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 HKGA201906260020Trim Tab · rustedLEFT ELEVATOR TRIM TAB CORRODED. R & R THE TRIM TAB OUTBOARD 2 HINGE FITTING IAW AMM 20-10-01-2 REV 43.SDR HKGA201906260016Support · crackedSUPPORT CRACKED. REMOVED AND REPLACED THE SUPPORT AND MATCH DRILLED NEW SUPPORT IAW SRM 51-40-02 REV 58).SDR HKGA201906260015Shear Tie · crackedREMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04, REV 10.
SDR HKGA201906260014Shear Tie · crackedREMOVED CRACKED SHEAR TIE AND MATCH DRILLED NEW SHEAR TIE IAW SRM 51-40-02, 51-25-00 REV 58. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 REV 58. TREATED AND APPLIED TOP COAT IAW CPM 51-21-04 REV 10.SDR HKGA201906250019Doubler · corrodedDOUBLER CORROED. MATCH DRILLED REPAIR PARTS IAW SRM 51-70-04, AND 51-40-02, REV 58. INSTALLED DOUBLER AND FILLER IAW STEP 2 OF ETD 2019-120-055992 AND SRM 51-40-02, REV 58. REMOVED REPAIRED DOUBLER IAW SRM 51-40-02, REV 58, CONFIRMED AFFECTED AREA CRACK FRSDR HKGA201906250018Cover · corrodedRUDDER HINGE COVER CORROED. CLEANED, PREPARED A NEW UPPER HINGE PANEL AND APPLIED PRIMER IAW CPM 51-21-04, AND 51-21-05. APPLIED TOP COAT IAW CPM 51-21-06.SDR HKGA201906250017Bearing · corrodedRUDDER HINGE BEARING CORRODED. R & R THE RUDDER LOWER HINGE BEARING IAW MM 20-40-03, REV 43.SDR HKGA201906250013Shear Tie · crackedSHEAR TIE FOUND DAMAGED. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SRM 51-40-02, REV 58. TREATED, PRIMED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10.
SDR HKGA201906250012Shear Tie · crackedSHEAR TIE CRACKED AT FRAME 44, BETWEEN STRINGERS 1 & 2. REMOVED AND REPLACED THE DAMAGED SHEAR TIE IAW SPM 51-40-02. TREATED AND APPLIED TOP COAT TO FASTENERS IAW CPM 51-21-04 REV 10.SDR HKGA201906250009Door · chafedOVERWING EXIT WAS CHAFED. REMOVED CHAFE DAMAGE IAW CPM 51-14-00. TREATED, PRIMED AND APPLIED TOP COAT TO AFFECTED AREA IAW CPM 51-21-04.SDR HKGA201906250011Intercostal · damagedINTERCOSTAL DAMAGED, REMOVED DAMAGE IAW EPM 51-14-00. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04.SDR HKGA201906240010Frame · damagedREMOVED DAMAGED FRAME AND MATCH DRILLED NEW FRAME IAW SRM 51-40-02 REV 58. INSTALLED A NEW FRAME 30 SEGMENT IAW SRM 51-40-02 REV 58.SDR HKGA201906250006Frame · gougedREMOVED DAMAGED AREA ON FRAME 35 BETWEEN STRINGERS 3 AND 4R IAW SRM 51-40-02, AND 53-00-04, REV 58. INSTALLED A REPAIRED DOUBLER IAW SRM 53-00-04, REV 58.
