPS WILL NOT RETRACT FULLY AFTER TAKEOFF. RETURNED TO EKO. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS CHECKS, LEAK CHECKS GOOD. P/N ON 320300-1007, S/N ON 0516, S/N OFF 1093.Feb 7, 2001 · N189SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR C2XA01IA204Light · inoperativeSJK - DURING C-CHECK INSPECTION, ONE CEILING EMERGENCY EXIT LIGHT AND ONE FLOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CEILING EMERGENCY EXIT LIGHT, AND OPERATIONALLY CHECKED THE FLOOR EMERGENCY EXIT LIFeb 6, 2001 · N15732 · Emb EMB120ER · Emergency LightingSDR C2XA01IA203Spar · crackedSJK - DURING C-CHECK INSPECTION, THE LEFT HAND AND RIGHT HAND SPAR CAPS WERE FOUND TO BE CRACKED AT RIB 17 USING EDDY CURRENT INSPECTION. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB-120 SRM 57-20-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN Feb 6, 2001 · N15732 · Emb EMB120ER · Wing SparSDR C2XA01IA202Support · crackedSJK - DURING C-CHECK INSPECTION, TWO WING SKIN SUPPORTS ON RIB 19, AND ONE SKIN SUPPORT ON RIB 20 OF THE LEFT WING WERE FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORTS IN ACCORDANCE WITH EMB-120 SRM 57-20-07, AND THE AIRCRAFT Feb 6, 2001 · N15732 · Emb EMB120ER · Wing Miscellaneous StructureSDR C2XA01IA076Circuit Breaker · trippedSHV - FLIGHT 3525, THE CREW REPORTED A SMOKE SMELL IN THE CABIN AREA. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE AVIONICS COOLING FAN CIRCUIT BREAKER TO BE POPPED. MAINTENANCE RESET THE CIRCUIT BREAKER,Feb 6, 2001 · N15730 · Emb EMB120ER · Air Distribution FanSDR GLBA2001029Plate · out of adjRETURN TO BLOCK - CARGO DOOR ANNUNCIATOR ILLUMINATED. ADJUSTED TARGET PLATE, OPS CHECKED SYSTEM GOOD.Feb 6, 2001 · N71GL · Emb EMB120ER · Door Warning SystemSDR SWIA972338Uplock Switch · out of adjWHEN LANDING GEAR WAS SELECTED UP THE RIGHT GEAR INDICATOR TWO RED LIGHTS, NO GREEN, AND WE COULD HEAR THAT A GEAR DOOR WAS OPEN. NORMAL INDICATIONS WHEN GEAR SELECTED DOWN. RETURNED TO MRY. ADJUSTED RIGHT MLG UPLOCK SWITCH IAW MM 32-61-01. SWUNG GEAR SEVEFeb 5, 2001 · N296SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972332Servo · failedWHEN CONTROL YOKE MOVED SIDE TO SIDE A NOISE IS HEARD IN THE FLOOR PANEL AREA. REPLACED AILERON SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON: 9961, S/N OFF: 5507.Feb 5, 2001 · N199SW · Emb EMB120ER · Autopilot Main ServoSDR C2XA01IA063Proximity Switch · inoperativeIAH - FLIGHT 3580, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, AND THE AIRCRAFT WAS Feb 5, 2001 · N47722 · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972333Windshield · malfunctionedEN ROUTE AT 22,000 FT NOTED SMOKE COMING FROM FORWARD PORTION OF GLARESHIELD. DIVERTED TO LAX. AFTER A DETAILED INSPECTION OF WIRING AND COMPONENTS LOCATED UNDER GLARESHIELD FOUND GROUND WIRE ON LT WINDSHIELD HEATING BLOCK TO HAVE BEEN ARCING AT THE TERMINALFeb 4, 2001 · N271YV · Emb EMB120ER · Windshield/Door Rain/Ice RemovalSDR SWIA972336Roller · damagedRIGHT DIRECT VISION WINDOW AFT ROLLER ASSEMBLY (ON BOTTOM) FELL APART. REPLACED SNAP RING ON AFT LOWER RIGHT DIRECT VISION WINDOW ROLLER. OPS CHECK GOOD.Feb 2, 2001 · N560SW · Emb EMB120ER · Flight Compartment WindowsSDR SWIA972328Actuator · malfunctionedFLAP CONTROL FAULT ON INBOARD FLAP PAIR, WHEN SELECTING FLAPS FROM 15 DEGREES TO 25 DEGREES ON LANDING. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR. OPS CHECKS AND LEAK CHECKS GOOD. P/N ON 320300-1005, S/N ON 0067, S/N OFF 0067.Feb 2, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972322Actuator · failedAFTER TAKEOFF, WHEN FLAPS WERE RETRACTED, CONTROL FAULT AND INBOARD FLAP LIGHT BAR (2ND DIGIT) ILLUMINATED. WHEN RESET PRESSED, LIGHT EXTINGUISHED APPROXIMATELY 10 SECONDS, THEN RE-ILLUMINATED. RETURNED TO FAT. MEGGER TESTED RIGHT INBOARD FLAP ACTUATOR WIREFeb 2, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972329Lock · failedDURING TAKEOFF ROLL, RED DOORS LIGHT ON MAP ILLUMINATED FOR ABOUT 2 SECONDS WITH POSSIBLE DOOR SPECIFIC LIGHT ILLUMINATING ON OVERHEAD PANEL. LIGHTS DID NOT REMAIN ON LONG ENOUGH TO DETERMINE WHICH OVERHEAD DOOR LIGHT ILLUMINATED. TAKEOFF ABORTED. RETURNED Feb 1, 2001 · N226SW · Emb EMB120ER · Door Warning SystemSDR SWIA972323Tab · bindingINFLIGHT WITH F/O AUTOPILOT ENGAGED THE AIRCRAFT LEVELED OFF TO CATCH THE COURSE AND FELT A VIBRATION LIKE TENSION BEING RELEASED ON THE CABLES TO THE AILERON. THE YOKE VIBRATED LEFT AND RIGHT, THEN EVERYTHING RETURNED TO NORMAL. DISENGAGED AUTOPILOT, TESTEDFeb 1, 2001 · N190SW · Emb EMB120ER · Aileron Tab Control SystemSDR SWIA972330Warning Light · illuminatedTRIM FAIL ILLUMINATED ON MAP. NO AURAL WARNING WHILE ON TAKEOFF ROLL. ABORTED TAKEOFF. MEL 22-10-1B, ELECT TRIM, MC 122. RE-RACKED NUMBER ONE AND NUMBER TWO APC-65S. OPERATED AND TESTED TRIM SYSTEM. NO DEFECTS NOTED, COULD NOT DUPLICATE.Feb 1, 2001 · N295SW · Emb EMB120ER · Data Recorders (Flight/Maintenance)SDR GLBA2001018Latch · damagedABORTED T/O, SERVICE DOOR ANNUNCIATOR ILLUMINATED. REPLACED LATCH, OPS CHECKED SYSYEM GOOD.Feb 1, 2001 · N297UX · Emb EMB120ER · Door Warning SystemSDR SWIA972315Wire · chafedDURING FLAP RETRACTION ON GROUND, GOT FLAP CONTROL FAULT AND ADVANCED SWS WITH INBOARD PAIR NOT MOVING. CLEARED ONLY AFTER RESET. REPLACED CHAFED WIRE AT LEFT INBOARD FLAP ACTUATOR CANNON PLUG. REPLACED RIGHT INBOARD FLAP ACTUATOR CANNON PLUG AND REPLACED Feb 1, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972313Relay · burnedBURNING SMELL IN COCKPIT INFLIGHT REPORTED BY FLIGHT CREW. ISOLATED SMELL AND EVIDENCE OF SMOKE TO K0543 FEEDER PROTECTION RELAY IN LEFT DC RELAY BOX. REMOVED AND REPLACED K0543 IAW MM 54-52-00 AND MM 24-52-00. RAN ENGINES, SYSTEMS OPS CHECKS GOOD. NO FURTFeb 1, 2001 · N568SW · Emb EMB120ER · DC Power Distribution SystemSDR