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 SWIA200413905Window Post · crackedLT PILOTS TO DV WINDSHIELD POST CRACKED LOWER FORWARD CORNER AT FS 3010. (ITEM FOUND AT C-CHECK INSPECTION.) COMPLIED WITH SB 120-53-0072 REV 0 21 FEB 00. REPAIR WORK PERFORMED IAW SRM 51-40-00.SDR SWIA200413913Actuator · malfunctionedFLAP DISAGREEMENT ON RETRACTION. REPLACED LEFT NACELLE FLAP ACTUATOR WITH A SERVICEABLE UNIT IAW MM 27-50-00. OPERATIONAL CHECK GOOD.SDR SWIA200414149Floorbeam · corrodedAFT FUSELAGE BAGGAGE PIT, FRAME 44, FLOOR CROSSBEAM CORRODED. REPLACED CROSSBEAM IAW SRM 51-40-02 AND 51-25-00.SDR SWIA200414148Seat Track · corrodedFUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS MARKED AT FR 17 - FR 32, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SEAT TRACK IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AMM 20-00-00.SDR SWIA200414147Seat Track · corrodedFUSELAGE; CORROSION FOUND ON SEAT TRACK (BROWN LINE) AND AROUND SCREW HEADS AS MARKED AT FR 15 - FR 31, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-21-02, AND AMM 20-00-00.SDR SWIA200414146Intercostal · corrodedINTERCOSTAL CORRODED AT FRAME 38 ON RIGHT SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-00, 51-40-02, AND 51-40-05.SDR SWIA200414145Floorbeam · corrodedFR 44 TO FR 47 RIGHT OUTBOARD SIDE ANGLE IS CORRODED ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02.SDR SWIA200414144Plate · corrodedFS 13630.0 TO FS 15050.0 LEFT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT STRAP IAW EMB 120 SRM 51-40-02.SDR SWIA200414143Plate · corrodedFS 13630.0 TO FS 15050.0 CENTER BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02.SDR SWIA200414142Floorbeam · corrodedCORROSION AT FR 40 TO FR 44 RIGHT SIDE ANGLE ON INBOARD AND OUTBOARD SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIGHT SIDE ANGLE IAW SRM 51-40-02.SDR SWIA200414141Floorbeam · crackedTWO CORNER ANGLE BRACKETS CRACKED AT ST 4121.5 BELOW FLOOR PANELS 221GF AND 222GF. ITEM FOUND AT C-CHECK INSPECTION. BRACKETS REPLACED IAW EMB 120 SRM 53-10-10 FIG 13, ITEM 10, 51-25-00, 51-30-01, 51-40-02, 51-22-00, AND 51-40-05.SDR SWIA200414140Plate · corrodedFS 13630.0 TO FS 15050.0 RIGHT INBOARD BUTT PLATE IS CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200414139Sill · corrodedFR 40 TO FR 44 LEFT SIDE SILL CORRODED ON UPPER AND LOWER SURFACES AND AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. INSTALL NEW CARGO DOOR SILL PLATE.SDR SWIA200414138Frame · crackedCRACKED FRAME FOUND AT FRAME 47 RIGHT OUTBOARD SIDE. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-70-05 FIG 1.SDR SWIA200413959Mount · corrodedLOWER ROD ENDS ON UPPER APU MOUNT SUPPORT RODS SEVERELY CORRODED. ITEM FOUND AT C-CHECK INSPECTION. ROD ENDS REPLACED. REF. 49-11-02.SDR SWIA200413958Pushrod · corrodedBOTH LEFT AND RIGHT ELEVATOR PUSH RODS AT ELEVATORS HAVE CORRODED ROD ENDS AND ASSOCIATED HARDWARE. ITEM FOUND AT C-CHECK INSPECTION. BOTH LT AND RT ELEVATOR PUSHROD ROD ENDS AND HARDWARE REPLACED IAW 27-31-04.SDR SWIA200413957Rib · crackedRIB AT FRAME 13 CRACKED (AS MARKED). ITEM FOUND AT C-CHECK INSPECTION. REPLACED RIB IAW SRM 51-40-02, 51-30-01, AND 51-25-00.SDR SWIA200413956Floor Support · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 13 - FR 38, STR 15L. