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 DALA2016061204541Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620CT. ZONE 600, DUE TO CORROSION FOUND ON ACCESS PLATE NR 620CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.Jun 11, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061204540Access Panel · corrodedCORROSION ON WING ACCESS PLATE 520CT AT SETTLEMENT AND COUNTERSKIN AREA. ZONE 500, DUE TO CORROSION FOUND ON ACCESS PLATE NR 520CT WAS REPLACED IAW SRM 57-10-01, CONDITION III.Jun 11, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061204539Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF WING ACCESS PLATE 520HB. ZONE 500. CORROSION ON COUNTERSKIN AT FUEL ACCESS PLATE 520HB WAS REMOVED, AND MAX DIAMETER ALLOWABLE IS 0.532 AND MAX DIAMETER MEASURED IS 0.565 IN AND WERE FOUND 3 HOLES ADJACENT OUT Jun 11, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061204538Longeron · corrodedCORROSION ON LONGERON 29LT AND SPLICE FROM BS Y=929 TO 1022 AT AFT CARGO COMPARTMENT, C2, SM. CORROSION WAS REMOVED, REWORKED AREA WAS TREATED, PAINTED, MEASURED, ORIGINAL THICKNESS: 0.125" REMAINING THICKNESS 0.110" THEREFORE IT'S WITHIN LIMITS IAW SRM 51-10Jun 11, 2016 · N961AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016061404594Skin · crackedRIGHT FUSELAGE BS 1095 SKIN CRACKED FROM FASTENER HOLE APPROXIMATELY .75" JUST ABOVE LONGERON 14R. VERIFIED BY EDDY CURRENT. REPAIRED RT FUSELAGE BS 1095 CRACKED SKIN FROM FASTENER HOLE JUST ABOVE LONGERON 14-R IAW ER/A 545684-14, REV. OR. ASSOCIATED ER/A 00Jun 10, 2016 · N966AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016061104537Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DB AT RT WING. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01 AND 51-10-04 AND FUEL ACCESS PLATE WERE MEASSURED, 4 HOLES FOUND OUT LIMITS .535, .534, .549, .554 IJun 10, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061104536Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620CB AT RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT AREA WAS REMOVED IAW SRM 57-10-01. FUEL ACCESS PLATE NR 620CB WAS MEASURED, 6 EAS, HOLES FOUND OUT LIMITS .554, .534, .546, .541, .565Jun 10, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061104535Cusp Web · crackedRT CUSP MEMBRANE CRACKED AT BS 675. REPAIRED CRACKED CUSP MEMBRANE IAW SRM 53-00-55, REPAIR 4.Jun 10, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061104534Cusp Web · crackedLEFT CUSP WEB CRACKED AT BS 218. INSTALLED REPAIR DOUBLER ON LT CUSP WEB IAW SRM 53-00-55, REPAIR 4.Jun 10, 2016 · N920AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016061104533Floor Panel · crackedCRACKED STIFFENERS ON PASSENGER CABIN FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-20-50.Jun 10, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016061104532Floor Panel · crackedCRACKED FLOOR PANEL 211ACF. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV.Jun 10, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016061404593Structure · crackedCRACK ON LT SIDE OF VERITCAL STABILIZER AT MATING SURFACE OF EMPENNAGE AT BS 116. REPAIRED CRACK ON LT SIDE OF VERTICAL STABILIZER AT MATING SURFACE OF EMPENNAGE BS 1116 IAW SRM 55-30-01, FIG 201, REPAIR 5.Jun 9, 2016 · N966AT · Boeing 717200 · Vertical StabilizerSDR DALA2016061004508Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Jun 9, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016061004507Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE NR 520MB. SM, CARD 40, ZONE 500. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 520 MB WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUJun 9, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061004506Longeron · corrodedCORROSION ON LONG 28 LT AND SPLICE FROM BS Y=927 TO Y=1037 AT AFT CARGO COMPARTMENT C2, SM, ZONE 180, CARD 5. CORROSION ON LONG 28 LT FROM BS Y=927 TO BS 1037 AT AFT CARGO COMPARTMENT WAS REMOVED IAW SRM 51-10-04, PAR. 26, 21, AND 15. MEASURE: ORIGINAL THICKJun 9, 2016 · N961AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016061004505Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK AREA OF WING ACCESS PLATE 520EB. SM, CARD 34, ZONE 500. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED ON ACCESS PLATE 520EB AND WAS MEASURED MAX. DIAMETER ALLOWABLE IS 0.532" AND WERE FOUND MORE 2 ADJACENTJun 9, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016061004502Floor Panel · damagedCRACK ON PASSENGER CABIN FLOOR PANEL NR 222ZF. SM, CARD 52, ZONE 000. FLOOR PANEL 222ZF WAS REPAIRED IAW SRM 53-00-00, REPAIR 2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. TREATED, PAINTED, AND APPLIED CIC IJun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016061004501Floor Panel · damagedDAMAGE AND MISSING FERRULES ON FLOOR PANELS, NR 222ABF, 222AAF, 222AEF, AND 222AKF AT PAX CABIN. SM, CARD 79, ZONE 000. DAMAGE FERRULES WERE REPLACED ON FLOOR PANELS NR 22ABF, 222AAF, 222AEF, AND 222AKF IAW ER/A 546544-14, REV. ORIGINAL ASSOCIATED ER/A 00-54Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016061004500Floor Panel · damagedDAMAGE AND MISSING FERRULES ON FLOOR PANELS 221FF, 221CF, 22BF, 22LF, 222JF, 222RF, AND 222UF. SM, CARD 77, ZONE 000. DAMAGE FERRULES ON FLOOR PANEL NR 222BF, 222RF, 222LF, 222JF, AND 221EF WERE REPLACED IAW DWG NR 9936546 AND ER/A 546544-14, REV. ORIGINAL FJun 9, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016061004499Frame · crackedCRACKED FRAME BS 696, LONG 26 RT AND FRAME BS 715, LONGERON 27R AT UNDERWING BARREL KEELBEAM INTERNAL STRUCTURE. SM, CARD 16, ZONE 140. FRAMES WERE REPAIRED IAW SRM 51-70-11, REPAIR 1, SRM 51-41-02, SRM 51-10-04 PAR 15 AND 21. RII COMPLETED.Jun 9, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016061004550Lanyard · disconnectedTHE PILOT DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT L1 DOOR HAD A DISCONNECTED LANYARD. THE LANYARD WAS DISCONNECTED FROM THE DOOR. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. MAINTENANCE RJun 8, 2016 · N969AT · Boeing 717200 · Escape SlideSDR DALA2016060904485Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSKIN AREA OF WING ACCESS PLATE NR 620CB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSKIN WERE REMOVED IAW SRM 57-10-01, MAX DIAMETER ALLOWABLE ON COUNTERSKIN IS 0.532", MAX DIAMETER MESURED IS 0.545" AND WERE FOUND 3 AJun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904484Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSKIN OF FUEL ACCESS PLATE NR 620MB. ZONE 600. CORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 620MB WAS REMOVED IAW SRM 57-10-01 MAX DIAMETER ALLOWABLE ON COUNTERSINK IS 0.532" MAX DIAMETER MEASURED Jun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904483Frame · crackedCRACKED FRAME BS 696, LONG 26LT AND FRAME 715, LONG 27 LT AT UNDERWING BARREL KEEL BEAM INTERNAL STRUCTURE. FRAMES WERE REPAIRED IAW SRM 51-70-11 REPAIR 1, FIG 201, SRM 51-41-02, SRM 51-10-04 PAR 15-21, 37, 51-41-05.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060904482Floor Panel · damagedDAMAGE AND MISSING FERRULES ON FLOOR PANELS NR 222AVF AND 223CF AT CABIN PAX. FLOOR PANEL NR 222AVF WAS REPLACED FERRUL IAW ER/A 546544-14 REV. ORIGINAL. FLOOR PANEL NR 223CF WAS FABRICATED IAW ER/A 546544-14 REV ORIGINAL.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060904481Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK OF WING ACCESS PLATE NR 620DT. RT WING. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED, MAX DIMENSION ALLOWABLE 0.660" MAX DIAMETER MESURED ARE 0.675" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SJun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904480Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF WING ACCESS PLATE NR 620EB. CORROSION ON COUNTERSINK AND SETTLEMENT WERE REMOVED AND WAS MEASURED MAX DIAM ALLOWABLE IS 0.532" AND MAX DIAMETER MEASURED IS 0.565" AND WERE FOUND MORE TO 2 HOLES ADJACENT IAW SRMJun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904479Skin · corrodedCORROSION ON CENTER WING UPPER SKIN, JUST FWD OF SLANT PANEL AND BS X= 40.5, CARD 3, ZONE 140). FUEL LINE WAS REMOVED AND INSTALLED IAW AMM 20-10-03 917-81 FASTENERS WERE REMOVED AND INSTALLED IAW SRM 51-41-05 CORROSION WAS REMOVED IAW SRM 57-10-01 AND (UT) WAJun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016060904478Door Frame · crackedCRACKED NLG DOOR JAMB BS Y=46 X=18 LT Z=-33 AT NLG W/W. NLG DOOR JAMB WAS REPAIRED IAW SRM 53-10-14, FIG 201.Jun 8, 2016 · N915AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060904477Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620LB AT RT WING. CORROSION ON COUNTERSINK AT ACCESS PLATE 620LB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.536, 0.550, AND 0.545 AND WAS REPLACED WITH CONDITION IJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904476Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520LB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520LB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .579, .538, .543 IAW SRM 57-10-01, ACCESS PLATE WAS REPLAJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904475Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520GB AT LT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS DOOR 520GB WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .560, .553 AND .558 IAW 57-10-01 ACCESS PLATE WAS REPLACJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904474Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520DB WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.552, 0.538, 0.563 IAW SRM 57-10-01 AND ACCESS PLJun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904473Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520CB AT LT WING. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 520CB WAS REMOVED AND MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.538 AND 0.540 ACCESS PLATE WAS REPLACED IAW SRM 57-1Jun 8, 2016 · N915AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060904472Angle · crackedCRACKED ANGLES BS 1168 BETWEEN LONGERON 3RTO 2L. ANGLES REPLACED IAW DWG 9911860, REV L AND SRM 51-41-02 AND SRM 51-41-05.Jun 8, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060904471Structure · corrodedCORROSION ON INTERNAL STRUCTURE BETWEEN BS 900 TO 910 BETWEEN LONGERON 25 TO 26L. STRUCTURE REPAIRED IAW SRM 53-02-01, REPAIR 1, 51-40-08, AND 51-10-04 PAR 15-21-37 AND 51-41-02.Jun 8, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060904470Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTER SKIN OF FUEL ACCESS PLATE NR 620FT. CORROSION SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE NR 620 FT WERE REMOVED IAW SRM 57-10-01. COUNTERSINK AND SETTLEMENT AREA WERE MEASURED AND COUNTERSINK MAX DIAMETER IS 0Jun 8, 2016 · N961AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016060804420Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14 REV ORG.Jun 7, 2016 · N961AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804419Web · corrodedCORROSION ON DIAPHRAGM FROM BS 195 TO 200 AND BETWEEN X -52 TO X -58. DIAPHRAGM WAS REPAIRED IAW SRM 51-70-10, FIG 201.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060804418Floor Panel · brokenBROKEN CORE ON FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546544-14, REV ORIGINAL.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804417Stiffener · crackedCRACK ON STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, 222AJF. SM, CARD 57 ZONE 000. STIFFENERS OF PASSENGER CABIN FLOOR PANELS 222AFF, 222ALF, AND 222AJF WERE REPAIRED IAW SRM 53-20-50, REPAIR 5, FIG 201 AND 202. CRACK L=0.235", CRACK L=0.324",Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016060804416Cusp Web · crackedCRACKS RT CUSP WEB BETWEEN BS 218 TO 237 X 44. CUSP WEB WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 9930538, REV CC.Jun 7, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060804415Frame · crackedCRACK ON FRAME ANGLE BS 1116, LONGERON 15L AT AFT ACCESSORY COMPARTMENT. THE ANGLE WAS REPLACED IAW DWG 5913595 REV.AP AND SRM 51-41-05, 51-41-02.Jun 7, 2016 · N961AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016060904486Support · crackedRIGHT WING, KEEL BEAM, BS 680, CRACKED LONGERON SUPPORT INSIDE BOX. REPLACED CRACKED LONGERON SUPPORT ON RT WING KEEL BEAM BS-680 REPAIR DOUBLER ON FORMER IAW ER/A 545683-14MA-O, STEP 8. WORK COMPLETE ASSOCIATED ER/A 00-545683 ADDED FOR AC 9525.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060804423Oven · smokeCREW REPORTED THE FORWARD GALLEY OVEN SMOKING FROM TOP VENT. CABIN CREW PULLED OVEN CIRCUIT BREAKER AND SMOKE SUBSIDED. MAINTENANCE FOUND PLASTIC INSIDE OVEN HAD BEEN BURNING. THE OVEN WAS REPLACED IAW AMM. COMPLIED WITH NO GO ODI PREVENTION FOR SMOKE IN CABJun 6, 2016 · N893AT · Boeing 717200 · Buffet/GalleysSDR DALA2016060804422Stop Fitting · crackedBS 1053 VENTRAL DOOR LOWER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED. REPLACED DOOR STOP IAW SRM 51-41-02, PAR. 4.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060804421Stop Fitting · crackedBS 1053, VENTRAL DOOR UPPER DOOR STOP FITTING ON CUTOUT SURROUND STRUCTURE CRACKED, HFEC VERIFIED, REPLACED DOOR STOP FITTING IAW SRM 51-41-02, PAR 4.Jun 6, 2016 · N966AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016060704396Floor Support · crackedCRACK ON FLOOR SUPPORT BS 636, X 0. CRACK WAS STOPP DRILLED IAW SRM 53-00-00, FIG 1. REPAIR PART WAS FABRICATED IAW SRM 53-00-00 FIG 201. REPAIR INSTALLED IAW SRM 51-40-02.Jun 6, 2016 · N915AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060704395Cusp Web · crackedCRACKED RT CUSP WEB AT X -44 TO X -54 BETWEEN BS 218 AND 237 AT CABIN FLOOR STRUCTURE. REPAIR ON CUSP WEB IAW SRM 53-00-55, FIG 219, REP 4.Jun 6, 2016 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016060704394Fitting · crackedCRACKED FITTING AT BS 737, X 43 AND Z -11. FITTING WAS REPLACED IAW SRM 51-41-05, 51-41-02, 51-40-08, AND 51-10-04 PAR 15 AND 21.Jun 6, 2016 · N915AT · Boeing 717200 · Fuselage Main, Attach Fittings
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