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 DALA2018050903266Longeron · crackedAFT ACCESSORY EMPENNAGE LONGERON 2L, BS 1132 WAS FOUND CRACKED ON THE AFT SIDE. ACCOMPLISHED A PERMANENT REPAIR IAW SRM 53-00-05, REPAIR 2.SDR DALA201805143265Floorbeam · corrodedCORROSION ON THE FLOORBEAM BS 180, X-10 TO X-43. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.SDR DALA201805143264Floor Support · corrodedCORROSION ON FLOOR SUPPORT, X=7, BS 200 CABIN. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-10-51-0I-2, AND 51-41-01-0G.SDR DALA2018051503374Computer · malfunctionedTHE CREW ABORTED THE TAKE-OFF AT 120 KNOTS AFTER THE "STAB TRIM" AURAL WARNING SOUNDED. THE STAB TRIM WAS SET WITHIN THE GREEN BOX AT 4.4 PRIOR TO THE TAKE-OFF ROLL. THE AIRCRAFT TAXIED BACK TO THE GATE. CORRECTIVE ACTION: MAINTENANCE HAS REPLACED THE FCC PER SDR DALA2018051403323Scuff Plate · crackedCRACKED SCUFF PLATE ON THE FWD R1 SERVICE DOOR. THE SCUFF PLATE WAS WELDED IAW ETI 17-18-089, REV ORIGINAL, AND ER/A 568360-14, REV ORIGINAL.SDR DALA2018051403322Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA2018051403321Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620DB ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA201805153320Access Panel · corrodedCORROSION ON SETTLMENT AREA AND COUNTERSINK HOLES OF FUEL ACCESS PANEL 620FT, RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00.SDR DALA2018051403298Lens · looseTHE EMERGENCY EXIT SIGN LENS IN THE CABIN WAS FOUND LOOSE. MAINTENANCE REPAIRED THE SIGN LENS AT THE L1 DOOR. OPS CHECKED OK IAW AMM 33-51. OK FOR SERVICE.SDR DALA201805143263Lens · missingTHE OVERHEAD EMERGENCY LIGHT LENS AT ROW 17ABC WAS MISSING. MAINTENANCE REPLACED THE LENS. OK FOR SERVICE.SDR DALA201805173101Lens · looseEMERGENCY EXIT SIGN LENS LOOSE. REINSTALLED THE LENS. AIRCRAFT IS OK FOR SERVICE.SDR DALA201805173100Cusp Web · crackedCRACKED LT CUSP WEB BS 647 AND 665, X 44 TO X 54. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9910151, REV CH.SDR DALA201805173099Cusp Web · crackedCRACKED RT CUSP WEB, BS 670, X -54 TO X -60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 223.SDR DALA2018051703098Cusp Web · crackedCRACKED LT CUSP WEB BETWEEN BS 660 AND 665, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 203, AND 51-41-02-0G.SDR DALA2018051703097Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 16 - 17L. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018051703096Frame Angle · crackedCRACKED FRAME ANGLE AT BS 1022, BETWEEN LONGERONS 13 - 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA20180573103Battery Pack · malfunctionedUPPER AFT CABIN EXIT DOOR SIGN FLASHING WHEN IN ARM POSITION. MAINTENANCE REPLACED LIGHT POWER SUPPLY AND BATTERY ABOVE AFT DOOR CEILING PANEL IAW AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL. AIRCRAFT OK FOR SERVICE.SDR DALA201805173102Skin · damagedFOUND DAMAGE ON THE LT INBD FLAP TRAILING EDGE WEDGE. PERFORMED A TEMP REPAIR IAW ER/A 568347-14.SDR DALA2018051703095Longeron · crackedCRACKED LONGERON 17L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2, FIG 201.SDR DALA2018051703094Cusp Web · crackedCRACK ON THE LT CUSP WEB, BETWEEN