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 ASOA20120830085Floor Support · corrodedDURING C-CHECK CENTER OMEGA BEAM FRAME 29 HAS CORROSION (LOCAL LEVEL 2) AT LOWER FLANGE AND SIDEWALL FOR CROSSBEAM ATTACHMENT POINT. MX PERFORMED REPAIR ON CENTER OMEGA BEAM FRAME 29 CROSSBEAM ATTACHMENT POINT IAW SRM 53-00-10. THE ACFT WAS APPROVED FOR RETUAug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Structure (General)SDR ASOA20120830086Floor Support · corrodedDURING C-CHECK CENTER OMEGA BEAM FRAME 32 HAS CORROSION AT BOTH LWR FLANGE AND SIDEWALL FOR CROSSBEAM ATTACHMENT POINT. MX PERFORMED REPAIR ON CENTER OMEGA BEAM FRAME 32-34 LWR FLANGE AND SIDEWALL FOR CROSSBEAM ATTACHMENT POINT IAW SRM 53-00-10. THE ACFT WASAug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120830087Floor Support · corrodedDURING C-CHECK CENTER OMEGA BEAM FRAME 38 HAS CORROSION (LOCAL LEVEL 2) AT CROSSBEAM ATTACHMENT POINT BOTH SIDEWALL AND LOWER FLANGE. MX PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAME 38 CROSSBEAM ATTACHMENT FLANGE IAW SRM 53-00-10. THE ACFT WAS APPROVED FORAug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120830088VFloor Support · corrodedDURING LT OMEGA BEAM HAS CORROSION (LOCAL LEVEL 2) AT CROSSBEAM ATTACHMENT POINT LOWER FLANGE FRAME 54. MX PERFORMED AND COMPLETED REPAIR OF LT OMEGA BEAM FRAME 54 IAW SRM 53-00-10, FIG 202, SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120830089Floor Support · corrodedDURING C-CHECK CENTER OMEGA BEAM AT FRAME 44 LOWER CROSSBEAM ATTACHMENT POINT HAS CORROSION (LOCAL LEVEL 2). MX PERFORMED AND COMPLETED REPAIR OF CENTER OMEGA BEAM AT FRAME 44 LOWER CROSSBEAM ATTACHMENT POINT IAW EC5310-01466. THE ACFT WAS APPROVED FOR RETURAug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Miscellaneous StructureSDR ASOA20120830090Skin · crackedDURING C-CHECK, CRACK AROUND RIVET FRAME 75, STRINGER 2L-3L VERIFIED WITH EDDY CURRENT. MX PERFORMED REPAIR BY INSTALLING FABRICATED REPAIR DOUBLER AND FILLER AT FRAME 75 BETWEEN STRINGER 2L-3L IAW EC5330-02313. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.Aug 30, 2012 · N16919 · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120830344Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 31 AT STRINGER 15R. FRAME 31 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 30, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120830348Angle · corrodedDURING INSPECTION, RAMP ANGLE CENTER OMEGA FRAME 20 WAS FOUND CORRODED. THE RAMP ANGLE CENTER OMEGA FRAME 20 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-20-03, AND CPM 51-22-04/03.Aug 30, 2012 · N565RP · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120829342Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 25 AT STRINGER 15R. FRAME 25 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120829343Frame · damagedDURING INSPECTION, A MISDRILLED HOLE WAS FOUND ON FRAME 30 AT STRINGER 15R. FRAME 30 AT STRINGER 15R WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.Aug 29, 2012 · N271SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120828310Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLES ON THE SERVICE DOOR THRESHOLD. MAINTENANCE REPLACED THE SERVICE DOOR SILL IN ACCORDANCE WITH SRM 53-20-10.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120828313Fitting · crackedDURING INSPECTION, THE SHEAR FOOT AT FRAME 68 BETWEEN STRINGERS 6L AND 7L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED AND INSTALLED IN ACCORDANCE WITH SRM 53-31-04.