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 CHQA201200023Computer · faultyCREW REPORTED THAT THE NAVIGATION 2 RADIO DASHED OUT DURING FLIGHT. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER NAVIGATION COMPUTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 22, 2012 · N377SK · Emb EMB135KL · Navigation SystemSDR CHQA201200024Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON FRAME 23 UNDER THE SERVICE DOOR AFT SILL BETWEEN STRINGER 15R AND 16R. FRAME 23 UNDER THE SERVICE DOOR AFT SILL WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-00933.Jan 20, 2012 · N374SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201200029Frame · crackedDURING INSPECTION, THE COCKPIT LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FRAME 10 WERE FOUND TO BE CRACKED. THE COCKPIT LEFT AND RIGHT FRAME 10 WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201200030Floor Support · crackedDURING INSPECTION, THE RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED OVER THE WING BOX. THE RIGHT OMEGA BEAM ANGLE WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200031Beam · corrodedDURING INSPECTION, THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM WAS FOUND TO BE CORRODED. THE CARGO DOOR SURROUND STRUCTURE LOWER BEAM WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA201200032Floor Support · corrodedDURING INSPECTION, THE RIGHT OUTBOARD OMEGA BEAM AT THE SERVICE DOOR WAS FOUND TO BE CORRODED. THE RIGHT OUTBOARD BEAM AT THE SERVICE DOOR WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-10.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200033Floor Support · corrodedDURING INSPECTION, THE LEFT INBOARD OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE LEFT INBOARD OMEGA BEAM AT FRAME 25 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200034Floor Support · corrodedDURING INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE CENTER OMEGA BEAM AT FRAME 25 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.Jan 19, 2012 · N374SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200020Beam · corrodedDURING INSPECTION, THE RIGHT INBOARD BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE RIGHT INBOARD BEAM AT FRAME 25 IN ACCORDANCE WITH SRM 53-00-10.Jan 16, 2012 · N378SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200013Unknown · malfunctionedCREW REPORTED THAT THEY RECEIVED A BRAKE OUTBOARD INOPERATIVE MESSAGE UPON LANDING. THE CREW NOTED THAT THE BRAKES FELT DIMINISHED DURING TAXI TO THE GATE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE BRAKING SYSTEMS WITH NO DEFECTS NOTED.Jan 13, 2012 · N372SK · Emb EMB135KL · Landing Gear Brake SystemSDR CHQA201200012Battery · dischargedDURING INSPECTION, THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 12, 2012 · N283SK · Emb EMB145LR · Emergency LightingSDR CHQA201200021Door Frame · corrodedDURING INSPECTION, THE CARGO DOOR SURROUND STRUCTURE AT FRAME 65 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE CARGO DOOR SURROUND STRUCTURE AT FRAME 65 IN ACCORDANCE WITH ETD 2012-145-000521 REV A.Jan 12, 2012 · N378SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA201200014Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. THE CARGO DOOR CUTOUT LOWER BEAM WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Jan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200015Frame · crackedDURING INSPECTION, THE LEFT AND RIGHT FORWARD FUSELAGE II, FRAME 10 WAS FOUND TO BE CRACKED AT THE INTERSECTION OF THE FRAME AND THE DIRECT VISION WINDOW LOWER BEAM. MAINTENANCE REPLACED THE LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FORWARD FUSELJan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201200016Seat Track · corrodedDURING INSPECTION, THE LEFT OUTBOARD SEAT TRACK BEAM BETWEEN FRAME 47 TO FRAME 52 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT OUTBOARD SEAT TRACK BEAM BETWEEN FRAME 47 AND FRAME 52. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITHJan 9, 2012 · N378SK · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201200017Beam · corrodedDURING INSPECTION, THE CENTER FUSELAGE 1 MIDDLE BEAM WAS FOUND CORRODED AT THE FRAME 20 LOCATION. MAINTENANCE REPLACED THE CENTER FUSELAGE 1 BEAM AT FRAME 20 AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Jan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200018Floor Support · corrodedDURING INSPECTION, THE RIGHT INBOARD OMEGA BEAM AT FRAME 27 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE RIGHT INBOARD BEAM AT FRAME 27 IN ACCORDANCE WITH SRM 53-00-10.Jan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200003Frame · crackedDURING C INSPECTION, A CRACK WAS FOUND ON FRAME 23. REPAIRED IN ACCORDANCE WITH SRM53-00-04 AND ETD 2012-145-000314 REVISION A.Jan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201200011Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE. REPAIRED IN ACCORDANCE WITH ETD 2012-145-000324 REVISION A. Jan 9, 2012 · N378SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA201200022Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES (PN: 140-042213-607 AND 140-04213-609) WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES IN ACCORDANCE WITH SRM 53-23-02.Jan 8, 2012 · N378SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200001Relay · faultyCREW REPORTED THAT THE LANDING GEAR LEVER WOULD NOT MOVE UP AFTER TAKEOFF. THE CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY K0352. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jan 2, 2012 · N270SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA201200009Frame · crackedDURING INSPECTION, THE COCKPIT LEFT FRAME 10, JUST BELOW THE SIDE WINDOW WAS FOUND CRACKED. THE COCKPIT LEFTD FRAME 10, JUST BELOW THE SIDE WINDOW, WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Dec 29, 2011 · N377SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100509Uplock · faultyCREW REPORTED THAT THEY RECEIVED A LANDING GEAR LEVER DISAGREE MESSAGE UPON GEAR RETRACTION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND CYCLED THE LANDING GEAR, AND THE RIGHT MAIN LANDING GEAR SHOWED IN TRANSIT UPON A SECOND GEAR RETRACTION. THE CREWDec 28, 2011 · N12530 · Emb EMB135LR · Landing Gear Retraction/Extension SystemSDR CHQA201100507Light · inoperativeDURING INSPECTION, THE EMERGENCY FLOOR TRACK LIGHTING BETWEEN SEATS 3 AND 5 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 SECTION OF THE FLOOR TRACK EMERGENCY LIGHTING. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 27, 2011 · N270SK · Emb EMB145LR · Emergency LightingSDR CHQA201100508Solenoid Valve · faultyCREW REPORTED THAT THEY FELT AN ABNORMAL VIBRATION AND NOISE FROM THE NOSE LANDING GEAR UPON GEAR RETRACTION. THE AIRCRAFT LANDED AT ITS INTENDED DESTINATION WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR DOORS TO NO BE FULLY CLOSING. THE NOSE LADec 27, 2011 · N12530 · Emb EMB135LR · Landing Gear Door Retract SectionSDR CHQA201100506Light · inoperativeDURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LAMP IN THE PASSENGER DOOR EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 26, 2011 · N379SK · Emb EMB135KL · Emergency LightingSDR CHQA201200002Skin · crackedDURING INSPECTION, THE LEFT WING LOWER SKIN, AT WING STATION YA-2360.17 WAS FOUND TO BE CRACKED. THE LEFT WING LOWER SKIN AT STATION YA-2360.17 WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-109980.Dec 23, 2011 · N377SK · Emb EMB135KL · Wing, Plate/SkinSDR CHQA201200007Floor Support · crackedDURING INSPECTION, THE CENTER FUSELAGE 3 RIGHT OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE CENTER FUSELAGE 3 RIGHT OMEGA BEAM ANGLE IN ACCORDANCE WITH SRM 53-23-02.Dec 23, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200008Beam · corrodedDURING INSPECTION, AN EXISTING REPAIR ON THE LEFT INBOARD BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT INBOARD BEAM AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10.Dec 23, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100496Wire · damagedCREW REPORTED THAT DURING CLIMB, AT 17,000 FEET, THEY RECEIVED A HIGH OIL PRESSURE INDICATION FOR THE NUMBER 2 ENGINE. AFTER LEVELING, THE CREW RAN THE QUICK REFERENCE HANDBOOK AND SET THE NUMBER 2 ENGINE TO IDLE THRUST. THE ENGINE OIL PRESSURE STOPPED INCREDec 22, 2011 · N563RP · Emb EMB145LR · Engine Oil System WiringSDR CHQA201200004Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REAR FUSELAGE 1 FLOOR STRUCTURE. THE CARGO DOOR LOWER BEAM WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200005Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT FRAME 23, JUST UNDER SILL NUMBER 1. THE RIGHT FRAME 23, JUST UNDER SILL NUMBER 1, WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-109968 AND SRM 53-00-04.Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201200006Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR SURROUND STRUCTURE FORWARD (PN: 145-25175-001) AND AFT (PN:145-25369-003) L SHAPE. THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L SHAPE WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-110089.Dec 22, 2011 · N377SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201200010Skin · dentedDURING INSPECTION, MAINTENANCE COMPLIED WITH DMI 750741/1, BY REPAIRING DENT IN THE LOWER WING RIGHT NEAR THE MAIN LANDING GEAR WHEEL WELL. THE REPAIR WAS PERFORMED IN ACCORDANCE WITH ETD 2011-145-109800.Dec 22, 2011 · N377SK · Emb EMB135KL · Wing, Plate/SkinSDR CHQA201100494Transducer · faultyCREW REPORTED THAT DURING LANDING ROLLOUT, THE BRAKES FAILED AT 80 KNOTS. THE CREW SLOWED THE AIRCRAFT USING THE EMERGENCY BRAKE. THE BRAKE SYSTEM BEGAN WORKING AS NORMAL WITHIN 10 KNOTS. THEY ALSO RECEIVED A RUDDER 1/2 INOP MSG ON THE EICAS. MAINTENANCE RDec 21, 2011 · N279SK · Emb EMB145LR · Landing Gear Brake SystemSDR CHQA201100495Battery · dischargedDURING INSPECTION, THE NUMBER 1 EMERGENCY LIGHT BATTERY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 21, 2011 · N291SK · Emb EMB145LR · Emergency LightingSDR CHQA201100492Battery · dischargedDURING INSPECTION, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT, CEILING AISLE EMERGENCY LIGHT 1 AND COCKPIT FLOOD LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 1 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTEDec 18, 2011 · N295SK · Emb EMB135KL · Emergency LightingSDR CHQA201100487Battery · dischargedDURING INSPECTION, THE RIGHT OVERWING EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 16, 2011 · N288SK · Emb EMB145LR · Emergency LightingSDR CHQA201100488Light · inoperativeDURING INSPECTION, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 16, 2011 · N288SK · Emb EMB145LR · Emergency LightingSDR CHQA201100490Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 4 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 16, 2011 · N294SK · Emb EMB145LR · Emergency LightingSDR CHQA201100491Battery · dischargedDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS CONNECTED TO THE NUMBER 2 EMERGENCY BATTERY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 16, 2011 · N294SK · Emb EMB145LR · Emergency LightingSDR CHQA201100504Skin · damagedDURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON FRAME 22 BETWEEN STRINGERS 19R-20R. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.Dec 16, 2011 · N375SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100505Skin · damagedDURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON STRINGER 20R BETWEEN FRAME 15-16. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.Dec 16, 2011 · N375SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100489Battery · dischargedDURING INSPECTION, THE EMERGENCY LIGHT POWER SUPPLY IN POSITION 4 FAILED THE FUNCTIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 15, 2011 · N563RP · Emb EMB145LR · Emergency LightingSDR CHQA201100485Controller · inoperativeCREW REPORTED THAT AFTER TAKEOFF THE AUTO PRESSURIZATION FAILED. THE CREW RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 14, 2011 · N289SK · Emb EMB145LR · Cabin Pressure ControllerSDR CHQA201100493Strut · lowCREW REPORTED THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON APPROACH. THE AIRCRAFT CONTINUED TO ITS DESTINATION, KCLE, AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND PERFORMED A WOW SIMULATION. OPERATIONAL CDec 14, 2011 · N291SK · Emb EMB145LR · Nose/Tail Landing Gear Strut/AxleSDR CHQA201100502Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM LOWER LIP AT FRAME 27. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT FRAME 27 IN ACCORDANCE WITH SRM 53-00-10.Dec 14, 2011 · N375SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100486Battery · dischargedDURING INSPECTION, THE EMERGENCY AISLE LIGHTS FROM THE ROW 8 TO ROW 12. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 14, 2011 · N562RP · Emb EMB145LR · Emergency LightingSDR CHQA201100478Battery · dischargedCREW REPORTED THAT THE EMERGENCY LIGHTS WERE ONLY PARTIALLY ILLUMINATED AND THAT THEY WOULD NOT EXTINGUISH WHEN CYCLING THE SWITCH. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 12, 2011 · N291SK · Emb EMB145LR · Emergency LightingSDR CHQA201100503Skin · corrodedDURING INSPECTION, A BLENDOUT ON THE LEFT SKIN BAY BORDERED BY FRAME 19-20 AND BETWEEN STRINGERS 14L-15L WAS FOUND CORRODED. MAINTENANCE REPAIRED THE BLENDOUT ON THE LEFT SKIN BETWEEN FRAME 19-20 AND STRINGERS 14L-15L IN ACCORDANCE WITH SRM 53-21-01.Dec 12, 2011 · N375SK · Emb EMB135KL · Fuselage Main, Plate/Skin
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