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 DALA2017091506899Tab · wornWEAR ON UPPER CORNER AT RUDDER TAB. THE RUDDER TAB WAS REPAIRED IAW SRM 55-41-01-2R-1, REPAIR 1, AND JIC 5464417.Sep 14, 2017 · N991AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2017091506898Cargo Track · corrodedCORROSION ON LT AND RT FWD AND AFT CARGO TRACK IN THE AFT CARGO BAY. THE CARGO TRACKS WERE REPLACED IAW SRM 51-41-01-0G, AND 51-41-02-0G.Sep 14, 2017 · N990AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017091506897Door Frame · corrodedCORROSION ON AFT LOWER CARGO DOOR FRAME. THE SECTION OF THE DOOR FRAME AND REPAIR SPLICE WERE REPLACED IAW SRM 53-20-15-2R-7.Sep 14, 2017 · N990AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017091406884Gusset · corrodedCORROSION ON GUSSETS ABOVE CARGO DOOR FRAME WEB. THE GUSSET WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-05-0G, AND DWG 5913537, REV D.Sep 14, 2017 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017091406883Longeron · corrodedCORROSION ON LONGERON 30, BS 927 TO 946 FOUND TO BE OUT OF LIMITS. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Sep 13, 2017 · N989AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017091406882Skin · corrodedCORROSION ON UPPER SKIN BS 727 TO 756. REPAIRED IAW ETI-17-17-162 R1 AND ER/A 560922-14, REV ORIGINAL.Sep 13, 2017 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017091406881Frame Splice · corrodedCORROSION ON FRAME CAP SPLICE, BS 946 BETWEEN LONGERONS 27L TO 28L. THE FRAME SPLICE WAS REPLACED IAW DWG 9919603, REV CC, AND SRM 51-41-05-0G.Sep 13, 2017 · N990AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017091406880Tab · stuckDURING RUDDER INSTALLATION, RUDDER CONTROL TAB WAS STRUCK ON RT SIDE.Sep 13, 2017 · N991AT · Boeing 717200 · Rudder, Plate/SkinSDR DALA2017091306859Floor Panel · damagedDAMAGE PAX CABIN FLOOR PANELS #220F, 221AF, 221CF, 221DF, 221EF, 221FF, 221KF, 221LF, 221QF, 222ABF, 222ACF, 222QF, 210F, 211AMF, 211ANF, 211ASF, AND 211ATF. (CPAX). NRC 00418: FLOOR PANEL #220F AND 210F DO NOT EXIST. THESE ARE IN ERROR IN TEXT DESCRIPTION. FSep 12, 2017 · N989AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017091306858Tab · debondedDEBONDED AILERON TRIM TAB UPPER SURFACE XAT=12 ON THE LT WING. TRIM TAB WAS REPAIRED IAW SRM 51-70-02-2R-3, REPAIR 3.Sep 12, 2017 · N991AT · Boeing 717200 · Aileron TabsSDR DALA2017091306857Stiffener · crackedCRACK ON VERTICAL STIFFENER LOWER EDGE ON BS 813 AT AFT CARGO BAY. STIFFENER WAS REPAIRED IAW SRM 53-00-00-2R-1, FIG 201.Sep 12, 2017 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017091306856Floorbeam · crackedCRACKED FLOORBEAM AT BS 737, RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05-0G, AND 51-41-02-0G.Sep 12, 2017 · N990AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017091306855Hinge · damagedELONGATED HOLES OF AFT/FWD HINGES ON AFT CARGO DOOR (C2). THE HINGES WERE REPLACED IAW AMM 52-31-02.Sep 12, 2017 · N990AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017091206829Battery Pack · dischargedON SERVICE CHECK MAINTENANCE FOUND THAT THE EXIT SIGN OVER BOTH LT AND RT AFT OVERWING EXITS DO NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK AT POWER SUPPLY B5-230 PER AMM 33-51. THE OPERATIONAL CHECK WAS GOOD.Sep 12, 2017 · N966AT · Boeing 717200 · Emergency LightingSDR DALA2017091206828Doubler · corrodedEXFOLIATED CORROSION ON PRODUCTION DOUBLER P/N 9915561-73 OF AFT PRESSURE BULKHEAD LWR AREA. CORROSION LEVEL 2. PRODUCTION DOUBLER P/N 9915561-73 WAS REPLACED PER SRM 51-41-02 AND SRM 51-41-05.Sep 12, 2017 · N991AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2017091206827Angle · corrodedCORROSION ON CUSP ANGLE BELOW FORWARD GALLEY SERVICE DOOR JAMB FROM STA Y= 159 TO Y= 208. CORROSION LEVEL 2 ON CUSP ANGLE BELOW FWD GALLEY SERVICE DOOR FROM STA Y=159 TO Y=208 WAS REPAIRED PER ETI-17-17-144 REV 2 AND ER/A 560881-14 REV ORIGINAL.Sep 11, 2017 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017091106826Finger Doubler · corrodedCORROSION ON FINGER DOUBLER BTW STA Y=937 TO Y=943 BTW LONG 25R TO 26R AT AFT CARGO COMPARTMENT IN REF NRC S/N 00321 (CCT). CORROSION LEVEL 2. FINGER DOUBLER