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 CHQA201100477Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON FRAME 23. MAINTENANCE REPAIRED THE RIGHT-HAND FUSELAGE AT FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 2011-145-109359.Dec 12, 2011 · N375SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100501Frame · crackedDURING INSPECTION, THE COCKPIT LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FRAME 10. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Dec 10, 2011 · N375SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100497Repair · corrodedDURING INSPECTION, THE LEFT BEAM EXISTING REPAIR AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10.Dec 9, 2011 · N375SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100498Beam · corrodedDURING INSPECTION, THE CENTER FUSELAGE I FLOOR STRUCTURE HAT BEAM AT FRAME 23 STATION WAS FOUND CORRODED. MAINTENANCE REPLACED THE CENTER FUSELAGE I FLOOR STRUCTURE HAT BEAM AT FRAME 23. THE NEW PART WAS INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-Dec 9, 2011 · N375SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100499Beam · corrodedDURING INSPECTION, THE LEFT OUTBOARD BEAM FROM FRAME 48 TO FRAME 53 UNDER THE SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT OUTBOARD BEAM FROM FRAME 48 TO FRAME 53 AND INSTALLED WITH SOLD RIVETS IN ACCORDANCE WITH SRM 51-40-02.Dec 9, 2011 · N375SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100500Angle · crackedDURING INSPECTION, THE RIGHT WING BOX OMEGA BEAM ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE RIGHT WING BOX OMEGA BEAM ANGLE IN ACCORDANCE WITH SRM 53-23-02.Dec 9, 2011 · N375SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100476Module · malfunctionedCREW REPORTED THAT AFTER TAKEOFF, AT APPROXIMATELY 700FT AGL, THE CABIN ALTITUDE ON THE EICAS WENT TO DASHES. THE CREW DECIDED TO RETURN TO KDTW. DURING THE RETURN, AT APPROXIMATELY 300FT AGL, THE CABIN ALTITUDE RETURNED TO THE EICAS. THE AIRCRAFT LANDED WIDec 8, 2011 · N564RP · Emb EMB145LR · Cabin Pressure Control SystemSDR CHQA201100465Battery · dischargedDURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY AND THE NUMBER 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Dec 3, 2011 · N562RP · Emb EMB145LR · Emergency LightingSDR CHQA201100466Brake Sys · malfunctionedCREW REPORTED THAT ON LANDING, THE LEFT BRAKES, BOTH THE PILOTS AND CO-PILOTS, NEEDED TO BE PUSHED NEARLY ALL THE WAY DOWN FOR THE BRAKES TO BE EFFECTIVE. MAINTENANCE PERFORMED SEVERAL TAXI CHECKS, NOTING THAT THERE WAS NO DIFFERENCE BETWEEN THE RIGHT AND LEFDec 3, 2011 · N381SK · Emb EMB135KL · Landing Gear Brake SystemSDR ASOA11IA007Engine · failedDURING TAKEOFF, THE CREW HEARD A LOUD BOOM FOLLOWED BY THE LOSS OF TEMP INDICATION ON THE NR1 ENGINE. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE WITHOUT INCIDENT. ON INSPECTION NR 1 ENGINE TURBINE WAS FOUND TO BE DAMAGED. SUP: R & R THE NR ENGDec 2, 2011 · N11137 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR CHQA201100479Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE FUSELAGE SKIN RF II BETWEEN FRAME 76 AND 77 AND STRINGERS 16R AND 18R. MAINTENANCE REPAIRED THE DENT ON THE FUSELAGE SKIN RF II BETWEEN FRAMES 76 AND 77 AND STRINGERS 16R AND 18R IN ACCORDANCE WITH SRM 53-32-01. A HDec 1, 2011 · N376SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100480Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT LOWER BEAM. MAINTENANCE REPLACED THE CARGO DOOR CUTOUT LOWER BEAM AND INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Nov 30, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100482Beam · corrodedDURING INSPECTION, THE LEFT BEAM UNDER THE OUTBOARD SEAT TRACK NUMBER 5, BETWEEN FRAME 47 TO FRAME 53 WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE LEFT BEAM UNDER THE OUTBOARD SEAT TRACK NUMBER 5, BETWEEN FRAME 47 TO FRAME 53 AND INSTALLED WITH SOLID RINov 30, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100481Frame · crackedDURING INSPECTION, THE LEFT FRAME 10 WAS FOUND CRACKED INSIDE THE COCKPIT BELOW THE SIDE WINDOW. MAINTENANCE REPLACED THE LEFT FRAME 10 INSIDE THE COCKPIT BELOW THE SIDE WINDOW AND INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100484Angle · crackedDURING INSPECTION, MID WING BOX OMEGA BEAN ANGLES WERE FOUND TO BE CRACKED AT FRAME 50 (PN: 140-04214-607 AND 140-04214-609). MAINTENANCE REPLACED THE MID WING BOX OMEGA BEAM ANGLES IN ACCORDANCE WITH SRM 53-23-02.Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100462Shear Plate · corrodedDURING INSPECTION, CORROSION WAS FOUND ON CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L SHAPE. MAINTENANCE REPLACED THE CARGO DOOR SURROUND STRUCTURE FORWARD AND AFT L-SHAPE. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH ETD 2011-145-108Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100463Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON FRAME 23 UNDER SILL NUMBER 1. MAINTENANCE REPAIRED THE RIGHT-HAND FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 2011-145-108720.Nov 29, 2011 · N376SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100461Battery · dischargedDURING INSPECTION, THE EMERGENCY LIGHT STRIPS AT THE AFT OF THE CABIN AND THE LEFT OVERWING AND RIGHT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTNov 28, 2011 · N578RP · Emb EMB145LR · Emergency LightingSDR CHQA201100460Sensor · faultyCREW REPORTED THAT DURING FLIGHT THEY RECEIVED A BLEED 2 LOW TEMP MESSAGE ON THE EICAS. THE CREW DIVERTED TO KLGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED 2 OUTLET TEMPERATURE SENSOR. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NNov 27, 2011 · N269SK · Emb EMB145LR · Pneumatic Indicating SystemSDR CHQA201100458Light · inoperativeDURING INSPECTION, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REVAMPED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 24, 2011 · N257JQ · Emb EMB145LR · Emergency LightingSDR CHQA201100459Light · inoperativeDURING INSPECTION, THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 24, 2011 · N284SK · Emb EMB145LR · Emergency LightingSDR CHQA201100457Fitting · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FRAME 65 SHEAR FOOT AT THE CARGO DOOR SILL. MAINTENANCE REPAIRED THE FRAME 65 SHEAR CLIP FOOT IN ACCORDANCE WITH IC2010-145-10445 WITH NO FURTHER DEFECTS NOTED.Nov 21, 2011 · N570RP · Emb EMB145LR · Fuselage Main, FrameSDR CHQA201100456Fadec · malfunctionedCREW REPORTED THAT WHILE ON APPROACH, E2 N1 ROLLED BACK TO 38 PERCENT WHILE E1 N1 STAYED AT 68 PERCENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET FADECS AND PERFORMED ENGINE RUNS WITH NO FURTHER DEFECTS NOTED.Nov 18, 2011 · N562RP · Emb EMB145LR · Fuel Control/Turbine EnginesSDR CHQA201100474Frame · crackedDURING INSPECTION, THE LEFT FRAME JUST BELOW THE COCKPIT WINDOW WAS FOUND TO BE CRACKED. THE LEFT FRAME JUST BELOW THE COCKPIT WINDOW WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Nov 18, 2011 · N372SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100453Switch · faultyCREW REPORTED THAT THEY RECEIVED A BLEED 1 VALVE FAIL MESSAGE DURING FLIGHT. THEY FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE VALVE WOULD NOT REOPEN. THEY RETURNED KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OVERHEAD PUSHBUTTON SWITCH. OPENov 17, 2011 · N285SK · Emb EMB145LR · Pneumatic Distribution SystemSDR CHQA201100454Wire · brokenDURING INSPECTION, IT WAS REPORTED THAT THE NUMBER 2 EMERGENCY PATH LIGHTING STRIP HAD A BROKEN WIRE. MAINTENANCE REPLACED THE PASSENGER AISLE EMERGENCY LIGHT STRIP, OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 17, 2011 · N571RP · Emb EMB145LR · Light System WiringSDR CHQA201100471Frame · crackedDURING INSPECTION, A CRACK WAS FOUND ON FRAME 23 AT STRINGER 16R. MAINTENANCE REPAIRED FRAME 23 AT STRINGER 16R IN ACCORDANCE WITH ETD 2011-145-108247 AND SRM 53-00-04.Nov 17, 2011 · N372SK · Emb EMB135KL · Fuselage Main, FrameSDR CHQA201100472Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON AN EXISTING REPAIR AT FRAME 20 ON THE LEFT INBOARD FLOORBEAM. THE LEFT INBOARD FLOOR BEAK AT FRAME 20 WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10.Nov 17, 2011 · N372SK · Emb EMB135KL · Fuselage Main, Floor BeamSDR CHQA201100473Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FUSELAGE 1 FLOOR STRUCTURE MIDDLE BEAM. THE CENTER FUSELAGE 1 FLOOR STRUCTURE MIDDLE BEAM WAS REPLACED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.Nov 17, 2011 · N372SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100451Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE REAR ELECTRONIC DOOR CUT OUT BOTTOM FRAME. MAINTENANCE REPLACED THE REAR ELECTRONIC DOOR CUTOUT BOTTOM FRAME IN ACCORDANCE WITH SRM 51-40-02. THE FINAL CORRECTIVE ACTION IS BEING SUBMITTED AS A SUPPLEMENT TO THE Nov 17, 2011 · N372SK · Emb EMB135KL · Fuselage Main, StructureSDR CHQA201100450Screw · brokenTHE FIRST OFFICER REPORTED THAT THE LAVATORY DOOR WAS STUCK CLOSED WITH THE CAPTAIN INSIDE DURING FLIGHT. AN EMERGENCY WAS DECLARED WHEN A PASSENGER APPROACHED THE COCKPIT TO ALERT THE CO-PILOT OF THE CAPTAIN'S SITUATION. THE CAPTAIN FREED HIMSELF FROM THE LNov 16, 2011 · N564RP · Emb EMB145LR · LavatoriesSDR CHQA201100468Skin · canningDURING INSPECTION, OIL CANNING WAS FOUND