SDR HKGA201906250008Frame · gougedBLENDED A GOUGE ON THE AFT SIDE OF FRAME 19 IAW CPM 51-14-02 REV 10. CONFIRMED CRACK FREE IN AFFECTED AREA IAW NDIM 51-00-03 REV 3. TREATED AND PRIMED AFFECTED AREA IAW CPM 51-21-04 REV 4.SDR HKGA201906250007Skin · dentedREWORKED DENT IAW SRM 51-7400 REV 58. CONFIRMED AFFECTED AREA CRACK FREE IAW NDIM 51-00-03 REV 3. TREATED, PRIMED, AND APPLIED TOPCOAT IAW CPM 51-21-04 REV 10.SDR HKGA201906250005Shear Tie · corrodedSHEAR TIE CORROED. REMOVED FR 19 SEGMENT FROM STR 1R-15R AND 2 DOUBLERS IAW SRM 51-40-02 REV 58. INSTALLED NEW FRAME AND 2 DOUBLERS IAW SRM 51-40-02 REV 08.SDR HKGA201906240004Cover Plate · corrodedREMOVAL AND INSTALLATION OF CARGO DOOR THRESHOLD COVER PLATE COMPLETE (PER ETD 2019-120-062528). PN: 120-16200-001 LOWER CARGO DOOR BEAMSDR HKGA201906240003Floorbeam · corrodedFLOOR BEAM SEGMENT CORRODED . INSTALLED A NEW FLOOR BEAM SEGMENT IAW SRM 51-40-02 REV 58.SDR HKGA201906240002Floor Support · corrodedREMOVED FLOOR BEAM UPPER SURFACE (REF. SRM 51-25-00). INSTALLED NEW FLOOR BEAM AT FRAMES 17 - 18 (REF. SRM 51-40-02 REV 58). PN: 120-05805-603 BUTT STRAP REPLACES 120-05805-003SDR HKGA201906240001Floor Support · corrodedUPPER SURFACE OF LH FLOOR BOARD ATTACH ANGLE BETWEEN FRAMES 15A - 16A WAS FOUND TO HAVE CORROSION. REMOVED FLOOR SILL (REF. SRM 51-40-02 REV 58). INSTALLED NEW FLOOR SILL (REF. SRM 51-40-02 REV 58).
PN: 120-05802-001 SILLSDR HKGA20181205004Hinge · crackedDURING AN INSPECTION, THE LT NACELLE FLAP INBOARD HINGE WAS FOUND CRACKED. REMOVED AND REPLACED FLAP ASSEMBLY IAW MM 27-50-03. OPERATIONAL CHECK GOOD.SDR JIKA20181119402A/C Pack · overheatedDISCREPANCY:
AFTER TAKING OFF FROM KPHX, THE CREW REPORTED DURING CLIMB THAT SMOKE WAS COMING OUT OF THE AIR VENTS. AFTER RUNNING THROUGH QRH THE CREW MADE THE DECISION TO RETURN TO KPHX. THE CREW STATED, SMOKE GOGGLES WEREN’T NECESSARY. INITIALLY THEY DIDSDR JIKA201809100402Actuator · defectiveAFTER T/O FROM KONT AND RETRACTING THE FLAPS AT APPROX 1000 FEET, FLAP DISAGREEMENT LIGHT ILLUMINATED. CREW PERFORMED A SYSTEM CHECK PER QRH AND WAS UNABLE TO CLEAR THE FLAP DISAGREEMENT WARNING. DECLARED AN EMERGENCY, RETURNED TO KONT AND LANDED WITHOUT INCIDSDR JIKA201809100401Warning System · false activationTHE CREW REPORTED AFTER TAKEOFF FROM KLAX, A FLAP DISAGREEMENT WARNING OCCURRED. THEY PERFORMED A SYSTEM CHECK IN ACCORDANCE WITH QRH AND RECYCLED THE FLAPS, BUT THE FLAP DISAGREEMENT WARNING RETURNED. THE CREW DECLARED AN EMERGENCY, AND LANDED AT KONT WITHOUTSDR HKGA201807274003Relay · burnedIN CRUISE, PILOT NOTICED A SMELL LIKE BURNING WIRE AND SMOKE WAS VISIBLE IN THE COCKPIT. DE-ICE LIGHT FAIL INDICATION ILLUMINATED AND THE NR 2 PITOT STATIC CIRCUIT BREAKER POPPED. AIRCRAFT DIVERTED TO THE NEAREST AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLESDR GLBA2018021900702Sign · unsecurePILOTS NOTED THAT THE EMERGENCY EXIT SIGN AT ROW 8 WON'T STAY ATTACHED.SDR HKGA20180201001Tube · rupturedSHORTLY AFTER TAKEOFF, THE PILOTS TURNED