Boeing 757-2Q8
Service difficulty reports · 2,798
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 aircraft_model_key = '7572Q8' 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.
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 aircraft_model_key = '7572Q8' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2017031802756Skin · damagedFOUND A DENT & GOUGE APPROXIMATELY 45 INCHES AFT OF THE E & E DOOR. ACCOMPLISHED A PERMANENT REPAIR AT BS 520 BETWEEN STRINGERS 27 & 28L IAW ERA 544898-14, REV A, SECTION III.SDR DALA2016031101844Frame · gougedBS 1280, FRAME GOUGED AT S-10R TO S-15R. REPAIRED BY ER/A514345-14, REV B. ERA 514345-14 UPDATED TO REV C 12 MONTH DTA TIME LIMIT IS REMOVED. LOGPAGES 1034697 AND 1863874 WILL TRACK REMAINING TIME LIMITS. CLOSED LOG AND REMOVED MONITOR INSPECTION.SDR FOTR20160229012Web · corrodedMAIN CABIN RT SIDE FLOOR CREASE WEB FUSELAGE BS 1620 TO 1640, RBL 62 HAS CORROSION ON LOWER SURFACE.SDR FOTR20160229011Seat Track · corrodedMAIN CABIN SEAT TRACK FUSELAGE BS 1630-1640, LBL 45.5 UPPER SURFACE HAS AREAS OF CORROSION.SDR FOTR20160229010Floorbeam · corrodedMAIN CABIN FUSELAGE BS 1320 FLOORBEAM HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE BETWEEN LBL 45.5 AND RBL 62.SDR FOTR20160229009Floorbeam · corrodedMAIN CABIN LT SIDE FUSELAGE BS 720, FLOORBEAM HAS AREAS OF CORROSION ON UPPER SUFACE AT LBL.62.SDR FOTR20160229008Floorbeam · corrodedMAIN CABIN FLOORBEAM FUSELAGE BS 1681, LBL 13 TO LBL 35, UPPER SURFACE IS CORRODED.SDR FOTR20160229007Floorbeam · corrodedMAIN CABIN FLOORBEAM AT FS 1681 IS CORRODED ON UPPER SURFACE, RBL 6.SDR FOTR20160229006Seat Track · corrodedMAIN CABIN RBL 24.75 SEAT TRACK IS CORRODED AT FUSELAGE BS 1280.SDR FOTR20160229005Floorbeam · corrodedMAIN CABIN FUSELAGE BS 365 FLOORBEAM HAS AREAS OF CORROSION AROUND CLIP NUTS ON UPPER SURFACE RBL 3 TO RBL 62.SDR FOTR20160229004Seat Track · corrodedMAIN CABIN BETWEEN FUSELAGE BS 1630-1640, SEAT TRACK HAS AREAS OF CORROSION RBL 45.5.SDR FOTR20160229003Floorbeam · corrodedMAIN CABIN FUSELAGE BS 1640 FLOORBEAM HAS AREAS OF CORROSION ON UPPER SURFACE BETWEEN LBL 62 AND RBL 62.SDR FOTR20160229002Frame · crackedMAIN CABIN RT BS 760 FRAME IS CRACKED BETWEEN STRINGERS 8 AND 9R.SDR FOTR20160229001Frame Splice · corrodedFRAME SPLICE AT BS 1300, STRINGER 25R FOUND CORRODED.SDR FOTR20160223002Skin · corrodedLOWER FUSELAGE SKIN HAS CORROSION AROUND FWD LAV PAN BS 430 BETWEEN STRINGER 26 TO 30L.SDR DALA2016021701147Skin · damagedDURING WALKAROUND, FOUND RT ENGINE LOWER BOTTOM, BEHIND L/E OF COWLING EXPOSED FIBERGLASS. DAMAGE IS OUT OF LIMITS IAW SRM 54-11-01, P102. REMOVED RT INLET COWL, INSTALLED NOSE INLET COWL RT ENGINE IAW MM 71-11.SDR IXXA20160217003Battery · dischargedLEFT FLASHLIGHT ON FLIGHT DECK BACK WALL, INOPERATIVE. CAUSAL FACTOR WAS ATTRIBUTED TO BATTERIES. R & R BATTERIES. OPERATIONAL CHECKED SATISFACTORY. ACFT RELEASED TO SERVICE.SDR FOTR20160206006Seat Track · gougedMAIN CABIN RBL 24.75 SEAT TRACK HAS GOUGES AT BS 1446.SDR FOTR20160206005Seat Track · gougedMAIN CABIN RBL 45.5 UPPER SURFACE HAS SEVERAL GOUGES IN SEAT TRACK BETWEEN BS 1080 TO 1180.SDR