Boeing 717-200
Service difficulty reports · 18,771
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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 DALA2019022601204Cusp Web · corrodedCORROSION ON CUSP WEB STA Y=940 TO 942 AND Y=542 TO 544 BTW X=-54 TO X=-44. CORROSION LEVEL 2, CUSP MEMBRANE STA Y=940 TO 942 AND Y=542 TO 544 BTW X=-54 TO X=-44 WERE REPAIRED PER SRM 53-00-55-2R-4 FIGURE 15.SDR DALA2019022501425Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP MEMBRANE WEB FROM STA Y=411 TO Y=414 RT SIDE AT PAX CABIN IN REF NRC S/N 00184. (5300-2020). (CPAX). NRC 0590: CORROSION LEVEL 2, CUSP MEMBRANE WEB FROM STA Y=411 TO Y=414 RT SIDE AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R-4 SDR DALA2019022751250Tray · corrodedCORROSION ON WATER WASTE TRAY (FUS). NRC 00083: CORROSION LEVEL 2,(UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07, PAR. 5, FIG. 3, SHEET 1-2. ORIGINAL THICKNESS ON WATER WASTE TRAYIS 0.071" AND MINIMUM REMAINING THICKNESS FOUND IS 0.020" THEREFORE IT IS OUT LIMITS SDR DALA2019022501203Battery Pack · dischargedTHE EMERGENCY LIGHTS AT EXIT ROW 18 ARE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING AT THE OVERHEAD PANEL AND REPLACED THE BATTERY PACK AND BATTERY. OPERATIONAL CHECK WAS GOOD PER B717 WDM 33-51 AND SWPM 20-20.SDR DALA2019022501202Cusp Web · corrodedCORROSION OUT OF LIMITS ON CUSP MEMBRANE (WEB) ON STA Y=855 RH SIDE AT PAX CABIN IN REF NRC 00170 (AMDS 5300-2020). NRC 0588: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) ON STA Y= 855 RH SIDE AT PAX CABIN WAS REPAIRED PER B-717 SRM 53-00-55-2R-4 FIGURE 216 AND SRM SDR DALA2019022501201Longeron · crackedCRACK ON LONGERON 6LH AT STA 1022. (CPAX). NRC 00432: SECTION LONGERON 6 LH BTW STA 1002 TO 1049 WAS REPLACED PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0958705)SDR DALA2019022501200Longeron · crackedCRACK FUSELAGE LONGERON BTW STA Y=1022 AND L5L AT AFTER CABIN AREA(CPAX). NRC 00477: SECTION LONGERON 5 LH BTW STA 1002 TO 1049 WAS REPLACED PER B717-200 SRM 51-41-02, 51-41-05, AND 53-00-05-2R. (LP #0958701)SDR DALA2019022501199Cusp Web · corrodedCORROSION ON CUSP MEMBRANE WEB FROM STA Y=908 TO Y=954 RH SIDE AT PAX CABIN (AMDS 5300-2020). (CPAX). NRC 00173: CORROSION LEVEL 2, CUSP MEMBRANE WEB FROM STA Y=908 TO Y=954 RH SIDE AT PAX CABIN WAS REPLACED PER B717-200 SRM 53-00-55-2R-4 FIG 225 SHEET 5, SRM SDR DALA2019022501198Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANELS 620LB AND 620MB (AD). NRC 00617: FUEL ACCESS PLATE #620MB WAS REPAIRED PER B-717 200 SRM 57-10-01-2R PAR. 5 B. CONDITION II. TOOL USED: DIGITAL CALIPER P/N: 500-171-30 S/N: A1720947 DUE DATE: 20MAR19 AND ACCESS PLATE #620LSDR DALA2019022501197Support · wornWORN SUPPORT ON CABIN PRESSURE BULKHEAD DOOR LOWER HINGE AREA (PTAS). NRC 00506: SUPPORT ON CABIN PRESSURE BULKHEAD DOOR LOWER HINGE AREA WAS REPAIRED PER B717-200 SRM 52-10-02-2R REP. 16, PAR 4, A, OPTION 1. (LP #0958537)SDR DALA2019022541194Frame · crackedL/H OVERWING FRAME AT STA 696 CRACKED REF 5310-01436-04A STEP #10. NRC 034-0001:5310-01436-04A/001 00021: REPLACED FRAME PER ROUTINE CARD 5310-01436-03A. (LP #0957078)SDR DALA2019022531193Battery Pack · inoperativeTHE