Allison AE-3007A

Service difficulty reports · 3,309

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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 CHQA201100311Light · inoperativeDURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 7, 2011 · N381SK · Emb EMB135KL · Emergency LightingSDR CHQA201100319Seat Track · corrodedDURING INSPECTION, THE LEFT OUTBOARD NUMBER 1 SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT OUTBOARD NUMBER 1 SEAT TRACK IN ACCORDANCE WITH AMM 53-01-06.Aug 7, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100309Battery · inoperativeDURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 6, 2011 · N296SK · Emb EMB145LR · Emergency LightingSDR CHQA201100310Relay · failedCREW REPORTED THAT DURING FLIGHT RECEIVED A COOLING PACK 2 VALVE CLOSED MESSAGE. COOLING PACK 1 WAS DEFERRED THE PREVIOUS DAY. AS A RESULT THE AIRCRAFT LOST PRESSURIZATION. THE CREW ALSO REPORTED, RECEIVED WING ANTI-ICE 1 AND WING ANTI-ICE 2 VALVE FAIL MESSAug 6, 2011 · N562RP · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA201100308Battery · dischargedDURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 5, 2011 · N566RP · Emb EMB145LR · Emergency LightingSDR CHQA201100307Rod · detachedCREW REPORTED THAT DURING FLIGHT THE LAVATORY DOOR WAS STUCK CLOSED WITH A PASSENGER INSIDE THE LAVATORY. THE CREW DIVERTED TO KSDF AND LANDED WITHOUT INCIDENT. MAINTENANCE FREED THE PASSENGER. FOUND THE LOWER LOCKING ROD ON THE LAVATORY DOOR TO BE DETACHEDAug 4, 2011 · N286SK · Emb EMB145LR · LavatoriesSDR CHQA201100318Angle · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RAMP ANGLE BETWEEN FRAME 19 AND FRAME 20. MAINTENANCE REPLACED THE RAMP ANGLE AND THE SUPPORT (PN: 145-22459-003) BETWEEN FRAME 19 AND FRAME 20 IN ACCORDANCE WITH SRM 51-40-02.Aug 3, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100321Crossbeam · corrodedDURING INSPECTION, THE CROSS BEAM AT FRAME 31 BETWEEN FLOORBEAM 0.0 AND FLOORBEAM -479.0 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CROSS BEAM AT FRAME 31 BETWEEN FLOORBEAM 0.0 AND FLOORBEAM -479.0 IN ACCORDANCE WITH SRM 51-20-03.Aug 3, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100315Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK FROM FRAME 36 TO FRAME 46 IN THE RIGHT CENTER AISLE. MAINTENANCE REPLACED THE RIGHT CENTER AISLE SEAT TRACK IN ACCORDANCE WITH EMB145 AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100316Floor Support · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE DIGITAL ON THE FLOORBEAM 479.0 BETWEEN FRAME 36 AND FRAME 39. MAINTENANCE REPLACED THE FLOORBEAM DIGITAL 479.0 BETWEEN FRAME 36 AND FRAME 39 IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100317Seat Track · corrodedDURING INSPECTION, CORROSION AND SCORING WAS FOUND ON THE LEFT FLOORBEAM SEAT TRACK FROM FRAME 47 TO FRAME 52. MAINTENANCE REPLACED THE LEFT FLOORBEAM SEAT TRACK BETWEEN FRAME 47 AND FRAME 52 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100320Floor Support · scoredDURING INSPECTION, THE LEFT OMEGA BEAM AT FRAME 31 WAS FOUND TO BE SCORED. MAINTENANCE BLENDED THE SCORES ON THE LEFT OMEGA BEAM AT FRAME 31 IN ACCORDANCE WITH SRM 51-10-03. FRAME 31 WAS DAMAGED DURING THE REPAIRS AT STRINGERS 15L AND 16L. MAINTENANCE REPAIAug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100322Seat Track · corrodedDURING INSPECTION, THE LEFT LATERAL WALL SEAT TRACK NUMBER 5 FROM FRAME 47 TO FRAME 53 HAS BEEN FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT LATERAL WALL SEAT TRACK NUMBER 5 FROM FRAME 47 TO FRAME 53 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100323Seat Track · corrodedDURING INSPECTION, THE RIGHT LATERAL WALL SEAT TRACK NUMBER 3 FROM