Boeing 717-200
Service difficulty reports · 18,771
Newest first. General aviation reporting is voluntary.
Query with SQL
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2019062703877Intercostal · corrodedEXFOLATION ON INTERCOSTAL STA Y=1037 AND LONG 30 AT AFT CARGO COMPARTMENT. NRC 00315: CORROSION LEVEL 2, INTERCOSTAL WAS REPLACED PER B717-200 SRM 53-20-51-0I 7 ITEM 12 AND 51-41-02-0G. (LP #1142061)SDR DALA2019062703876Retainer · crackedCRACK AT AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS FOUND (CPIL). NRC 00654: AFT UPPER EDGE RETAINER ON LH SLIDE WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R. (LP #1142006)SDR DALA2019062603866Fuse · failedTHE TAIL CONE EMERGENCY WALKWAY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THAT THE INTERNAL 5A FUSE IN THE POWER SUPPLY B5-260 HAD BLOWN. THE POWER SUPPLY AND BATTERY PACK WERE REPLACED IAW B717 AMM 33-51-03. ALL OPERATIONAL CHECKS WERE GOOD. THSDR DALA2019062603865Longeron · crackedCRACKED LONGERON 13L, BS 1037. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2 FIG. 201 (SHEET 1).SDR DALA2019062603864Longeron · corrodedLONGERON 30 CORROED BS 1022. THE LONGERON WAS REPLACED IAW SRM 53-20-05 PROCEDURE 3 ITEM 9, 51- 41-02-OG, AND 51-41-05-OG.SDR DALA2019062603863Longeron · crackedCRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REPAIR 2, FIG. 201. (SHEET 2).SDR DALA2019062603862Floor Panel · crackedCRACKS ON FLOOR PANEL 211AKF AT FLIGHT COMPARTMENT. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R-2, PROCEDURE 2, REPAIR 2.SDR DALA2019062603861Cusp Web · crackedCRACKED CUSP WEB BS 560 - 579 RT SIDE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, 51-41-02-0G, AND 51-41-05-0G PAR 8.SDR DALA2019062603860Longeron · corrodedCORROSION BTW LONGERON 25L, BS 1002 - 1037 AT CARGO COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2 AND SRM 51-40-08-0G.SDR DALA2019062603859Skin · crackedCRACK AT FUSELAGE SKIN BS 1076 BETWEEN LONGERON 13 & 14R. THE SKIN WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.SDR DALA2019062603858Skin · damagedDAMAGE ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT. REWORKED AREA ON FUSELAGE SKIN STA 832 ONE INCH BELOW STRINGER 25LT WAS REPAIRED PER PERMANET REPAIR IAW SRM 53-02-01- 2R FIG. 202 (SHEET 13).SDR DALA2019062603857Skin · crackedCRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH (FUS). NRC 597: CRACK AT FUSELAGE SKIN STA 1087 BETWEEN LONGERON 13/14RH WAS REPAIRED PER ETI-17-19-075 REV 5 AND ER/A 579256-14 REV. ORIG.SDR DALA2019062503830Frame Angle · corrodedEXFOLEATED FRAME CLIP ON STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT. NRC 00302: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1022 BTW LONG 27 LH AND 27RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9912243 REV. JS. (LSDR DALA2019062503828Skin · corrodedCORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30. CORROSION ON LOWER SKIN OF STA Y=851 AND STRINGER 30 WAS REPAIRED PER B-717-200 SRM 53-20-70-2R-1 FIG .201.SDR DALA2019062503827Cusp Web · crackedCRACK ON CUSP MEMBRANE (WEB) AT Y=813 RH SIDE. AREA WAS CLEANED PER PS 900-1-2-1NO. GVI WAS PERFORMED AND NO CORROSION WAS FOUND PER B717-200 AMM 05-21-02-210-802. CRACK WAS REPAIRED PER B717-200 SRM 53-00-00-2R AND 51-41-02-0G.SDR DALA2019062403801Frame · crackedCRACK ON FRAME BS 696 LH SIDE.FRAME REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03A.SDR DALA2019062403800Frame · crackedAD 2013-19-22 CRACK ON FRAME STA 696 RH SIDE. NRC 00371: FRAME STA 696 RH SIDE WAS REPLACED PER AD 2013-19-22 TASK CARD 5310-01436-03B. (LP #1137896)SDR DALA2019101875947Tab · damagedPD: UPPER AND LOWER SKIN DAMAGE, GATE CONTACTED AILERON SURFACE. CA: PERFORMED CSVE INSPECTION, REPAIRED UPPER AND LOWER AILERON SKIN, REPAIRED OUTBOARD