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200413955Floor Support · corrodedCORROSION FOUND AROUND A/NUT HOLES AS MARKED ON FLOOR SUPPORT STRUCTURE AT FR 14 - FR 39, STR 15R. ITEM FOUND AT C-CHECK INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200413954Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. BUTTPLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200413953Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200413952Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE AS MARKED ON FLOORBEAM BUTTSTRAPS AT FR 13 - FR 38, Y 0.00 (CENTER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED INTERCOSTAL IAW SRM 51-25-00, 51-40-02, AND 51-40-05.SDR SWIA200413951Floor Support · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOOR SUPPORT STRUCTURE AT FR 38 - 40, STR 15R. ITEM FOUND AT C-CHECK INSPECTION. BUTT PLATE REPLACED IAW EMB 120 SRM 51-40-02.SDR SWIA200413950Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW SRM 51-40-02.SDR SWIA200413949Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 0.00 (CENTER). ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02.SDR SWIA200413948Floorbeam · corrodedFUSELAGE CORROSION FOUND AROUND A/NUT HOLES AND SURFACE ON FLOORBEAM BUTTSTRAP AT FR 38 - FR 40, Y 479.00 L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED BUTT PLATE IAW EMB 120 SRM 51-40-02.SDR SWIA200413947Seat Track · corrodedFUSELAGE SEAT TRACK CORRODED BEYOND LIMITS AT FR 38, 479.00 LT. ITEM FOUND AT C-CHECK INSPECTION. SEAT TRACK REPLACED IAW EMB 120 SRM 51-25-00, 51-40-06, 51-40-02, 51-22-00.SDR SWIA200413934Connector · malfunctionedUPON RETRACTING FLAPS AFTER DEPARTURE, GOT FLAP CONTROL FAULT. FOUND MOISTURE IN BOTH OB FLAP ACTUATOR CONNECTOR PLUGS, CLEANED AND REINSTALLED CONNECTOR PLUGS. OPERATIONAL CHECK GOOD.SDR SWIA200413933Ground Wire · brokenEMERGENCY EXIT SIGN ABOVE FA JUMPSEAT DOES NOT ILLUMINATE. REPAIRED GROUND WIRE AT LIGHT ASSY. OPERATIONAL CHECK GOOD.SDR SWIA200413887Actuator · malfunctionedMULTIPLE FLAP CONTROL FAULTS WITH DISAGREEMENT AND ASYMMETRY LIGHTS ON THE GROUND AND IN THE AIR. REMOVED AND REPLACED INBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD.SDR SWIA200413919Wire · brokenEMERGENCY FLOOR LIGHTING SYSTEM HAS ONE BULB INOPERATIVE. REMOVED AND REPLACED BROKEN SPLICE WITH NEW ENVIRONMENTAL SPLICE, OPERATIONAL CHECKS GOOD.SDR SWIA200413875Control Unit · malfunctionedFLAP AND ADVANCED SWS LIGHTS ON MAP ILLUMINATED WITH ASSOCIATED CONTROL FAULT. REPLACED FLAP CONTROL UNIT, OPERATIONAL CHECK GOOD.SDR SWIA200413889Servo · malfunctionedLEFT RUDDER PEDAL FEELS LIKE IT IS SCRAPING SOMETHING. REPLACED RUDDER SERVO. OPERATIONAL CHECKS GOOD.SDR SWIA200413888Connector · dirtyAFTER SELECTING FLAPS 15 DEGREES, FLAP WARNING CONTROL FAULT ASSOC WITH FLAP AND ADV SWS ON MAP PANEL. CLEANED FLAP TRACKS AND CONNECTORS. ALL SYSTEM'S OPERATIONAL CHECK GOOD.SDR SWIA200413883Odor · detectedON TAKEOFF ROLL BOTH PILOTS SMELLED SMOKE AND LAV SMOKE DETECT ALARM SOUNDED. C/B POPPED. REMOVED AND REPLACED RCCB 0208 WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.SDR SWIA200413871Servo · malfunctionedELECTRIC TRIM DOES