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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWIA200413488Support Bracket · crackedRIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413487Support Bracket · crackedRIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02.SDR SWIA200413486Support Bracket · crackedRIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413485Structure · crackedLEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202.SDR SWIA200413484Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02.SDR SWIA200413483Support Bracket · crackedLEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.SDR SWIA200413482Support Bracket · crackedLEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.SDR SWIA200413481Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.SDR SWIA200413480Frame · crackedFRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EMB 120 SRM 53-00-04 PG 201-204.SDR SWIA200413326Frame · crackedLEFT OUTBOARD NACELLE BRACKET ATTACHED TO GEAR DOOR HINGE POINT FRAME AND CRADLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ON LEFT OUTBOARD HALF FRAME ATTACH BRACKET IAW 120 SRM 51-10-02 PG 2 SEC 2B.SDR SWIA200413305Lamp · inoperativeEMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209.SDR SWIA200413280Control Unit · malfunctionedON CLIMBOUT THE OUTBOARD FLAPS INDICATED A SINGLE BAR ASSEMETRY. RETURNED TO FAT. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB 120 MM 27-50-00. OPS CHECK GOOD.SDR SWIA200413277Servo · malfunctionedCAPTAIN'S AUTOPILOT CONTINUOUS AURAL TRIM FAIL MESSAGE AND TRIM FAIL ON MAP, AND AP PANEL. REPLACED ELEVATOR TRIM SERVO SVO-65. CAPT'S AUTOPILOT OPS CK GOOD IAW MM 22-10-00.SDR SWIA200413273Socket · damaged1ST 3 LIGHTS OF THE FLOOR LEVEL EMERGENCY EXIT LIGHTS ARE NOT ILLUMINATING. INSTALLED INSULATING BOOT ON E-LIGHT SOCKET OVER PAX DOOR ENTRANCE. EMERGENCY LIGHTS OPS CHECK NORMAL. ALL PANELS AND ITEMS REMOVED FOR ACCESS SECURED.SDR GLBA20030623Battery Pack · dischargedEMERGENCY EXIT LIGHTS IN ROW 5A DIM, R & R EMERGENCY BATTERY PACK PN D366-04-001SDR GLBA20030619Landing Gear · malfunctionedLT MLG WOULD NOT RETRACT, PREFORMED GEAR SWING NO DEFECTS NOTED OPS CK GOODSDR SWIA200413303Windshield · crackedRIGHT WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD IAW EMB MM 56-10-01. P/N ON&OFF: NP-151311-2, S/N OFF: 98099H2740.SDR SWIA200413252Annunciator · malfunctionedSMOKE TRIPLE CHIME IN FLIGHT ON FINAL DESCENT. LAV SMOKE DETECTOR LIGHTS FLASHING. NO SMOKE IN CABIN AT ALL, OR LAV. REMOVED AND REPLACED SMOKE DETECTOR ANNUNICATOR PANEL WITH SERVICEABLE PANEL. OPS CHECK GOOD.SDR SWIA200413327Bracket · crackedRT HYDRAULIC PACK VERTICAL MOUNT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD HALF OF VERTICAL MOUNT BRACKET ASSY PER SRM 51-40-02.SDR SWIA200413253Warning System · malfunctionedDURING TAXI-IN, RECEIVED SPORADIC TRIPLE CHIME TAKEOFF TRIM WITH TRIM IN GREEN BAND. PERFORMED TEST AFTER SHUT DOWN AND DID NOT PASS. RERACKED AURAL WARNING UNIT AND RESET AURAL WARNING CB. OPS CHECKS GOOD.SDR SWIA200413223Acm · malfunctionedUNABLE TO COOL COCKPIT WITH ENGINE OR APU BLEED, LOW OR NORM SELECTED ON GROUND. SMOKE IN COCKPIT ASSOCIATED WITH DUCT OVERHEAT LIGHT. REPLACED AIR CYCLE MACHINE IAW MM 21-50-05, OPS CHECK GOOD.SDR SWIA200413256Servo · malfunctionedFEEL A BINDING WHEN MOVING AILERONS. REMOVED AND REPLACED AILERON SERVO WITH SERVICEABLE UNIT IAW EMB 120 MM CHAPTER 22-10-05. OPS CHECK GOOD.SDR SWIA200413230Panel · brokenEMERGENCY LIGHT PANEL ON FLOOR IN GALLEY BROKEN. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT ON FLOOR AT GALLEY IAW EMB 120 MM 20-10-00. OPS CHECK GOOD.SDR SWIA200413225Battery Pack · inoperativeREAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 17366-04-001, S/N OFF 397.SDR SWIA200413229Selector · malfunctionedIN CRUISE FLIGHT FLAP, ADV SWS AND CONTROL FAULT LIGHTS ILLUMINATED AND CLEARED THEMSELVES MULTIPLE TIMES. REMOVED AND REPLACED FLAP SELECTOR LEVER. OPS CHECKS GOOD IAW EMB MM 27-50-01.SDR SWIA200413233Control Unit · malfunctionedOUTBOARD FLAP PAIR CAUSES DISAGREEMENT ON FLAP RETRACTION AFTER TAKEOFF. FIXES ITSELF AND RETRACTS FLAPS AFTER ABOUT 2 SECS, HAPPENED ON 3 FLIGHTS. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECK GOOD IAW EMB MM 27-50-06.SDR SWIA200413227Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT STAY ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-50-01. OPS CHECK GOOD.SDR SWIA200413189Wire · brokenFIRST OFFICER'S STALL WARNING SHAKER INOP. REPAIRED BROKEN WIRE NEAR SHAKER CONNECTOR ON CONTROL COLUMN OF FIRST OFFICER'S SIDE. OPS CHECKS GOOD.SDR SWIA200413226Fire Loop · inoperativeNR 2 ENGINE DETECTOR INOP. ENGINE WHEEL WELL LIGHT ILLUMINATED. REMOVED NR 2 ENGINE FIRE LOOP AND REPLACED WITH A SERVICEABLE LOOP IAW MM 26-21-01. OPS CHECK GOOD. P/N 3601-75-450/160C.SDR SWIA200413153Actuator · malfunctionedON TAKEOFF DURING GEAR RETRACTION LEFT MAIN WOULD NOT RETRACT. REPLACED LEFT GEAR MAIN ACTUATOR IAW RII 32-302. OPS AND LEAK CHECK GOOD.SDR SWIA200413151Control Panel · malfunctionedELECTRIC ODOR & SMOKE COMING FROM CENTER CONSOLE. REMOVED AND REPLACED PRESS SYSTEM/EMERGENCY PARK BRAKE PANEL AND LIGHTING ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 120-40220-001.SDR SWIA200413148Connector · contaminatedON TAXI CHECK, GOT OUTBOARD FLAP CONTROL FAULT UPON APPLICATION TO FLAPS 15; RESET SUCCESSFULLY AS PER QRH, THEN HAPPENED 2 MORE TIMES UPON SETTING FLAPS 15 DURING TAXI BACK TO GATE. REMOVED WATER FROM CONNECTOR. OPS CHECKED NORMAL.SDR SWIA200413142Annunciator · faultyIN CRUISE FLIGHT, FLAP ADV SWS, AND CONTROL FAULT LIGHTS ILLUMINATED. RESET THE SYSTEM PER QRH, 5 MINUTES LATER, FLAP ADV SWS, CONTROL FAULT, ASYMMETRY, AND FLAP DISAGREEMENT ALL ILLUMINATED. ALSO HAD ERRATIC READINGS ON FLAP INDICATOR. REMOVED AND REPLACEDSDR SWIA200413334Support Channel · crackedRIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL AT INBOARD IAW EMB120 SRM 51-10-02 SEC 2 ITEM C.SDR SWIA200413333Support · crackedCAPTAIN'S DV WINDOW AFT SUPPORT CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SUPPORT BRACKET IAW 120 SRM 51-10-02 PAR 3. P/N: 120-12545-001.SDR SWIA200413332Rib · crackedLT INBOARD LEADING EDGE RIB HAS A SMALL CRACK. DISCOVERED DURING C-CHECK INSPECTION. DOUBLER REINFORCEMENT ADDED AT AFFECTED AREA OF LT LEADING EDGE RIB IAW EMB120 SRM 51-10-02 PG 2 SEC 2B.SDR SWIA200413331Support · damagedCRACKED VERTICAL SUPPORT ON INBOARD SIDE OF LEFT WHEEL WELL WHERE ENGINE CABLES RUN THROUGH. REPLACED VERTICAL SUPPORT AT INBOARD SIDE OF LEFT NACELLE IAW SRM 120 51-10-02 PG 2 SEC 2B.SDR SWIA200413330Frame · crackedRT NACELLE FRAME NR 1 CRACKED INBOARD AND OUTBOARD AT TORSION BAR MOUNTS. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT NACELLE FRAME IAW 120 SB 120-54-0036 AND RII. PART II COMPLIED WITH.SDR SWIA200413329Seat Track · corrodedLEFT AFT FLOOR SEAT TRACK CORRODED, MARKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT AFT FLOOR SEAT TRACK AS NEEDED.SDR SWIA200413328Seat Track · corrodedRIGHT AFT SIDEWALL SEAT TRACK CORRODED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT AFT SIDEWALL SEAT TRACK AS NEEDED.SDR SWIA200413264Clip · crackedMIDDLE LOWER SKIN CLIP CRACKED AT RIB 16, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED MIDDLE LOWER SKIN CLIP AT RIB 16 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR SWIA200413263Clip · cracked2 ND FROM AFT LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED 2ND FROM AFT LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR SWIA200413262Clip · crackedMIDDLE LOWER SKIN CLIP CRACKED AT RIB 15, RIGHT WING. DISCOVERED DURING C-CHECK INSPECTION. REPLACED MIDDLE LOWER SKIN CLIP AT RIB 15 ON RIGHT WING WITH SERVICEABLE UNIT IAW SRM 57-20-07.SDR SWIA200413261Support Bracket · crackedSUPPORT BRACKET AFT CENTER OF PILOT'S DV WINDOW CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED SKIN SUPPORT BRACKET, AFT CENTER OF PILOT'S DV WINDOW PER SRM 51-40-02 AND RII 53-301.SDR SWIA200413146Actuator · malfunctionedELEVATOR TRIM ACTUATOR FREEZES UP AT HIGH ALTITUDES. SIGNIFICANT SNAP-BACK WITH BOTH MANUAL AND ELECTRIC TRIM INPUTS, 17,000 FT AND HIGHER. REPLACED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS WITH SERVICEABLE UNITS IAW AMM 27-32-02. OPS CHECK GOOD. P/N: 5299-1SDR SWIA200413141Transducer · malfunctionedON DESCENT, RECEIVED STALL WARNING AURAL AND MAP LIGHT FOR SYSTEM 1; ALSO HAD -SPD- FLAG ON EADI, INTERMITTENT THROUGH LANDING. REMOVED AND REPLACED AOA TRANSDUCER AND STALL WARNING COMPUTER. OPS CHECKS GOOD. STALL WARNING COMPUTER P/N OFF: C-81806-3, S/N OSDR SWIA200413135Control Panel · malfunctionedAFTER INITIAL POWER-UP AND -AURAL UNIT OKAY-, THE NR 2 STALL SHAKER, CLACKER AND PUSHER ACTIVATED CONTINUOUSLY (AOA VANES WERE CENTERED). REMOVED AND REPLACED STALL WARNING PANEL WITH A SERVICEABLE PANEL. OPS CHECK GOOD AT THIS TIME. P/N: 120-34428-505.SDR SWIA200413140Lamp · inoperativeROW 6 SEAT -A- EMERGENCY LIGHT POD DOES NOT ILLUMINATE. REMOVED AND REPLACED LAMP AT SEAT 6A. EMERGENCY LIGHT OPS CHECKS GOOD.SDR SWIA200413126Shutoff Valve · stuckAPU BLEED OPEN, CROSSBLEED OPEN, LEFT PAC -LOW-, RIGHT PAC -OFF-, THE CABIN FILLED WITH SMOKE. FOUND RIGHT PACK PRESSURE SHUTOFF, VALVE STUCK OPEN ALLOWING CONTINUOUS AIRFLOW TO INOP PACK. REMOVED AND REPLACED VALVE IAW 21-50-01. OPS CHECKS GOOD. S/N OFF: SDR SWIA200413125Actuator · failedDURING CLIMBOUT OF SEA, THE RIGHT RUDDER PEDAL TRAVEL WAS RESTRICTED TO ABOUT 2-4 INCHES THEN JAMMED AND WOULD NOT TRAVEL ANY FURTHER. A/C WAS ABOVE 120 KNTS ACCELERATING TO 180 KNTS. CONDUCTED RUDDER HEALTH CHECK IAW 27-22-00. TOP (BLUE) ACTUATOR FAILS. B
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