EMERGENCY LIGHTS AT ROW 20 AFT TO LAVS AND AFT OVERWING UPPER LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY PACKS AT STA 726 (ROW 20), STA 803 (ROW 22), AND STA 879 (ROW 25) PER B717 AMM 33-51. OPERATIONAL CHECK IS GSDR DALA2019022531192Angle · crackedCRACKED ANGLE ON FWD BULKHEAD OF CENTER TANK THROUGH FWD CARGO COMPARTMENT LONG 24RH (CCD). NRC 0556: ANGLE ON FWD BULKHEAD OF CENTER TANK THROUGH FWD CARGO COMPARTMENT LONG 24RH WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #0956228)SDR DALA2019022531191Tee Fitting · crackedCRACK ON ANGLE "T" LOWER EDGE STA Y= 408 AT FWD CARGO DOOR (PTAS). NRC 00554: ANGLE "T" WAS REPLACED PER B717-200 SRM 51-41-02-0G AND DWG #9957664 REV. N. (LP #0955845)SDR DALA2019022531190Longeron · corrodedCORROSION ON LONGERON #30 FROM STA Y=927 TO Y=1007 AT AFT CARGO COMPARTMENT (CCT). NRC 00253: CORROSION LEVEL 2, SECTION LONGERON 30 FROM STA Y=900 TO Y=1012 WAS REPLACED (SPLICE REPAIR) DUE EXCESSIVE CORROSION PER B717-200 SRM 53-20-05-2R-1. (LP #0955764)SDR DALA2019022531189Cusp Web · crackedCRACK ON CUSP MEMBRANE BEETWEN STA 813 TO 832 RH CABIN PAX FLOOR. NRC 00149: CUSP MEMBRANE BEETWEN STA 813 TO 832 RH CABIN PAX FLOOR AREA WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4-7037. (LP #0955758)SDR DALA2019022531188Door Sill · damagedDURING BUY BACK OF BLEND REPAIR FOUND LOW SPOT ON AFT CARGO COMPTARTMENT DOOR SILL AFT OF DOOR DOWN STOP FITTING. MKD. NRC 001-0307:5231-2002/006 00178: REPLACED DOOR JAMB REF B717 SRM 53-20-15-2R PROCED 7. (LP #0955479)SDR DALA2019022201116Liner · crackedCRACK ON LINER PANEL 211EF (CPIL). NRC 00407: LINER PANEL 211EF WAS REPAIRED PER B717-200 SRM 53-00-00-2R. (LP #0954932)SDR DALA2019022201115Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #221BF, 221HF, 221FF, 221JF, AND 221AF. (W-1). NRC 00501: FLOOR PANELS #221BF, 221HF, 221FF, 221JF, AND 221AF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0953908)SDR DALA2019022201114Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL #221LF. (W-1). NRC 00503: FLOOR PANEL #221LF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0953896)SDR DALA20190221082Power Supply · inoperativeTHE EMERGENCY EXIT SIGN IS INOPERATIVE AT LOCATIONS:102. MAINTENANCE FOUND THE AFT LIGHT AND ESCAPE SECTION EMERGENCY LIGHT POWER PACK TO BE INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS RETURNED SDR DALA2019022101081Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=427/Y=446 RH X=65. NRC 00298: CUSP WEB BTW STA Y=427/Y=446 RH X=65 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 215. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON CUSP WEB BTW STA Y=427/Y=446 RH X=65. NO CRACKS WERE FOUNDSDR DALA2019022101080Seat Track · corrodedCORROSION ON SEAT TRACK X=-22 FROM STA 200-218 AT FWD WET AREA (W1). NRC 00535: CORROSION LEVEL 2, SEAT TRACK X=-22 FROM STA Y=200 TO Y=301 WAS REPAIRED PER B717-200 SRM 53-20-52-2R FIGURE 201 (SHEET 1) REP. 5 AND 51-41-01-0G. (LP #0953284)SDR DALA2019022101079Seat Track · corrodedFORWARD GALLEY FLOOR - RIGHT INBOARD SEAT TRACK HAS CORROSION. NRC 001-0213:2561-1001/001 00245: REPLACED PER B717 SRM 53-20-52-2R-5 FIG 201. (LP #0952566)SDR DALA2019022001071Pan · crackedCRACKED RING PAN IN STA Y=851 AND L=12R, Y=889 AND L=12R, Y=889 AND L=14R, Y=908 AND L=14R. ALSO Y=946 AND L=14R AT CPAX. RING PAN REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, FIG 202. TYPE B. (ET)(HFEC) WAS ACCOMPLISHED ON RING PAN STA Y=851/L=12R; Y=8SDR DALA2019022001070Pan · crackedCRACK RING PAN IN STA Y=908 AND L=14L, Y=870 AND L=12L, Y=851 AND L=12L. ALSO Y=832 AND L=12L AT CPAX. RING PAN REPAIRED PER SRM 56-20-02-2R PROCEDURE 1, REPAIR 1, FIG 202. TYPE B. (ET)HFEC INSPECTION WAS ACCOMPLISHED ON RING PAN IN STA Y=908 AND L=14L, Y=870 SDR DALA2019022001069Floor Support · crackedCRACK ON FLOOR SUPPORT AT WING BOX AREA STA Y=655 BTW X=44 AND X=-44. FLOOR SUPPORT AT WING BOX AREA STA Y=655 BTW X=44 AND X=-44 WAS REPLACED PER SRM 51-41-05.SDR DALA2019021901028Fitting · crackedCRACK ON INNER FITTING NEAR LOWER EDGE STA Y=390 AT FWD CARGO DOOR (PTAS). NRC 00178: INNER FITTING WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0950665)SDR DALA2019021901027Cusp Web · corrodedEXCESSIVE CORROSION AT CUSP WEB BETWEEN STA 541/560 X=-65 IN REF NRC 00299. NRC 00549: CORROSION LEVEL 2, CUSP WEB BETWEEN STA 541/560 X=-65 WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG. 215 TABLE 2. (ET) HFEC INSP WAS ACCOMPLISHED ON CUSP WEB BETWEESDR DALA2019021901026Fitting · corrodedCORROSION ON FITTING STA Y=210 AND X=-11 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00378: CORROSION LEVEL 2, FITTING STA Y=210 AND X=-11 AT FWD WET AREA WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0950557)SDR DALA2019021901025Housing · wornWEAR ON HOUSING AT FWD CARGO DOOR HANDLE (PTAS). NRC 00179: HOUSING WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0950064)SDR DALA2019021901024Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=180 AND Y=200 AND X=-44 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00372: CORROSION LEVEL 2, FLOOR SUPPORT BTW STA Y=180 AND Y=200 AND X=-44 WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP #094997SDR DALA2019021901023Threshold · corrodedCORROSION FOUND AT AFT CARGO DOOR THRESHOLD. REPLACED AFT CARGO DOOR JAMB REF SRM 53-20-15-2R PROC 7.SDR DALA2019021801021Battery Pack · failedEMERGENCY LOWER LIGHTS WERE FOUND INOPERATIVE AT 21B AND 20CDE. MAINTENANCE FOUND THAT THE BATTERY PACK AT STA 804 HAD FAILED. THE BATTERY PACK WAS REPLACED PER B717 AMM 33-51-18. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5547384)SDR DALA2019021801020Floor Panel · delaminatedDELAMINATION FLOOR PANEL #211ASF AND 211AQF. NRC 00498: FLOOR PANEL #211ASF AND 211AQF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #0949287)SDR DALA2019021801019Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=180 AND 200 BTW X=-9 TO X=-43 AT FWD WET AREA (IN REF. AMDS 5300-2010)(W1). NRC 00371: CORROSION LEVEL 2, FLOOR SUPPORT STA Y=180 AND 200 BTW X=-9 TO X=-43 AT FWD WET AREA WAS REPLACED PER B717-200 SRM 51-41-02 AND SRM 51-41-05SDR DALA2019021801018Pan · crackedCRACK ON RING PAN BETWEEN STA 756 AND 775 AND STRINGER 14 AND 15 AT RH CABIN PAX. NRC 00265: CRACK ON RING PAN BETWEEN STA 756 AND 775 AND STRINGER 14 AND 15 AT RH CABIN PAX WAS REPAIRED PER BOEING 717-200 SRM 56-20-02-2R-1- FIGURE 202 DETAIL E. (LP #0948837)SDR DALA2019022761249Skin · damagedUNIDENTIFIED REWORKED AREA ON WING SKIN, UPPER SURFACE, AFT OF FRONT SPAR AFT OF #3 SLAT. (M). NRC 001-0296 5720-2003/002 00152: PRI 575373-14 REV A REV O-1. REWORKED AREA WAS REPAIRED PER ER/A 575373-14 REV A ITEMS 1-12. (LP #0946139)SDR HALA2019021500057Proximity Sensor · failedATB / RIGHT MAIN GEAR "RED" INDICATION UPON RETRACTION. THREE GREEN ON DOWN POSITION.