THE BLEEDS TO NORMAL IAW AFTER TAKEOFF CHECKLIST AND RECEIVED A RED LT DUCT LEAK ANNUNCIATION. PERFORMED THE QRH PROCEDURES AND RETURNED TO THE AIRPORT. MAINTENANCE TROUBLESHOT THE ISSUE TO THE LEFT CROSS BLEED TUBE ASDR GN0A201801090001Garlock Seal · burstDURING CRUISE FLIGHT AT 24000, OIL WARNING LITE LEFT ENGINE CAME ON. CREW NOTED OIL PRESSURE AT 40PSI FOR LEFT ENGINE, CREW REFERENCED QRH, PILOT ADVISED ATLANTA CENTER OF PROBLEM AND REQUESTED FL2000. SECURED ENGINE PER QRH. REQUESTED DIRECT CLT AND WAS GIVENSDR 2018F00068Altimeter · faultyAFTER TAKEOFF AND CLIMBING, THE PILOTS WERE QUESTIONED BY ATC ABOUT THEIR ALTITUDE BEING 1200 FT WHEN THEY WERE LEVELING AT 4000 FT. CREW INFORMED ATC THAT THEIR ALTITUDE WAS 4000 FT, HOWEVER ATC REPLIED AGAIN THAT THEY WERE SHOWING THEM AT 1200 FT. THE CAPTASDR HKGA20171207008Relay · intermittentDURING APPROACH THE LANDING GEAR DID NOT EXTEND WHEN THE GEAR HANDLE WAS PLACED IN THE DOWN POSITION. THE FLIGHT CREW BEGAN EMERGENCY PROCEDURES AND ACTIVATED THE ELECTRICAL OVERRIDE SYSTEMS AND THE GEAR EXTENDED AND THE FLIGHT CREW RECEIVED THREE GOOD DOWN ANSDR GLBA2017120400694Proximity Sensor · faultyPILOTS REPORTED THAT AFTER LANDING, THE AIRCRAFT HAD NO NOSE WHEEL STEERING BY TILLER OR RUDDER. CREW ALSO NOTED THAT THE IDLE UNLOCK LIGHTS ILLUMINATED AND ELECTRONIC LIGHTS ILLUMINATED ON THE MAP. PACKS STARTED SMOKING BECAUSE THE GROUND COOLING FANS WERE NOSDR GLBA2017111700692Sliding Window · obstructedTHE CREW REPORTED THAT THE CAPTAIN'S SIDE WINDOW IS STIFF AND DIFFICULT TO CLOSE. MAINTENANCE FOUND A LOOSE PIECE OF EXCESS SEALANT JAMMING LOWER SEAL AREA, REMOVED LOOSE PIECE. SEALING SURFACE REMAINED INTACT AND WINDOW CLOSES NORMALLY. PRESSURIZED AIRCRAFT SDR GLBA2017101900688Latch · brokenMAINTENANCE REPORTED THAT THE PAX DOOR BOTTOM LATCH WAS BROKE. REMOVED AND REPLACED THE LATCH IAW SRM 51-40-02.SDR GLBA2017101600687Lock · lack of lubePILOTS REPORTED THAT THE MAIN DOOR LOCK MECHANISM STICKS. MAINTENANCE CLEANED AND LUBRICATED THE DOOR ROLLERS, OPS CHECKED GOOD.SDR GLBA2017100400686Circuit Breaker · failedTHE CREW REPORTED THAT THE EMERGENCY BUSS OFF LIGHT ILLUMINATED DURING DESCENT. THE ISSUE WAS ISOLATED TO EMERGENCY DC BUSS NR 2 FAILURE. EXTENDED GEAR BY ELECTRICAL OVERRIDE. AN EMERGENCY WAS DECLARED PRIOR LANDING. MAINTENANCE INSPECTED WIRING & COMP IN LSDR GLBA2017092500684Line · disconnectedPILOTS REPORTED THAT THE NR 1 PACK FAILED IN FLIGHT AND THERE WAS SMOKE IN THE CABIN. MAINTENANCE PERFORMED AN OPS CHECK OF THE LEFT PACK, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOT FURTHER AND FOUND A PNEUMATIC LINE DISCONNECTED FROM TEST PORT AT LEFT HEASDR GLBA2017082100680Door · detachedPILOTS REPORTED THAT THE RIGHT MAIN OTBD GEAR DOOR IS WIDE OPEN AND WON'T CLOSE. MAINTENANCE FOUND THE RIGHT OTBD GEAR DOOR UNLATCHED, ATTACHED THE OUTER GEAR DOOR. OPS CHECKED GOOD.SDR GLBA2017082100679Door · unlatchedPILOTS REPORTED THAT THE RIGHT MAIN GEAR DOOR IS OPEN AND WON'T CLOSE. MAINTENANCE