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 COMA9610379Stringer · corrodedINSPECTION REVEALED THE FUSELAGE FWD SECTION OF STRINGER 18L CORRODED. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-A, REV IR, DATED 11-6-96.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610378Skin · corrodedINSPECTION REVEALED THE LOWER FUSELAGE SKIN CORRODED BENEATH THE NR 2 COM ANTENNA. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2089-1 REV IR, DATED 11-7-96.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610377Support · corrodedINSPECTION REVEALED THE FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610376Support · corrodedINSPECTION REVEALED THE FUSELAGE CENTER SECTION LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610374Support · corrodedINSPECTION REVEALED THE FUSELAGE CENTER SECTION AFT LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610373Crossbeam · corrodedINSPECTION REVEALED THE FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 16 CORRODED. THE CROSSBEAM WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610372Butt Strap · corrodedINSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT-STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610371Support · looseINSPECTION REVEALED THE AFT RIGHT EMERGENCY EXIT MECHANISM BELLCRANK SUPPORT MOUNTING RIVETS, THROUGH DOOR SKIN TO BE LOOSE CAUSING EXCESSIVE PLAY IN THE DOOR OPENING MECHANISM. THE RIVETS WERE REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51, NO OTHER Dec 9, 1996 · N168CA · Emb EMB120RT · Emergency ExitsSDR COMA9610370Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 2 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/SkinSDR COMA9610369Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 1 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/SkinSDR COMA9610368Rib · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING RIB NR 1, CL RIB DAMAGED. REMOVED AND REPLACED IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Rib/BulkheadSDR COMA9610367Spar Cap · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing SparSDR COMA9610366Spar Web · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing SparSDR COMA9610365Aux Spar Cap · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9610364Aux Spar Web · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623.Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Miscellaneous StructureSDR COMA9610363Frame · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE FRAME 10 WEB, INBD AND OUTBD SIDES DAMAGED. PERFORMED REPAIRS IAW COMAIR ENGINEERING ORDER 54-005.Dec 9, 1996 · N168CA · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/RibSDR COMA9610362Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: LEFT AND RIGHT NACELLE LOWER SKINS DAMAGED. REMOVED AND REPLACED LT AND RT NACELLE LOWER SKINS IAW COMAIR ENGINEERING ORDER 54-005.Dec 9, 1996 · N168CA · Emb EMB120RT · Nacelle/Pylon, Plate/SkinSDR COMA9610361Stringer · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: RIGHT NACELLE INBD STRINGER NR 1 DAMAGED. REMOVED AND REPLACED STRINGER IAW EMBRAER DOCUMENTS EDU-014/96 AND EST-420-96.Dec 9, 1996 · N168CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA9610360Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FUSELAGE CENTER SECTION II, LOWER SKIN PANEL FROM FS 9964.5 TO FS 13056.0 DAMAGED. REMOVED AND REPLACED SKIN IAW ENGINEERING ORDER 53-012.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610359Skin · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FWD LOWER SKIN PANEL JUST AFT OF THE NLG DAMGED. PERFORMED REPAIR IAW COMAIR ENGINEERING ORDER 53-012.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610358Bulkhead · damagedDETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: FWD PRESSURE BULKHEAD DAMGED. PERFORMED REPAIR IAW COMAIR ENGINEERING 53-012.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, BulkheadSDR COMA9610355Skin · corrodedDURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFORCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610354Sill · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT SILL CORRODED. REPLACED SILL WITH NEW PART PER EMB120 SRM STANDARD PRACTICES CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610353Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT BUTT STRAP CORRODED. REPLACED BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610352Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD CENTER FLOOR SUPPORT STRUCTURE BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610351Butt Strap · corrodedDURING 2C INSPECTION, FOUND FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610350Crossbeam · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT LT CROSSBEAM CORRODED. REPLACED CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610349Sill · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT SILL CORRODED. REPLACED LT SILL PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610348Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51 AND AERODESIGN REPORT 31671-2, REV IR, DATED 12-4-96.