Embraer EMB-120ER

Service difficulty reports · 8,287

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 aircraft_model_key = 'EMB120ER'
  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 SWIA972311Downlock Sensor · failedSELECTING GEAR UP NOSE INDICATION WAS A GREEN, B RED. WHEN CYCLING TO GEAR DOWN INDICATION - LEFT: A & B RED, NOSE: B RED, A GREEN, RIGHT; A&B RED. AFTER 5 MINUTES GEAR DROPPED BY ITSELF AND 6 GREEN LIGHTS. REPLACED DOWNLOCK PROX SENSOR FOR A-SYSTEM ON THE Jan 25, 2001 · N251YV · Emb EMB120ER · Landing Gear Position and WarningSDR CA010213016Hinge · cracked(CAN) LEFT MLG OUTBOARD AFT DOOR AFT HINGE ASSY FOUND BROKEN DURING LINE CHECK. HINGE FITTING IS ALUMINIUM ALLOY CASTING WHICH ALSO CONNECT TO MLG BY PUSH PULL ROD FOR DOOR CLOSURE AFTER RETRACTION. EVIDENCE OF EXISTING C RACK ABOUT 0.75 INCH LONG FOUND ON BROJan 24, 2001 · Emb EMB120ER · Landing Gear DoorsSDR SWIA972309Pressure Switch · failedMIDDLE LEFT DEICE INOP INFLIGHT. DIVERTED TO FAT FROM VIS. REPLACED LEFT MIDDLE DEICE BOOT PRESSURE SWITCH AND PATCHED SMALL HOLE IN BOOT. OPS CHECKS GOOD. P/N ON: 211C117-183, S/N ON: N735, S/N OFF: 088D10021A.Jan 24, 2001 · N560SW · Emb EMB120ER · Airfoil Anti/De-ice SystemSDR SWIA972306Actuator · failedFLAP CONTROL FAULT ON FLAP RETRACT, WOULD NOT RESET. OUTBOARD FLAP PAIR STUCK AT 15 DEGREES. RETURNED TO SFO. (3RD REPEAT). READ FAULT CODES AND TROUBLESHOOTING CODES SOL SHORT TO GROUND IAW INSTRUCTION PROVIDED. CLEANED OUT LEFT OUTBOARD FLAP ACTUATOR EXTEJan 24, 2001 · N293SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR GLBA2001012Sensor · shortedMLG CB POPPED, NO GREEN (DOWNLOCK) INDICATION ON B-SYSTEM. REMOVED AND REPLACED PROX SENSOR, SYSTEM OPS CHECKED GOOD.Jan 24, 2001 · N297UX · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA972292Detector · malfunctionedRECEIVED HDG FLAG ON BOTH EHSIS AND MFD AFTER TAKEOFF. RETURNED TO SLC. ADJUSTED NUMBER TWO FLUX DETECTOR IAW MM 34-21-00. AHRS SYSTEM OPS CHECK GOOD.Jan 24, 2001 · N270YV · Emb EMB120ER · Directional Gyro and Indicating SystemSDR SWIA972291Smoke · detectedLEFT PACK INFLIGHT SET OFF LAV SMOKE DETECTOR. RETURNED TO PDX. REPOSITIONED RAM AIR DOOR SWITCH TO CORRECT POSITION. OPS CHECKS GOOD. SECURED PANEL AND CONTROL KNOB.Jan 24, 2001 · N218SW · Emb EMB120ER · Cabin Cooling SystemSDR SWIA972318Actuator Cable · out of adjAT V1 AIRCRAFT BRAKES SEEMED TO LOCK UP. ABORTED TAKEOFF. INSPECTED AND ADJUSTED BLUE HYDRAULIC SYSTEM ACTUATION CABLES. OPS CHECK AND PRESSURE CHECK GOOD. TAXI CHECK GOOD IAW EMB120 MM 32-41-00.Jan 23, 2001 · N204SW · Emb EMB120ER · Hydraulic System, MainSDR SWIA972307Relay · failedWHEN CLEARED FOR TAKEOFF, SET CONDITION LEVERS TO MAXIMUM, AUTO FEATHER AURAL WARNING SOUNDED. ABORTED TAKEOFF. WHEN T/O POWER SET FIRST OFFICER NOTICED RIGHT NP DID NOT SPOOL UP TO 65 PERCENT. REPLACED REVERSION (EEC) RELAYS K0059, K0060 PER WM 20-00-00, AJan 22, 2001 · N292SW · Emb EMB120ER · Propeller Feathering/ReversingSDR SWIA972288Handle · stuckFORWARD DOOR WOULD NOT OPEN FULLY WHEN OPENED FOR PASSENGER DE-PLANNING, HANDLE IS STUCK IN HALF-TRAVEL POSITION. REMOVED BROKEN LOCKING CAM ROD PUSH END FORWARD AND REPLACED WITH ROD END IAW EMB 120 MM 52-11-00. OPS CHECK GOOD. OPERATES NORMALLY.Jan 22, 2001 · N301YV · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA972305Connector · contaminatedOUTBOARD FLAPS WOULD NOT RAISE OR LOWER FROM FLAPS 15 DEGREES AFTER DEICE. FOUND DEICE FLUID ON OUTBOARD FLAP CANNON PLUGS (LEFT AND RIGHT). CLEANED CANNON PLUGS WITH CONTACT CLEANER. OPS CHECK GOOD.Jan 21, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972304Spring · lack of lubeELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK.Jan 21, 2001 · N207SW · Emb EMB120ER · Elevator Control SystemSDR GLBA2001008Actuator · inoperativeRETURN TO BLOCK, LEFT GEAR WOULD NOT RETRACT ON T/O. REMOVED AND REPLACED UPLOCK ACTUATOR.Jan 20, 2001 · N297UX · Emb EMB120ER · Landing Gear ActuatorSDR C2XA01IA039Actuator · out of adjIAH - FLIGHT 3490, THE CREW REPORTED THAT THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT MAIN LANDING GEAR ACTUATOR TO BE OUTJan 20, 2001 · N15730 · Emb EMB120ER · Landing Gear ActuatorSDR C2XA01IA099Floorbeam · crackedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND FLOORBEAM WAS FOUND TO BE CRACKED AT FRAME 38. MAINTENANCE PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB120 SRM 51-70-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 19, 2001 · N12715 · Emb EMB120ER · Fuselage Main, Floor BeamSDR SWIA972285Indicator · failedLEFT ANALOG TORQUE GAUGE DROPPED TO ZERO ON TAKEOFF ROLL BELOW V1. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT TORQUE GAUGE AS PER MM. OPS CHECKS GOOD. P/N ON: SEDL-OC2R, S/N ON: 961D, S/N OFF: 141.Jan 19, 2001 · N216SW · Emb EMB120ER · Engine BMEP/Torque IndicatingSDR SWIA972284Control Panel · malfunctionedAFTER TAKEOFF, AUTO PILOT TURNED ON BY ITS SELF. RETURNED TO FIELD. WHILE ON THE GROUND THE AUTO PILOT TURNED ON BY ITS SELF. RAN THE TRIM WHEEL FULL NOSE DOWN AFTER DISCONNECTING AND TRANSFERRING TO FIRST OFFICERS SIDE IT AGAIN TURNED ITSELF ON. REPLACEDJan 19, 2001 · N568SW · Emb EMB120ER · Autopilot ComputerSDR C2AX01IA031A/C Pack · failedCLL - FLIGHT 3463, THE CREW REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED, THE OXYGEN MASKS DEPLOYED, AND THE AIRCRAFT RETURNED TO CLL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE NUMBER TWO PACK HAD FAILEDJan 17, 2001 · N57734 · Emb EMB120ER · Cabin Cooling SystemSDR C2XA01IA032Power Supply · inoperativeIAH - FLIGHT 2913, DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT REMAIN ILLUMINATED WHEN TESTED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER ONE EMERGENCY LIGHT POWER SUPPLY TO BE INOPERATIVE. MAINTENANCE REJan 16, 2001 · N40717 · Emb EMB120ER · Emergency LightingSDR SWIA972276Actuator · failedCONTROL FAULT ON TAXI OUT, ON BOTH THE OUTBOARD PAIRS. QRH UNSUCCESSFUL. TROUBLESHOT FLAP SYTEM SELF DIAGNOSIS INDICATED LEFT OUTBOARD ACTUATOR ON FCU. REMOVED AND REPLACED LEFT FLAP (OUTBOARD) ACTUATOR IAW EMB 120 MM 27-50-07. SYSTEM OPS CHECK GOOD. P/N Jan 16, 2001 · N291SW · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA972275Eec · malfunctionedLEFT EEC FAILED ON TAKEOFF ROLL. ABORTED TAKEOFF. CLEANED ALL CANNON PLUGS AND GROUND RAN LEFT ENGINE. OPS CHECK GOOD.Jan 16, 2001 · N187SW · Emb EMB120ER · Fuel Controlling SystemSDR SWIA972290Computer · failedLEFT NACELLE FLAPS FAULT DISCREPANCY DURING RETRACTION. REPLACED FLAP COMPUTER. OPS CHECK BAD. REPLACED LEFT NACELLE FLAP ACTUATOR. OPS AND LEAK CHECK GOOD. WORK ACCOMPLISHED IAW EMB120 MM 27-50-00 AND RII 27-307. FLAP COMP P/N: 347200-1001, S/N ON: 02Jan 14, 2001 · N204SW · Emb EMB120ER · Engine Cowl FlapsSDR C2XA01IA034O-Ring · crackedIAH - FLIGHT 2908, THE CREW REPORTED THAT THE NUMBER TWO ENGINE LOST OIL PRESSURE IN FLIGHT WITH A LARGE VISUAL OIL LOSS ON THE RIGHT SIDE OF THE AIRCRAFT. THE CREW SHUTDOWN THE NUMBER TWO ENGINE BEFORE 40 PSID, AND RETURNED TO IAH WHERE IT LANDED WITHOUT INCJan 14, 2001 · N15730 · Emb EMB120ER · Turbine Engine Oil SystemSDR SWIA972281Switch · out of adjABORT TAKEOFF AT 90 KNOTS FOR CARGO DOOR WARNING. RETURNED TO GATE. ADJUSTED FORWARD CARGO DOOR MICROSWITCH IAW MM 52-30-00. OPS CHECK GOOD.Jan 14, 2001 · N233SW · Emb EMB120ER · Door Warning SystemSDR SWIA972270Warning System · malfunctionedTAKEOFF TRIM AURAL WARNING ON TAKEOFF. ABORTED TAKEOFF. TRIM IN GREEN BAND. POWERED DOWN AIRCRAFT. POWERED UP AIRCRAFT. PERFORMED OPERATIONAL CHECK OF AURAL TRIM WARNING SEVERAL TIMES. TRIM AURAL WARNING OPERATES NORMAL. OPS CHECKS GOOD. COULD NOT DUPLJan 14, 2001 · N562SW · Emb EMB120ER · Data Recorders (Flight/Maintenance)SDR SWIA972267Indicator · failedON TAKEOFF, PASSING THROUGH 80 KNOTS RIGHT NP GAUGE FLUCTUATED FROM 100 PERCENT DOWN TO 50 PERCENT A FEW TIMES. ABORTED TAKEOFF. REPLACED RIGHT NP INDICATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON B939, S/N OFF 105AB.Jan 13, 2001 · N584SW · Emb EMB120ER · Propeller Indication SystemSDR C2XA01IA098Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 38 AND 40. MAINTENANCE PERFORMED A SPLICE REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5310-01163 REV-B, AND THE AIRCRJan 12, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA097Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 40. MAINTENANCE PERFORMED A SPLICE REPAIR TO THE AFFECTED SECTION OF OMEGA BEAM IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHJan 12, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA972287Tail Cone · out of positionELEVATOR CONTROL BINDING IN MIDDLE OF THROW. FOUND ELEVATOR CONTACTING RIGHT SIDE OF TAIL CONE AT MID THROW. REPOSITIONED AND SECURED TAIL CONE. CHECKS OK.Jan 12, 2001 · N271YV · Emb EMB120ER · Aerodynamic FairingsSDR SWIA972265Actuator · frozenAFTER LEVEL OFF AT FL200 IT APPEARED THAT ELEVATOR TRIM WAS NOT TURNING WHEN COMMANDED BY AUTOPILOT. AUTOPILOT WAS DISENGAGED AND ELEVATOR TRIM WAS FROZEN. AFTER DISENGAGE BELOW FREEZING LEVEL FOR 1.5 MINUTES, TRIM MOVED FREELY. REPLACED LEFT AND RIGHT ELEVJan 12, 2001 · N293SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA972264Wire · brokenTAKEOFF AURAL WARNING TRIM WITH TRIM IN GREEN ARC. ABORTED TAKEOFF. FOUND BROKEN WIRE FOR RIGHT HAND SENSOR AT TAIL CONE. RECONNECTED PER WIRING MANUAL 20-21-00 AND CHECKED RIGGING OF RIGHT HAND SENSOR PER MM 27-32-00. OPS CHECK GOOD.Jan 12, 2001 · N292UX · Emb EMB120ER · Instrument System WiringSDR SWIA972279Latch · looseAT 90 KNOTS TAKEOFF ROLL, GOT DOOR WARNING ON MAP AND FLASHING MASTER WARNING. NO TRIPLE CHIME LIGHT WENT OFF ON DECELERATION. FOUND INBOARD FUEL SERVICE DOOR AFT CAMLOC TO BE LOOSE AND PUSHED THROUGH. REPLACED CAMLOC AND ADJUSTED SWITCH ON OUTBOARD FUEL SEJan 11, 2001 · N229SW · Emb EMB120ER · Fluid Service DoorsSDR SWIA972269Actuator · frozenAFTER LEAVING FL240 RUDDER TRIM FROZEN. RUDDER FREE WITH AND WITHOUT YAW DAMPNER TRIM BEGAN WORKING OUT OF 8-7 THOUSAND FEET. REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW RII 27-301. OPS CHECKS GOOD.Jan 11, 2001 · N268UE · Emb EMB120ER · Rudder ActuatorSDR C2XA01IA019Light · malfunctionedBTR - FLT 3533 - THE CREW REPORTED THAT THE FORWARD CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE APPLIED POWER TO THE AIRCAFT AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW EMB-120 MM 33-50-00. NO DEFECTS WERE NOTED AND TJan 10, 2001 · N40717 · Emb EMB120ER · Emergency LightingSDR SWIA972273Connector · contaminatedNR 2 PITOT HEAT FAILED IN FLIGHT, AUTO PILOT FAILED, HIGH SPEED WARNING WENT OFF WHEN FIRST OFFICER'S AIRSPEED FLUCTUATED. EN ROUTE FROM MRY TO LAX. DIVERTED TO SBA. FOUND CONTAMINATION OF WATER IN NUMBER TWO PITOT CANNON PLUG. DRIED WATER AND CLEANED CONTJan 10, 2001 · N284YV · Emb EMB120ER · Pitot/Static Anti-Ice SystemSDR SWIA972266Warning System · illuminatedPROP DEICE FAILURE IN BOTH CYCLES. CIRCUIT BREAKER TRIPPED. FOLLOWED QRH PROCEDURES. PROP