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 DALA2017072405666Longeron · crackedCRACKED LONGERON 6L AT BS 1022. THE LONGERON WAS REPAIRED IAW SRM.Jul 24, 2017 · N951AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017072405665Skin · crackedCRACK ON FUSELAGE SKIN NEAR TO AFT HINGE OF LT AFT NLG DOOR. SKIN WAS REPAIRED IAW SRM.Jul 23, 2017 · N951AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017072405664Door Frame · crackedCRACKED NLG DOOR FRAME AT BS 47 LONGERON 27L AND 27R. NLG DOOR FRAME WAS REPAIRED IAW SRM.Jul 23, 2017 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017072305671Sign · detachedMID CENTER EXIT SIGN. BACKSIDE COVER HAS FALLEN OFF. INSTALLED THE COVER.Jul 22, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017072305661Support · corrodedCORROSION ON SUPPORTS OF R1 EMERGENCY SLIDE BETWEEN BS 148 TO 218 AT PAX CABIN. THE SUPPORTS WERE REPLACED IAW SRM.Jul 22, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072305660Former · crackedCRACKED LT AND RT FORMERS ON BS 679 KEEL BEAM AREA. THE FORMERS WERE REPAIRED IAW SRM.Jul 22, 2017 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017072305659Former · crackedCRACKED LT AND RT FORMERS BS 694 KEEL BEAM AREA. THE FORMERS WERE REPAIRED IAW SRM.Jul 22, 2017 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017072305658Former · crackedCRACKED RT FORMER ON BS 715 KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM.Jul 22, 2017 · N951AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017072305657Beam · crackedCRACKED BEAM NR 4 ON FWD EDGE AT FWD SERVICE DOOR R1. THE BEAM WAS REPLACED IAW SRM.Jul 22, 2017 · N951AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017072205656Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 387 BETWEEN RBL 54 TO 60. REPAIRED.Jul 21, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072205655Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 419 BETWEEN RBL 54 TO 60. RT CUSP WEB WAS REPAIRED.Jul 21, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072205654Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 472 BETWEEN RBL 54 TO 60. RT CUSP WEB WAS REPAIRED.Jul 21, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072105580Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=401 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. DAMAGE ON RT CUSP WEB STA Y=401 BETWEEN X=-54 TO X=-60 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 219 AND SRM 51-41-02-OG.Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072105579Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=430 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. RT CUSP WEB STA Y=430 WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 219.Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072105578Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=488 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 216.Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072105577Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=348 BETWEEN X=-54 TO X=-60 IN REFERENCE OF NRC 435. CUSP WEB WAS REPAIRED PER SRM 53-00-55-23R-4.Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072105576Attach Fitting · corrodedCORROSION ON RT GRILL CLIPS ABOVE CUSP WEB MEMBRANE BTW STA Y=484 TO Y=503 (2E/A), Y=517 TO Y=527 (2E/A), Y=572 (1E/A), Y=660 TO Y=679 (2E/A), AND Y=920 (1E/A) X=60 IN REF 5300-2020 (CPAX). CLIPS WERE REPLACED PER SRM 51-41-02-0G AND DWG 5913698 REV "K".Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017072005564Cusp Web · corrodedCORROSION ON LH CUSP WEB MEMBRANE UPPER/LOWER SURFACE STA Y=865 BTW X=54 TO X=60. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R FIG 215.Jul 20, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072405670Blower · failedAT GATE PRIOR TO PUSH BACK, A STRONG ELECTRICAL ODOR EMANATED FROM THE AFT LAVATORY AREA IN THE CABIN. MAINTENANCE FOUND THE LAVATORY BLOWER MOTOR CIRCUIT BREAKER HAD TRIPPED OPEN. MAINTENANCE REPLACED THE LAVATORY WASTE VENT SYSTEM BLOWER.Jul 19, 2017 · N919AT · Boeing 717200 · Waste Disposal SystemSDR DALA2017072005563Cusp Web · corrodedCORROSION ON LT CUSP WEB MEMBRANE UPPER/LOWER SURFACE STA Y=842 BTW X=54 TO X=60. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R FIG 216.Jul 19, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017072005562Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCESS PLATES 520CT AND 520FT. ACCESS PLATE 520CT AND 520FT ARE OUT OF LIMITS AND WERE REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.Jul 19, 2017 · N951AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017072005561Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK ON FUEL TANK ACCES PLATE 620CT. ACCESS PLATE 620CT WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR. 5.Jul 19, 2017 · N951AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017072005560Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL TANK ACCESS PLATE 620DT. DUE TO EXCESSIVE DAMAGE BY CORROSION, ACCESS PLATES 620DT IS OUT OF LIMITS. NOT ALLOWED MORE THAN 2 ADJACENTS REPAIRS BUSHINGS AND MAXIMUM 6 PER ACCESS AND FUEL ACCESS PLATE 620DT WAS REPLACED PER SRM 5Jul 19, 2017 · N951AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017072005559Attach Fitting · corrodedCORROSION ON LT GRILL CLIPS ABOVE CUSP WEB MEMBRANE BTW STA Y=313 TO Y=503 (4E/A), Y=541 TO Y=560 (2E/A), Y=589 TO Y=617 (2E/A), Y=636 TO Y=674 (3E/A), AND Y=908 TO Y=927 (2/EA) X=60 IN REF 5300-2020. CLIPS WERE REPLACED PER SRM 51-41-05-0G, 51-41-02-0G, AND DJul 19, 2017 · N951AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017071905528Web · crackedCRACKED WEB ON L1 DOOR OM LONG L11. WEB ON LT DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1 FIGURE 201.Jul 18, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017071905527Structure · wornWORN ON LOWER INTERNAL STRUCTURE RT CORNER AT AFT CABIN EMERGENCY EXIT VENTRAL DOOR. WORN ON LOWER INTERNAL STRUCTURE RT CORNER AT AFT CABIN EMERGENCY EXIT VENTRAL DOOR WAS REPAIRED PER SRM 52-10-02-2R REP 16 OPTION 3.Jul 18, 2017 · N951AT · Boeing 717200 · Emergency ExitsSDR DALA2017071805526Pan · crackedCRACKED PAN ON UPPER FWD. PASSENGER ENTRANCE DOOR L1. PAN ON UPPER FWD WAS REPAIRED PER SRM 52-10-02 REPAIR 3 FIG 201.Jul 17, 2017 · N951AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017071705456Power Supply · malfunctionedAFT EMERGENCY EXIT LIGHT FLICKERING / INTERMITTENT. REPLACED AFT OVERHEAD POWER SUPPLY AND BATTERY PACKS. OPS CHECKED GOOD IAW AMM 33-54.Jul 16, 2017 · N937AT · Boeing 717200 · Emergency LightingSDR DALA2017071605558Floor Panel · damagedDAMAGE FLOOR PANELS 211ANF, 211ASF, 211ATF, 211GF, AND 211MF. FLOOR PANEL 211 ANF WAS FABRICATED AND FLOOR PANEL 211 ASF AND 211 ATF WERE REPAIRED PER SRM 53-20-50. FLOOR PANELS 211ANF, 211ASF, 211ATF WERE INSTALLED ON 2040-0057 AND THE COVERS ON COCKPIT FLOORJul 15, 2017 · N951AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017071705455Battery Pack · inoperativeNO POWER SUPPLY TO FWD CEILING EMERGENCY LIGHTS. REPLACED EMERGENCY LIGHT BATTERY PACK B5 227 IAW AMM 33-51-03. OPS CHECKED GOOD. EMERGENCY LIGHTS ON CEILING OPS OK FOR SERVICE.Jul 15, 2017 · N954AT · Boeing 717200 · Emergency LightingSDR DALA2017071605454Spar Cap · distressedDISTRESS AT LT & RT SIDES OF VERTICAL STABILIZER LE SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017071605453Spar Cap · cracked0.5 INCH CRACK WAS FOUND ON VERTICAL STAB. FRONT SPAR CAP RT SIDE. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017071605452Spar Cap · damagedELONGATED HOLES AT THE LT & RT SIDES OF VERTICAL STABILIZER L.E. FRONT SPAR CAP. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017071605451Fairing · damagedDURING INSPECTION, AN ELONGATED HOLE ON THE LE REMOVABLE FAIRNG LT SIDE WAS FOUND. REPAIRED IAW ETI-17-17-084, REV 3, AND ER/A 559503-14AD, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Vertical StabilizerSDR DALA2017071605450Angle · crackedCRACKED ANGLE ON AFT/LOWER CORNER OF RT WINDOW RING PAN BS 986. THE ANGLE WAS REPLACED IAW SRM 56-20-02-2R-1, AND DWG 3914137, REV C.Jul 15, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017071605449Floorbeam · corrodedCORROSION ON FLOORBEAM BS 200, RBL 5 AND BTW RBL 46 TO RBL 56. REPLACED IAW SRM 51-41-02-0G, AND SRM 51-41-05-0G.Jul 15, 2017 · N951AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017071605448Web · crackedCRACKED WEB LOWER SURFACE BETWEEN BS 176 AND RBL 57 IN THE E & E BAY. REPAIRED IAW SRM 53-00-00-2R, 51-41-02-0G, AND 51-41-05-0G.Jul 15, 2017 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017071605447Frame · crackedCRACKED FRAME BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017071605446Frame · crackedCRACKED FRAME BS 1022 ON LONGERON 7L AT PASSENGER CABIN AREA. REPAIRED IAW ETI 17-17-083, REV 1, AND ER/A 559502-14, REV ORIGINAL.Jul 15, 2017 · N982AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017071605445Access Door · damagedRT SIDE OF ACFT DAMAGED AROUND RIGHT THRUST REVERSER HCU ACCESS DOOR. REPAIRED THE DOOR IAW ER/A 556431-14, REV. ORIGINAL.Jul 15, 2017 · N994AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017071605444Longeron · crackedLONGERON 22R AT BS 1074 IS CRACKED, REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 2.Jul 15, 2017 · N994AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017071605443Doubler · crackedTHRUST REVERSER HCU ACCESS DOOR INTERNAL DOUBLER CRACKED, BS 1074 LONGERON 22R, . NO WORK ACCOMPLISHED ON THIS NON-ROUTINE CARD. THIS NON-ROUTINE WRITTEN FOR SDR TRACKING ONLY. T/R HCU ACCESS DOOR CUT OUT INTERNAL DOUBLER STA 1074 LONGERON 22RT REPAIRED ON NR-Jul 15, 2017 · N994AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017071605442Fitting · crackedCRACKED LOWER FITTING IN THE AFT CARGO COMPARTMENT. THE FITTING WAS REPLACED IAW DWG 5910157, REV CW, SRM 51-41-01, 51-41-02, AND 51-41-05.Jul 15, 2017 · N951AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017072305662Skin · damagedON ARRIVAL, FOUND A DENT AND GOUGES 28 INCHES AFT OF WATER SERVICE PANEL ON ACFT LEFT. REPAIRED IAW ER/A 560289-14.Jul 14, 2017 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2017071700189Control Cable · frayedLEFT SLAT BY WING TIP, IT'S NOT FLUSH LIKE OTHER SIDE. INSPECTED LT SLAT AND FOUND NR 5 SLAT RETRACT CABLE FRAYED. REMOVED NR 5 SLAT CABLE PER AMM 27-81-02-000-801. INSTALLED NR 5 SLAT RETRACT CABLE 194A PER AMM 27-81-02-400-801. REMOVAL AND INSTALLATION OF NRJul 14, 2017 · N479HA · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2017071505440Frame · dentedBS 1076 FRAME AT LONGERON 22R IS DENTED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME BETWEEN LONGERONS 25R TO LONGERON 19R, USING 7075 "0." 050 DIM 44"X4" IAW B717 SRM 51-40-08 AND DRW #9958239 REV AB. PART HEAT TREATED FROM "0" CONDITION TO "T6" IAW AMS 2Jul 14, 2017 · N994AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017071505439Former · crackedFRAME BS 1074 RT FORMER CRACKED BETWEEN LONGERONS 21R TO 22R. REMOVED, FABRICATED, AND INSTALLED A NEW FORMER IAW SRM 51-40-08 AND DRW #9958239 REV AB, PART HEAT TREAT FROM "0" CONDITION TO T6" IAW AMS 27-70. (LP #0117308)Jul 14, 2017 · N994AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017071505438Frame · crackedFRAME BS 1074 CRACKED BETWEEN LONGERONS 21R AND 22R. . REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-40-08, AND DWG 9958239, REV AB,Jul 14, 2017 · N994AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017071505437Longeron · crackedCRACKED LONGERON 2R BETWEEN BS 794 AND 813. LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2, 51-41-02-0G, AND 51-41-05-0G.Jul 14, 2017 · N951AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017071505436Door Frame · corrodedCORROSION ON THE LT WEB DOOR FRAME BS 200, LONGERONS 17 AND 18L REPAIRED IAW ETI-17-17-093, REV. 2 AND ER/A 559514-14 REV. ORIGINAL.Jul 14, 2017 · N982AT · Boeing 717200 · Fuselage Main, Structure
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