BS 908 AND 912, X 54 TO X 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.SDR DALA2018051703004Plate · corrodedCORROSION ON THE RT PLATE BETWEEN BS 1037 - 1053, X-57 TO X-60. THE PLATE WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9981474, REV L.SDR DALA2018050102956Doubler · wornWORN RT PRODUCTION DOUBLER Z=11 IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. THE DOUBLER WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 16, REPAIR 16.SDR DALA2018050202978Pan · crackedRT WINDOW RING PAN CRACKED, FWD UPPER CORNER, BS 351. REPAIRED IAW SRM 56-20-02-2R1 FIG. 202.SDR DALA2018050102955Doubler · wornWEAR ON PRODUCTION DOUBLER LOWER SURFACE FROM BS 370 TO 416, THE FWD CARGO DOOR. THE DOUBLER WAS REPLACED IAW DWG 5910141, REV FE, AND SRM 51-41-02-0G.SDR DALA2018050102954Pan · crackedCRACKED LT WINDOW RING PAN FWD LOWER CORNER BS 832, 851, 889, AND 908. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1 FIG.202.SDR HALA2018042400185Smoke Detector · unknownTESTED CARGO SMOKE DETECTOR & DID NOT TEST WITH PUSH BUTTON DEPRESSED. PERFORMED CARGO SMOKE TEST IAW AMM 26-13-01. NO DEFECTS NOTED. OK FOR SERVICE.SDR DALA2018042402773Battery Pack · inoperativeDURING A SERVICE CHECK, PERFORMED AN EMERGENCY LIGHTS TEST, FOUND SEVERAL EXIT LIGHTS THAT WOULD NOT STAY ILLLUMINATED. REPLACED THE BATTERY AND POWER SUPPLY IAW AMM 33-51. OPS TESTED GOOD IAW AMM 33-51.SDR DALA2018042002652Structure · crackedCRACK WAS INDICATED IN 6 LOCATIONS ON THE RIGHT VERTICAL STAB AREAS. REPAIRED PER PRI 567609-14AD. ER/A, 567609-14AD, MATCHES PRI.SDR DALA2018041802583Light · inoperativeSEVERAL CEILING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THEM ALL PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.SDR DALA2018041802584Bracket · damagedFOUND THE EMERGENCY LIGHT BATTERY PACK BRACKET TO BE DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.SDR DALA2018041602479Wire · looseTHE AFT EMERGENCY EXIT LIGHT CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE FOUND A LOOSE WIRING AND SECURED IT. THE EMERGENCY EXIT LIGHT WORKS PROPERLY.SDR DALA2018041602535Scuff Plate · crackedCRACKED AND ELONGATED HOLES AT AFT CARGO COMPARTMENT SCUFF PLATE. AFT CARGO COMPARTMENT SCUFF PLATE WAS REPAIRED PER ER/A 542149-14MA REV A.SDR HALA2018041600170Coalescer Bag · odorELECTRICAL ODOR COMING FROM AIR CON SYSTEM. OPS CHECKED ALL INTERIOR LIGHTS AND EXTERIOR LIGHTS. CHECKED THE FLIGHT CONTROLS. NO ELECTRICAL ODOR NOTED. CLEANED LEFT PACK DUCT FROM ACM TO COALESER BAG. REPLACED THE LEFT COALESER BAG IAW AMM 21-54-08. OK FOR SERSDR DALA2018041602478Switch · intermittentTHE UPPER EMERGENCY LIGHTS AT 20DC AND 20B WERE FOUND TO BE INOPERATIVE. MAINTENANCE CYCLED THE EMERGENCY SWITCH AND ALL OPERATIONS CHECKED NORMAL.SDR HALA2018041600168Coalescer Bag · odorFA NOTED A STRANGE ODOR IN THE FWD AND AFT CABIN. REMOVED AND REPLACED THE COALESCER BAGS IAW AMM 21-54-01, OPS CHECKED GOOD. ACCOMPLISHED NR 1 & 2 ENGINE RUNS, RAN AIR SYSTEM, NO DEFECTS NOTED. OK TO CONTINUE SERVICE.SDR DALA2018041602480Engine · seizedTHE CREW SAFELY ABORTED TAKEOFF AT 120 KNOTS, FOLLOWING A NR 1 ENGINE COMPRESSOR STALL. MAINTENANCE FOUND THE NR 1 ENGINE SEIZED AND METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED.SDR DALA2018041502477Frame · corrodedCORROSION ON FRAME BS 1022, BETWEEN LONGERONS 27L TO 27R. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018041202381Power Supply · failedTHE 1L DOOR EMERGENCY EXIT LIGHT WAS NOTED TO BE INOPERATIVE. MAINTENANCE FOUND THAT THE POWER SUPPLY FOR THE DOOR SIGN HAD FAILED AND THEY REPLACED PS B5-123 AND BATTERY PER AMM 33-51. OPERATIONAL CHECK WAS GOOD.SDR DALA2018041102370Skin · dentedSKIN DAMAGE AT APPROX STATION 200 LONGERON 17R. DENT FOUND TO BE .210 DEEP 12" LONG MAX DIA. 1.5" - OUT OF LIMITS PER SRM 53-01-01-1A3. REMOVED DAMAGE PER SRM 53-03-01-2R-1 FIG 205. FABRICATED, DRILLED, AND INSTALLED DOUBLER PER SRM 53-03-01-2R-1 FIG 205.SDR DALA2018041202382Skin · damagedFOUND SKIN DAMAGE AT APPROX STATION 200 AND LONGERON 17R. DENT IS 0.210" DEEP, 12 INCH LONG, WITH A MAX DIAMETER OF 1.5". FOUND TO BE OUT OF LIMITS PER SRM 53-01-01-1A3. REPAIR ACCOMPLISHED ON NRC 004, LOG 0504045.SDR DALA2018041202369Web · crackedCRACK ON WEB OF VENT LOUVER STA Y=1200 AND 1:00 POSITION APPROX AT AFT ACCESSORY COMPT. WEB OF VENT LOUVER STA Y=1200 AND 1 HRS POSITION WAS REPAIRED PER SRM 53-00-00-2R FIG 201.SDR DALA2018041102328Angle · crackedCRACK ON SPLICE AND ANGLE ON INNER SKIN LT WING L/E STA XOS:296. SPLICE AND ANGLE WERE REPLACED ON INNER SKIN LT WING L/E STA XOS:296 PER SRM 51-41-02-0G, 51-41-05-0G, 57-40-01, AND DWG 9919326 REV E.SDR DALA2018041002316Longeron · crackedCRACKED LONGERON 2R, BS 1134 IN THE AFT ACCESSORY COMPARTMENT AREA. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, FIG 201.SDR DALA2018040902285Bracket · brokenLOUD BUZZING NOISE AND VIBERATION UNDER THE FLOOR AT ROW 19A. FOUND EIGHT RUBBER NUTS AT THE LT OVERWING FILLET PANEL. RAN HYD PUMPS AND FUEL PUMPS, ALL SOUND OK. INSPECTED THE UPPER LT WING FILLET AREA AND FOUND MIDDLE SUPPORT BRACKET FOR FWD OVERWING FILLESDR DALA2018040902284Rub Strip · damagedCORROSION, DISBONDED, AND CRACKED RUB STRIPS AT LH FILLET PANELS FROM BS 560 TO 917. THE RUB STRIPS WERE REPLACED IAW SRM 53-20-70-01, AND SRM 51-20-05.SDR DALA2018040802282Skin · crackedCRACKED FUSELAGE SKIN BS 1076, BETWEEN LONGERONS 13R - 14R. THE SKIN WAS REPAIRED IAW ER/A 567482-14 ,REV. ORIGINAL AND ETI-17-18-063 REV. 3.SDR DALA2018040802281Frame Angle · crackedCRACKED FRAME ANGLE, BS 1023, LONGERON 7R. THE FRAME ANGLE WAS REPAIRED IAW ETI-17-18-068, REV 2, AND ER/A 567515-14, REV ORIGINAL.SDR DALA2018040802280Door Frame · crackedCRACKED DOOR FRAME WEB BS 207, LONGERON 11L. THE DAMAGED AREA WAS REPAIRED SRM 53-10-15-2R, PROCEDURE 1.SDR DALA2018040702315Access Panel · corrodedCORROSION OUT OF LIMITS IAW NRC 00520. CORROSION ON FUEL ACCESS PANEL 520EB, LT WING. THE FUEL ACCESS PANEL WAS REPLACED IAW AMM 28-00-00 AND JIC CARD 2040-0010 JOB 001-0295.SDR DALA2018040902286Charger · malfunctionedTHE EMERGENCY EXIT SIGN AT THE R1 DOOR AND THE EMERGENCY EXIT SIGN ABEAM FIRST CLASS LAVATORY ARE FLICKERING WHILE IN FLIGHT. MAINTENANCE REPLACED THE AFT BATTERY CHARGER UNDER THE FWD FOLD DOWN PANEL. OPS CHECKED GOOD IAW AMM 33-51. OK FOR SERVICE.
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