STILL FAILED. RETURNED TO LAX. RAN DEICE SYSTEM IAW 20-10-00. ALL CHECKS OK AT THIS TIME.Jan 10, 2001 · N584SW · Emb EMB120ER · Propeller/Rotor Anti-Ice/De-Ice SystemSDR SWIA972262Warning Light · illuminatedRIGHT DUCT LEAK LIGHT ILLUMINATED PRIOR TO TAKEOFF. CLOSED RIGHT BLEED VALVE AND LIGHT REMAINED ILLUMINATED FOR MORE THAN 3 MINUTES. SHUT DOWN RIGHT ENGINE. LIGHT REMAINED ILLUMINATED FOR FOUR MINUTES, UNTIL POWER DOWN. ABORTED TAKEOFF. RAN RIGHT ENGINE AJan 10, 2001 · N218SW · Emb EMB120ER · Pneumatic Distribution SystemSDR C2XA01IA095Intercostal · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA113Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND BUTT STRAP WAS FOUND TO BE CORRODED AT STATION 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-22-00 AND 51-40-02, AND THE AIRCRAFTJan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA111Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 13255 TO STATION 15050. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPJan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA096Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 11430 TO 13255. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS AJan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA1095Intercostal · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND T-SECTION AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED T-SECTION IN ACCORDANCE WITH EMB120 SRM 51-20-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Jan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA094Beam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN FRAMES 37 AND 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED OMEGA BEAM IN ACCORDANCE WITH EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FORJan 9, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR SWIA972283Bulb · burned outCEILING EMERGENCY LIGHT OVER ROW TWO INOP. INSTALLED NEW BULB AND RESPECTIVE FUSE LAMP. CHECKS GOOD.Jan 9, 2001 · N560SW · Emb EMB120ER · Emergency LightingSDR SWIA972261Connector · contaminatedFLAP DISAGREEMENT ON SELECTION OF FLAP 45 DEGREES (OUTBOARD FLAPS WOULD NOT EXTEND BEYOND LAST LIGHT BAR ON FLAP ANNUNCIATOR PANEL). FOUND GLYCOL IN LEFT OUTBOARD CANNON PLUG. CLEANED PLUG. OPS CHECK GOOD.Jan 9, 2001 · N188SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR C2XA01IA110Duct · crackedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, RIGHT HAND EXHAUST DUCT WAS FOUND TO BE CRACKED ON THE OUTBOARD SIDE. MAINTENANCE PERFORMED A WELD REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC7810-01002, AND THE AIRCRAFT WAS APPROVEJan 8, 2001 · N12715 · Emb EMB120ER · Engine Collector/Tailpipe/NozzleSDR C2XA01IA109Crossbeam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 13509.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SEJan 8, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA108Crossbeam · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE AFT CROSSBEAM AT STATION 12445.0 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SEJan 8, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA107Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO STATION 13255.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, ANJan 8, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01IA106Strap · corrodedMYR - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND AFT BUTT STRAP WAS FOUND TO BE CORRODED FROM STATION 12130.0 TO 13509.0. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IN ACCORDANCE WITH EMB-120 SRM 51-40-02, AND THE AJan 8, 2001 · N12715 · Emb EMB120ER · Fuselage Miscellaneous Structure
Back to Embraer EMB-120ER