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 DALA2018082085143Lever · out of adjustTAILCONE DEPLOYMENT FAILED TEST USING INTERNAL RELEASE HANDLE. READING LESS THAN MINIMUM REQUIREMENT. MAINTENANCE ADJUSTED BOTH BOTTOM AND UPPER RIGHT LATCH LEVERS IAW AMM 53-52-01 830-802. THE TAILCONE OPERATION NOW TESTS PROPERLY IAW AMDS W/C 5352-2001.SDR DALA2018082085142Door Frame · corrodedSEVERAL AREAS ON THE FORWARD LOWER CARGO DOOR FRAME HAD SIGNS OF CORROSION. REPLACED THE FWD CARGO DOOR LOWER FRAME PAN IAW SRM 53-20-15-2R, REPAIR 6.SDR HALA2018081700383Electrical Sys · no testEMERGENCY POWER NOT TESTING. PERFORMED FUNCTIONAL TEST OF EMERGENCY POWER SYSTEM IAW AMM 24-24-00. OPS CHECKED OK, NO FAULTS NOTED.SDR DALA2018081600053Tab · delaminatedDURING INSPECTION, FOUND DELAMINATION ON UPPER AND LOWER SKIN SURFACE OF THE LT AILERON TAB.SDR DALA2018081605102Cam · cockedTAILONE RELEASE CAM TAB WAS CLOCKED INCORRECTLY. ADJUSTED THE RELEASE CAM IAW AMM 53-52-03.SDR DALA201808165103Cradle · inoperativeDURING A SERVICE CHECK, MAINTENANCE FOUND THE AFT TAILCONE EMERGENCY LIGHTS TO BE INOPERATIVE. THE EMERGENCY CRADLE ASSEMBLY WAS REPLACED IAW AMM 33-51. OPS CHECKED GOOD.SDR HALA2018081400372Pitot Tube · failedCAPTAIN`S PITOT AUX FAILED. AIR TURNBACK, REMOVED AND REPLACED AUX PITOT TUBE IAW AMM 34-11-01.SDR DALA2018081325034Longeron · damagedLONGERON 24L WAS FOUND DAMAGED BETWEEN BS 389 - 490. CUT OUT THE SECTION OF THE LONGERON. FABRICATED REPAIR SPLICES AND CUT A NEW LONGERON. WORK ACCOMPLISHED IAW SRM 53-00-05, REPAIR 2. ACCOMPLISHED HFEC IAW NDT SPM 06-10-01.001, NO CRACKS INDICATED. INSDR DALA2018081325033Longeron · damagedLONGERON 25L WAS FOUND DAMAGED BETWEEN BS 427 - 490. CUT AND REMOVED THE SECTION OF THE LONGERON . ACCOMPLISHED HFEC IAW NDT SPM 06-10-01. 001, NO CRACKS INDICATED. FABRICATED A REPLACEMENT LONGERON AND SPLICES. INSTALLED THE LONGERON SECTION IAW SRM 53-00-SDR DALA2018081305059Skin · corrodedSURFACE CORROSION FOUND AT THE LT UPPER WING SKIN, STRINGER 5 LWS 343 TO 348.5. THE CORROSION WAS BEYOND THE LIMITS IAW SRM 57-10-01, ALLOWABLE DAMAGE 1.SDR DALA2018080804928Sign · missingTHE L1 DOOR UPPER EXIT SIGN WAS MISSING. MAINTENANCE INSTALLED A NEW EXIT SIGN IAW AMM 33-51.SDR DALA2018080704894Frame · crackedCRACK INDICATION GREATER THAN 0.125 INCH AT THE BS 696 FRAME TAB UPPER RADIUS. REPLACED THE FRAME IAW AMDS 5310-01436-03B.SDR HALA0218080800362Static Inverter · malfunctionedDURING EMERGENCY POWER TEST, A BUZZING SOUND WAS OBSERVED FROM THE EE COMPARTMENT AND ACCOMPANIED BY AN EMERGENRY POWER TEST FAIL. REPLACED THE STATIC INVERTER IAW AMM 24-24-01, OPS CHECKED OK. OK FOR SERVICE.SDR DALA2018080604876Skin · damagedFUSELAGE SKIN AT BS 1110, LONGERON 24R WAS DAMAGED. REPAIRED THE SKIN IAW ER/A 569013-14, REV ORIGINAL.SDR DALA2018080604875Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN BS 1116 - 1140, LONGERON 23R - 25R. REPAIRED THE SKIN IAW ER/A 569014-14, REV