Boeing 717-200

Service difficulty reports · 18,771

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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 = '717200'
  ORDER BY difficulty_date DESC"

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SDR DALA2017022101378Channel · crackedCRACK ON CHANNEL OF FLOOR PANEL. REPAIRED IAW SRM 51-20-05.Feb 20, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022001377Floor Panel · crackedCRACK ON FLOOR PANEL 221S. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50, FIG 202, SHEET 1. STOP DRILLED AND NO CRACKS WERE FOUND IAW SRM 53-20-50, FIG. 202.Feb 19, 2017 · N993AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022001375Angle · crackedCRACKED AFT UPPER ANGLE NR 2 ON INTERNAL STRUCTURE OF THE RT FWD OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735 REV G, AND SRM 51-41-05.Feb 19, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017022001374Floor Panel · delaminatedFLOOR PANEL DELAMINATED. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.Feb 19, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017022001373Cusp Web · corrodedCORROSION ON RT CUSP WEB BETWEEN BS 455-459, 488-490, RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4, FIG. 215.Feb 19, 2017 · N929AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021901371Rub Strip · corrodedCORROSION ON RUB STRIP OF FUEL ACCESS PANEL ON RT WING. THE RUB STRIP WAS REPLACED IAW SRM 57-10-01 2R-3, REP 3, PAR 6.Feb 18, 2017 · N993AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017021901370Floor Panel · brokenBROKEN LAVATORY FLOOR PANEL. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.Feb 18, 2017 · N929AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017021901369Door Frame · crackedCRACKED DOOR FRAME WEB BS 207 LONGERON 11L. THE DOOR FRAME WEB WAS REPAIRED IAW SRM 53-10-15-2R.Feb 18, 2017 · N993AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017021901372Floor Panel · delaminatedDELAMANATED FLOOR PANEL IN THE COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50 2R, PROCEDURE 3, REPAIR 3.Feb 17, 2017 · N993AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017021801367Rub Strip · corrodedCORROSION ON RT RUB STRIP AT UPPER FUEL ACCESS DOOR 620FT. THE CORROSION WAS REMOVED IAW SRM 57-10-01 2R-3, REP 3, PAR 6.Feb 17, 2017 · N993AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017022101437Former · corrodedLT FILLET FORMER AT STA 851 HAS CORROSION AROUND SCREW HOLES AT LOWER END. REPLACED LT FILLET FORMER "ITEM-10 ANGLE" AT STA 851 THAT WAS CORRODED BEYOND LIMITS NOMINAL .050" LOSS=.023 REMAINING .027" IAW SRM 51-41-02 0G, 53-20-71 0I-1 AND DWG 5971058.Feb 16, 2017 · N988AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017021801366Cusp Web · corrodedRIGHT OTBD CUSP WEB HAS AREAS OF CORROSION FROM BS 851 - 870. BLENDED, AND FOUND OUT OF LIMITS IAW SRM 53-00-55 1A. FABRICATED A DOUBLER AND RING DOUBLER. INSTALLED IAW SRM 53-00-55 2R-4.Feb 16, 2017 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021701304Cusp Web · crackedRIGHT CUSP WEB AT BS 218 - 237 IS CRACKED. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4.Feb 16, 2017 · N974AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021701303Skin · crackedFUSELAGE SKIN BS 1022 ABOVE LONGERON 14R CRACKED. REPAIRED THE SKIN IAW ER/A 553675-14 REV 0.Feb 16, 2017 · N988AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017021701300Beam · crackedL1 DOOR HAD A CRACKED BEAM NR 1 AT FWD EDGE. REPAIRED IAW SRM 52-10-02, FIGURE 202, REPAIR 7.Feb 16, 2017 · N929AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017021701299Floor Support · corrodedCORROSION ON SETTLEMENT AREA OF FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW DWG #9936534-179 REV BW.Feb 16, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021701298Frame · crackedCRACKED FRAME ANGLE BS 679, MLG WHEEL WELL CANTED KEEL. FRAMES WERE REPAIRED IAW SRM 51-70-11 2R.Feb 16, 2017 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017021701297Pan · wornAFT CABIN BULKHEAD DOOR WORN ON RT LOWER INTERNAL PAN AT VENTRAL STAIR DOOR. OUT OF LIMITS. REPAIRED IAW SRM 52-10-02 2R, REPAIR 16.Feb 16, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021701296Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 620FT AND 620DT. REPLACED THE ACCESS PANELS.Feb 16, 2017 · N993AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017021701293Pan · crackedCRACK ON LEFT RING PAN, FWD LOWER CORNER BS 636 - 927. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R FIG 202 TYPE B, 51-41-02 0G, AND 51-41-05 0G.Feb 16, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017021601273Fitting · crackedCRACKED FRAME CLIP ON STA 1022 BTW LONG 13 /14 RT. REPAIR ON FRAME CLIP WAS ACCOMPLISHED PER SRM 53-00-06.Feb 16, 2017 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017021601272Fitting · crackedCRACKED FRAME CLIP ON STA 1022 BTW LONG 13 /14 LT. REPAIR ON FRAME CLIP WAS ACCOMPLISHED PER. SRM 53-00-06 REPAIR 2.Feb 16, 2017 · N993AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017021601271Angle · corrodedCORROSION ON SETTLEMENT OF RT CONSOLE STA Y=145 X=-45 AT COCKPIT. SETTLEMENT ANGLE OF RT CONSOLE ON STA Y=145 X=-45 AT COCKPIT WAS REPLACED PER SRM 51-41-02, 51-41-01, AND DWG 9936533-11 REV CM.Feb 15, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021601270Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=145 X=-46 AT COCKPIT. FLOOR SUPPORT WAS REPLACED PER SRM 53-10-51, SRM 51-40-08, AND SRM 51-41-02.Feb 15, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021601269Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=256 BTW X=-22 TO X=22 AT PAX CABIN IN REF NRTC 406 (AMDS 5300-2010). SUPPORT WAS REPLACED PER SRM 51-40-08 AND SRM 51-41-05.Feb 15, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021601268Skin · damagedRUDDER LT SKIN LOWER EDGE IS DAMAGED AT MARKED LOCATION. PRIMED OUT DAMAGE FABRICATED DOUBLER .032 FILLER .050. ALODINE, PRIMED, AND TOP COAT REPAIR AND INSTALLED IAW SRM 51-70-13-2R-1-01 FIG 201 IAW PSM 900-2-4-1 NR 2 PSM 900-3-6 NR 3 IAW AMM 51-21-10 370-805Feb 14, 2017 · N974AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2017021501232Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS AT BOTH L1 AND R1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.Feb 14, 2017 · N996AT · Boeing 717200 · Emergency LightingSDR DALA2017021501231Pan · crackedCRACK ON LT RING PAN, AFT UPPER CORNER BS 813 - 832, 832 - 851, 851 - 870. LEFT RING PAN, REPAIRED IAW SRM 56-20-02-2R FIG 202 TYPE B, 51-41-02 0G, AND 51-41-05 0G.Feb 14, 2017 · N929AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017021501230Floor Support · corrodedSEVERAL CORROSION POINTS ON FLOOR SUPORTS BS 148 AND 218, RBL 7 AND 54. FLOOR SUPPORT REPLACED IAW SRM 51-41-01 AND SRM 51-41-05.Feb 14, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021501229Skin · crackedSKIN CRACKED BS 1133 OTDB OF LONGERON2L. REPAIRED THE SKIN IAW ER/A 553669-14AD REV 0.Feb 14, 2017 · N923AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017021501266Skin · corrodedFORWARD CARGO HAS CORROSION ON SKIN INBOARD OF LONGERON 28L BETWEEN STA 636 AND STA 655. REMOVED CORRODED INTERNAL DOUBLER AND INSTALLED NEW INTERNAL DOUBLER BETWEEN STATIONS 636 AND 655 IAW SRM 51-41-02 AND 51-41-05 AND DWG 5940882.Feb 13, 2017 · N923AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017021401187Seat Track · damagedLEFT INBD SEAT TRACK BS 268 - 368, LBL 22 HAS SCRATCHED, AND CORROSION. BLENDED THE SEAT TRACK, AND FOUND TO BE OUT OF LIMITS AND REPAIRED IAW SRM 53-20-52 2R-1.Feb 13, 2017 · N988AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017021401186Cusp Web · corrodedCORROSION ON LEFT CUSP WEB LBL 60, BS 910 - 920. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55. REPAIRED IAW SRM 53-00-55 2R-4.Feb 13, 2017 · N988AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021301149Cusp Web · crackedCRACKED RT CUSP WEB STA Y=953 BTW X=-54 TO X=-60 (AMDS 5300-2020) (CPAX) (IN REF CARD 00194). CUSP WEB STA Y= 953 WAS REPAIRED PER SRM 53-00-55 REPAIR 4 FIG 212. HFEC WAS ACCOMPLISHED ON RT CUSP WEB STA Y=953 BTW X=-54 TO X=-60 CPAX PER NDT SPM 06-10-01.001, NFeb 12, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021301148Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200 BTW X=12 TO X=-7). FLOOR SUPPORTS WERE REPLACED PER SRM 51-41-05.Feb 12, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021201146Cusp