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"

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.

SDR DALA2016062404924Skin · puncturedFUSELAGE SKIN PUNCTURED. APPROXIMATELY 2" AFT OF FS 1087, BETWEEN L-3R AND L-4R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/May 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404923Skin · puncturedFUSELAGE PUNCTURE BETWEEN FS 1095 AND FS 1116, AT L-8R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC PER NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404922Skin · puncturedFUSELAGE SKIN GOUGE AND PUNCTURE JUST AFT OF FS 1178, L-11R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A, ER/A MATCHES ALL PRIS. CMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404921Skin · puncturedFUSELAGE SKIN PUNCTURED AT FS 1087, L-7R AND L-8R. REMOVED DAMAGE, DEBURRED. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOGMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404920Skin · gougedSEVERE GOUGE AT FS 1133 BETWEEN L-8R AND L-9R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVED MOMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404919Skin · damagedDENTS AND GOUGES BETWEEN FS 1116 AND FS 1144, BETWEEN L-7R AND L-8R, 2 EACH. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136, ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A ER/A MATCHES ALL PRIMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404918Skin · dentedDENT IN FUSELAGE AT FS 1076 BETWEEN L-7R AND L-9R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG AND REMOVEMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404917Skin · dentedMULTIPLE DENTS AT FUSELAGE STA 1087 BETWEEN L-3R AND L-7R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LOG ANDMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016062404916Skin · gougedMULTIPLE GOUGES FROM FS 1095 TO FS 1144 BETWEEN L-4R AND L-7R. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01. 001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051903994Skin · dentedFUSELAGE SKIN DENTED BETWEEN BS 1087-1116, STRINGERS 22 -23L. BLENDED AREA IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 6-10-01.001. NO CRACK NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISH UT THICKNESS IAW NDT/SPM 04-00-03. ALODINE AND PMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051903993Skin · dentedRT APU DOOR DENTED 7.0312" DEEP. ACCOMPLISHED HFEC IAW NDTSPM 06-10-01.001 NO CRACKS NOTED. ALODINE AND PRIMED.May 18, 2016 · N939AT · Boeing 717200 · Auxiliary Power Unit (APU) DoorsSDR DALA2016051903992Skin · dentedRIGHT FUSELAGE DENTED BETWEEN BS 1053-1076. STRINGERS 22-23R. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001. NO CRACKS NOTED.May 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051903991Skin · dentedRIGHT FUSELAGE DENTED AT BS 1022 - 1037, L21 - 22R. BLENDED AREA FOR HFEC. IAW SRM 53-01-01. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ACCOMPLISHED UT THICKNESS OF AREA IAW NDTSPM 04-00-03.May 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051904046Skin · dentedLT FUSELAGE DENT 3" X 2", .0937" DEEP. BS 1159, STR 20-21L. BLENDED IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACKS NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISHED UT INSPECTION IAW NDT/SPM 04-00-03. ALODINE AND PRIMED; May 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051904044Skin · gougedLEFT FUSELAGE GOUGE, DENT 3" X 2.5" X .1250" DEEP BETWEEN BS 1076-1087, STR 20L. DURING CLEAN-UP OF GOUGE NOTICED RIVET SHEARED. REMOVED REMAINING FASTENER. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACK NOTED. ACCOMPLISHED GVI WITH NO VISABLE DAMAGE NOMay 18, 2016 · N939AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051904036Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 100 AND LONGERON 28R. FUSELAGE SKIN WAS PERFORMED IAW SRM 53-10-01, FIG 201.May 18, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2016051900200Downlock Sensor · failedWHEN RAISING GEAR LT MAIN INDICATED UNSAFE, RED. DID NOT FEEL ANY TURBULENCE WHEN UNSAFE INDICATION WAS ON. R & R LT MAIN GEAR DOWN/LOCKED PROXIMITY SENSORS IAW AMM 32-61-04 OPERATIONAL CHECK OK. GEAR SWING PENDING. ACCOMPLISHED FUNTIONAL TEST OF THE LANDIMay 18, 2016 · N484HA · Boeing 717200 · Landing Gear Position and WarningSDR 2016FA0000250Position Sensor · failedLEFT GEAR UNSAFE LIGHT WITH GEAR HANDLE IN UP POSITION. REPLACED SENSOR LINK & CHECK ADJUSTMENT OF LT MLG GEAR UP & LATCHED PROXIMITY SENSOR. GND OPERATIONS CHECK OK IAW AMM 32-61-00.May 18, 2016 · N484HA · Boeing 717200 · Landing Gear Position and WarningSDR DALA2016052004040Shear Tie · crackedBS 1022, BELOW LONGERON 14R FOUND SHEAR TIE CRACKED DURING INSPECTION WITH ORN 66647-200-0049. REPLACED SHEAR TIE IAW SRM 51-41-05, PARA 2.