NOT FUNCTION ABOVE 180 KTS.REMOVED AND REPLACED ELECTRIC TRIM MOTOR, REFERENCE 22-10-05. OPERATIONAL CHECK GOOD.SDR SWIA200413882Odor · detectedAT 27,000 FT, SMOKE WARNING ILLUMINATED. VISIBLE SMOKE REPORTED IN CABIN. AIRCRAFT WAS DESCENDED WITH BLEED/PACK CONFIGURATION IN LOW/LOW, SMOKE CLEARED. REMOVED LEFT ACM & GROUND COOLING FAN, INSPECTED COMPONENTS FOUND NO DEFECTS. INSPECTED INLETS AND OUTSDR SWIA200413862Lamp · burned outFRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD.SDR GLBA20030726Warning Light · false indicationLANDING GEAR GIVES FALSE INDICATION, PERFORMED LANDING GEAR EXTENSION COULD NOT DUPLICATESDR SWIA200413878Computer · malfunctionedSTALL SYSTEM NR 1 WILL NOT TEST. REPLACED NR 1 AOA TRANSDUCER, NR 1 STALL WARNING COMPUTER AND STALL WARNING PANEL ASSY. CLEANED MPU CONNECTOR. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 14882-304, P/N C-81817-1, S/N ON 955, S/N OFF 1101, P/N C-818SDR SWIA200413855Selector · malfunctionedPILOT REPORTS CONTROL FAULT WHEN SELECTING FLAPS FROM 15 TO 25 DEGREES. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPERATIONAL CHECK GOOD. P/N 120-6920-615CON, S/N OFF 120182.SDR SWIA200413856Pressure Switch · malfunctionedRUDDER SPEED SWITCH LIGHT ILLUMINATED ON MAP. REPLACED BOTH RUDDER GREEN SYSTEM AND BLUE SYSTEM HYDRAULIC PRESSURE SWITCHES WITH SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.SDR SWIA200413849Rccb · malfunctionedON DESCENT INTO IAH, NOTICED BURNING SMELL IN COCKPIT. SHORTLY AFTER, THERE WAS AUDIBLE CHATTER IN WHAT SOUNDED LIKE A RELAY OPENING/CLOSING. REPLACED LEFT PACK RCCB. OPERATIONAL CHECKS GOOD.SDR SWIA200413838Servo · malfunctionedLT RUDDER IS HANGING UP OR CATCHING (BINDING). INSTALLED SERVICEABLE SERVO FOR RUDDER PEDALS AS REQUIRED. REF 22-10-05, OPERATIONAL CHECK GOOD.SDR 2004F00388Propeller · malfunctionedUPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION, FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIPSDR 2004F00387Propeller · malfunctionedUPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. HE CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION. FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRISDR 2004F00386Propeller · malfunctionedUPON TAKE OFF THE PILOT REPORT THAT LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. CHOSE TO LAND THE AIRCRAFT SGF FOR FUTHER INVESTIGATION FOUND GAUGES WERE READING CORRECTLY AND ON THE GROUND RUN UP STILL ONLY PRODUCED 85 PERCENT. THE LAST LEG OF THE TRIP WAS CSDR SWIA200413839Lamp · burned outEMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AT AFT EMERGENCY EXIT. OPERATIONAL CHECK GOOD.SDR SWIA200413826Actuator · malfunctionedON FINAL APPROACH WITH FLAPS 45 DEGREES, RECEIVED A FLAP CONTROL FAULT AND DISAGREEMENT LIGHTS. REMOVED AND REPLACED BOTH NACELLE FLAP ACTUATORS IAW MM REF 27-50-00. OPERATIONAL CHECK GOOD. P/N: 308200-1007, S/N OFF: 0163.SDR 2004F00390Indicator · malfunctionedUPON TAKEOFF PILOT REPORTED THAT THE LT PROPELLER WOULD ONLY MAKE 85 PERCENT NP. ABORTED THE LAST LEG AND CHOSE TO LAND. A GROUND RUN UP DETERMINED THAT THE LT NP WAS READING CORRECTLY. THE CAUSE FOR THIS DESCREPANCY IS YET UNKNOWN.
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