SECTION Y=937 TO 943 WAS REPLACED PER SRM 51-41-02-0G AND DWG 5911424 REV CZ.Sep 11, 2017 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017091106825Skin · crackedCRACK ON FUSELAGE SKIN STA Y=1076 LONG 14L. FUSELAGE SKIN STA Y=1076 LONG 14L WAS REPAIRED (PERMANENT REPAIR) PER ER/A 560880-14 REV ORIGINAL AND ETI-17-17-143 REV 2.Sep 10, 2017 · N990AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017091106824Skin · corrodedCORROSION ON CENTER WING UPPER SKIN PLATE RT SIDE FROM STA Y 664 TO Y 715 BTW XCW 43 AND XCW 58. CORROSION LEVEL 2. CENTER WING UPPER SKIN PLATE RT WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI 17-17-151 REV 1 AND AREAS WHITIN LIMITS WSep 10, 2017 · N990AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017091106823Skin · corrodedSEVERAL CORROSION POINTS ON CENTER WING UPPER SKIN PLATE BTW Y=660 AND Y=756, BTW X=22 AND X=26, ALSO ON Y=750 BTW X=22 AND X=44. CORROSION LEVEL 2. CENTER WING UPPER SKIN PLATE WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI-17-17-151 RSep 10, 2017 · N990AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017091106822Skin · corrodedCORROSION ON CENTER WING UPPER SKIN PLATE RT SIDE REF STA Y 746, BTW XCW 22 TO XCW 49. CORROSION LEVEL 2. CENTER WING UPPER SKIN WAS REPAIRED (AS-IS CONDITION) PER ER/A 560894-14 REV ORIGINAL AND ETI-17-17-151 REV 1.Sep 10, 2017 · N990AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017091006820Rub Strip · corrodedCORROSION AND DISBONDED LT RUB STRIP ON SETTLEMENT AREA AF FILLET FUSELAGE PANELS. THE RUB STRIP WAS REPLACED IAW SRM 53-20-70-01 AND SRM 51-20-05.Sep 9, 2017 · N989AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017091006819Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 - 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.Sep 9, 2017 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017091006812Floor Panel · crackedCRACKED COCKPIT FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R, REP 3, AND INSTALLED IAW CARD 2040-0058.Sep 9, 2017 · N991AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017091006811Intercostal · crackedCRACKED INTERCOSTAL BS 636, BL 0 ON CEILING AREA AT FWD CARGO COMPARTMENT. THE INTERCOSTLE WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.Sep 9, 2017 · N961AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017091006810Cusp Web · crackedCRACKED CUSP WEB BS 889 TO 908, BETWEEN LBL 56 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 2R-4, FIG 226.Sep 9, 2017 · N991AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017091006809Skin · corrodedCORROSION ON UPPER RT WING SKIN AFT EDGE BETWEEN XCW -22 TO XCW -58 ON THE RT MLG WHEEL WELL. REPAIRED IAW ETI-17-17-151, REV 1, AND ER/A 560894-14, REV ORIGINAL.Sep 9, 2017 · N990AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017091006807Skin · debondedDISBONDED UPPER SKIN OF INBD SPOILER PANEL XRS 220, LT WING. THE SPOILER PANEL WAS REPAIRED IAW ETI-17-17-154, REV ORIGINAL, ER/A 560897-14, REV ORIGINAL, AND JIC CARD 2000-8149-01.Sep 9, 2017 · N989AT · Boeing 717200 · SpoilersSDR DALA2017091006806Access Panel · crackedCRACK ON ACCESS PANEL 211GR. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-70-11-2R, FIG 201.Sep 9, 2017 · N989AT · Boeing 717200 · Fuselage Structure (General)SDR DALA2017091006805Splice · corrodedCORRODED LOWER SEAL DEPRESOR SPLICES AT FWD CARGO DOOR FRAME. THE SEAL DEPRESSOR SPLICES WERE REPLACED IAW SRM 53-20-15-0I-1, FIG 1, SHEET 2, AND 51-41-02-0G.Sep 9, 2017 · N990AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017090906797Frame · crackedCRACKED RH FRAMES STA Y=679, Y=694, AND Y=715 AT CANTED KEEL AREA. (FUS). NRC 00364: FRAMES WERE REPAIRED PER B717-200 SRM 51-70-11-2R. CRACKS WERE FOUND WITH FOLLOW DIMENTIONS: STA Y=679 1) 2.350", 2) 2.500"; STA Y=694 1) 2.750"; STA Y= 715 1) 1.650", 2) 0.75Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017090906796Frame · crackedCRACKED LH FRAMES STA Y=679, Y=694, AND Y=715 AT CANTED KEEL AREA. (FUS). NRC 00365: FRAMES WERE REPAIRED PER B717-200 SRM 51-70-11-2R. CRACKS WERE FOUND WITH FOLLOW DIMENTIONS: STA Y=679 1) 2.350"; STA Y=694 1) 1.370", 2) 1.350", 3) 0.800"; STA Y= 715 1) 0.7Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017090906804Cusp Web · crackedCRACKED CUSP WEB BS 674, LBL 44. THE CUSP WEB WAS REPLACED IAW SRM 53-00-55-2R-4, FIG 226.Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017090906803Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERON 13 - 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243 REV JS, SRM 51-41-05, AND SRM 51-41-02.Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017090906802Frame Angle · crackedCRACKED LT ANGLE AT BS 1022, BETWEEN LONGERONS 13 & 14L. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JV, SRM 51-41-02-0G, AND SRM 51-41-02-0G.Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017090906801Structure · damagedELONGATED HOLES ON FWD CARGO DOOR. REPAIRED IAW ETI-17-17-157, REV 2, AND ER/A 560915-14, REV ORIGINALSep 8, 2017 · N989AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017090906800Longeron · crackedCRACKED LONGERON 2R, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Sep 8, 2017 · N990AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017090906799Door Frame · crackedCRACKED DOOR FRAME LBL 46, LBL 17, AND RBL 17 AT NLG WHELL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, REPAIR 2, FIG 201.Sep 8, 2017 · N990AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017090906798Longeron · crackedCRACK ON LONGERON 3R, BS 1144. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Sep 8, 2017 · N990AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017090906795Floor Panel · delaminatedDELAMINATED FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R, REP 3.Sep 8, 2017 · N990AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017090906794Pan · wornWORN PAN ON ATTENDANT`S SEAT AREA AT AFT CABIN DOOR. THE PAN WAS REPAIRED SRM 52-10-02-2R-15 AND THE ANGLE WAS REPAIRED IAW ER/A 560896-14, REV ORIGINAL AND ETI-17-17-153 REV ORIGINAL.Sep 8, 2017 · N989AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017090806792Angle · corrodedCORROSION ON THE ANGLE OF THE RT CONSOLE FROM BS 137 TO 157 BETWEEN RBL 44 TO 54. NEW ANGLE WAS REPLACED PER B-717-200 DWG #9936533 REV. CM, SRM 51-41-01 AND SRM 51-41-02. (LP #0203440)Sep 8, 2017 · N991AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2017090806793Rub Strip · crackedCRACK AND MISSING PLASTIC RUBSTRIP ON FLOOR PANEL #211AKF AND 211AMF (CPIL). NRC 00473: CRACK ON FLOOR PANEL #211AKF AND 211AMF WAS REPAIRED PER B717 SRM 53-00-00-2R-1 FIG. 201 (SHEET 2) AND MISSING PLASTIC RUBSTRIP WAS INSTALLED PER B717 SRM 51-41-02-0G. (ET)Sep 7, 2017 · N989AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017090806791Skin · crackedCRACKED FUSELAGE SKIN BETWEEN BS 1076 AND LONGERON 14R ABOVE THE RT PYLON. REPAIRED IAW ER/A 560871-14, REV ORIGINAL.Sep 7, 2017 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017090806790Latch · corrodedCORROSION SLIDE LATCHES BS 160 TO 200, RBL 54. THE SLIDE SUPPORTS WERE REPLACED IAW SRM 51-40-08-0G.Sep 7, 2017 · N990AT · Boeing 717200 · Emergency EquipmentSDR DALA2017090806789Door Frame · crackedCRACK ON THE RT NLG DOOR FRAME. NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R, REP 2.Sep 7, 2017 · N991AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017090806788Door Frame · crackedCRACK ON Y=42 LT SIDE OF NLG DOOR FRAME. THE NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R, REP 2.Sep 7, 2017 · N991AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017090806787Floor Panel · crackedCRACKED PASSENGER CABIN FLOOR PANEL 222XF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.Sep 7, 2017 · N989AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017090806786Skin · damagedSCRATCHES ON THE SKIN AROUND THE LT ALTERNATE STATIC PORT. THE SKIN WAS REPAIRED IAW ETI-17-17-163, REV ORIG, AND ER/A 560924-14, REV ORIG.Sep 7, 2017 · N989AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017090706702Fitting · crackedCRACKED LEFT FITTING BS 1063, LBL 17, Z=20. IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR FRAME. A NEW FITTING WAS INSTALLED IAW SRM 51-41-05, 51-41-02, AND 51-40-08.Sep 7, 2017 · N991AT · Boeing 717200 · Fuselage Main, Attach Fittings
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