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016052004037Former · crackedLOWER FUSELAGE, LT FILLET, BS 674-L27L, CRACKED STR IN BOX. MARKED ON OUTSIDE. REPAIRED FORMER BS 674, L27L IAW ER/A 545672-14, REV 0. ASSOCIATED ER/A 54-567214 ADDED FOR AC 9516.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016051803990Cusp Web · crackedCUSP WEB CRACKED AT BS 813. REPAIRED THE CUSP WEB IAW SRM 53-00-55, REPAIR 4, FIG 216.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051803988Skin · crackedSTA 1037 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051803987Skin · crackedBS 1037, ABOVE LONGERON 14L EXTERNAL SKIN CRACKED, HFEC VERIFIED. CUTOUT CRACKED SKIN AND INSTALLED REPAIR IAW PRI 545670-14, REV 3 AND ER/A 545670-14.May 17, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051703986Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING BY THE FIRST CLASS LAVATORY HAD FAILED. MAINTENANCE REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE OPS CHECK WAS GOOD.May 17, 2016 · N950AT · Boeing 717200 · Emergency LightingSDR DALA2016052004047Structure · damagedLT ENGINE LOWER APRON DAMAGED AFT EDGE 3" X .5". REPLACED LT ENGINE FIXED COWLING APRON IAW AMM 71-14-01-400-801.May 16, 2016 · N939AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR HALA2016051400247Seat Track · damagedMAIN CABIN SEAT TRACK HAS SCRATCHES AND GOUGES BETWEEN STA 646-823, RBL 22. BLENDED OUT SCRATCHES AND GOUGES AT MAIN CABIN SEAT TRACK BETWEEN STA 646-823, RBL 22. NDT AREA IAW NDT SPM PT4 04-00-07, ORIGINAL MST .100 WITH MST LOSS OF .042, MST REMAINING .58, May 14, 2016 · N480HA · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2016051400249Tab · crackedMAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.May 14, 2016 · N480HA · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2016051400248Tab · crackedMAIN CABIN TAB CRACKED ON DOOR SURROUNDED INNER SKIN AT STA 210, LONG 15L, CRACK IS 1" LONG. REMOVED DAMAGED TAB ON INNER SKIN AT FS 210 AND REPAIRED IAW SRM 53-10-15-2R-1, REPAIR 1.May 14, 2016 · N480HA · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051503930Skin · delaminatedDELAMINATED RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214. RT WING INBD SPOILER UPPER SURFACE BETWEEN BS XRS 189-214 WAS REPAIRED IAW SRM 51-70-02, REPAIR 3. RT WING INBD SPOILER, PANEL WAS REMOVED AND INSTALLED TO FACILITATE OTHER ACTIVITIES IAWMay 14, 2016 · N919AT · Boeing 717200 · SpoilersSDR DALA2016051503929Frame · crackedCRACKED FRAME ANGLE BS 1087 BTW LONGERONS 13-14R AT AFT ACCESSORIES COMPARTMENT. FRAME ANGLE WAS REPLACED IAW AMM 21-22-01, 21-51-04, SRM 51-41-02, 51-41-05, DWG 9971140, REV F.May 14, 2016 · N919AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2016051300245Pan · corrodedFUSE AFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION. REPAIRED PAN AT AFT CARGO COMPARTMENT LOWER DOOR, BS 974 TO 954 IAW SRM 53-20-15-2R-7, REPAIR 7. REMOVED DAMAGE AFT CARGO DOOR LOWER DOOR PAN IAW SRM 51-40-07, REMOVED 2 EA STRAPS FORMay 13, 2016 · N480HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052104173Structure · crackedLOWER FUSELAGE, RT FILLET, BS 696 STRINGER 27R, CRACKED STRINGER END. REPAIRED DAMAGED FORMER AT BS 696-L27R IAW ERA 545672-14.May 13, 2016 · N957AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016051603931Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.May 13, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR HALA2016051300182Pan · corrodedAFT CARGO COMPARTMENT LOWER DOOR PAN BS 974 HAS EXFOLIATED CORROSION.May 13, 2016 · N480HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016051200246Support · corrodedCORROSION ON FALSE TRACK STA 1002, RBL 18. REMOVED -65 AND -67 SUPPORTS IAW SRM 51-41-01. REMOVED CORROSION FROM SUPPORTS, -65 SUPPORT WITHIN LIMITS, -67 SUPPORT OUT OF LIMITS IAW SRM 53-00-00, FIG 103. REINSTALLED -65 SUPPORT AND NEW -67 SUPPORT IAW SRM 5May 12, 2016 · N480HA · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016052004041Cusp Web · corrodedLEFT CUSP WEB CORRODED AT BS 446 - 927. BLENDED CORRODED AREAS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-55, FIG 101.