FRAME 36 TO FRAME 47 HAS BEEN FOUND TO BE CORRODED. MAINTENANCE REPLACED THE RIGHT LATERAL WALL SEAT TRACK NUMBER 3 BETWEEN FRAME 36 AND FRAME 47 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100324Seat Track · corrodedDURING INSPECTION, THE RIGHT LATERAL WALL SEAT TRACK NUMBER 4 FROM FRAME 47 TO FRAME 53 HAS BEEN FOUND TO BE CORRODED. MAINTENANCE REPLACED THE RIGHT LATERAL SEAT TRACK NUMBER 4 BETWEEN FRAME 47 AND FRAME 53 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100325Frame · crackedDURING INSPECTION, CHANNEL FRAME 10 WAS FOUND TO BE CRACKED AT THE COCKPIT RIGHT DIRECT-VISION WINDOW CUTOUT. MAINTENANCE REPLACED CHANNEL FRAME 10, RIGHT SIDE IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100326Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FLOORBEAM 0.0 FRAME 23 TO FRAME 29. MAINTENANCE REPLACED THE FLOORBEAM FROM FRAME 23 TO FRAME 29 IN ACCORDANCE WITH SRM 51-40-00.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Main, Floor BeamSDR CHQA201100327Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SEAT TRACK FROM FRAME 46 TO FRAME 52 IN THE CENTER AISLE. MAINTENANCE REPLACED THE RIGHT CENTER AISLE SEAT TRACK FROM FRAME 46 TO FRAME 52 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100329Tee Fitting · corrodedDURING INSPECTION, THE "T" ANGLE ON THE FORWARD SIDE OF THE CARGO DOOR RAMP WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CORRODED "T" ANGLE ON THE FORWARD SIDE OF THE CARGO DOOR RAMP IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA201100330Tee Fitting · corrodedDURING INSPECTION, THE "T" ANGLE ON THE AFT SIDE OF THE CARGO DOOR RAMP WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE "T" ANGLE ON THE AFT SIDE OF THE CARGO DOOR RAMP IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Cargo/Baggage DoorsSDR CHQA201100331Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR FOOT ON THE FORWARD SIDE OF THE CARGO DOOR RAMP BEHIND THE "T" ANGLE AT FRAME 65. MAINTENANCE CUT THE DAMAGED SECTION OF SHEAR FOOT AND INSTALLED NEW SEGMENT IN ACCORDANCE WITH ETD 2011-145-102968. PART INFAug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100332Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LOWER SERVICE DOOR THRESHOLD. MAINTENANCE REPLACED THE LOWER SERVICE DOOR THRESHOLD IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100333Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 20 AROUND THE CARBON FIBER PLATE. MAINTENANCE REPAIRED THE LEFT FLOOR SILL AROUND THE CARBON FIBER ANGLE IN ACCORDANCE WITH SRM 53-00-01.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100334Support Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT SIDEWALL SEAT TRACK LATERAL SUPPORT BRACKET AT FRAME 50. MAINTENANCE REPLACED THE RIGHT SIDEWALL SEAT TRACK LATERAL SUPPORT BRACKET AT FRAME 50 IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100335Seat Track · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT LATERAL WALL SEAT TRACK NUMBER 4 FROM FRAME 36 TO FRAME 47. MAINTENANCE REPLACED THE LEFT LATERAL WALL SEAT TRACK NUMBER 4 FROM FRAME 36 TO FRAME 47 IN ACCORDANCE WITH AMM 53-01-06.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100336Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON FRAME 10 AT THE COCKPIT LEFT DIRECT-VISION WINDOW CUTOUT. MAINTENANCE REPLACED THE LEFT FRAME 10 SECTION AT THE COCKPIT LEFT DIRECT-VISION WINDOW CUTOUT IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100337Support Bracket · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE RIGHT SIDEWALL SEAT TRACK LATERAL SUPPORT BRACKET FROM FRAME 42 TO FRAME 47. MAINTENANCE REPLACED THE RIGHT SIDEWALL SEAT TRACK LATERAL SUPPORT BRACKET FROM FRAME 42 TO FRAME 47 IN ACCORDANCE WITH SRM 51-40-02.