Allison AE-3007A

Service difficulty reports · 3,309

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 engine_model_key = 'AE3007A'
  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 CHQA20120806266Frame · crackedDURING INSPECTION, THE COCKPIT LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE COCKPIT LEFT FRAME 10 WAS REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120806267Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE. THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010938-1 REVISION A.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20120806268Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE. THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010938-1 REVISION A.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Main, StructureSDR CHQA20120806269Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO SURROUND STRUCTURE LOWER BEAM. THE CARGO SURROUND STRUCTURE LOWER BEAM WAS REPLACED AND THE NEW PART WITH INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806270Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON CENTER FUSELAGE I FLOOR STRUCTURE LEFT OMEGA BEAM AT FRAME 20. THE CENTER FUSELAGE I FLOOR STRUCTURE LEFT OMEGA BEAM AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806271Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE MIDDLE BEAM. THE CENTER FUSELAGE I FLOOR STRUCTURE MIDDLE BEAM WAS REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806276Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE LEFT SILL NUMBER 1. THE CENTER FUSELAGE I FLOOR STRUCTURE LEFT SILL NUMBER 1 WAS REPLACED AND INSTALLED WITH A SOLID RIVET.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806277Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I LEFT GUSSET NUMBER 1. THE CENTER FUSELAGE FLOOR STRUCTURE GUSSET NUMBER 1 WAS REPLACED AND INSTALLED WITH SOLD RIVETS IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806278Support Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE MIDDLE ANGLE SUPPORT. THE CENTER FUSELAGE I FLOOR STRUCTURE MIDDLE ANGLE SUPPORT WAS REPLACED AND INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-03.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806279Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE PASSENGER DOOR FORWARD U-SHAPE. THE CENTER FUSELAGE I FLOOR STRUCTURE PASSENGER DOOR FORWARD U-SHAPE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806280Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE I FLOOR STRUCTURE GALLEY ANGLE. THE CENTER FUSELAGE I FLOOR STRUCTURE GALLEY ANGLE WAS REPLACED AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806281Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON CENTER FUSELAGE I FLOOR STRUCTURE FORWARD SERVICE DOOR SILL. THE CENTER FUSELAGE I FLOOR STRUCTURE FORWARD SERVICE DOOR SILL WAS REPLACED ON AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806282Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II FLOOR STRUCTURE LEFT SILL NUMBER 2. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806283Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II FLOOR STRUCTURE RIGHT SILL NUMBER 1. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806284Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE II FLOOR STRUCTURE RIGHT SILL NUMBER 2. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806285Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE LEFT SILL NUMBER 4. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806286Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE LEFT SILL NUMBER 6. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806287Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE RIGHT SILL NUMBER 5. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806288Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE RIGHT SILL NUMBER 3. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806289Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE RIGHT SILL NUMBER 4. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806290Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE RIGHT GUSSET NUMBER 4. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806291Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE III FLOOR STRUCTURE LEFT GUSSET NUMBER 5. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806292Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV FLOOR STRUCTURE LEFT SILL NUMBER 7. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806293Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV FLOOR STRUCTURE LEFT GUSSET TOILET. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806294Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV TOILET FLOOR STRUCTURE MID GUSSET. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806295Gusset · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV FLOOR STRUCTURE RIGHT GUSSET. THE GUSSET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120806296Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE IV FLOOR STRUCTURE LEFT TOILET SILL. THE SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.Aug 6, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120805239Skin · crackedCREW REPORTED, FOUND A NON-LINEAR CRACK IN THE PAINT. MAINTENANCE REPAIRED THE SKIN AT FRAME 16R TO FRAME 17R AT STRINGERS 14R TO 15R IN ACCORDANCE WITH SRM 53-21-01.Aug 5, 2012 · N270SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120804251Axle · chippedDURING INSPECTION, THE RIGHT OUTBOARD AXLE WAS FOUND TO HAVE CHIPPED CHROME. THE RIGHT OUTBOARD AXLE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010780.Aug 4, 2012 · N382SK · Emb EMB135KL · Main Landing Gear Strut/Axle/TruckSDR CHQA20120803230Engine · leakingCREW REPORTED A BURNING OIL SMELL IN THE COCKPIT DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. MAINTENANCE REPLACED THE NUMBER 1 ENGINE. OPERATIONAL CHECKS WERE GOOD WITH NO DEFECTS OR SMELLS NOTED.Aug 3, 2012 · N269SK · Emb EMB145LR · Engine (Turbine/Turboprop)SDR CHQA20120803231Battery · dischargedCREW REPORTED THAT UPON ARRIVING AT THE AIRCRAFT, THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPED AND THE FORWARD HALF OF THE EMERGENCY LIGHTS WERE ON AND THE BACK HALF WERE NOT. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WEAug 3, 2012 · N287SK · Emb EMB145LR · Emergency LightingSDR CHQA20120803264Floor Support · crackedDURING INSPECTION, THE RIGHT OMEGA BEAM ANGLE WAS FOUND CRACKED BETWEEN FRAME 47 AND FRAME 48. THE RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 3, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120803265Floor Support · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLE WAS FOUND CRACKED BETWEEN FRAME 47 AND FRAME 48. THE LEFT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 3, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120802252Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT DOOR FRAME. MAINTENANCE REPAIRED THE CORROSION ON THE PASSENGER DOOR FRAME IN ACCORDANCE WITH ETD 2012-145-010897.Aug 2, 2012 · N382SK · Emb EMB135KL · Passenger/Crew DoorsSDR CHQA20120802254Torque Box · crackedDURING INSPECTION, A CRACK WAS FOUND IN FASTENER HOLE AFT CENTER POSITION OF RIGHT WING INBOARD FLAP TORQUE BOX. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ETD 2012-145-010898.Aug 2, 2012 · N382SK · Emb EMB135KL · Trailing Edge FlapsSDR CHQA20120802255Torque Box · crackedDURING INSPECTION, A CRACK WAS FOUND IN FASTENER HOLE AFT INBOARD POSITION OF LEFT WING INBOARD FLAP TORQUE BOX. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ETD 2012-145-010898.Aug 2, 2012 · N382SK · Emb EMB135KL · Trailing Edge FlapsSDR CHQA20120801228Pressure Switch · faultyCREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYSTEM 1/2 Aug 1, 2012 · N276SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20120801229Pressure Switch · faultyCREW REPORTED THAT DURING CLIMBOUT, AT 10,000 FEET, THEY RECEIVED A RUDDER SYSTEMS 1/2 INOP MESSAGE, AUTO-PILOT FAIL, AND YAW DAMPER FAIL MESSAGES. THE CREW FURTHER REPORTED THAT THE AUTO-PILOT FAIL AND YAW DAMPER FAIL MESSAGES CLEARED WHILE THE RUDDER SYS 1/Aug 1, 2012 · N276SK · Emb EMB145LR · Rudder Control SystemSDR CHQA20120730235Skin · puncturedDURING INSPECTION, A PUNCTURE WAS DISCOVERED ON THE RUDDER II LEFT AND RIGHT SKIN. MAINTENANCE REPAIRED THE DAMAGED AREA OF THE SKIN AND RIBS IN ACCORDANCE WITH ETD 2012-145-010622.Jul 30, 2012 · N291SK · Emb EMB145LR · Rudder, Plate/SkinSDR CHQA20120730236Skin · puncturedDURING INSPECTION, A PUNCTURE WAS DISCOVERED ON THE RUDDER II LEFT AND RIGHT SKIN. MAINTENANCE REPAIRED THE DAMAGED AREA OF THE SKIN AND RIBS IN ACCORDANCE WITH ETD 2012-145-010622.Jul 30, 2012 · N291SK · Emb EMB145LR · Rudder, Plate/SkinSDR CHQA20120730253Shear Plate · crackedDURING INSPECTION, A CRACK IN THE SHEAR FOOT AT FRAME 73 AND STRINGERS 8R AND 9R WAS DISCOVERED. MAINTENANCE REPLACED THE SHEAR FOOT IN ACCORDANCE WITH SRM 53-31-04.Jul 30, 2012 · N382SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA20120729227Switch · inoperativeCREW REPORTED THAT THE EMERGENCY LIGHTS WERE TURNED ON AND WOULD NOT TURN OFF WHILE ON THE GROUND. MAINTENANCE REPLACED THE FLIGHT DECK EMERGENCY LIGHT SWITCH. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 29, 2012 · N287SK · Emb EMB145LR · Emergency LightingSDR CHQA20120728226Switch · faultyCREW REPORTED THAT ON DESCENT, WITH THE WINDSHIELD HEAT TURNED ON FOR ABOUT 10 MINUTES, A SLIGHT ELECTRICAL ODOR WAS PRESENT. CREW FURTHER REPORTED THAT BOTH WINDSHIELDS WERE NOT HEATING. WINDSHIELD HEAT WAS TURNED OFF AND THE ODOR DISSIPATED. MAINTENANCE RJul 28, 2012 · N258JQ · Emb EMB145LR · Windshield/Door Rain/Ice RemovalSDR CHQA20120727246Support Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS.Jul 27, 2012 · N572RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120727247Support Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AND AFT SUPPORT FITTINGS.Jul 27, 2012 · N572RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120726241Shear Plate · crackedDURING INSPECTION A CRACK WAS FOUND IN SHEAR FOOT FRAME 61 BETWEEN STRINGER 6R-7R. MAINTENANCE REPLACED THE SHEAR FOOT AT FRAME 61.Jul 26, 2012 · N572RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120726242Shear Plate · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 68 BETWEEN STRINGER 6L-7L. MAINTENANCE REPLACED THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND 7L.Jul 26, 2012 · N572RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120725232Bearing · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE AFT EDGE AT THE TOP OF THE UPPER LEFT BEARING HALF OF THE MAIN LANDING GEAR FITTING. THE CORROSION WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-010402 REVISION A.Jul 25, 2012 · N291SK · Emb EMB145LR · Wing, Landing Gear Attach FittingsSDR CHQA20120725240Door Frame · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE MAIN PASSENGER LOWER DOOR FRAME AT THE AFT STOP, SECOND FROM THE BOTTOM, WITH THE DOOR IN THE OPEN POSITION. MAINTENANCE REPAIRED THE DAMAGED AREA IN ACCORDANCE WITH ETD 2012-145-010458.Jul 25, 2012 · N572RP · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120725249Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT SILL BETWEEN FRAMES 61 AND 64. MAINTENANCE REMOVED THE CORROSION IN ACCORDANCE WITH SRM 51-10-03, THE REMAINING MATERIAL WAS FOUND TO BE WITHIN LIMITS IN ACCORDANCE WITH SRM 53-31-10.Jul 25, 2012 · N291SK · Emb EMB145LR · Fuselage Miscellaneous Structure
Back to Allison AE-3007A