// REMOVED AND REPLACED MLG DOWN/LOCK PROX SENSOR ASSY PER AMM TASK 32-61-04-000-801.SDR DALA2019022741248Skin · crackedREF AA 5530-01048 AND AD 2018-10-08RIGHT HAND SIDE VERTICAL STAB LEADING EDGE ATTACH (2EA) HOLES HAVE CRACK INDICATIONS, FIRST 2 HOLES ABOVE SPLIT LINE (MKD). NRC 075-0001:5530-01048-02/002 00226: PRI 575376-14 REV 0-1. CRACK WAS REPAIRED PER ER/A 575376-14 RESDR HALA2019021200056Vane · out of adjustATB / FCF FAILED = ACFT ROLLS RIGHT AT FLAP 40. ADJUSTED R/H MID FLAP FIX VANE PER AMM
24-20-02.SDR DALA2019021200916Door Frame · corrodedCORROSION ON AFT CARGO DOOR JAMB. REPLACED DOOR JAMB REF SRM 53-20-15-2R PROC 7.SDR DALA201902110864Frame · crackedOVER WING FRAME CRACKED R/H STA Y=696.00. CONDITION 3, CRACK EQUAL TO OR GREATER THAN 0.125. (VISUAL INSPECTION). NRC 029-0003:5310-01436-04C/002 00043: REPLACED CRACKED FRAME REF JOB 83-0002 TASK CARD 5310-01436-03B STEPS 1-47. (LP #0938117)SDR DALA201902110863Frame · crackedOVER WING FRAME CRACKED R/H STA Y=674.00. CONDITION 3, CRACK EQUAL TO OR GREATER THAN 0.125. (VISUAL INSPECTION). NR 029-0003:5310-01436-04C/001 00042: REPLACED CRACKED FRAME REF JOB 83-0002 TASK CARD 5310-01436-03B STEPS 1-47. (LP #0938115)SDR DALA2019021109862Wire · brokenDURING SERVICE CHECK, MAINTENANCE NOTED THAT ONE FLOOR LEVEL EMERGENCY LIGHT WAS INOPERATIVE ON THE CATWALK. LIGHT L2-847. MAINTENANCE THEN FOUND A WIRE BROKEN AT THE CONNECTOR P1-3038. THE WIRE WAS REPAIRED PER SWPM 20-31. OPERATIONAL CHECK WAS GOOD. (LP #432SDR DALA202208405373Vane · unknownPD: WORN BUSHINGS INBD/OUTBD TORQUE TUBE FITTINGS / CA: WORN BUSHINGS IN TORQUE TUBE FTGS. REPLACED WORN BUSHINGS IN TORQUE TUBE FTGS. PER CMM 27-50-2 DELTA REV 14.SDR DALA2019021580965Vane · corrodedCORROSION ON LH AFT MOVABLE FLAP VANE AT LH FLAP. (AI). NRC: 00140 CORROSION LEVEL II, CORROSION WAS FOUND OUT OF LIMITS PER B717-200 SRM 57-53-02-0I-1 ITEM 1 AND SRM 57-00-00-1A FIGURE 103. AFT LH MOVABLE FLAP VANE WAS REPLACED PER B717-200 AMM 27-50-03 400-8SDR DALA2019020800845Window Frame · crackedCRACK ON UPPER AFT CORNER CLEAR VIEW WINDOW FRAME LH SIDE. (CPIL). NRC 00390: UPPER AFT CORNER WINDOW OPENING LH SIDE WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1, ER/A 575163-14 REV. ORIG., AND ETI-17-19-015 REV. ORIG. ASSOCIATED ER/A 00-575163 ADDED FOSDR DALA2019020700822Window · crackedCRACK ON UPPER AFT CORNER CLEAR VIEW WINDOW RT SIDE. UPPER AFT CORNER CLEAR VIEW WINDOW RT SIDE WAS REPAIRED PER SRM 56-10-02-2R REPAIR 1, ER/A 575163-14 REV ORIG, AND ETI-17-19-015 REV ORIG.SDR DALA2019020500805Fitting · corrodedCORROSION ON FLOOR FITTINGS G-7 (CPAX). CORROSION LEVEL 2, FLOOR FITTING OF G-7 WAS REPLACED PER ER/A 535099-14MA REV H AND CMM 25-30-16 REPAIR SECTION.
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