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 DALA2018013000520Skin Panel · wornNON REMOVABLE VERTICAL STAB L/E PANEL IS WORN/FRETTED ON SKIN LOWER SURFACE AT ZFS 52.267, CENTER UPPER END OF PANEL. RESTORED FINISH PER SRM 55-30-01-1A.SDR DALA201801240085Tab · delaminatedDURING NON ROUTINE UNSCHEDULED CHECK, FOUND THE AILERON TAB TO BE DELAMINATED.SDR DALA2018012200359Lens · damagedF/A REPORTED THAT THE AFT RIGHT EMERGENCY CEILING LIGHT LENS IS DAMAGED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51. OPS CHECKED SATISFACTORY.SDR DALA2018012200357Battery Pack · inoperativeDURING WALK AROUND, PILOT FOUND THE EMERGENCY LIGHTS L2-793 AND L2-794 TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-121 BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD AND THE AIRCRAFT WAS OK FOR SERVICE.SDR DALA2018012200358Battery Pack · inoperativeMAINTENANCE FOUND THE FORWARD OVERWING EMERGENCY EXIT DOOR SIGNS NOT ILLUMINATING. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD.SDR DALA2018011600246Wire · unsecureCEILING EMERGENCY LIGHT INOPERATIVE AT 17CDE. FOUND A LOOSE WIRE ON THE SOCKET. SECURED THE CONNECTOR. OPS NORMAL.SDR DALA2018011200245Skin · corrodedDURING A C CHECK, FOUND CORROSION THE LT WING UPPER SKIN. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01 ALLOWABLE DAMAGE 1. THE CORROSION WAS BLENDED IAW SRM 51-10-02 AND PERFORMED A UT THICKNESS INSPECTION IAW NDT SPM 04-00-00. THE SKIN WAS REPLACESDR DALA2018010900169Skin · damagedSKIN DAMAGE 3 FT AFT OF L1 DOOR JUST ABOVE CUSP LINE. FUSELAGE STATION Y236 BETWEEN LONGERON L17 AND L18. DENT 2 X 2.5 X .125 INCH DEEP WITH HORIZONTAL GOUGE .5 X .125 X .OO8 INCH DEEP. REMOVED DAMAGE SKIN FROM L18 TO L15 FSY 229 TO FSY 245.5. FABRICATED REPSDR DALA2018010800148Lens · unsecureEMERGENCY EXIT COVER DIFFUSER LENS MISSING FROM CEILING EXIT LIGHT AT ROW 1. MAINTENANCE LOCATED THE EMERGENCY EXIT COVER AND SECURED IAW AMM 33-51. OK FOR SERVICE.SDR DALA2018010500147Battery Pack · dischargedEMERGENCY EXIT SIGN ON FWD BULKHEAD ABOVE F/A JUMPSEATS AT DOOR 1L IS IN DIM MODE AT ALL TIMES, EVEN IF SWITCH IS OFF AND ALL OTHER EMERGENCY EXIT SIGNS ARE OFF. WHEN EMERGENCY EXIT SIGNS TURNED ON, ALL THE OTHERS COME ON BRIGHT EXCEPT FOR THIS LIGHT, WHICH FLSDR HALA2018010200001Eec · faultedATB, "SELECT FADEC ALTN" DISPLAYED ON EAD. CHECKED MCDU AND FOUND FAULT ON EEC 1 NR 1 ENG. REMOVED AND REPLACED EEC NR 1.SDR DALA2018010300038Terminal Block · smokeDURING PRE FLIGHT, THE CREW NOTICED AN ODOR IN THE COCKPIT, THEN HAD SMALL AMOUNT OF SMOKE COMING FROM THE FIRST OFFICER`S WINDSHIELD TERMINAL BLOCK. MAINTENANCE REPLACED THE WINDOW AND TERMINAL BLOCK.SDR DALA2017123009014Lens · damagedEMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. MAINTENANCE REPLACED LIGHT ASSY IAW DRAWING BR9051. OPS CHECKED GOOD.SDR DALA2017122909004Retainer · brokenTAIL SLIDE COVER RETAINER BROKEN. REPLACED THE RETAINER. OK FOR SERVICE.SDR DALA2017122608920Slide · out of toleranceON SERVICE CHECK FOUND R1 SLIDE IN NO GO RANGE. REPLACED SERVICE DOOR SLIDE IAW T/C 2561-9005. INSTALLED A NEW R1 DOOR SLIDE. OPS CHECKED NORMAL.SDR HALA2017122600330Compressor Blade · missingATB/ RIGHT ENGINE COMP STALL ON EICAS AUDIBLE BANG HEARD BY CREW. BORESCOPE REQUIRED. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND 6 EA PLUGS. REMOVED HP TURBINE STAGE 2, LP TURBINE STAGE 1, LP TURBINE STAGE 2 PLUGS. REMOVED BREATHER OUTLET. BORESCOPED NR 2 ENSDR HALA2017122500329Warning Message · false activationAIR TURNBACK DUE TO A STICK PUSHER FAILED MESSAGE. TROUBLESHOT WITH NO FAULTS FOUND.SDR DALA2017122708918Battery Pack · inoperativeEMERGENCY LIGHTS AT 19A AND C ABOVE THE OVERWING EXITS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY (P1-12) AT POWER SUPPLY IAW AMM 33-51.SDR HALA2017122600319Via · malfunctionedRETURNED TO DEPARTURE AFTER GEAR RETRACTION. RADIO ALTIMETER BEGAN TO ALERT. STICK PUSHER FAILED, WINDSHEAR DETECT FAILED, BANK ANGLE SHOWED RAD AT 30 DEGREE LIMIT. CONTINUITY CHECKED DATA BUSS WIRES FROM RA NR 1 R5-1006B G2 AND G3 TO VIA 31 AND VIA NR 2.SDR HALA2017122600318Blade · missingNR 2 ENGINE COMPRESSOR STALLED IN FLIGHT. REMOVED HIGH PRESSURE COMPRESSOR FAIRING AND SIX PLUGS. REMOVED HP TURBINE STAGE 2, LP TURBINE STAGE 1, LP TURBINE STAGE 2 PLUGS. REMOVED BREATHER OUTLET. BOROSCOPED THE NR 2 ENGINE HPC THROUGH ACCESS PORT D FOUND A SDR DALA2017122708919Power Supply · inoperativeON SERVICE CHECK, MAINTENACE FOUND FOUR EMERGENCY EXIT LIGHTS, IN THE TAIL COMPARTMENT PASSAGE WAY TO BE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-260) IAW AMM 33-51. OPS CHECK WAS NORMAL.SDR DALA2017122909003Angle · corrodedAN ANGLE IS CORRODED AT C2 BB LOWER DOOR CUT OUT, FWD SIDE TO AFT OF MIDDLE FITTING. REPAIRED IAW SRM 53-20-15, REPAIR 7.SDR DALA201812210058Tab · delaminatedCUSTOMER FOUND DURING INSPECTION CHECK DELAMINATION ON LOWER AND UPPER SURFACE- FULL SKIN REPLACEMENT REQUIREDSDR DALA2017122108917Engine · odorODOR PREVALENT AFTER TAKEOFF AND THROUGHOUT FLIGHT. ODOR STRONGEST FROM RT PACK ON THE NR 2 ENGINE BLEED. NO CONTAMINATION WAS FOUND. FOUND TURBINE OIL ODOR ISOLATED TO THE NR 2 ENGINE. SUSPECT ISSUE WITH BUFFER AIR VALVE. REPLACED NR 2 ENGINE BUFFER AIR VSDR HALA2017122000307Sensor · malfunctionedRECEIVED A BLEED AIR LT FAIL, WHILE CLIMBING THRU 10,000. RETURNED TO DEPARTURE. REPLACED THE LT PM SENSOR IAW AMM 36-12-04. ENGINE RUN CHECKED GOOD. WIRING CHECKED FROM PM SENSOR TO PSC CHECKED GOOD.SDR HALA2017121900305Slide · unsecureFWD ENTRY DOOR SLIDE NOT STORED PROPERLY. RE-SECURED MED DOOR SLIDE PER MM 25-61-01, CONDITION AND SECURITY CK OK TO CONTINUE.SDR DALA2017121800027Life Vest · out of positionMAINTENANCE FOUND THAT THE LIFE VESTS WERE BLOCKING THE EMERGENCY EXIT DOOR AFTER THE REVENUE FLIGHT ARRIVED. THE LIFE VESTS WERE REPOSITIONED TO THEIR PROPER LOCATION PER B717 AMM 25-62. (LP #4135006)SDR DALA2017121008489Power Supply · inoperativeLEFT & RIGHT AFT OVERWING EXIT IDENTIFIERS FOUND TO BE INOPERATIVE. (5 LTS). MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY (B5-119) PER B717 AMM 33-51. ALL OPERATIONAL CHECKS WERE NORMAL. (LP #3885940)SDR DALA2017121108490Engine · surgesSHIP 9573 - THE CREW EXPERIENCED AN ENGINE SURGE AND HIGH EXHAUST TEMPERATURES WITH THE #2 ENGINE SO THE FLIGHT DIVERTED TO CAE. THE PILOT DID REDUCE POWER ON THE PROBLEM ENGINE SINCE THAT ENGINE DID NOT RECOVER FROM THE SURGE. THE QRH DIRECTED TO SHUTDOWN THESDR DALA2017120608443Scuff Plate · corrodedFURTHER CORROSION FOUND UPON REMOVAL OF FORWARD CARGO DOOR SCUFF PLATE AROUND FASTENER HOLES - MARKED. NRC 001-0301: 5231-2003/001 00076 REPAIRED PER B717 SRM 53-00-15-2R. (LP #0326750)SDR HALA2017120300290Retract Cylinder · faultyAFTER T/O L&R MAIN GEAR INDICATED UNSAFE. REMOVED & REPLACED LT MAIN LANDING GEAR RETRACT CYLINDER.SDR DALA2017112808353Skin · crackedCRACK ON INBOARD RT WING BUTE DOOR. INNER SKIN WAS REPLACED PER DWG 5919571 REV BG AND SRM 51-41-02.SDR DALA2017112908379Light · fodTHE CAPTAIN REPORTED A FIRE IN THE CABIN AT THE L1 DOOR AND TAXIED THE AIRCRAFT BACK TO THE GATE. THE FLIGHT ATTENDANT USED THE FIRE EXTINGUISHER ON A BURNING NAPKIN IN THE OVERHEAD LIGHT FIXTURE. THE NAPKIN REMAINS WERE REMOVED BY THE FLIGHT ATTENDANT. MAINSDR DALA2017112708330Battery Pack · inoperativeMAINTENANCE FOUND THE EMERGENCY LIGHT BATTERY INOPERATIVE AT LOCATION B5-260. MAINTENANCE REPLACED THE BATTERY IAW AMM 33-55. OPS NORMAL.SDR DALA2017112608328Skin · damagedELONGATED SCREW HOLES AT LOWER SKIN. THE SKIN DOUBLER WAS REPLACED IAW SRM 51-41-01, AND DWG 5919571, REV BG.SDR DALA2017112608327Cusp Web · crackedCRACK ON THE RT CUSP WEB BETWEEN BS 650 - 655, RBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW ER/A 562407-14, REV ORIGINAL AND ETI 17-17-243, REV 2.SDR DALA2017112508326Doubler · corrodedCORROSION ON THE AFT CARGO BAY PRODUCTION DOUBLER IN THE JAMB AREA BETWEEN BS 965 - 979, LONGERONS 27 - 28R.SDR DALA2017112708352Cover · missingTHE EXIT SIGN IN THE FIRST CLASS AISLE IS MISSING THE COVER. MAINTENANCE INSTALLED A NEW COVER. OK FOR SERVICE.SDR DALA2017112408325Skin · crackedCRACK ON VERTICAL STABILIZER SKIN. THE SKIN WAS REPLACED IAW SRM 51-41-02 0G, 51-40-05 0G, AND DWG 5936143, REV AS.SDR DALA2017112408324Cargo Track · corrodedCORROSION ON THE CARGO TRACK BS 892 TO 954 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 , 51-41-05, AND 51-41-02.SDR DALA2017112408323Cargo Track · corrodedCORROSION ON THE CARGO TRACK BS 994 TO 1022, IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01.SDR DALA2017112408322Cargo Track · corrodedCORROSION ON CARGO TRACK BS 813 TO 1022 LT SIDE IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.SDR DALA2017112408321Stiffener · crackedCRACKED STIFFENER AT THE 12 HR POSITION, ON AFT CABIN PRESSURE BULKHEAD. THE STIFFENER WAS REPLACED IAW DWG 9915562, REV P, AND SRM 51-41-05.SDR DALA2017112308320Skin · wornWEAR ON INTERNAL FACE OF SLAT SKIN SS 119, RT WING NR 1 SLAT. REPAIRED IAW ETI-17-17-240, REVISION 2, AND ER/A 562401-14, REVISION ORIGINAL.SDR DALA2017112308319Door Frame · corrodedCORROSION ON DOOR FRAME BS 954 TO 994 IN THE AFT CARGO BAY. THE DOOR FRAME WAS REPLACED IAW SRM 51-41-02, AND SRM 51-41-05.SDR DALA2017112308318Fitting · crackedCRACK ON FITTING, LONGERON 22R, BS 661. REPAIRED IAW ETI-17-17-236, REV 2, AND ER/A 562397-14, REV ORIGINAL.SDR DALA2017112208317Torque Tube · corrodedCORROSION WAS FOUND ON THE RUDDER TORQUE TUBE ASSY. THE RUDDER TORQUE TUBE WAS REPAIRED IAW ER/A 562416-14, REV ORIGINAL.SDR DALA2017112208316Structure · corrodedCORROSION ON BARREL NUTS WAS FOUND. THE BARREL NUT HOLES WERE REPAIRED IAW ETI-17-17-231, REV 5, AND ER/A 562391-14, REV ORIG. BOLTS AND NUTS WERE REPLACED IAW AMM 20-20-22.SDR DALA2017112108242Longeron · damagedLONGERON 17L FOUND DAMAGED BEHIND FUSELAGE SKIN. REMOVED SECTION OF THE LONGERON, FABRICATED A 35 INCH SECTION OF REPLACEMENT LONGERON IAW SRM 53-00-05-2R-2, FIG 201, SHEET 1, AND INSTALLED IAW SRM 53-00-05-2R-2, FIG 201. COMPLIED WITH THE PERMANENT REPAIR IASDR DALA2017112108241Gusset · crackedCRACKED GUSSET AT LONGERON 7R AT BULKHEAD BS 1022. THE GUSSET WAS REPAIRED IAW ER/A 562380-14, REV ORIGINAL, AND ETI-17-17-226, REV ORIGINAL.
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