N179CA

Service difficulty reports · 64

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N179CA' AND registry_match = 'registration'
  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 JIKA2021062901Hmu · failedWHILE CRUISING AT 10,000 FEET, WITHOUT WARNING THE NUMBER 2 ENGINE FAILED. FIRST OFFICER CALLED OUT "POWER LOSS" ON NUMBER 2, MEMORY ITEMS AND QRH WERE COMPLETED. ATC AND DISPATCH WAS ADVISED. KRIV WAS CHOSEN AS NEAREST SUITABLE AIRPORT, SINGLE ENGINE APPROACHJun 29, 2021 · N179CA · Emb EMB120 · Engine (Turbine/Turboprop)SDR COMA9910176Wire · failedTRIM FAIL WARNING DURING TAKEOFF. REPAIRED PROX SENSOR WIRE SPLICE AT ELEVATOR TRIM.Nov 18, 1999 · N179CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9910140Windshield · bird strikeBIRD STRIKE DURING TAKEOFF. C/W BIRD STRIKE INSPECTION, NO DAMAGE FOUND.Aug 24, 1999 · N179CA · Emb EMB120RT · Flight Compartment WindowsSDR COMA9910138Actuator · malfunctionedFLAP CONTROL FAULT. REPLACED THE LEFT HAND OUTBOARD FLAP ACTUATOR.Aug 19, 1999 · N179CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9910127Stringer · crackedWHILE PERFORMING A MAINTENANCE SERVICE CHECK, MECHANIC NOTICED SMALL FUEL LEAK ON BOTTOM SKIN OF LEFT WING JUST FORWARD OF AND OUTBOARD OF ACCESS PANEL 522EB. INTERNAL INVESTIGATION REVEALED A CRACK IN STRINGER 10A AT THE RIVET HOLE THAT WAS LEAKING FUEL, SEVAug 3, 1999 · N179CA · Emb EMB120RT · Wing, Longeron/StringerSDR COMA9910112Pcu · leakingRUDDER POWER CONTROL UNIT LEAKING HYDRAULIC FLUID. CHANGED RUDDER POWER CONTROL UNIT.Jul 1, 1999 · N179CA · Emb EMB120RT · Rudder Control SystemSDR COMA9910098Annunciator · malfunctionedFLAPS FAIL WARNING. REPLACED THE FLAP ANNUNCIATOR UNIT.Jun 22, 1999 · N179CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9910080T6 Warning · activatedABORTED TAKEOFF DUE TO T6 WARNING. DOWNLOADED DFDR, FOUND ALL PARAMETERS TO BE WITHIN LIMITS PER PRATT P WHITNEY MAINT MANUAL 02-10-00. NO ACTION REQUIRED.May 11, 1999 · N179CA · Emb EMB120RT · Engine EGT/TIT Indicating SystemSDR COMA9910059Sign · inoperativeEMERGENCY EXIT SIGN AT 5A IS INOPERABLE. REPLACED EXIT SIGN.Apr 10, 1999 · N179CA · Emb EMB120RT · Emergency LightingSDR COMA9910052Wire · shortedEMERGENCY LIGHTS CIRCUIT BREAKER TRIPS WHEN SYSTEM TESTED. REPAIRED SHORTED WIRING AT F/A LIGHT PANEL.Apr 4, 1999 · N179CA · Emb EMB120RT · Light System WiringSDR COMA9910040Selector · malfunctionFLAP CONTROL FAULT. REPLACED FLAP SELECTOR LEVER.Mar 6, 1999 · N179CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9910027Retract Mech · dirtyFLAP DISAGREEMENT WARNING ATER TAKEOFF. CLEANED DIRT FROM FLAP TRUCKS.Jan 31, 1999 · N179CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9910024Connector · looseDURING CLIMBOUT FROM MCO WITH GEAR SELECTED UP, RT GEAR RED LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE FIELD. REINSTALLED RT GEAR A AND B PROXIMITY SENSOR CONNECTOR.Jan 24, 1999 · N179CA · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9910020Bushing · out of positionWHILE PERFORMING LANDING GEAR FREE-FALL CHECK, THE LEFT MAIN LANDING GEAR WOULD NOT GO TO THE LOCKED POSITION WITHOUT EXCEEDING THE MAX PULL LIMITS. FURTHER INVESTIGATION REVEALED THE OUTBOARD BUSHING FOR THE MAIN DRAG AND LOCKING STRUT HINGE PIN TO HAVE MIGRJan 24, 1999 · N179CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9910004Hyd Fluid · contaminatedRIGHT HAND HYDRAULIC RESERVOIR LOW PRESSURE WARNING. REMOVED CONDENSATE WATER FROM RESERVOIR.Jan 4, 1999 · N179CA · Emb EMB120RT · Hydraulic System, MainSDR COMA9810168Wire · shortedEMERGENCY FLOOR LIGHT SYSTEM CIRCUIT BREAKER TRIPPED. WOULD NOT RESET. REPAIRED SHORTED WIRE NR W272-0009-24.Aug 5, 1998 · N179CA · Emb EMB120RT · Light System WiringSDR COMA9810069Auto Pilot · malfunctionedAUTOPILOT AND TRIM FAIL WARNING DURING TAKEOFF. DEFERRED AUTOPILOT SYSTEM. AIRCRAFT RETURNED TO SERVICE.Mar 17, 1998 · N179CA · Emb EMB120RT · Autopilot SystemSDR COMA9710425Flap Annunciator · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR UNIT.Oct 13, 1997 · N179CA · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9710326Valve · malfunctionLEFT HAND BLEED AIR OVERHEAT WARNING ON AFTER TAKEOFF. REPLACED THE LEFT HAND HIGH PRESSURE BLEED AIR SHUT OFF VALVE.Jul 7, 1997 · N179CA · Emb EMB120RT · Pneumatic Distribution SystemSDR COMA9710296Crossbeam · corrodedON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT CROSSBEAM WAS FOUND CORRODE. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710295Support · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710294Strap · corrodedON 2C TASK 164-01Z, THE CARGO COMPARTMENT AFT RT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710293Angle · corrodedON 2C TASK 152-01Z, THE AFT EMERGENCY EXIT CUTOUT LOWER ANGLE WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710292Strap · corrodedON 2C TASK 161-01Z, THE CARGO COMPARTMENT LT BUTT STRAP, AT CARGO DOOR OPENING, WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710291Crossbeam · corrodedON 2C TASK 151-01Z, THE CABIN FLOOR SUPPORT LT CROSSBEAM WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710290Crossbeam · corrodedON 2C TASK 152-01Z, THE CABIN FLOOR SUPPORT RT CROSSBEAM WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710289Strap · corrodedON 2C TASK 151-01Z, THE CABIN FLOOR SUPPORT LT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710288Strap · corrodedON 2C TASK 152-01Z, THE CABIN FLOOR SUPPORT RT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710287Strap · corrodedON 2C TASK 152-01Z, THE CABIN FLOOR SUPPORT RT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710286Support · corrodedON 2C INSPECTION, THE CABIN AFT RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES. THE SEAT TRACK WAS FOUND CORRODED AND REPLACED, AT WHICH TIME THE SUPPORTING SECTION WAS FOUND CORRODED. NEITHER IS COVERED BY A 2C TASK May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710285Strap · corrodedON 2C TASK 162-01Z, THE CARGO COMPARTMENT FLOOR SUPPORT FWD RT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710284Beam · corrodedON 2C TASK 5310-131-91I, THE CABIN FLOOR SUPPORT FWD CENTER OMEGA BEAM WAS FOUND CORRODED AND DAMAGED BY SCREW IMPROPERLY INSTALLED. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 2181-6, REV IR, 5-19-97.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710283Sill · corrodedON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT SILL WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710282Sill · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT SILL WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710281Strap · corrodedON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT BUTT STRAP WAS FOUND CORRODED AND REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710280Strap · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710279Strap · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710278Strap · corrodedON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FWD CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAPT 51 STANDARD PRACTICES, AND AERODESIGN REPORT NR 1671-1, REV A, 1-28-97.May 23, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710277Strap · corrodedON 2C TASK 161-01Z, THE CARGO COMPARTMENT FLOOR SUPPORT LT BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM STANDARD PRACTICES.May 20, 1997 · N179CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710242Light · brokenFLOOR PATH EMERGENCY LIGHT IS BROKEN AT THE GALLEY AREA. REPLACED THE LIGHT ASSY.May 6, 1997 · N179CA · Emb EMB120RT · Emergency LightingSDR COMA9710226Light · inoperativeRT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. DEFERRED RT FWD OVERWING EMERGENCY LIGHT PER MEL 33-50-01, CAT C.May 1, 1997 · N179CA · Emb EMB120RT · Emergency LightingSDR COMA9710185Fire Module · failedRT ENGINE FIRE WARNING LIGHT ON. REPLACED DEFECTIVE FIRE DETECTION CONTROL MODULE.Mar 24, 1997 · N179CA · Emb EMB120RT · Fire DetectionSDR COMA9710162Autofeather Sys · malfunctionedDURING APPROACH TO TLH, THE RIGHT HAND ENGINE AUTOFEATHER SYSTEM ACTIVATED. COULD NOT DUPLICATE DISCREPANCY. INSPECTION OF AUTOFEATHER SYSTEM FOUND NO DEFECTS.Feb 24, 1997 · N179CA · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA9610430Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETEIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RANGDec 26, 1996 · N179CA · Emb EMB120RT · Propeller AssemblySDR COMA9610429Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHIION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THE THICKNESSES RADec 26, 1996 · N179CA · Emb EMB120RT · Propeller AssemblySDR COMA9610428Bearing · wornPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. INSPECTION REVEALED UNEVEN WEAR ON THE BLADE BEARING INSERT. WEAR HAD OCCURED IN AN OVAL FASHION AND INSERT WALL THICKNESS HAD DETERIORATED FROM ORIGINAL .100\ WITH THICKNESS RANGING FDec 26, 1996 · N179CA · Emb EMB120RT · Propeller AssemblySDR COMA9610410Pitchlock Screw · failedPROPELLER ASSEMBLY WAS ORIGINALLY REMOVED FOR ENGINE RELATED MAINTENANCE. ONCE REMOVED, THE ACTUATOR PITCHLOCK SCREW FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 INCH. PITCHLOCK SCREW WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER.Dec 23, 1996 · N179CA · Emb EMB120RT · Propeller AssemblySDR COMA9610314Ahc 85 · failedCOPILOT'S AHRS FAILED. REPLACED THE AHC-85.Oct 28, 1996 · N179CA · Emb EMB120RT · Integrated Flight SystemSDR COMA9610312Atuator · malfunctionFLAP DISAGREEMENT WARNING DURING LANDING APPROACH. REPLACED THE RT FLAP OUTBD ACTUATOR.Oct 23, 1996 · N179CA · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610303Actuator · malfunctionedAFTER LANDING, WHEN FLAPS SELECTED UP, THE LT INBD FLAP INDICATED 15 DEGREES AND THE RT INBD FLAP INDICATED 45 DEGREES. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE RT INBD FLAP ACTUATOR FOR TROUBLESHOOTING.Oct 12, 1996 · N179CA · Emb EMB120RT · Trailing Edge Flap Actuator
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