FOTR20160206003Frame · gougedMAIN CABIN LT SIDE BS 1240, FRAME IS GOUGED BETWEEN STR 8L AND 9L.SDR FOTR20160206002Floorbeam · corrodedMAIN CABIN BS 1640 FLOORBEAM UPPER SURFACE HAS CORROSION LBL 62 TO RBL 62.SDR FOTR201602060006Floorbeam · corrodedMAIN CABIN BS 1640, RBL 55, WL 208 FLOORBEAM IS CORRODED.SDR FOTR201602060005Floorbeam · corrodedUPPER CHORD AT BS 1681 FROM LBL 58 TO RBL 58 HAS CORROSION.SDR FOTR201602060004Frame · gougedMAIN CABIN FRAME BS 1280, LT HAS GOUGES.SDR FOTR201602060003Shear Web · corrodedMAIN CABIN AFT SHEAR WEB UPPER SURFACE HAS AREAS OF CORROSION BS 1681-1720, RBLL 62, LBL 62.SDR FOTR201602060002Floorbeam · corrodedFLOORBEAM AT BS 377.7, LBL 4 IS CORRODED.SDR DALA2016020800970Bottle · low pressureL2 DOOR SLIDE BOTTLE PRESSURE IS IN THE RED NO GO AREA. REPLACED L2 DOOR SLIDE IAW WC 7608834.SDR DALA2016020400995Light · no testDURING 3L DOOR SLIDE DEPLOYMENT TEST, EMERGENCY LIGHTS ON SLIDE DID NOT ILLUMINATE. ALL OTHER PARAMETERS OK. REPLACED L3 DOOR SLIDE IAW ADMS 2566-92-01-3L DOOR SLIDE INSTALLATION OK.SDR FOTR20160107001Door Frame · puncturedFWD ELECTRICAL EQUIPMENT BAY DOOR CUTOUT, FWD FRAME BS 231, BL-0 IS PUNCTURED.SDR DALA2016010700070Structure · crackedNDT PREFORMED, CRACKED FOUND ON LOWER RIVET OF PREVIOUS REPAIR-AFT CARGO DOOR-LWR FWD CORNER FLT ENGINEERING STRUCTURE INDICATED, ACCEPTED FOR FEERY FLIGHT WITHOUT LIMITATION. REMOVED PREVIOUS REPAIR IAW SRM 51-40-02, ACCOMPLISHED PERMANENT REPAIR IAW ER/A 5SDR DALA2016010700069Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CAP IN SEVERAL LOCATIONS AT BS 365 AND BETWEEN BL 0.0 TO RBL 64. COMPLIED WITH ERA 538386-14 REV ORIGINAL IN MAIN CABIN ON UPPER CAP AT BS 365 BETWEEN BL O.0 TO RBL 70, SECTION 1 PERMANENT REPAIR ASSOCIATED ER/A 14-538386 ADDED FSDR DALA2016010400043Wedge · dentedLEFT WING INBD MAIN FLAP T/E WEDGE DENTED ON UPPER AND LOWER SURFACES, 55" TO 77" FROM OTBD END. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON LT WING INBD MAIN FLAP T/E WEDGE IAW ER/A 536953-14, ORIGINAL REV, DAMAGE DIMENSIONS= 23" X 10", P/N 113N2603.SDR DALA2016010400042Wedge · damagedREPAIR INBD RT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA, APPROXIMATELY 15.5" X 10.5", ON RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.SDR DALA2016010400041Wedge · dentedLT WING INBD MAIN FLAP T/E WEDGE UPPER AND LOWER SKINS HAVE 10.5" X15" DENTED AREA LOCATED 62"-77" FROM OTBD END. ACCOMPLISHED REPAIR OF THE DISCREPANT AREA ON LT INBD MAIN FLAP T/E WEDGE, APPROXIMATELY 17" X 10.5", IAW SRM 51-70-10.SDR DALA2016010400040Wedge · dentedRIGHT INBD MAIN FLAP T/E WEDGE UPPER SURFACE HAS TWO DENTS WITH SHARP CREASES. ACCOMPLISHED REPAIR OF THE TWO DISCREPANT DENTS, APPROX 1" EACH, ON RT INBD MAIN FLAP T/E WEDGE UPPER SURFACE IAW SRM 51-70-10.SDR DALA2015123107783Wedge · dentedNR 10 L/E SLAT T/E WEDGE UPPER SURFACE HAS SHARP DENT AT INBD END. HOT BOND REPAIRED IAW SRM 51-70-10.SDR DALA2015123107782Wedge · damagedINBD LT FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. REPAIRED IAW SRM 51-70-10.SDR DALA2015123107781Skin · damagedLEFT INBD MAIN FLAP UPPER PANEL FROM MF BS 74.0 TO MF BS 