FOUND THE RIGHT OUTBOARD GEAR DOOR UNLATCHED, RELATCHED. OPS CHECK GOOD.SDR JIKA2017071401Seal · wornDURING CLIMB OUT FROM KPDX REPORTED THAT THE LT“DUCT LEAK ANNUNCIATOR ILLUMINATED. THE CREW FOLLOWED THE QRH AND TURNED THE LT BLEED VALVE OFF AND THE LIGHT EXTINGUISHED. FOLLOWED THE QRH PROCEDURES AND TURNED THE LT BLEED BACK ON AND THE LIGHT RE-ILLUMINATED.SDR GLBA2017071100674Brake Sys · weakPILOTS REPORTED THAT THE BRAKES REQUIRE EXCESSIVE PRESSURE TO ACTIVATE. STOPPING POWER IS VERY LIMITED. MAINTENANCE R & R THE NR 2 BRAKE AND NR 4 BRAKE IAW MM 32-41-05, OPS CHECKED GOOD. R & R THE NR 1 BRAKE ASSY IAW MM 32-41-05, OPS CHECKED GOOD. R & R THE NSDR GLBA2017070700673Valve · failedPILOTS REPORTED THAT THE BRAKES REQUIRE EXCESSIVE PEDAL PRESSURE TO HAVE ANY EFFECT. R & R THE BRAKE METERING VALVES IAW MM 32-41-02. LEAK & OP CHECKED GOOD.SDR GLBA2017070500671Cable · bindingPILOTS REPORTED THAT SEAT 4A RECLINES AND BLOCKS THE EXIT ROW. MAINTENANCE UNJAMMED THE ACTUATOR CABLE END. SEAT DOES NOT RECLINE WITH BUTTON PRESSED OR NOT PRESSED. TRAVEL OF ACTUATOR FIXED WITH C CLIP.SDR GLBA2017063000670Wire · shortedTHE PILOTS REPORTED THAT DURING TAKEOFF, THE F/O'S EFIS TUBES FLICKERED AND THEN THERE WAS A COMPLETE ELECTRICAL FAILURE, LOST BRAKES, STEERING AND ALL RADIO COMMUNICATIONS. EMERGENCY BRAKES WHERE USED TO STOP THE AIRCRAFT. AFTER SHUTDOWN NUMEROUS AIRCRAFT SYSDR GLBA2017062600667Fuse · malfunctionedPILOTS REPORTED THAT THE BRAKES REQUIRE EXCESSIVE PRESSURE AND TRAVEL TO ACTIVATE. STOPPING POWER IS VERY LIMITED. MAINTENANCE RESET THE NR 2 HYDRAULIC FUSE IAW MM 32-41-04-5, OPS CHECKED GOOD.SDR GLBA2017061900666Relay · burnedPILOTS NOTED THAT THE FO'S SIDE PANEL IS HOT TO THE TOUCH AND SMELLS LIKE BURNING WIRES. MAINTENANCE FOUND THE FEEDER PROTECTION RELAY TO BE BURNED AND BROKEN. R & R THE FEEDER PROTECTION RELAY IAW MM 24-52-00.SDR GLBA2017061900665Brake Sys · malfunctionedPILOTS REPORTED THAT THE BRAKES REQUIRE EXCESSIVE PRESSURE AND TRAVEL TO ACTIVATE. MAINTENANCE BLED THE BRAKE SYSTEM IAW MM, OPS CHECKED GOOD.SDR GLBA2017052200662Switch · failedMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR CLOSES ITSELF WHEN OUTSIDE BOTTOM IS RELEASED. FOUND EXTERIOR DOOR CLOSE SWITCH FAILED WITH CONTINUITY AT ALL TIMES. R&R SWITCH BY SOLDERING AIM 14.3.7 DOOR. OPS CHECKS GOOD AMM 52-12-00-3C.SDR GLBA2017052200661Accumulator · low pressureMAINTENANCE REPORTED THAT THE AIRSTAIR DOOR ACCUMULATOR NEEDS TO BE CHARGED. SERVICED AIRSTAIR DOOR ACCUMULATOR IAW MM 12-13-06.SDR GLBA2017052200660Selector Valve · failedTHE CREW REPORTED THAT THE FWD DOOR ACTUATING SYSTEM WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SELECTOR VALVE IAW MM 52-12-01. OPS & LEAK CHECKED GOOD.SDR GLBA2017051500655Spring · brokenMAINTENANCE REPORTED THAT THE THIRD STEP ON THE MAIN CABIN DOOR HAS A BROKEN SPRING. REMOVED AND REPLACED THE CABIN DOOR STEP SPRING AND SPACER, OPS CHECKED GOOD IAW 52-10-05.
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