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 COMA0010300Tire · dischargedRIGHT HAND MLG TIRE LOW PRESSURE. REPLACED WHEEL TIRE ASSY.SDR 20000810SH018Angle · crackedDURING A ROUTINE MAINTENANCE C-CHECK, CRACKS WERE FOUND ON THE LEFT SIDE OF THE VERTICAL STABILIZER CHINE ANGLE BETWEEN STA 16128.0 AND STA 16144.9 AT 3 WORKING RIVETS. POSSIBLE CAUSE. FATIGUE/VIBRATION. SUBMITER RECOMMENDED A DETAILED INSPECTION CALL OUT DSDR 20000810SH017Frame · crackedDURING ROUTINE MAINTENANCE C-CHECK, A CRACK WAS FOUND ON BOTH ENGINE NACELLE FRAMES NR 1. THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING HOLE AND THE OUTBOARD EDGE OF THE FRAME. SUBMITTER RECOMMENDED REPLACINGSDR C2XA00IA198Bulb · failedIAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT FUSELAGE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA196Connector · dirtyIAH - FLT 3371 - ON APPROACH, THE CREW REPORTED THAT THE RIGHT OUTBOARD FLAP RETRACTED TO 15 DEGREES UNCOMMANDED. THE CREW LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED, CLEANED, AND REINSTALLED THE CANNON PLUG ON RIGHT OUTBOARD FLAP ASSEMBLY, AND OPERSDR ASOA00082Battery · inoperativeCREW REPORTED SEVERAL FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR C2XA00IA255Seat Track · corrodedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 31 TO FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW WITH EMB120 SRM 53-01-05, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR C2XA00IA254Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE RIGHT NACELLE NR 1 FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA00IA253Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, NDI TESTING REVEALED A CRACK IN THE LEFT NAELLE NUMBER ONE FRAME. MAINTENANCE REMOVED AND REPLACED HE AFFECTED FRAME, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ASOA00081Control Panel · inoperativeFLT 4915 - CREW REPORTED THAT AFTER F/O WENT TO ASA FREQUENCY A-25 C/B POPPED. THE F/O LIGHTS EXTINGUISHED AND SMOKE WAS OBSERVED. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN TXK. MAINTENANCE REPLACED THE F/O AUDIO CONTROL PANEL. OPERATIONAL CHECKS WERSDR C2XA00IA192Door · disconnectedIAH - FLT 3581 - THE CREW REPORTED THAT THE LEFT FORWARD NOSE GEAR DOOR WOULD NOT CLOSE AND A LOUD NOISE COMING FROM THE NOSE LANDING GEAR COMPARTMENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RECONNECTED THE LEFT FORWARD NLG DOOR AND OPERATISDR SWIA971858Light · inoperativeEMERGENCY LIGHTS FRONT LEFT FLOOR AND MIDDLE CEILING AND SIDE INOP. REPLACED FORWARD EMERGENCY LIGHT BATTERY, OPS CHECKS GOOD. S/N: 263, S/N OFF: 12741896.SDR SWIA971857Light · inoperativeEMERGENCY LIGHTING INOP FORWARD FLOOR AND LEFT WALL EXIT SIGN. AFTER PROPER CHARGING, OPS CHECK OF EMERGENCY LIGHTING SYSTEM PER MM 335000 CHECKS GOOD.SDR COMA0010248Sequence Valve · out of adjLEFT HAND MLG DID NOT RETRACT. ADJUSTED THE MLG DOORS SEQUENCE VALVES. RETRACT CHECKS SATISFACTORY.SDR COMA0010247Solenoid · failedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED.\NREPLACED THE FLIGHT-IDLE STOP SOLENOID.SDR COMA0010244Computer · malfunctionedATTITUDE DISPLAY WARNING ON MAP. REPLACED THE NR 2 AHRS COMPUTER.SDR SWIA971863Flap Track · roughFLAP DISAGREEMENT INVOLVING OUTBOARD FLAP PAIRS. QRH FOLLOWED WITH NO SUCCESS, RETURNED TO FIELD. FLAP EXTENDED NORMALLY ON APPROACH. RETRACTED NORMALLY ON GROUND. CHECKED ALL FLAP ACTUATORS WITH BREAKOUT BOX, NO DEFECTS APPARENT. SMOOTHED OUT BURR ON LEFSDR COMA0010245Actuator · malfunctionedLEFT HAND MLG DID NOT RETRACT. REPLACED THE RETRACT ACTUATOR.SDR COMA0010243Warning System · false activationTAKE OFF TRIM CONFIG WARNING. COULD NOT DUPLICATE. TRIM AURAL WARNING SYSTEM CHECKS SATISFACTORY.SDR COMA0010246Landing Gear · malfunctionedLEFT HAND MLG DID NOT RETRACT. COULD NOT DUPLICATE. RETRACTION CHECKS SATISFACTORY.SDR COMA0010210Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7/25/99.SDR ASOA00078Line · brokenAFTER TAKEOFF, AIRCRAFT LOST GREEN HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY AND LANDED SAFELY IN MCN. MAINTENANCE REPAIRED BROKEN GE ACTUATOR LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SWIA971852Controller · malfunctionedON DESCENT, FLAP AND ADVANCED STALL WARNING LIGHTS ILLUMINATED ALONG WITH CONTROL FAULT LIGHT AND SECOND ROW OUTBOARD FLAP LIGHTS ON FLAP