ON THE FUSELAGE SKIN CENTER FUSELAGE I BETWEEN FRAME 19 AND FRAME 20 AND STRINGERS 1L AND 2L. MAINTENANCE REPAIRED THE CENTER FUSELAGE I SKIN BETWEEN FRAME19 AND FRAME 20 BETWEEN STRINGERS 1L AND 2L IN ACCORDANCE WITH Nov 16, 2011 · N372SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100469Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE LEFT FUSELAGE SKIN ON STRINGER 11L BETWEEN FRAME 23 AND FRAME 24. MAINTENANCE REPAIRED THE SKIN ON STRINGER 11L BETWEEN FRAME 23 AND FRAMES 24 IN ACCORDANCE WITH ETD 2011-145-108265.Nov 16, 2011 · N372SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100470Structure · 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 ERD 2011-145-108193.Nov 16, 2011 · N372SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100475Doubler · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE TOILET WASTE VALVE SKIN DOUBLER. MAINTENANCE REPLACED THE TOILET WASTE VALVE SKIN DOUBLER. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Nov 16, 2011 · N372SK · Emb EMB135KL · Fuselage Main, Plate/SkinSDR CHQA201100441Battery · dischargedCREW REPORTED THAT AFTER LANDING THE EMERGENCY LIGHTS CAME ON AND WOULD ONLY TURN OFF IN THE ARM AND ON SWITCH POSITIONS. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 15, 2011 · N293SK · Emb EMB145LR · Emergency LightingSDR CHQA201100440O-Ring · leakingCREW REPORTED THAT THEY RECEIVED A BLEED LEAK 1 MESSAGE ON THE EICAS. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE WENT AWAY. THE CREW DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE THE O-RINGS AT THE BLEED JOINTS IN THENov 14, 2011 · N292SK · Emb EMB145LR · Pneumatic Distribution SystemSDR C2XA11IA258Engine · malfunctionedDURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION WARNING HOWEVER NO VISUAL SMOKE WAS NOTED. THE AIRCRAFT DIVERTED TO ICT AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED ENGINE RUNS AND DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. TNov 12, 2011 · N11127 · Emb EMB145XR · Engine (Turbine/Turboprop)SDR CHQA201100439Beam · corrodedDURING INSPECTION, THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REPLACED THE CARGO DOOR CUT OUT SILL BEAM IN ACCORDANCE WITH SRM 51-20-03, 51-40-06, AND 51-40-02.Nov 11, 2011 · N296SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100437Battery · dischargedDURING INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY, OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 10, 2011 · N567RP · Emb EMB145LR · Emergency LightingSDR CHQA201100425Ballast · defectiveCREW REPORTED THAT ON DESCENT THERE WAS AN ELECTRICAL ODOR IN THE CABIN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LIGHTING BALLAST AT ROW 3 AND ROW 5. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Nov 8, 2011 · N377SK · Emb EMB135KL · Passenger Compartment LightingSDR CHQA201100442Nut · damagedDURING INSPECTION, THE RUDDER 2 PROTRACTOR ANCHOR NUT WAS FOUND TO BE MISSING. THE RUDDER 2 PROTRACTOR ANCHOR NUT WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-107755.Nov 8, 2011 · N297SK · Emb EMB135KL · Rudder StructureSDR CHQA201100443Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD BEAM BETWEEN FRAME 46 AND FRAME 53. MAINTENANCE REPLACED THE LEFT OUTBOARD BEAM BETWEEN FRAME 46 AND FRAME 53. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Nov 8, 2011 · N297SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100444Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE LOWER BEAM. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Nov 8, 2011 · N297SK · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA201100426Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 28. MAINTENANCE INSPECTED AND REMOVED THE CORROSION FROM THE FLOOR SILL AT FRAME 28 RIGHT. CORROSION WAS LESS THEN 30 PERCENT OF MATERIAL THICKNESS, THE REMAINING THICKNESS IS 0.041 INCHNov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100427Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02.Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100428Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02.Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100429Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 39. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 39 IN ACCORDANCE WITH SRM 51-40-02.Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100430Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02.Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA201100431Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02.Nov 7, 2011 · N562RP · Emb EMB145LR · Fuselage Miscellaneous Structure
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