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 DALA2016041202792Pan · crackedCRACKED RING PAN BETWEEN BS 237 - 256 AT UPPER, FWD CORNER AREA. RING PAN BETWEEN BS 237-256 WAS REPAIRED IAW SRM 56-20-02, FIG 202.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016041202791Pan · crackedCRACKED RING PAN BETWEEN BS 636-655 AT LWR/FWD CORNER AREA. CFS, SM, CARD 23, ZONE 201. RING PAN BETWEEN BS 636-655 WAS REPAIRED IAW SRM 56-20-02, FIG 202.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016041202790Floor Panel · puncturedPUNCTURED ON FLOOR PANEL NR 222HF. DAMAGE WAS REPAIRED IAW SRM 53-00-00, FIG 102.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016041202789Cusp Web · corrodedCORROSION ON RT CUSP WEB X=-57 TO 61 BS 446-465 LOWER SURFACE AT FLOOR STRUCTURE. CFS, SM, CARD 31, ZONE 200. CUSP WEB WAS REPAIRED X=-57 TO 61 BS 446-465 IAW SRM 51-10-4, PAR 26, 53-00-55, FIG 209, AND 51-41-02.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041202788Longeron · crackedCRACK LONGERON 2 RT AND BS 1133 AT AFT ACCESORY COMAPRTMENT. SM, CARD 13, ZONE 310. CRACK LONG 2 RT WAS REPAIR IAW SRM 53-00-05, FIG 201, R2, 51-10-04, PAR 21 AND 15, 51-41-05. RII COMPLETED.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016041202787Longeron · crackedCRACK LONGERON 2 LT AND BS 1133 AT AFT ACCESSORY COMPARTMENT. SM, CARD 12, ZONE 310. CRACK LONGERON 2 LT WAS REPAIRED IAW SRM 53-00-05, R2, FIG 201, 51-10-04, PAR 21 AND 14, 51-41-05. RII COMPLETED.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016041202786Web · corrodedCORROSION AT FLOOR WEB BETWEEN BS 194, BS 187 X=53.5, SM, W1, CARD 73, ZONE 200. FLOOR WEB WAS REPAIRED IAW SRM 53-00-00, REPAIR 1, FIG 201, 51-41-02, AND 51-10-04, PAR 37.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041102739Battery Pack · malfunctionedDURING SERVICE CHECK, MAINTENANCE FOUND THEY COULD NOT CONTROL THE EMERGENCY LIGHTING IN THE CABIN FROM THE F/A PANEL. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS, LOCATED IN THE AFT CARGO, AND THE OPS CHECK WAS GOOD.Apr 10, 2016 · N927AT · Boeing 717200 · Emergency LightingSDR DALA2016041102738Power Supply · malfunctionedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY LIGHTING WOULD NOT TURN OFF. LIGHTS WOULD REMAIN ON AFTER POWER WAS REMOVED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Apr 10, 2016 · N927AT · Boeing 717200 · Emergency LightingSDR DALA2016041102737Cusp Web · corrodedCORROSION ON RT CUSP WEB X=-56 TO 61 BS 465-484 LOWER SURFACE AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 101, 51-41-02, AND 51-10-04, PAR 37. EQUIPMENT PANAMETRICS NDT 35, DATE 25-AUG-16 TRANSDUCER SONOPEN V260SM.Apr 10, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041102736Cusp Web · puncturedPUNCTURED LT CUSP WEB BS 728 X=56 AT C PASSENGER STRUCTURE. LEFT CUSP WEB BS 728 X=56 AT CABIN PAX WAS REPAIRED IAW SRM 53-00-00, FIG 102.Apr 10, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041402894Frame · corrodedBS 974 AT STRINGER 30 HAS APPROXIMATELY 6" OF CORROSION COMMON TO FRAME. BLENDED CORRODED AREA IAW SRM 53-00-00, FIG 103. FOUND OUT OF LIMITS IAW SRM 53-20-07. NEW FRAME FABRICATED AND HEAT TREATED IAW DPS 900-4-1 NR 1, PG 16 12-20-10, PG 25 1-17-12, INSTAApr 9, 2016 · N956AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041002735Seat Track · not reportedOUT OF LIMITS, SEAT TRACK X=-44, BS 256. AREA WAS ATTENDED IAW SRM 53-20-52, FIG 201 51-10-04, 51-41-01.Apr 9, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041002734Cusp Web · crackedCRACK ON RT CUSP WEB X=-44 TO 50, BS 674. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R4 CRACK LENGTH .125.Apr 9, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041002733Cusp Web · corrodedCORROSION ON RT CUSP WEB X=-57 TO 61 FROM BS 916 TO BS 930 AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 51-41-02, 53-00-55, FIG 216, AND 51-10-04, PAR 21, 15 AND 37.Apr 9, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041002732Web · crackedCRACKED WEB BS 218 X=19 AT PAX CABIN IN REF CARD 55, A/C ZONE 200. CARD 82, ZONE 200. WEB WAS REPAIRED IAW SRM 51-70-10, FIG 201, 51-41-05, AND 51-10-4, LENGTH CRACK .125".Apr 9, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016040902731Longeron · corrodedCORROSION ON LONGERON 29L FROM BS 907 TO 964 AT AFT CARGO COMPARTMENT. LONGERON WAS REPLACED IAW SRM 53-20-05, 51-40-08, 51-40-08, 51-41-02, 51-41-05, AND 51-10-4 PAR 15, 21.Apr 8, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016040802708Door Frame · corrodedAFT CARGO COMPT DOOR LOWER JAMB UNDER SCUFF PLATE CORRODED BS 954-994. REPAIRED IAW SRM 53-20-15, REPAIR 7.Apr 8, 2016 · N927AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017061404724Skin · damagedDENT AND SCRAPE IN THE RT SKIN AT BS 577 - 580, BETWEEN STRINGERS 25R - 26R. CLEANED AREA. ACCOMPLISHED HFEC INSPECTION IAW SRM 53-01-01 & AMM NDT SPM 06.10.01.001. NO CRACKS INDICATED. THE DENT WS FOUND TO BE 0.092 DEEP BY 2 INCHES WIDE. IAW SRM 53-01-01, COApr 7, 2016 · N997AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016041502926Longeron · corrodedLONGERON 29L IN BS 908-960 IS CORRODED IN SEVERAL AREAS. REMOVED RIVETS ON STR 29L IAW SRM 51-41-02, INSTALLED NEW RIVETS ON STR 29L IAW SRM 51-41-02 BLENDED CORROSION ON STR 29L FROM BS 908-960 IAW SRM 53-00-05. REPAIR 3 C/W THICKNESS CHECK IAW MD/B NTSPM 0Apr 7, 2016 · N956AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016060704397Engine · fireTHE CREW SAFELY ABORTED THE TAKEOFF AT LESS THAN 80 KTS DUE TO A FIRE INDICATION ON THE NR 1 ENGINE. THE FIRE WAS CONFIRMED, BUT THE CAUSE HAS NOT BEEN IDENTIFIED. MAINTENANCE HAS REPLACED THE NR 1 ENGINE.Apr 6, 2016 · N974AT · Boeing 717200 · Engine (Turbine/Turboprop)SDR DALA2016041103477Light · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT THE LT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.Apr 5, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016041502924Skin · crackedFUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14R AT SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW BS 1087, STR 14R IAW ER/A 544359-14.Apr 5, 2016 · N956AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016041502923Skin · crackedFUSELAGE SKIN CRACKED, HFEC VERIFIED, BS 1087 ABOVE STR 14L SHEAR TIE FASTENER. REPAIRED FUSELAGE CRACKED SKIN IAW ER/A 544359-14.Apr 5, 2016 · N956AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016041402893Support · crackedRIGHT SIDE OF CENTER TANK, RBL 45, SEAT TRACK SUPPORT IS CRACKED AT BOTTOM OF SUPPORT, MARKED. REPLACED SEAT TRACK SUPPORT IAW SRM 51-40-02 AND 53-20-51, FIG 1, SHEET 2 OF 3.Apr 5, 2016 · N956AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040602655Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Apr 5, 2016 · N987DN · Boeing 717200 · Emergency LightingSDR DALA2016040602654Seat Track · corrodedLT CTR