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610347Stringer · corrodedDURING 2C INSPECTION, FOUND FUSELAGE STRINGER 18L CORRODED AT FWD END, FS 4088.0. REPAIRED STRINGER PER AERODESIGN REPORT NR 1990-2, REV IR DATED 9-15-96.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610346Crossbeam · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 HAD CORROSION. REPLACED RT CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610345Butt Strap · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610344Support Section · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORTING SECTION CORRODED. REPLACED SUPPORTING SECTION WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610343Support Section · corrodedDURING 2C INSPECTION, FOUND FUSELAGE FWD RT SIDEWALL SEAT TRACK SUPPORTING SECTION CORRODED. REPLACED RT SUPPORT SECTION WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610342Sill · corrodedDURING 2C INSPECTION, FOUND FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL CORRODED. REPLACED RT SILL WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610341Crossbeam · crackedDURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS CRACKED BY MAINTENANCE PERSONNEL. THE CROSSBEAM WAS REPAIRED PER ERODESIGN REPORT NR 2117-1, REV IR, DATED 12-3-96.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610340Skin · corrodedDURING 2C INSPECTION, FOUND FUSELAGE BELLY SKIN SEVERELY CORRODED AT FRAME 23. THE DAMAGE WAS REPAIRED PER EMB120 SRM 53-00-01, FIG 202.Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA610375Support · corrodedINSPECTION REVEALED THE FUSELAGE CENTER SECTION RT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB120SRM STANDARD PRACTICES, CHAPTER 51.Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR GLBA96237Gear Handle · failedFSD - GEAR WOULD NOT COME UP. MAINTENANCE REMOVED AND REPLACED GEAR HANDLE. OPERATIONAL CHECKS GOOD. (M)Dec 8, 1996 · N129AM · Emb EMB120RT · Landing Gear SelectorSDR COMA9610357Prox Sensor · inoperativeLANDING GEAR WILL NOT RETRACT, HANDLE WILL NOT MOVE TO UP POSITION. REPLACED LEFT STRUT PROX SENSOR, OPS CHECK GOOD.Dec 8, 1996 · N189CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610356Actuator · out of adjustAFTER TAKEOFF, RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. RETURN TO AIRPORT. ADJUSTED RIGHT MAIN LANDING GEAR ACTUATOR, OPS CHECK GOOD.Dec 6, 1996 · N257CA · Emb EMB120RT · Landing Gear ActuatorSDR WTAA960210Hydraulic Line · brokenFAT - GREEN HYDRAULIC LOW PRESSURE AND LOW LEVEL LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT OUTBOARD SEQUENCE VALVE HYDRAULIC PRESSURE LINE LEAK AND OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVDec 5, 1996 · N284UE · Emb EMB120RT · Hydraulic System, MainSDR COMA9610339Fuel Door · not closedSERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN - SECURED DOOR CLOSED AND AIRCRAFT CONTINUED SERVICE.Dec 4, 1996 · N462CA · Emb EMB120RT · Fluid Service DoorsSDR WTAA960209Circuit Breaker · trippedSFO - TRIM WARNING ON TAKEOFF REPORTED. TAKEOFF ABORTED. MAINTENANCE RESET AURAL WARNING CIRCUIT BREAKER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)Dec 3, 1996 · N120AM · Emb EMB120RT · Central WarningSDR COMA9610338Deice Boots · wornLT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS.Dec 3, 1996 · N205CA · Emb EMB120RT · Airfoil Anti/De-ice SystemSDR C2XA96CL044Annunciator · failedCLE - FLT 4244 - THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP CONTROL FAULT WHICH WOULD NOT RESET. THE AIRCRAFT RETURNED TO BASE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE FLAP ANNUNCIATOR ASSEMBLY. OPERATIONAL CHECKS WEREDec 3, 1996 · N58733 · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR WTAA960208Connector · water contamACV - FLAP DISAGREEMENT ON CLIMB-OUT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE CLEANED MOISTURE FROM CANNON PLUG ON OUTBOARD FLAP ACTUATOR AND RERACKED COMPUTER. OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X)Dec 2, 1996 · N120AM · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR C2XA96IA292Stringer · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE AFFECTED PORTION OF STRINGER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE STRINGER REPAIR WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS ENDec 2, 1996 · N47722 · Emb EMB120RT · Wing, Longeron/StringerSDR WTAA960207Engine · low oilSFO - LEFT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. CREW SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED LEFT ENGINE WITH FOUR QUARTS OIL. LEAK AND OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)Nov 27, 1996 · N271YV · Emb EMB120RT · Turbine Engine Oil SystemSDR GLBA96230Oil Press Ind · malfunctionedLAN - LEFT ENGINE OIL PRESSURE INDICATOR UNRELIABLE. MAINTENANCE CHECKED OIL QUANTITY, CONNECTIONS, INDICATORS. TEST FLIGHT NORMAL. (X)Nov 26, 1996 · N281UE · Emb EMB120RT · Engine Oil Pressure
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