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage, Seat/Cargo Attach FittingsSDR CHQA201100338Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM DIGITAL UNDER THE CO-PILOT'S OUTBOARD SEAT RAIL. MAINTENANCE REPLACED THE FLOOR BEAM DIGITAL UNDER THE CO-PILOT'S SEAT RAIL IN ACCORDANCE WITH SRM 51-40-08.Aug 2, 2011 · N270SK · Emb EMB145LR · Fuselage Main, Floor BeamSDR CHQA201100304Light · inoperativeDURING INSPECTION, THE EMERGENCY LIGHT PROXIMITY STRIP LOCATED IN FRONT OF THE LAVATORY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT PROXIMITY STRIP IN FRONT OF THE LAVATORY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTEDAug 1, 2011 · N286SK · Emb EMB145LR · Emergency LightingSDR CHQA201100303Transceiver · defectiveCREW REPORTED THAT THE WEATHER RADAR WAS NOT DEPICTING THE WEATHER AS SEEN VISUALLY OUTSIDE THE AIRCRAFT. THE CREW TRIED USING BOTH AUTOMATIC AND MANUAL GAIN MODES, BUT RADAR REMAINED THE SAME. THE CREW DIVERTED TO KCMH AND THE AIRCRAFT LANDED WITHOUT INCIDEJul 29, 2011 · N562RP · Emb EMB145LR · Weather Radar SystemSDR CHQA201100328Hinge · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE HINGE COVER FOR THE PASSENGER DOOR ROTATION ARM. MAINTENANCE REPLACED THE HINGE FOR THE PASSENGER DOOR ROTATION ARM IN ACCORDANCE WITH SRM 51-40-02.Jul 29, 2011 · N270SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA201100302Battery · dischargedDURING INSPECTION, THE EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER FOUR EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 28, 2011 · N285SK · Emb EMB145LR · Emergency LightingSDR CHQA201100301Battery · dischargedDURING INSPECTION, THE AIRSTAIR CEILING AND COCKPIT STEP EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER ONE EMERGENCY BATTERY, LOCATED IN THE FORWARD CLOSET. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Jul 26, 2011 · N569RP · Emb EMB145LR · Emergency LightingSDR CHQA201100288Proximity Switch · intermittentCREW REPORTED THAT DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT WHEN THE GEAR WAS SELECTED UP. RECEIVED A "LG/LEVER DISAGREE" MESSAGE ON THE EICAS AND THE THREE GEAR INDICATION BOXES WERE RED. WHEN THE GEAR WAS SELECTED DOWN, ALL GEAR INDICATIONS SHOWED Jul 25, 2011 · N270SK · Emb EMB145LR · Landing Gear Position and WarningSDR CHQA201100289Unknown · odorCREW REPORTED THAT DURING DESCENT, AT FL200, AN ELECTRICAL SMOKE ODOR ENTERED THE COCKPIT AND CABIN. THE CREW DECLARED AN EMERGENCY. AFTER APPROXIMATELY TEN MINUTES THE SMELL DISSIPATED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS FOLLOWED BY EMERGENCY PERJul 25, 2011 · N565RP · Emb EMB145LR · Air Distribution SystemSDR CHQA201100290Flex Coupling · tornCREW REPORTED THAT DURING FLIGHT THE NUMBER 2 COOLING PACK WAS MAKING A LOUD RUSHING AIR NOISE. THEY ALSO REPORTED A SLIGHT BURNING SMELL FROM THE NUMBER 2 COOLING PACK. MAINTENANCE DEFERRED THE NUMBER 2 COOLING PACK. THE DEFERRAL WAS CLEARED LATER THAT DAYJul 25, 2011 · N575RP · Emb EMB145LR · Cabin Cooling SystemSDR CHQA201100291Trim System · malfunctionedCREW REPORTED THAT DURING CLIMB, AT APPROXIMATELY 3,000 FEET, THE MAIN PITCH TRIM WAS INOPERATIVE. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND RETURNED TO KMKE. THE CREW ALSO REPORTED THAT THE BACK-UP PITCH TRIM WORKED AS NORMAL. THE AIRCRAFT LANDED Jul 25, 2011 · N12530 · Emb EMB135LR · Stabilizer Control SystemSDR CHQA201100305Angle · corrodedDURING INSPECTION, THE CARGO DOOR CUT-OUT FORWARD LATERAL L-SHAPE WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE CARGO DOOR CUTOUT FORWARD LATERAL L-SHAPE IN ACCORDANCE WITH ETD2011-145-102611 REVISION A.Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100306Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR LOWER CUTOUT BEAM IN ACCORDANCE WITH SRM 51-40-02.Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100300Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE CHANNEL OF THE CARGO FRAME AT FRAME 66 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE CHANNEL CARGO FRAME AT FRAME 66 BETWEEN STRINGER 17L AND 18L IN ACCORDANCE WITH ETD 2011-145-102616.Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100299Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPAIRED THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 17L AND 18L IN ACCORDANCE WITH ETD 2011-145-102599 REVISION A.Jul 25, 2011 · N290SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100286Carbon Seal · leakingCREW REPORTED THAT DURING TAKEOFF THERE WAS SMOKE IN THE CABIN AND COCKPIT. THE CREW ABORTED TAKE-OFF AND REPORTED THAT THEY RECEIVED NO FIRE INDICATIONS AND ALL ENGINE INDICATIONS WERE GOOD. AS SOON AS THE TAKEOFF WAS ABORTED THE SMOKE BEGAN TO CLEAR. MAINJul 24, 2011 · N276SK · Emb EMB145LR · Turbine Engine Oil SystemSDR CHQA201100287Proximity Switch · out of adjustCREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR LEVER WOULD NOT MOVE UP. AT 400 FEET AGL THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ALONG WITH IC WOW 1/2 INOP MESSAGE. ALL OTHER INDICATION APPEARED NORMAL. THE CREW RETURNED TO KSDF AND LANDEJul 24, 2011 · N379SK · Emb EMB135KL · Landing Gear Position and WarningSDR CHQA201100292Duct · disconnectedCREW REPORTED, RECEIVED AN AILERON MIS-TRIM MESSAGE FOLLOWED BY AN AUTO-PILOT FAIL. THE CREW REPORTED THAT THE AILERONS WERE BINDING AND THEY HAD TO BE FORCED FREE. THE AIRCRAFT LANDED IN KDCA WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO KCMH FOR FURTHER TJul 23, 2011 · N258JQ · Emb EMB145LR · Air Distribution SystemSDR CHQA201100282Solenoid Valve · inoperativeCREW REPORTED THAT DURING FLIGHT THERE WAS A LOUD THUMPING NOISE FOLLOWED BY A RUSHING AIR SOUND AND VIBRATION UNDER THE COCKPIT FLOOR BOARDS. THERE WERE NO GEAR INDICATIONS. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS MET BY MAINTENANCE PERSONNEL. MAINTENJul 22, 2011 · N375SK · Emb EMB135KL · Landing Gear Door ActuatorSDR CHQA201100285Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUT-OUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR CUT-OUT LOWER BEAM IN ACCORDANCE WITH SRM 51-40-02.Jul 18, 2011 · N275SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100275Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE CARGO FRAME AT FR. 66 AT STRINGER 16L. MAINTENANCE REPAIRED THE CARGO FRAME 66 AT STRINGER 16L IN ACCORDANCE WITH ETD 2011-145-102244.Jul 15, 2011 · N275SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100283Fitting · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE MOLDING UNDER THE LEFT ELEVATOR ACCESS PANEL 335HB. MAINTENANCE REPLACED THE MOLDING UNDER THE LEFT ELEVATOR ACCESS PANEL 335HB IN ACCORDANCE WITH SRM 51-40-02.Jul 13, 2011 · N275SK · Emb EMB145LR · Elevator Miscellaneous StructureSDR CHQA201100284Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT AND RIGHT FRAME 10 UNDER THE SIDE COCKPIT WINDOW. THE LEFT (PN:145-02-409-001) AND RIGHT (PN: 145-02-409-001) FRAME 10 UNDER THE SIDE COCKPIT WINDOW WERE REPLACED IN ACCORDANCE WITH SRM 51-40-02.Jul 13, 2011 · N275SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100274Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE AFT AND FORWARD L-SHAPE SHEAR CLIP. MAINTENANCE REPAIRED THE CARGO DOOR FORWARD AND AFT :-SHAPE SHEAR CLIPS IN ACCORDANCE WITH ETD 2011-145-10245.Jul 13, 2011 · N275SK · Emb EMB145LR · Fuselage Miscellaneous Structure
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