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120828315Skin Splice · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CIRCUMFERENTIAL SKIN SPLICE BETWEEN FRAMES 60 AND 61 AND STRINGERS 20R AND 21R. THE SKIN SPLICE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012305.Aug 28, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120827341Floor Support · corrodedDURING INSPECTION, THE CENTER OMEGA BEAM AROUND THE ANCHOR NUT WAS FOUND CORRODED BETWEEN FRAME 24 AND FRAME 25. THE CENTER OMEGA BEAM AROUND ANCHOR NUT BETWEEN FRAME 24 AND FRAME 25 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012075.Aug 27, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120826301Ballast · burnedCREW REPORTED A STRONG ELECTRICAL BURNING SMELL ABOVE ROW 12A. MAINTENANCE FOUND THE CEILING LIGHT BALLAST AT 12A TO BE BURNT. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 8/29/2012 BY REPLACING THE CEILING LIGHTING BALLAST AT ROW 12A. OPERATIONAL CHAug 26, 2012 · N281SK · Emb EMB145LR · Emergency LightingSDR CHQA20120825300Wire · damagedMAINTENANCE REPORTED THAT THE AFT FLOOR PROXIMITY STRIP WIRING WAS DAMAGED AT THE PROXIMITY STRIP. THE AFT FLOOR PROXIMITY STRIP WAS REPLACED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 25, 2012 · N294SK · Emb EMB145LR · Light System WiringSDR CHQA20120824339Structure · corrodedDURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053.Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120824340Structure · corrodedDURING INSPECTION, THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS FOUND TO BE CORRODED. THE FORWARD AND AFT LATERAL L-SHAPE ON THE CARGO DOOR SURROUND STRUCTURE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012053.Aug 24, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120823338Beam · corrodedDURING INSPECTION, THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS FOUND TO BE CORRODED. THE LOWER BEAM ON THE CARGO DOOR CUTOUT WAS REPLACED AND THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.Aug 23, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822298Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT LATERAL "L" AT THE CARGO DOOR THRESHOLD. FRAME 65 WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011847 AND SRM 51-40-02.Aug 22, 2012 · N258JQ · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120822303Arm · gougedDURING INSPECTION, THE AIRSTAIR DOOR RIGHT ROTATING ARM HAD GOUGES WHERE THE DOOR ACTUATOR ATTACHES. MAINTENANCE BLENDED THE DAMAGE IN ACCORDANCE WITH SRM 51-10-03 AND ETD 2012-145-011902 REVISION A.Aug 22, 2012 · N273SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120822321Skin · dentedDURING INSPECTION, A DENT WAS FOUND ON THE LEFT FUSELAGE SKIN, AFT OF PILOT WINDOW ON FRAME 13. THE DENT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012367A.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120822322Skin · damagedDURING INSPECTION, A BLEND WAS FOUND ON THE LEFT FUSELAGE SKIN BETWEEN FRAME 53 AND FRAME 54 ON STRINGER 13L. THE SKIN ON THE LEFT FUSELAGE BETWEEN FRAME 53 AND 54 ON STRINGER 13L WAS REPAIRED IN ACCORDANCE WITH SRM 53-24-01.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120822323Skin · damagedDURING INSPECTION, A BLEND WAS FOUND ON THE LEFT FUSELAGE SKIN BETWEEN FRAME 70 AND FRAME 71 ON STRINGER 19L. THE LEFT FUSELAGE SKIN BETWEEN FRAME 70 AND FRAME 71 ON STRINGER 19L WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-012145.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120822324Uplock Bracket · crackedDURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07.Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20120822325Uplock Bracket · crackedDURING INSPECTION, THE NOSE LANDING GEAR UPLOCK HOLDING BOX LEFT AND RIGHT WALL WAS FOUND CRACKED. THE NOSE LANDING GEAR UPLOCK HOLDING BOX WAS REPAIRED IN ACCORDANCE WITH SRM 53-11-08, 51-40-02, AND AMM 32-33-07.Aug 22, 2012 · N271SK · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR CHQA20120822332Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822333Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822334Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822335Angle · crackedDURING INSPECTION, THE LEFT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED AT FRAME 48. THE LEFT OMEGA BEAM ANGLES AT FRAME 48 WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822337Floor Support · corrodedDURING INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 HAD AND EXISTING REPAIR THAT WAS FOUND TO BE CORRODED. THE LEFT OMEGA BEAM AT FRAME 20 EXISTING REPAIR WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10.Aug 22, 2012 · N271SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120822346Skin · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LEFT WING UPPER SKIN AT THE GROUND SPOILER CENTER HINGE CUTOUT. THE LEFT WING UPPER SKIN AT THE GROUND SPOILER HINGE CUTOUT WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011887.Aug 22, 2012 · N271SK · Emb EMB145LR · Wing, Plate/SkinSDR CHQA20120820263Light · inoperativeDURING INSPECTION, THE THIRD EMERGENCY FLOOR PROXIMITY STRIP LIGHT WAS FOUND TO BE INOPERATIVE. THE ITEM WAS DEFERRED. THE DEFERRAL WAS CLEARED ON 8/23/2012 BY REPLACING THE THIRD EMERGENCY FLOOR LIGHT PROXIMITY STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FAug 20, 2012 · N576RP · Emb EMB145LR · Emergency LightingSDR CHQA20120817297Sill · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR SILL PLATE AT ALL 3 NUT PLATE LOCATIONS. THE SERVICE DOOR SILL WAS REPLACED IN ACCORDANCE WITH SRM 51-40-08.Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120817299Beam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE BAGGAGE DOOR CUTOUT RIB 15R FRAME 65 THROUGH FRAME 68. THE BEAM WAS REPLACED IN ACCORDANCE WITH SRM 51-10-03.Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120817302Support · crackedDURING INSPECTION, THE RIGHT OMEGA BEAM SUPPORT WAS FOUND TO BE CRACKED AT FRAME 47. MAINTENANCE REPLACED THE RIGHT OMEGA BEAM SUPPORT AT FRAME 47 IN ACCORDANCE WITH SRM 51-40-02.Aug 17, 2012 · N258JQ · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120816314Skin · dentedDURING HEAVY MAINTENANCE A PREVIOUSLY DAMAGED SECTION OF SKIN AFT OF THE PASSENGER DOOR NEAR FRAME 19-20 AND STRINGER 12L -13L WAS REPAIRED IN ACCORDANCE WITH ETD 2011-145-03683A CLOSING DMI 591816/3 AND 591816/1.Aug 16, 2012 · N266SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120813274Skin · damagedDURING HEAVY MAINTENANCE, A LIGHTNING STRIKE ON BOTTOM FUSELAGE SKIN BETWEEN FRAME 28 AND 29 ON STRINGER 20R WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-011016 REVISION B, DETAIL B.Aug 13, 2012 · N288SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120813275Skin · damagedDURING HEAVY MAINTENANCE, A LIGHTNING STRIKE ON BOTTOM FUSELAGE SKIN BETWEEN FRAME 12 AND 13 BETWEEN STRINGER 20R AND 21R. REPAIRED IN ACCORDANCE WITH SRM 53-10-01.Aug 13, 2012 · N288SK · Emb EMB145LR · Fuselage Main, Plate/SkinSDR CHQA20120812260Structure · corrodedDURING INSPECTION, CORROSION WAS FOUND BETWEEN THE MAIN PASSENGER DOOR NUT PLATES AND THE DOOR STRUCTURE. MAINTENANCE REPLACED THE LOWER CORNER PROFILE IN ACCORDANCE WITH SRM 51-40-02.Aug 12, 2012 · N286SK · Emb EMB145LR · Passenger/Crew DoorsSDR CHQA20120810245Light · inoperativeDURING INSPECTION, THE NUMBER 4 EMERGENCY LIGHT PROXIMITY STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT PROXIMITY STRIP. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.Aug 10, 2012 · N378SK · Emb EMB135KL · Emergency LightingSDR CHQA20120809244Tire · separatedCREW REPORTED THAT THE LEFT INBOARD TIRE SEPARATED ON TAKEOFF CAUSING DAMAGE TO THE LEFT FLAP. THE CREW DECLARED AN EMERGENCY ON LANDING AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. UPON FURTHER INSPECTION, A DENT WAS FOUND ON THE LEFT FUSELAGE BETWEEN FAug 9, 2012 · N577RP · Emb EMB145LR · Wheel/Ski/FloatSDR CHQA20120809256Rib · crackedDURING INSPECTION, A CRACK WAS DETECTED IN THE LEFT WING RIB INBOARD TORQUE BOX FORWARD CENTER FASTENER HOLE. MAINTENANCE REAMED THE HOLE SIZE TO 0.261 DIAMETERS IN ACCORDANCE WITH SRM 51-20-03, A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH NO CAug 9, 2012 · N286SK · Emb EMB145LR · Wing, Rib/BulkheadSDR CHQA20120809257Rib · crackedDURING INSPECTION, A CRACK WAS DETECTED IN THE RIGHT WING RIB INBOARD TORQUE BOX FORWARD CENTER FASTENER HOLE. MAINTENANCE REAMED THE HOLE SIZE TO 0.308" DIAMETERS IN ACCORDANCE WITH SRM 51-20-03, A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS PERFORMED WITH WIAug 9, 2012 · N286SK · Emb EMB145LR · Wing, Rib/BulkheadSDR CHQA20120809258Threshold · corrodedDURING INSPECTION, CORROSION WAS FOUND IN THE SERVICE DOOR THRESHOLD AT THE SCREW HOLES. THE SERVICE DOOR THRESHOLD WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-02.Aug 9, 2012 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120809259Shear Plate · crackedDURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 67 BETWEEN STRINGERS 6L AND 7L. MAINTENANCE FABRICATED A NEW SHEAR CLIP DOUBLER IN ACCORDANCE WITH SRM 53-31-04 AND INSTALLED THE NEW SHEAR CLIP AT FRAME 67 BETWEEN STRINGERS 6L AND 7L IN ACCORDANCEAug 9, 2012 · N286SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120809261Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND IN FRAME 22 AT THE LOWER SCREW HOLE FOR THE LINER. THE CORROSION WAS REMOVED IN PER SRM 51-10-03. THE REMAINING MATERIAL (0.068") IS ACCEPTED AS PERMANENT IN ACCORDANCE WITH ETD 2012-145-011370 REVISION A.Aug 9, 2012 · N286SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120809262Frame · corrodedDURING INSPECTION, A GOUGE WAS FOUND IN FRAME 60 BETWEEN STRINGERS 4L AND 5L. MAINTENANCE REPAIRED THE DAMAGED AREA IN ACCORDANCE WITH SRM 53-00-04, 51-20-03, 21-21-04, 51-21-05, AND 51-40-02.Aug 9, 2012 · N286SK · Emb EMB145LR · Fuselage Main, FrameSDR CHQA20120807272Floor Support · corrodedDURING INSPECTION, THE CENTER FUSELAGE IV FLOOR STRUCTURE RIGHT OMEGA BEAM WAS FOUND TO BE CRACKED AND CORRODED AROUND ANCHOR NUT BETWEEN FRAME 59 AND FRAME 60. THE RIGHT OMEGA BEAM ON THE CENTER FUSELAGE IV FLOOR STRUCTURE WAS REPLACED AND INSTALLED WITH A SAug 7, 2012 · N288SK · Emb EMB145LR · Fuselage Miscellaneous StructureSDR CHQA20120807273Spar Cap · damagedDURING INSPECTION, THE RIGHT-HAND WING FRONT SPAR LOWER CAP HOLES FOR LEADING EDGE ARE ELONGATED FROM YA-2723.00 TO YA-3815.00.THE RIGHT-HAND WING FROM SPAR LOWER CAP HOLE FOR LEADING EDGE FROM YA-2723.00 TO YA-3815.00 WERE REPAIRED IN ACCORDANCE WITH ETD 2012Aug 7, 2012 · N288SK · Emb EMB145LR · Wing Spar
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