SWIA972335Connector · damagedON TAKEOFF ROLL RECEIVED A TRIPLE CHIME WITH AURAL TRIM WARNING. AIRCRAFT TRIM WAS SELECTED IN GREEN ARC TO 34 PERCENT. ABORTED TAKEOFF. FOUND PIN-L AT PO349 SEVERED. INSTALLED NEW PINS AT JO349 AND PO349 IAW 20-00-00. GROUND OPS CHECK GOOD.Jan 31, 2001 · N215SW · Emb EMB120ER · Central WarningSDR SWIA972317Door · damagedDURING TAKEOFF ROLL PRIOR TO V1 RECEIVED RED DOOR LIGHT ON MAP AND RED FLASHING WARNS LIGHT. ABORTED TAKEOFF. FOUND OUTBOARD REFUEL DOOR FWD FASTENER BAD AND POPPED OUT. REPLACED FASTENER AND RESECURED FORWARD DOOR. OPS CHECKS GOOD.Jan 31, 2001 · N299SW · Emb EMB120ER · Fluid Service DoorsSDR SWIA972314Connector · failedLEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. FOUND CANNON PLUG P5 ON LEFT EEC WITH FAULT. REMOVED AND REPLACED LEFT EEC HARNESS IAW EMB 120 MM 73-21-00, OPS CHECK GOOD. P/N ON 3115911-01, S/N ON AA4313, S/N OFF AA3712.Jan 31, 2001 · N187SW · Emb EMB120ER · Fuel Controlling SystemSDR SWIA972312Selector Knob · malfunctionedFLAP CONTROL FAULT ON TAXI OUT ALL SEGEMENTS. INSTALLED SERVICEABLE FLAP SELECTOR S/N 120031R. OPS CHECK GOOD.Jan 31, 2001 · N585SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR C2XA01IA074Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE MIDDLE EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 30, 2001 · N16724 · Emb EMB120ER · Emergency LightingSDR SWIA972321Warn Panel · malfunctionedON TAKEOFF ROLL RECEIVED HIGH SPEED AURAL WARNING THROUGH 80 KNOTS. ABORTED TAKEOFF. PERFORMED INSULATION TEST ON ALL WIRES IN HIGH SPEED WARNING SYSTEM. WIRES CHECK GOOD. REMOVED AND REPLACED AURAL WARNING UNIT WITH SERVICEABLE UNIT IAW 31-53-02. HIGH SPJan 30, 2001 · N214SW · Emb EMB120ER · Central WarningSDR SWIA972334Connector · contaminatedFLAP DISAGREEMENT AFTER TAKEOFF WHEN RETRACTING FLAPS TO 0 DEGREES. QRH PROCEDURES COMPLIED WITH AND DISAGREEMENT REMAINED. RETURNED TO SLC. CLEANED GLYCOL FROM OUTBOARD FLAP CANNON PLUGS. CYCLED FLAPS SEVERAL TIMES, INDICATION AND OPS CHECK GOOD.Jan 29, 2001 · N217SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972303Fcu · malfunctionedAFTER TAKEOFF OUTBOARD FLAPS WOULD NOT RETRACT ABOVE 5 DEGREES INDICATED AND CONTROL FAULT WARNING OCCURRED. CONTROL FAULT WOULD NOT RESET. CONTINUED AT 180 KNOTS. FLAPS EXTENDED NORMALLY FOR LANDING. AFTER LANDING OUTBOARD FLAPS WOULD NOT RETRACT ABOVE 15Jan 29, 2001 · N293SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972319Servo · malfunctionedWHILE PERFORMING FLIGHT CONTROL TEST ON TAXI CHECK, THE ELEVATOR CONTROL SEEMED TO SNAG OR CATCH ON SOMETHING MIDWAY OF TRAVEL. RETURNED TO GATE. REMOVED AND REPLACED ELEVATOR AUTO PILOT SERVO IAW MM 27-00-03. OPS CHECKS GOOD. P/N ON: 622-5734-002, S/N ONJan 28, 2001 · N190SW · Emb EMB120ER · Autopilot Main ServoSDR SWIA972298Warning System · false indicationHIGH SPEED AURAL WARNING UPON APPLICATION OF TAKEOFF POWER. PRESSURIZED PITOT STATIC SYSTEM USING TEST BOX THROUGH ENTIRE AIRSPEED RANGE IAW MM 34-17-01. AURAL WARNING OPS CHECKS GOOD. RAN BOTH ENGINES AT TAKEOFF POWER IN TAKEOFF CONFIGURATION WITH NO HIGH Jan 28, 2001 · N214SW · Emb EMB120ER · Central WarningSDR SWIA972308Actuator · failedWHEN CYCLING FLAPS FROM 45 DEGREES TO 0 DEGREES, FLAPS GET A DISAGREEMENT ON THE NACELLE FLAPS AT ABOUT 25 DEG - 15 DEG. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT. CYCLED FLAPS SEVERAL TIMES. OPS CHECKS GOOD.Jan 27, 2001 · N289YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR C2XAO1IA061Bracket · crackedIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR INBOARD AFT GEAR DOOR HAD A BROKEN FORWARD HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 27, 2001 · N16731 · Emb EMB120ER · Landing Gear DoorsSDR C2XA01IA060Bracket · crackedIAH - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR OUTBOARD AFT GEAR DOOR HAD A BROKEN AFT HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 27, 2001 · N16731 · Emb EMB120ER · Landing Gear DoorsSDR SWIA972297Control Unit · failedWHEN SELECTING FLAPS UP AFTER TAKEOFF HAD A CONTROL FAULT FOR THE OUTBOARD FLAPS. FOLLOWED QRH PROCEDURE BUT WOULD NOT RESET. RETURNED TO SFO. REPLACED FLAPS CONTROL UNIT. FLAP SYSTEM OPS CHECKS OK. P/N ON: 347-200-1001, S/N ON: 0034.Jan 27, 2001 · N293SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972320Uplock · out of adjUPON ATTEMPTING TO RAISE LANDING GEAR, RECEIVED A RED-A LIGHT AND A RED-B LIGHT. VISUALLY NOTICED THAT GEAR DOORS FOR LEFT AND RIGHT GEAR DO NOT CLOSE. DIVERTED TO FAT. ADJUSTED LEFT AND RIGHT UPLOCK HOOK PLUNGERS IAW 32-11-01. SWUNG GEAR SEVERAL TIMES IAWJan 26, 2001 · N299SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972301Harness · damagedLEFT MAIN GEAR INDICATION LIGHT (A) WOULD NOT EXTINGUISH. RECYCLED GEAR BUT UNABLE TO GET A THREE GREEN INDICAITON. GEAR WOULD NOT DROP UNTIL ELECTRICALLY OVERRODE LANDING GEAR. RETURNED TO SLC. REMOVED AND REPLACED LEFT MAIN LANDING GEAR A-HARNESS IAW MM Jan 26, 2001 · N212SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972300Indicator · malfunctionedJUST AFTER GEAR RETRACT ON TAKEOFF, ERRONEOUS HIGH SPEED WARNING SOUNDED TWO TIMES THEN EXTINGUISH. TEN MINUTES LATER JUST BEFORE LEVEL OFF AT 26000 WARNINGS START AGAIN AND PERSIST. PULLED POWER BACK IN CRUISE AND WARNING CEASED. RETUNED TO SLC. REMOVED AJan 26, 2001 · N203SW · Emb EMB120ER · Airspeed/Mach IndicatorSDR SWIA972299Probe · failedDURING TAKEOFF ROLL JUST AFTER TORQUE REACHED 80 PERCENT AND 100 PERCENT , FIRST OFFICER SAW TORQUE ON NR 1 (LEFT) ENGINE DROP. DIGITAL DROPPED TO 4 PERCENT AND ANALOG DROPPED TO 10 PERCENT BUT WAS FLUCTUATING. JUST AS TAKEOFF WAS ABORTED THE LEFT ENGINE LOSJan 26, 2001 · N237SW · Emb EMB120ER · Engine BMEP/Torque Indicating
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