HINGE FITTING, REPAIRED DAMAGED CLOSEOUT PANEL, REPLACEDSNUBBERS, RESTORED FINISH, BALANCED, REF. CMM 27-1SDR DALA2019062653856Cargo Track · damagedELONGATED HOLES ON RH TIE TRACK STA 954 AT AFT CARGO COMPARTMENT. NRC 00277: TIE TRACK RH ON STA 895 TO STA 954 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 53-20-51-0I-7 IDENTIFICATION 7, ITEM 8, FIG.2 (SHEET 2), PER B717-200 SRM 51-41-01-0G AND 51-4SDR DALA2019062543825Frame Angle · corrodedCORROSION ON FRAME CLIP STA Y=1002 BTW LONG 26LH-25LH AT AFT CARGO COMPARTMENT (C2). NRC 0711: CORROSION LEVEL 2, FRAME CLIP AT STA Y=1002 BTW LONG 26LH-25LH WAS REPAIRED PER B717-200 SRM 51-41-02-0G, 53-00-06-2R REPAIR 2 PAR. 4. A. FIG. 201, AND DWG #9957739 SDR DALA2019062543824Cusp Web · corrodedCORROSION ON REPAIR OF CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE (PAX CAB). NRC 00308: CORROSION LEVEL 2, MAINTENANCE FOUND CORROSION ON THE EXISITING REPAIR OF THE CUSP MEMBRANE (WEB) FROM Y=465 TO Y=484 RH SIDE: SO THIS REPAIR WAS REPLACED PER B717-200SDR DALA2019062543823Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=20 AT CABIN PAX. (CPAX). NRC 00351: CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. MINIMUM REMAINING THICKNESS IS 0.028 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-SDR DALA2019062543822Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1022 TO Y=1076 X=-20 AT CABIN PAX. CORROSION LEVEL 2, CORROSION WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26. REMAINING THICKNESS IS ONLY 0.025 AND THEREFORE IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A ALLOWABLE DAMAGSDR DALA2019062543821Cusp Web · corrodedCORROSION ON RH CUSP WEB BTW STA Y=565-567 IS OUT OF LIMITS. CUSP WEB WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG.215.SDR DALA2019062533820Frame · corrodedCORROSION ON FRAME STA 889 LONG 30 WAS FOUND OUT OF LIMITS PER B717 SRM 53-00-00-1A FIG 103. CORROSION LEVEL 2, FRAME AT STA 889 LONG 30 WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3 FIGURE 201, SHEET 1.SDR DALA2019062533819Barrier · corrodedCORROSION ON VAPOR BARRIER LH SIDE STA X=22 AND STA Y=715 AT PAX CAB (CPAX). NRC 00535: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113 ADDED FOR AC 9563. (LP #1136277)SDR DALA2019062533818Barrier · corrodedCORROSION ON VAPOR BARRIER STA X=54 AND STA Y=663 TO STA Y=715 AT PAX CABIN. CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579177-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533817Skin · corrodedCORROSION ON UPPER SKIN STA Y=717 X=-19 AND Z-10 AT WING BOX. NRC 00483: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533816Skin · corrodedCORROSION ON UPPER SKIN STA Y=708 X=-24 AND Z-10 AT WING BOX. NRC 00482: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579114-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533815Frame Angle · corrodedEXFOLATION FRAME CLIP STA Y=927 BTW LONG 24LH TO LONG 26RH AT AFT CARGO COMPARTMENT. NRC 00192: CORROSION LEVEL 2, FRAME CLIP AT STA Y=927 BTW LONG 26LH AND 26RH WAS REPLACED PER B717-200 DWG #9915524 REV. P, PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2019062533814Barrier · corrodedCORROSION ON VAPOR BARRIER STA X=22 AND STA Y=715 TO STA Y=737 AT PAX CAB (CPAX). NRC 00534: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I.SDR DALA2019062533813Doubler · corrodedCORROSION ON DOUBLER FROM STA Y=737 TO Y=748 BTW X=44 TO X=60 AND Z-10 AT WING BOX. NRC 00486: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL.SDR DALA2019062533812Skin · corrodedCORROSION ON UPPER SKIN FROM STA Y=715 TO Y=737 BTW X=44 TO X=60 AND Z=-10 AT WING BOX. NRC 00481: CORROSION LEVEL 2, CORROSION WAS REPAIRED PER ER/A 579113-14 REV. ORIGINAL: SECTION I. ASSOCIATED ER/A 14-579113.SDR DALA2019062523811Longeron · corrodedCORROSION ON SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT IN REFERENCE NRC 00284. (C2). NRC 683: CORROSION LEVEL 2, SECTION LONG 27LH FROM STA Y=984 TO STA Y=1010 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G ANDSDR DALA2019062523810Frame · corrodedEXFOLATION ON FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT. NRC 00296: CORROSION LEVEL 2, FRAME STA Y=1037 BTW LONG 25RH TO 25LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R.SDR DALA2019062433798Beam · crackedCRACKED BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE (L1) (PTAS). NRC 00080: BEAM #1, 2, AND 7 ON FWD PASSENGER DOOR INTERNAL STRUCTURE WERE REPAIRED PER B717-200 SRM 52-10-02-2R-13, 52-10-02-2R-8, AND 52-10-02-2R-7.SDR DALA2019062433797Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE. (CPAX). NRC 00533: CRACK ON RINGPAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433796Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE. (CPAX). NRC 00534: CRACK ON RINGPAN OF PASSEGER WINDOW, UPPER AFT AND UPPER LOWER CORNER, BETWEEN STA 813 AND 832, LH SIDE WAS REPAIRED PER B717-200 SRM 56SDR DALA2019062433795Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE. (CPAX). NRC 00535: CRACK ON RINGPAN OF PASSEGER WINDOW LOWER AFT CORNER, BETWEEN STA 908 AND 927, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433794Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE. (CPAX). NRC.00536: CRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 851 AND 870, LH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (SDR DALA2019062433793Pan · crackedCRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN. CRACK ON RH FWD/ LOWER RING PAN STA Y= 579 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433792Pan · crackedCRACK ON RINGPAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927, RH SIDE. CRACK ON RING PAN OF PASSEGER WINDOW UPPER FWD CORNER, BETWEEN STA 908 AND 927 RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062433791Skin · damagedCRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14R. FUSELAGE SKIN STA 1022 BETWEEN LONG. 13/14RH (FUS) WAS REPAIRED PER ERA/A 579005-14 REV. ORIGINAL, SECTION I PERMANENT REPAIR AND ETI-17-19-077 REV. 3.SDR DALA2019062433790Pan · crackedCRACKS ON PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR PAN AROUND LOWER HINGE AREA AT GALLEY SERVICE DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R REPAIR 4 FIG. 201.SDR DALA2019062423789Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE. RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 832 AND 851, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062423788Pan · crackedCRACK ON RING PAN OF PASSEGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE. (CPAX). NRC 00539: RINGPAN OF PASSENGER WINDOW UPPER AFT CORNER, BETWEEN STA 813 AND 832, RH SIDE WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1135004)SDR DALA2019062423787Pan · crackedCRACKED RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN. RH FWD UPPER RING PAN STA 889-908 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1.SDR DALA2019062423786Pan · crackedCRACKED RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN. RH LOWER AFT CORNER, ON RING PAN STA 813- 832 AT PAX CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.SDR DALA2019062423785Pan · crackedCRACKED LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN. LH AFT LOWER CORNER RING PAN STA 696-715 AT PASSENGER CABIN WAS REPAIRED PER SRM 56-20-02-2R-1.SDR DALA2019062423784Pan · crackedCRACKED RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN (CPAX). NRC 00627: RH FWD UPPER RING PAN STA 737-756 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 56-20-02-2R-1. (LP #1134973)
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