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051603959Pin · misinstalledTHE TAILCONE FAILED TO DEPLOY DURING ROUTINE DROP TEST. MAINTENANCE DISCOVERED THAT THE RELEASE LATCH T-PIN NR 12 FOR THE TAILCONE WAS NOT PROPERLY ENGAGED. THE T-PIN WAS REENGAGED AS DESIGNED AND IN COMPLIANCE WITH AMDS 5352-2001 THE SYSTEM WAS RIGGED TO SPEMay 12, 2016 · N906AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016051603958Cable · damagedMAINTENANCE DISCOVERED THAT THE TAILCONE EMERGENCY RELEASE KEVLAR CABLE WAS DAMAGED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.May 12, 2016 · N939AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016051303918Cusp Web · crackedCUSP WEB CRACKED AT BS 813 RIGHT. REPAIRED CUSP WEB AT FS 813 BY REMOVING DAMAGE AND INSTALLING A DOUBLER IAW SRM 53-00-55, REPAIR 4, FIG 216.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051303917Seat Track · corrodedF/O'S AFT OTBD SEAT TRACK IS CORRODED IN SEVERAL PLACES. REPLACED F/O AFT SEAT TRACK IAW SRM 51-41-01, PARA 2 DUE TO PART BEING CORRODED OUT OF LIMITS.May 12, 2016 · N957AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016051303915Skin · crackedSKIN CRACKED AT APPROXIMATELY FS 1095 AND APPROX 6" ABOVE RT PYLON-M. REPAIRED SKIN CRACK AT FS 1095 IAW ER/A 54669-14. SRM 51-40-05, PG 1 IDENTIFY REPAIRED IAW ER/A 54669-14. ASSOCIATED ER/A 54-566914 ADDED FOR AC 9516.May 12, 2016 · N957AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051303914Skin · corrodedUPPER WING TO CENTER TANK PLANK ON FORWARD BULKHEAD CORRODED FROM BL0 TO RBL 58. REPAIRED UPPER CENTER TANK PLANK SKIN IAW ER/A 545622-14, REV A.May 12, 2016 · N924AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051203891Intercostal · crackedINTERCOSTAL CRACKED IN FWD CARGO CEILING AT BL 0, BS 636. REPAIRED DAMAGED INTERCOSTAL AT BS 636, BL-0 IAW SRM 53-00-00, REPAIR 1.May 11, 2016 · N957AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016051203888Skin · canningDENT WITH OIL CAN EFFECT ON EXTERNAL FUSELAGE, SKIN BS 1189 CANT TO 1200 CANT BETWEEN 6-7 O'CLOCK POSITION, SM, FS. FUSELAGE SKIN WAS REPAIRED IAW ER/A 545165-14, REV ORIGINAL.May 11, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051203887Bearing · wornFREEPLAY ON AILERON SECTOR BUSS AT LT WING. FREE PLAY ON AILERON SECTOR BUS WAS CORRECTED BY REPLACING BEARING ON BUS SECTOR IAW CMM 27-10-16. RII COMPLETED BY INSPECTION.May 11, 2016 · N919AT · Boeing 717200 · Aileron Control SystemSDR HALA2016051100178Latch · looseRIGHT GEAR UNSAFE LIGHT AFTER GEAR RETRACTION. FOUND THAT MLG LATCH WAS LOOSE. REPLACED 4 BOLTS, RESECURED BOLTS IAW AMM 32-34-01 ACCOMPLISHED DOOR LATCH AJUSTMENT IAW AMM 52-34-01-820-801, UP TO STEPS 2 D,1,F. ACCOMPLISHED 2 D, 2 TO 2 E, 2, OPS CHECK GOOD.May 11, 2016 · N487HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR HALA2016051000248Doubler · crackedCRACK ON GROUND CONDITION AIR ACCESS DOOR LANDING, FWD INBD CORNER AND AFT INBD CORNER. R & R CRACKED DOUBLER AT GROUND CONDITIONED AIR ACCESS DOOR LANDING IAW DWG 5911429, REV 02 AND SRM 51-41-02, LEAK CHECK GOOD IAW AMM 21-22-07.May 10, 2016 · N480HA · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016051203890Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON LT WING FUEL ACCESS PANEL. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PANEL REPLACED IAW SRM 57-10-01 UNDER CONDITION III.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016051203889Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON RT WING FUEL ACCESS PLATE NR 620CB AND 620EB IN REF ORNRC 48, ZONE 000, CARD 53, ZONE 000. DUE TO CORROSION OUT OF LIMITS FUEL ACCESS PLATE NR 620CB AND 620EB WERE REPLACED IAW SRM 57-10-01 UNDER CONDITION III.May 10, 2016 · N919AT · Boeing 717200 · Wing, Plate/SkinSDR HALA2016051000176Tire · failedRIGHT OTBD TIRE, NR 4, TREAD SEPARATED. VERIFIED TIRE PRESSURE PRIOR TO REMOVAL, FOUND AT 185 PSI, TIRE WARM. R & R NR 4 MAIN WHEEL AND TIRE ASSY IAW AMM 32-41-01, SPIN CHECKED GOOD. FOUND SMALL DENT IN THE RT INLET ACOUSTIC PANEL APPROXIMATELY 6" OTBD OF PMay 10, 2016 · N484HA · Boeing 717200 · Tire
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