SEAT TRACK BS 148-1053, X=44.5 HAS MULTIPLE DISCREPANCIES. BLENDED LBL 44.5 LT CTR SEAT TRACK, BS 140-STA 200, STA 246-STA 1053. SEAT TRACK IS WITHIN ALLOWABLE LIMITS IAW SRM 53-20-52. REPLACED SECTION OF SEAT THAT IS OUT OF LIMITS BS 200-BS 246 IAW SApr 5, 2016 · N956AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016040602653Cusp Web · corrodedAREA OF CORROSION ON OUTER CUSP WEB NEAR S18R APPROXIMATELY BS 207. REPLACED CUSP WEB IAW SRM 51-41-02, PG 1-4, 51-41-05, PG 1.Apr 5, 2016 · N956AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016040502626Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY SIDEWALL WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Apr 5, 2016 · N894AT · Boeing 717200 · Emergency LightingSDR DALA2016050103466Cusp Web · corrodedUPPER CABIN FLOOR CUSP WEB, BS 470, RBL 56 HAS CORROSION ON UPPER SURFACE. BLEND AND CHECK LIMITS, REF OR NRC 66531-0200-0114. REPAIRED CORRODED CUSP WEB AT BS 470, RBL 56 IAW SRM 53-00-55, FIG 207.Apr 4, 2016 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016040400111Support Fitting · corrodedWING TO BS 832 LOWER END OF SUPPORT FAIRING CORRODED. LT SIDE, ON EXISTENT REPAIR. REMOVED CORROSION AT WING TO BS 832 LOWER END OF SUPPORT FAIRING LT SIDE ON EXISTENT REPAIR, FOUND 100 PERCENT TO BE OUT OF LIMITS IAW SRM 53-00-00 AND R & R PREVIOUS REPAIR IApr 4, 2016 · N478HA · Boeing 717200 · Fuselage, Wing Attach FittingsSDR DALA2016040602652Longeron · corrodedLONGERON 30 IN BS 908-960 HAS SEVERAL AREAS OF CORROSION. BLENDED CORROSION FROM BS 908-960, L30 IN AFT CARGO IAW SRM 53-00-05, REPAIR 3. THICKNESS CHECK PERFORMED IAW NTSPM 04-00-07, ORIGINAL THICKNESS .125, .093 LEG, REMAINING THICKNESS ON LEG AT BS 954 ISApr 4, 2016 · N956AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR HALA2016040400101Pseu · malfunctionedWHEN LANDING GEAR EXTENDED, INDICATORS REMAINED 3 RED. RECYCLED, THEN 3 GREEN. COMPLIED WITH OPS TEST OF LANDING GEAR POSITION INDICATOR IAW AMM 32-61-06-700-801. PENDING FUNCTIONAL TEST OF MAIN AND NLG EXTENSION AND RETRACTION. ACCOMPLISHED FUNCTIONAL TESTApr 4, 2016 · N489HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR DALA2016040502568Cusp Web · corrodedRIGHT CUSP WEB BS 389-503 UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW CUSP WEB IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05.Apr 4, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016040502567Cusp Web · corrodedLEFT OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4.Apr 4, 2016 · N894AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016033102497Longeron · corrodedLONGERON 30, FROM BS 974 TO 1003 CORRODED ALSO ADDITIONAL AREAS OF CORROSION FOUND ON LONGERON 30, FROM BS 927 TO 974. CLEANED, INSPECTED, AND BLENDED ALL AREAS OF CORROSION IAW SRM 53-00-00. NOMINAL THICKNESS FOUND WAS .125 FOUND WAS .074 ALL AREAS WERE BLEMar 31, 2016 · N954AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016033102566Skin · dentedDENT ON RUDDER TAB L/H SIDE, 33" FROM LOWER EDGE AND 5" FROM AFT EDGE. CUT OUT DAMAGED AREA IN RUDDER TAB LT SIDE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01.Mar 30, 2016 · N987DN · Boeing 717200 · Rudder, Tab StructureSDR DALA2016033102565Skin · dentedDENT ON RUDDER TAB RT SIDE, 35" FROM LOWER EDGE AND 6.5" FROM AFT EDGE. CUTOUT DAMAGED AREA ON RUDDER TAB RT SIDE 35" FROM LOWER EDGE AND ACCOMPLISHED A HOT BOND DOUBLER REPAIR IAW SRM 55-41-01, REPAIR 