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.

SDR COMA0010169Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING UPPER SURFACE 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 NR 1226-21, REV Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010168Skin · gougedUPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE RIGHT HAND FORWARD LOWER FUSELAGE SKIN AT STRINGER 17R WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA0010167Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW CAPTAIN''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010166Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-022-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW F/O''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REJun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010165Skin · gougedUPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN AND PREVIOUS REPAIR DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01, FIGURE 201.Jun 14, 2000 · N261CA · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA0010164Skin · delaminatedUPON COMPLIANCE OF 2C INSPECTION TASK 612-01Z, THE RIGHT WING OUTBOARD LEADING EDGE WAS FOUND TO BE DELAMINATED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 57-40-01, FIGURE 201.Jun 14, 2000 · N261CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA0010163Stringer · crackedTHE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED JUST INBOARD OF RIB 8. THE STRINGER WAS REPAIRED PER EMB120 SRM 57-20-01, FIGURE 201 AND AERODESIGN REPORT NR 3694-1, REV IR, DATED 6-12-00.Jun 12, 2000 · N261CA · Emb EMB120RT · Wing, Longeron/StringerSDR COMA0010201Door · looseDOOR WARNING DURING TAKEOFF. SECURED LOOSE FUEL SERVICE DOOR.Jun 11, 2000 · N249CA · Emb EMB120RT · Fluid Service DoorsSDR ASOA00071Clamp · brokenFLT 4901 - CREW REPORTED THE RIGHT DUCT LEAK LIGHT CAME ON AFTER AIRCRAFT GOT TO THE GATE. FLIGHT ATTENDANT REPORTED A SMELL IN THE CABIN AND THE LAVATORY SMOKE DETECTOR WENT OFF. MAINTENANCE FOUND THAT THE BOOT CLAMP FOR THE AIR DUCT TO THE HEAT EXCHANGER WJun 10, 2000 · N267AS · Emb EMB120RT · Cabin Cooling SystemSDR COMA0010162Sensor · malfunctionedTAKEOFF TRIM WARNING. REPLACED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR.Jun 9, 2000 · N267CA · Emb EMB120RT · Elevator Tab Control SystemSDR ASOA00068Audio Panel · smokeFLT 4075 - CAPTAIN REPORTED DURING APPROACH INTO ROA, HAD HEAVY SMELL OF SOMETHING BURNING WITH VISIBLE SMOKE COMING FROM CAPTAINS AUDIO PANEL. AIRCRAFT LANDED SAFELY. MAINTENANCE REPLACED CAPTAINS AUDIO CONTROL PANEL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFJun 8, 2000 · N246AS · Emb EMB120RT · Audio Integrating SystemSDR COMA0010160Shutoff Valve · malfunctionedCABIN PRESSURE INCREASES AND DECREASES WITH POWER LEVER MOVEMENT. REPLACED THE PRSOV.Jun 8, 2000 · N268CA · Emb EMB120RT · Cabin Pressure Control SystemSDR COMA0010161Battery · dischargedOVERHEAD EMERGENCY LIGHT AT ROW 6 IS INOPERABLE. REPLACED BATTERY PACK.Jun 7, 2000 · N269CA · Emb EMB120RT · Emergency LightingSDR ASOA00067Brake · crackedFLT 4917 - AT POSITION AND HOLD CREW ROLLED AIRCRAFT OUT ONTO RUNWAY 17L WHEN THE AIRCRAFT SUDDENLY CAME TO A STOP. AIRCRAFT WOULD NO LONGER MOVE SO CREW INFORMED TOWER AND ASKED AIRCRAFT NEXT TO PLANE TO CHECK FOR FLAT TIRES. AIRCRAFT WAS TUGGED BACK TO THEJun 6, 2000 · N258AS · Emb EMB120RT · Landing Gear Brake SystemSDR C2XA00IA154Battery Pack · dischargedIAH - DURING A-CHECK INSPECTION, THE PASSENGER ENTRANCE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY PACK IAW EMB 120 MM 33-50-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Jun 5, 2000 · N58733 · Emb EMB120RT · Emergency LightingSDR C2XA00IA177Seat Track · corrodedLEFT SEAT TRACK OUTBOARD END AT FRAME NR 40 TO NR 37 CORRODED. REMOVED LEFT SEAT TRACK FOR BEING OUT OF LIMITS IAW EC 2510-01016. INSTALLED TRACK IAW CONTINENTAL EXPRESS EC 2510-01016. (M)Jun 3, 2000 · N16724 · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR C2XA00IA178Intercostal · corrodedRIGHT INTERCOSTAL AT FRAME NR 40 CORRODED. REMOVED INTERCOSTAL, MATCH DRILLED NEW INTERCOSTAL, INSTALLED INTERCOSTAL IAW EMB-120 SRM 51-40-02. (M)Jun 3, 2000 · N16724 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA00IA191Strap · corrodedRIGHT FLOOR SEAT TRACK BUTT SPLICE AFT FRAME NR 28 HAS LIGHT CORROSION. REMOVED CORROSION IAW CONTINENTAL EXPRESS EMB120 SRM 51-40-02. ALODINED AND PRIMED IAW EMB120 CPM 51-21-05. (M)Jun 3, 2000 · N16724 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA00IA190Beam · corrodedFOUND CORROSION ON FRAME AFT OF STATION 38 RT FLOORBEAM. REMOVED SEAT TRACK AND BUTT STRAP AT FRAME STATION 38 TO ACCESS BEAM RIGHT SIDE. REMOVED CORROSION, FOUND OUT OF LIMITS IAW EMB120 CPM 51-14-00. FABRICATED REPAIR ANGLE IAW EC5310-01043. HEAT TREATEDJun 3, 2000 · N16724 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR C2XA00IA189Strap · corrodedRIGHT BUTT SPLICE AT FRAME NR 40 TO NR 38 CORRODED. REMOVED CORRODED BUTT SPLICE, TRIMMED AND DRILLED UP NEW PIECE, INSTALLED NEW BUTT SPLICE PER EMB120 SRM 51-40-02. (M)Jun 3, 2000 · N16724 · Emb EMB120RT · Fuselage Miscellaneous StructureSDR ASOA00065Panel · inoperativeFLT 4998 - CAPTAIN REPORTED EMERGENCY LIGHTS NOT ARMED. MAINTENANCE REPLACED THE MULTIPLE ALARM PANEL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Jun 1, 2000 · N241AS · Emb EMB120RT · Emergency LightingSDR COMA011008Crossbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-011 THE FRAME 12 CROSS BEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR ASOA00064Frame · crackedDURING INSPECTION, FOUND NR 1 NACELLE FRAME CRACKED. MAINTENANCE REPAIRED CRACK IAW EMB 120-54-0027B. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)May 31, 2000 · N229AS · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR ASOA00063Strap · corrodedDURING INSPECTION, FOUND CORROSION ON CABIN FLOOR SILLS, CROSS MEMBERS, AND BUTTSTRAPS. MAINTENANCE REPAIRED CORROSION IAW EMB CPM 51-144-01 AND MM 51-21-04. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)May 31, 2000 · N229AS · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010159Clip · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5720-522-0II, THE RIB NR 5 SKIN CLIP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Wing Main, Frame StructureSDR COMA0010158Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FRAME 43 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010157Angle · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5320-243/244-02I, THE WING TO FUSE FAIRING LOWER ATTACH ANGLES WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1226-9.May 31, 2000 · N257CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA0010156Beam · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER OMEGA BEAM WAS FOUND TO BE CRACKED IN TWO PLACES AND CORRODED IN ANOTHER. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1716-5.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010155Channel · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z, DOOR CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Passenger/Crew DoorsSDR COMA0010154Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-221/222-15I, THE FRAME 9 LEFT AND RIGHT SKIN SUPPORTS WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 660-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, StructureSDR COMA0010153Frame · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE FRAME 22 CHANNEL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3674-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, FrameSDR COMA0010152Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE RT FLOOR CROSSBEAM FRAME 33 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010151Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE CARGO AFT RIGHT HAND SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3661-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010150Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE CARGO FORWARD RIGHT HAND SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3661-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010149Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND FLOOR CROSSBEAM AT FRAME 19 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010148Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FRAME 16 FLOOR T SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010147Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 231/232-01Z, THE RIGHT HAND FORWARD SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010146Threshold · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND NR 1 SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010145Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE RIGHT HAND NR 1 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010144Floorbeam · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE LEFT HAND FLOOR CROSSBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010143Floor Support · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LEFT HAND FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010142Support Bracket · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 231/232-01Z, THE LEFT HAND NR 1 SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010141Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE LEFT HAND NR 6 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010140Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE LEFT HAND NR 4 BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010139Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 141/142-01Z, THE LEFT HAND NR 2 BUTT STRAP WAS FOUND TO BE CORROCED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA0010138Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LEFT HAND NR 1 BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010137Strap · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER NR 1 BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-12O STRUCTURAL REPAIR MANUALSTANDARD PRACTICES.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010136Plate · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE LT FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-2.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010135Plate · corrodedUPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CENTER FWD BUTT PLATE WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA0010134Shear Tie · crackedUPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-O1I, THE FRAME 12 SKIN SUPPORT WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 3653-1.May 31, 2000 · N257CA · Emb EMB120RT · Fuselage Main, Structure
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