Web · crackedCRACK ON LT CUSP WEB AT STA Y= 674. HFEC INSPECTION WAS ACCOMPLISHED AND CRACKS WERE FOUND (1.500") AND (2.500") PER NDT SPM 06-10-01.001. DAMAGE WAS REMOVED PER SRM 53-00-55 2R-4 REPAIR 4 FIG 212. CUT OUT WAS TREATED AND PAINTED PER SRM 51-10-04 PAR 21 AND 15Feb 11, 2017 · N993AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017021101137Pan · crackedCRACK ON LT RING PAN AT STA Y= 909 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 5Feb 10, 2017 · N993AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017021101136Pan · crackedCRACK ON LT RING PAN AT STA Y= 877 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMFeb 10, 2017 · N993AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017021101135Pan · crackedCRACK ON LT RING PAN AT STA Y= 831 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMFeb 10, 2017 · N993AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017021101134Pan · crackedCRACK ON LT RING PAN AT STA Y= 637 UPPER SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS PERFORMED ON TRIMMED AREAS NO CRACKS WERE FOUND ON EDGES PER NDTSPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRMFeb 10, 2017 · N993AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017021101133Pan · crackedCRACK ON RT RING PAN AT STA Y= 889 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE TRIM-OUT PER NDT SPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM Feb 10, 2017 · N993AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017021501267Door · corrodedL1 PASSENGER DOOR AIRSTAIR DOOR HAS CORROSION IN FORWARD AND AFT LOWER CORNERS AND AROUND AND INCLUDING NUT CLIPS AND GOUGES IN LOWER FLANGE. INSTALLED NEW AIRSTAIR DOOR IAW AMM 52-63-01 420-801, AND SRM 51-40-02, 51-40-04.Feb 9, 2017 · N923AT · Boeing 717200 · Entrance StairsSDR DALA2017030201695Plate · damagedAFT CARGO DOOR SEAT PLATE PULLED AWAY FROM FUSELAGE. REPAIRED IAW ER/A (2) 555305-1, SECTION 1, STEPS 1-8.Feb 8, 2017 · N924AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017020901066Cover · missingMAINTENANCE DISCOVERED THAT THE EMERGENCY EXIT SIGN DIFFUSER COVER WAS MISSING. MAINTENANCE REPLACED THE COVER AND THE OPS CHECKED GOOD.Feb 8, 2017 · N950AT · Boeing 717200 · Emergency LightingSDR DALA2017020801035Seat Track · corrodedSEAT TRACK RBL 44.5 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 900 - 986. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-30-07 FIG 18, 53-00-00-1A. LOCATED AND DRILLED REPLACEMENT SEAT TRACK IAW SRM 51-40-08, INSTALLED IAW SRM 53-20-52-2R-5, 51-41-01, 5Feb 7, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017020801034Frame · crackedBS 1022 BULKHEAD REAR FRAME ANGLE IS CRACKED STRINGER 7L, VERIFIED WITH HFEC . REPAIRED IAW SRM 51-70-11 REPAIR 1.Feb 7, 2017 · N923AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017020600959Cover · looseTHE FLIGHT ATTENDANT DISCOVERED THAT AN EMERGENCY EXIT SIGN DIFFUSER COVER AT DOOR L1 WAS LOOSE. MAINTENANCE REINSTALLED THE COVER AND THE OPERATIONAL CHECK WAS GOOD.Feb 4, 2017 · N955AT · Boeing 717200 · Emergency LightingSDR DALA2017020901078Cusp Web · crackedUPPER CABIN CUSP WEB FOUND CRACKED AT STA 832 LBL 58. UPPER CABIN CUSP WEB CRACK REPAIRED IAW SRM 53-00-55-R2-4. REMOVED AND INSTALLED SEAT TRACK TO ACCESS, IAW SRM 51-40-04-06. ALODINED AND PRIMED AREA, IAW SRM 51-10-04 PG 10. 17-21. CUSP REPAIR PERFORMED AT Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017020601004Seat Track · corrodedRIGHT CENTER SEAT TRACK STA 556-656 RBL 44.5 HAS CORROSION AND NEED PAINT TOUCHED UP. REPAIRED SEAT TRACK SECTION RBL 44.5 BETWEEN STA 581-644 BLENDED OUT OF LIMITS IN SEVERAL AREA'S .048 MAT LOSS FROM .100 ORG IAW B717 SRM 53-20-52 FIG 101 & REPAIR 5/7001.Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017020601003Seat Track · corrodedLEFT CENTER SEAT TRACK HAS AREAS OF CORROSION, GOUGING, AND AREAS OF MISSING PRIMER AND TOPCOAT FROM STA 556 TO STA 656. REPAIRED SEAT TRACK SECTION 44.5 BETWEEN STA 533-646 BLENDED TRACK OUT OF LIMITS MAT LOSS WAS .050 FROM .100 ORIGINAL TAG 2736 IAW SRM 53-2Feb 3, 2017 · N923AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
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