PANEL. FOLLOWED QRH AND RESET, WARNINGS CORRECTED. AFTER LANDING ALL WARNINGS RETURNED AND WOULD NOT RESET. REMOVED ANDSDR SWIA971851Controller · malfunctionedON DESCENT, FLAP AND ADVANCED STALL WARNING LIGHTS ILLUMINATED ALONG WITH CONTROL FAULT LIGHT AND SECOND ROW OUTBOARD FLAP LIGHTS ON FLAP PANEL. FOLLOWED QRH AND RESET, WARNINGS CORRECTED. AFTER LANDING ALL WARNINGS RETURNED AND WOULD NOT RESET. CLEANED FLASDR COMA0010242Beam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FLOOR SUPPORT FWD CENTER OMEGA BEAM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #2181-9, IR, 6/23/00.SDR COMA0010241Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND CABIN FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010240Strap · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 163-01Z, THE CARGO COMPARTMENT AFT LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010239Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT LT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010238Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT LT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010237Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE FUSELAGE FRAME 38 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3674-4, IR, 6/24/00.SDR COMA0010236Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-O1I, THE CABIN FLOOR SUPPORT CENTER CROSSBEAM AT FRAME 12 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010235Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LEFT HAND CABIN FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARED PRACTICES.SDR COMA0010234Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RIGHT HAND FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010233Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND CABIN FLOOR SUPPORT CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010232Angle · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT ANGLE UNDER PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3711-1, IR, 6/24/00.SDR COMA0010231Angle · corrodedUPON COMPLIANCE OF 2C INSPECTION TAXK 131-01Z, THE CABIN FLOOR SUPPORT ANGLE UNDER PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3711-1, IR 6/24/00.SDR COMA0010230Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LEFT HAND CABIN FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010229Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LEFT HAND CABIN FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010228Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 262-01Z, THE CARGO DOOR AFT TRACTS TOP MOUNT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1657-3, IR, 6/12/00.SDR COMA0010227Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-O5I, THE FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #660-1, IR, 2/16/93.SDR COMA0010226Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-222-05I, THE RIGHT HAND FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #660-1, IR, 2/16/93.SDR COMA0010225Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE CABIN FWD RT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010224Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FORWARD CENTER FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010223Buttstrap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FLOOR SUPPORT FORWARD CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1671-1, REV A, 1/28/97.SDR COMA0010221Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT FWD LT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010220Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1226-21, IR, 7/6/99.SDR COMA0010219Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE FUSELAGE SKIN BELOW THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR #SST-1569/00SDR COMA0010218Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, THE FUSELAGE FRAME 13A SKIN SUPPORT AT STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3653-I, IR, 5/6/00.SDR COMA0010217Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE SKIN SUPPORT, COCKPIT OVERHEAD LEFT SIDE WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.SDR COMA0010216Support Bracket · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW AS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
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