1 AND TC 2000-8149-04.Mar 30, 2016 · N987DN · Boeing 717200 · Rudder, Tab StructureSDR 2016F00094Skin · delaminatedDURING NON ROUTINE MAINTENANCE, CHECK SPOILER FOUND DELAMINATED.Mar 30, 2016 · N998AT · Boeing 717200 · SpoilersSDR DALA2017033003179Skin · damagedDURING ATG4 MODIFICATION, MAINTENANCE NOTED THAT ALL FIVE HOLES COMMON TO THE SKIN OF THE SHEAR TIE WERE DAMAGED AND DID NOT PASS NDT INSPECTION. REPAIRED IAW ER/A 00-545433.Mar 29, 2016 · N975AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2016032800107Spar · crackedLT WING AFT SPAR CRACKED AT XR 5324 INSIDE OF FUEL TANK ACCESS PANEL 520HB. REPAIRED THE SPAR IAW PRI EA 16126- P1 AND FINAL EA 16126, REV IR AND E105-478280-PERM.Mar 28, 2016 · N478HA · Boeing 717200 · Wing SparSDR DALA2016032902390Spar · corrodedLEFT CENTER TANK UPPER REAR SPAR CORRODED AT XCW 13, 18, 52, & 59L. CORROSION ON UPPER CENTER TANK WAS REPAIRED IAW ER/A 543586-14, FASTENER HOLES DAMAGED COMMON TO CORROSION BLENDOUT AREA. WERE REPAIRED IAW PRI, REV 3, 543589-14 AND ER/A 543589-14, REV ORIGMar 28, 2016 · N894AT · Boeing 717200 · Wing SparSDR DALA2016032802330Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS IN ROWS 1-14 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Mar 28, 2016 · N985AT · Boeing 717200 · Emergency LightingSDR DALA2016032802331Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY EXIT LIGHTING AT ROW 19 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Mar 26, 2016 · N951AT · Boeing 717200 · Emergency LightingSDR DALA2016032702329Skin · crackedBS 1087 ABOVE STRINGER 14R, SKIN HAS A 2 DIRECTIONAL CRACK, VERTICAL LEG .5" & HORIZONAL LEG .1250". HFEC VERIFIED IAW NDT SPM 06-10-01.001 REQUEST ENGINEERING DISPOSITION. REPAIRED CRACK AT BS 1087, 514R IAW ER/A 543584-14 ASSOCIATED ER/A 00-543584 ADDED Mar 26, 2016 · N894AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016040502569Structure · not reportedPERFORMED DETAIL VISUAL INSPECTION OF LT AND RT CUSP WEB TO TOP OF SKIN ATTACH ANGLE FROM FS 157 TO 1022. REPLACED AT CUSP WEB FS 655 TO FS 737 IAW SRM 51-41-02, REPAIR RT CUSP WEB IN SEVERAL LOCATIONS IAW SRM 53-00-85, REPAIR NR 4.Mar 25, 2016 · N954AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016032402269Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Mar 24, 2016 · N972AT · Boeing 717200 · Emergency LightingSDR HALA2016032300110Fitting · corrodedWING TO BS 832 FITTING ON LONGERON 30 CORRODED. REMOVED CORROSION AT WING TO BODY BS 832 FITTING ON LONGERON 30 ORIGINAL MATERIAL 125" REMAINING .098" AND LOSS OF .027", FOUND OUT OF LIMITS IAW SRM 53-00-00. R & R FITTING IAW DWG 5971098, REV E AND DWG S1440Mar 23, 2016 · N478HA · Boeing 717200 · Fuselage, Wing Attach FittingsSDR HALA2016032200109Fitting · corrodedLT WING FLAP INBD FLAP TRACK FITTING CORRODED. REMOVED CORROSION ON L/W FLAP INBD FLAP TRACK FITTING EDGE DAMAGED. REMOVED OVER .100, OUT OF LIMITES IAW SRM 57-00-00 R & R FITTING IAW MM-57-55-25.Mar 22, 2016 · N478HA · Boeing 717200 · Trailing Edge FlapsSDR DALA2016032202625Floorboard · delaminatedMAIN CABIN FLOORBOARD 222YF IS DELAMINATED WITH 2 EA DAMAGED STIFFENERS AND 1 EACH COVER DAMAGED. MAIN CABIN FLOORBOARD FOUND TO BE 50 PERCENT DELAMINATED AND OUT OF LIMITS IAW SRM 53-20-50 ALLOWABLE DAMAGE 1. FABRICATED NEW FLOORBOARD IAW SRM 51-41-08, 51-4Mar 22, 2016 · N987DN · Boeing 717200 · Fuselage Floor Panel
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