Embraer EMB-120RT
Service difficulty reports · 5,310
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 = 'EMB120RT' 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 = 'EMB120RT' 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 COMA0010090Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE FUSLAGE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010089Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010088Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010087Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010086Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010085Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010083Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010082Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010081Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010080Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES.SDR COMA0010079Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010078Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010077Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z , THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A AND STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-1, REV IR, SDR COMA0010076Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 222-01Z, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.SDR COMA0010075Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145-/96.SDR COMA0010074Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 231-01Z, WHILE GAINING ACCESS THE LT COCKPIT SKIN SUPPORT BRACKET BEHIND TO DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010073Floorbeam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145/96.SDR COMA0010072Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-02I, THE RT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13, REV IR, 2-SDR COMA0010071Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-02I, THE LT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13 REV IR, 2-7SDR COMA0010070Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 25-12, WHILE ACQUIRING ACCESS THE CARGO DOOR TORSION BAR FWD SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1397-1, SDR COMA0010069Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE SKIN SUPPORT BRACKET AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010068Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-022, THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01 PG 201-204.SDR COMA0010065Pcu · out of rigRIGHT PROPELLER NP INDICATED 97 PERCENT MAX. FOUND TRANSFER TUBE TO PCU RIGGING DISCREPANCY. ADJUSTED RIGGING AND ACFT. RETURNED TO SERVICE.SDR COMA0010064Circuit Breaker · trippedLEFT HAND, FLIGHT IDLE STOP SOLENOID, CIRCUIT BREAKER IS TRIPPED. RESET CIRCUIT BREAKER, TESTED SYSTEM FOUND TO OPERATE NORMAL.SDR C2XA00IA129Strap · corrodedDURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO JUST PAST FRAME 14. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 53-10-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR C2XA00IA128Seat Track · corrodedDURING CONTINENTAL EXPRESS C-CHECK, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW EMB120 SRM 53-20-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA127Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT NACELLE FRAME ONE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5410-01034, AND THE AIRCRAFT WAS APPROVED FOR RESDR ASOA00048Stringer · crackedDURING INSPECTION, FOUND RT STR NR 10 CRACKED. MAINTENANCE REPAIRED CRACK FOLLOWING EO 120-57-0097 WHICH OUTLINES PROCEDURES FOR STR 10 CRACK REPAIR. (X)SDR COMA0010063Bulb · failedAFT, CEILING EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.SDR C2XA00CL037Fan · odorBUF - FLT 3206 - CREW REPORTED THAT COCKPIT AND CABIN FILLED WITH SMOKE WITH BOTH PACKS ON, APU ON, AND BOTH ENGINES OFF. MAINTENANCE INSPECTED APU, PACK COOLING FANS. GROUND RUN COULD NOT DUPLICATE PROBLEM, BUT NR 1 PACK COOLING FAN HAD STRONG OIL SMELL. PSDR C2XA00CL036Smoke · detectedAXO - FLT 3032 - CREW REPORTED THE COCKPIT AND CABIN FILLED WITH SMOKE IN-FLIGHT. AIRCRAFT RETURNED TO AZO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE BLEED AIR SYSTEM AND FOUND NO DEFECTS. PERFORMED GROUND RUNS WITH AIR CONDITION SYSTEM ON AND FOUNSDR C2XA00IA114Battery Pack · dischargedIAH - DURING SERVICE CHECK INSPECTION, THE AFT EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB120 MM 33-50-02, AND THE AICRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)SDR ASOA00046Pcu · inoperativeFLT 4180 - CLIMBING THROUGH 20,500 FEET, THE LEFT NP DROPPED TO 97 PERCENT THEN CONTINUED TO DROP TO 91 PERCENT. OIL PRESSURE WAS GOOD. CREW CALLED MAINTENANCE CONTROL AND WAS TOLD TO CONTINUE TO DFW. APPROXIMATELY 75 MILES FROM DFW, CREW RECEIVED OIL AURALSDR ASOA00045SLead · inoperativeFLT 8501 - CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER LEVERS WERE PULLED BACK BELOW 35 PERCENT TORQUE IN BOTH AUTO AND MANUAL LOW BLEEDS AT HIGH ALTITUDES. TEARDOWN REPORTS SHOWED A CRACKED OIL SUPPLY LEAD IN THE GAS GENERATOR CASE CAUSED OIL CONTAMISDR ASOA00045Acm · inoperativeFLT 8501 - CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER LEVERS WERE PULLED BACK BEOW 35 PERCENT TORQUE IN BOTH AUTO AND MANUAL LOW BLEEDS AT HIGH ALTITUDES. MAINTENANCE REMOVED NR 1 ENGINE ASSEMBLY IAW EMB MM. MAINTENANCE IS WAITING ON TEAR DOWN REPORSDR COMA0010062Circuit Breaker · trippedFLIGHT IDLE CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. PERFORMED OPS CHECKS WITH NO FAULTS.SDR C2XA00IA119Sequence Valve · inoperativeIAH - FLT 205B, DURING FLIGHT, CREW REPORTED THE LEFT HAND MAIN LANDING GEAR FORWARD DOOR WOULD NOT CLOSE WHEN THE GEAR WAS RETRACTED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED GEAR DOOR SEQUENCE VALVE IAW EMB120 MM 32-32-04, AND THE AIRCRAFT WAS APPROVEDSDR COMA0010061Placard · missingEMERGENCY EXIT PLACARD MISSING. REPLACED PLACARD.SDR COMA0010060Duct · leakingLEFT HAND BLEED AIR DUCT LEAK WARNING. TIGHTENED LOOSE HOSE CLAMPS AT LEFT HAND ACM.SDR ASOA00041Battery Pack · inoperativeFLT 4262 - CREW REPORTED FORWARD EMERGENCY LIGHTS BLINK WHEN TURNED ON AND THEN GO OUT. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR ASOA00039Stringer · corrodedDURING INSPECTION, FOUND A STRINGER ON THE BELLY OF THE AIRCRAFT CORRODED. ATL MAINTENANCE REPLACED CORRODED STRINGER IAW EMB120 SRM 53-20-03. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA00CL034Hydraulic Line · failedCLE - FLT 3210 - THE CREW REPORTED THAT AFTER TAKEOFF, LOST ALL GREEN HYDRAULIC PRESSURE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND CHAFFED HYDRAULIC LINE AT RESERVOIR. MAINTENANCE REPLACED HYDRAULIC LINE. SDR COMA0010059Engine · out of adjDURING TAKEOFF OIL PRESSURE INDICATED 68 PSI. ADJUSTED ENGINE OIL PRESSURE TO M/M SPECIFICATIONS.SDR COMA0010058Sign · brokenEXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA0010057Angle · crackedWHILE PERFORMING OTHER MAINTENANCE TO THE PASSENGER DOOR, THE FUSELAGE ENTRY WAY DOOR SILL ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES.SDR COMA0010056Angle · corrodedWHILE REPLACING THE FUSELAGE PASSENGER DOOR ENTRYWAY LOWER SILL ANGLE, THE SUPPORT ANGLE UNDERNEATH WAS FOUND SEVERELY CORRODED. THE ANGLE WAS REPLACED PER EMB120 SRM STANDARD PRACTICES.SDR COMA0010055Wire · damagedFLOOR TRACK LIGHTING AT ROW 1 IS INOPERABLE. REPLACED THE CABLE ASSY.SDR COMA0010052Skin · corrodedON A MAINTENANCE SERVICE CHECK, MECHANIC NOTED POPPED RIVET HEAD ON EXTERNAL SKIN, FRAME 21, LOWER LEFT SIDE, AND SEVERAL BULGES IN SKIN. UPON FURTHER INSPECTION, FOUND CORROSION BETWEEN SKIN AND TITANIUM STRAP. CUT OUT CORRODED AREA, FABRICATED AND INSTALLESDR COMA0010053Potentiometer · malfunctionedLANDING GEAR SELECTOR COULD NOT BE SELECTED UP. REPLACED THE NWS FEEDBACK POT.SDR COMA0010054Solenoid · malfunctionedFLIGHT IDLE SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED THE LEFT HAND SOLENOID.
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