209 FOUND DAMAGE CORE FROM INBD TO OTBD END AND FWD TO AFT SIDES AND ONE HOLE IN CORE. REPAIRED IAW SRM 51-70-10 AND ER/A 538384-14 ORIGINAL REVISION.SDR DALA2015123107780Wedge · damagedRT INBD FLAP T/E WEDGE, DO TO FLAP TRACK FAIRING NOT FITTING IN PLACE. ACCOMPLISHED REPAIR OF THE RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-70-10.SDR DALA2015122807731Harness · frayedEMERGENCY ESCAPE SLIDE HARNESSES FOR L1, L2, L4 AND R1 DOORS ARE WORN AND FRAYED OFF, A/C PARTS. PROCURED REPLACEMENT, EMERGENCY ESCAPE SLIDE HARNESSES, 4 EA FOR L-1, L-2, L-4 AND R-1 PASSENGER DOOR, INSTALLATION ACCOMPLISHED ON CARDS 5211-9001-1L, 5211-9001SDR DALA2015122307797Door Frame · corrodedAFT CARGO DOOR LOWER AFT EDGE SIDE FRAME HAS CORROSION. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO DOOR LOWER AFT EDGE SIDE FRAME REF ER/A 541042-14, REV ORIGINAL.SDR DALA2015122307796Skin · dented1 EA DENT ON FWD CARGO LT FRAME UPPER FLANGE AND ONE DENT ON SIDE OF FRAME AT BS 700 BETWEEN STR 23L-25L. TRIMMED OUT THE DENTS. ACCOMPLISHED PERMANENT REPAIR REF SRM.SDR IXXA20151221083Light · inoperativeL4 DOOR SLIDE ENGAGE LIGHT NOT ON WHEN DOOR IS ARMED. DEFERRED MAINTENANCE ITEM 46637, INITIATED WITH SPECIAL CONDITIONS IAW AMM 25-66-05-2. CAT C NO FLY DATE 01 01 2016. RELAMPED L4 DOOR ARMED INDICATOR LIGHT IAW AMM 33-13-00. OPERATIONAL CHECKED SATISFACSDR DALA2015122007693Floorbeam · corrodedCP53-251-01-MAIN CABIN, CORROSION ON FRAME UNDER NUTPLATES BS 1681 AND BETWEEN RBL 57-LBL 57. REMOVED CORROSION UNDER NUTPLATES ON MAIN CABIN FRAME, FLOOR BEAM, UPPER CHORD AT BS 1681 BETWEEN RBL57-LBL57, REF SRM 53-00-51, FIG 101, DET III AND ACCOMPLISHED PESDR DALA2015121907692Seat Track · corrodedCORROSION ON MAIN CABIN FLOOR STRUCTURE, SEAT TRACK FLANGE, BS 680 TO BS 740, RBL 45.5. REMOVED CORROSION ON MAIN CABIN FLOOR STRUCTURE SEAT TRACK FLANGE BS TO BS 740, RBL 45.5. BLENDOUT MEASURE 60" X 2" X 0.059" MIN MATERIAL REMAINING. ORIGINAL THICKNESS TSDR DALA2015122107779Frame · damagedFUSELAGE FRAME HAS TWO HOLES MISDRILLED, BS 1000, RBL 10. ROUTED OUT DAMAGE ON FRAME IAW SRM 53-00-07, REPAIR 1 PERFORMED HFEC OF CUTOUT AND HFEC INSPECTION OF EXITING FASTENER HOLES IAW SRM 53-00-07, REPAIR 1 FIG 204 NO CRACKS FOUND MADE INSURANCE CUT IAW SSDR FOTR20151211001Frame · dentedFWD FUSELAGE BS 231, BL 0 FRAME IS DENTED.SDR DALA2015121807668Seat Track · corrodedCABIN FLOOR STRUCTURE BS 695-733, RBL 45, SEAT TRACK SUPPORT CORRODED. REMOVED CORRODED AREA FROM BS 695-733 CABIN FLOOR STRUCTURE, RBL 45, FOUND 8, AREAS, L-3.5" W-0.090, D-0.025", L-1.3" W- 0.070" D-0.010", L-1.4 W-0.070 D-0.015, L-1.5" W-0.085" D- 0.019",SDR FOTR20151210001Skin · dentedLEFT WING NR 1 SLAT UPPER SURFACE OF THE T/E WEDGE HAS A DENT THAT IS OUT OF LIMITS DUE TO OVERLAPPING DENTS WS 785-800.SDR DALA2015121207590Frame · dentedWHILE WORKING NRC 100-41, DISCOVERED 2 EA DENTS ON AFT CARGO FRAME BS 1320 BETWEEN STR 24R AND STR 26R. CUTOUT 2 EA DAMAGED AREAS AT BS 1320 BETWEEN STR 24R & 26R IAW SRM 53-00-07, REPAIR 5. DIMENTIONS OF BOTH CUTOUTS W=1.0 " X L=1.125" X 0.5"R ORIGINAL MATE
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