ORIGINAL.SDR DALA2018080604874Doubler · damagedTHE FUSELAGE SKIN BUTTSPLICE DOUBLER WAS DAMAGED AT BS 1116 BETWEEN LONGERONS 24R AND 23R. REMOVED, FABRICATED, AND INSTALLED A NEW BUTTSPLICE DOUBLER IAW SRM 51-40-02, AND DWG 5911429, REV DZ.SDR DALA2018080604873Longeron · damagedLONGERON 23R, BS 1110 WAS DAMAGED. CUT OUT DAMAGED SECTION OF THE LONGERON AND REPAIRED IAW SRM 53-00-05, REPAIR 2.SDR DALA2018080604872Longeron · damagedLONGERON 24R, BS 1110 WAS DAMAGED. CUT OUT THE DAMAGED SECTION AND REPAIRED THE LONGERON IAW SRM 53-00-05, REPAIR 2.SDR DALA2018080604871Frame · damagedFRAME BS 1116, BETWEEN LONGERONS 23R AND 24R WAS DAMAGED. REMOVED, FABRICATED, AND INSTALLED A NEW FRAME IAW SRM 51-40-02, AND DWG 9915559, REV AB.SDR DALA2018080604870Frame · damagedFRAME BS 1116, LONGERON 24R WAS DAMAGED. REPLACED THE FRAME SECTION IAW SRM 51-40-02, AND DWG 5913596, REV AN.SDR DALA2018080604893Slide · looseTAILCONE SLIDE PACK WAS LOOSE AND UNRAVELED. INSTALLED A NEW TAILCONE SLIDE IAW AMM 25-61-02, AND AMDS CARD 5352-4002.SDR DALA201808064878Lens · damagedEMERGENCY EXIT LIGHT LENS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.SDR DALA201808064877Lens · damagedEMERGENCY EXIT LENS WAS DAMAGED. MAINTENANCE SECURED THE DAMAGED EXIT SIGN LENS.SDR DALA201808064869Battery Pack · inoperativeTHE LEFT AND RIGHT AFT OVER WING EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERY B5-119 IAW AMM 33-51. OPS CHECKED NORMAL.SDR DALA2018080604879Lens · damagedEMERGENCY EXIT LENS WAS DAMAGED.SDR DALA201808145058Skin · crackedMAINTENANCE FOUND A CRACK INDICATION COMMON TO THE 1ST FASTENER HOLE ON THE LT AND 2ND FASTENER HOLE ON THE RT BELOW THE ZFS 52.26 IN THE SKIN LAYER ONLY. REPAIRED IAW ER/A 520320-14AD, REV B.SDR DALA2018073104781Release Cable · out of positionAFT INTERNAL TAILCONE RELEASE SYSTEM FAILED THE DROP TEST. IT REQUIRED MORE THAN 35LBS PULL TO ACTIVATE. MAINTENANCE REROUTED THE INTERNAL HANDLE RELEASE CABLE TO THE PROPER ROUTING IAW AMM 53-52-01. TAILCONE RELEASE REPEAT OPERATIONAL CHECK WAS GOOD.SDR DALA2018073104780Battery Pack · dischargedMULTIPLE CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-121 AND B5-235 REF AMM 33-51. OPERATIONAL CHECK IS GOOD.SDR HALA2018072600406Inverter · malfunctionedWHEN ARMING EMERGENCY PWR, EMER AC COMES OFFLINE. REMOVED AND REPLACED STATIC INVERTER PER AMM 24-24-01. OK FOR SVC.SDR HALA2018072600405Conduit · brokenRIGHT MLG SLOW TO RETRACT. RED UNSAFE LIGHT ON CONSOLE AND CONFIG SD REMAINED ILLUMINATED FOR 2 MINUTES AFTER RETRACTION. FOUND RIGHT MAIN LANDING GEAR DOWN LOCK SENSOR CONDUITS BROKEN. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOWN LOCK PROX SENSOR ASSEMBLSDR DALA2018072504673Cover · looseTHE FWD CENTER AISLE CEILING EMERGENCY EXIT SIGN COVER IS LOOSE. MAINTENANCE REATTACHED THE EXIT SIGN. OPERATIONAL CHECK IS GOOD.SDR HALA2018072300337Duct · disconnectedON GROUND WITH APU RUNNING. PODS FAILED. TAIL TEMP HIGH. CHECK FOUND THE RT PACK OUTLET DUCT DISCONNECTED IN AFT ACCESSORY BAY. RECONNECTED THE RT PACK OUTLET DUCT. RAN APU, LEAK AND SECURITY CHECKED OK.SDR DALA2018072304610Spar · crackedNR 1 HOLE FROM TOP RT VERT STAB FRONT SPAR HAS CRACK INDICATION. REPAIR COMPLETE REF ER/A 570300-14AD ORIGINAL. ASSOCIATED ER/A 14-570300.SDR DALA201808145057Skin · crackedMAINTENANCE REPORTED A CRACK IN ONE OF THE RT LEADING EDGE SKIN. REPAIRED IAW ER/A 570300-14AD, REV O.SDR DALA201808145056Skin · crackedMAINTENANCE REPORTED A CRACK IN ONE OF THE RT LEADING EDGE SKIN ATTACH FASTENER HOLES. THE HOLE IS THE NR 1 ABOVE ZFS 52.267. REPAIRED IAW ER/A 570300-14AD, REV O.SDR HALA2018072300330Inverter · inoperativeWHEN TESTING ELEC EMERGENCY POWER GOT A/C EMER BUS OFF LT. REMOVED AND REPLACED STATIC INVERTER PER AMM 24-24-01. OPS CHECK GOOD PER AMM 24-24-00-720-803.SDR DALA2018072304611Battery Pack · dischargedTHE EMERGENCY OVERWING LIGHT WOULD NOT TURN OFF. REPLACED OVERWING LIGHT BATTERY PACK PER AMM 33-51-06.SDR HALA2018072000326Smoke Detector · no testFWD CARGO SMOKE DETECTOR NR 8 FAILED TO TEST. REMOVED AND REPLACED THE SMOKE DETECTOR IAW AMM 26-13-01. OPS CHECKED AND SECURITY CHECKED GOOD.SDR HALA2018072000327Smoke Detector · false activationCARGO SMOKE FWD FAILED. PERFORMED AN OPS TEST OF THE SMOKE DETECTION SYSTEM IAW FIM 26-13 TASK 801. OPS CHECKED GOOD. OK FOR SERVICE.SDR DALA2018071704513Fuel Filter · leakingDISCOVERED FUEL LEAK FROM NR 1 ENGINE WHILE AIRBORNE. FOUND FUEL LEAKING FROM LEFT ENGINE LOW PRESSURE FUEL FILTER. HELICOIL HAD BACKED OUT OF FILTER HOUSING AND O-RING DEFORMED AND LEAKED. R&I LEFT ENGINE LOW PRESSURE FUEL FILTER HOUSING PER AMM 73-11-01. R&ISDR DALA2018071604493Light · damagedTHE EMERGENCY SEAT MOUNTED LIGHTING IS DAMAGED AND INOPERATIVE AT SEAT 27C. MAINTENANCE RESECURED THE PANEL. OK FOR SERVICE.SDR DALA2018071604492Sign · looseTHE EMERGENCY EXIT SIGN COVER AT DOOR 1L IS LOOSE. MAINTENANCE RESECURED EXIT THE EEPL SIGN AT 1L DOOR. AIRCRAT IS OK FOR SERVICE.SDR DALA2018071604487Power Supply · inoperativeTHE AFT DOOR EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY IAW AMM 33-51-03. OPERATIONAL CHECK WAS GOOD.SDR DALA2018071604490Light · unsecureTHE FORWARD MOST EMERGENCY EXIT LIGHT IS NOT SECURELY FASTENED TO THE CEILING AS DESIGNED. MAINTENANCE SECURED THE LIGHT ASSEMBLY AS REQUIRED. OK FOR SERVICE.SDR DALA2018071104447Skin · corrodedON WALKAROUND FOUND AFT LAV PANEL SKIN CORRODED AND BULGING. REPAIRED ON N/R 1, REF ERA 569907-14.SDR DALA2018070504367Strake · damagedCOMPOSITE DAMAGED/MISSING. LT WING STRAKE. LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0275:0593-2011/009 00096 C/W TASK CARD.SDR DALA2018070404366Cowling · crackedCRACKS ON INLET COWL BULLNOSE AROUND FASTENERS IN INTERIOR MARKED. REPLACED NR 1 ENGINE INLET COWL REF AMM 71-11-05.SDR DALA2018070404359Light · brokenFOUND EMERGENCY LIGHT L2-938 BROKEN AFT COMPARTMENT. REPLACED TERMINALS NEEDS LIGHT ASSY MOUNTED. MOUNTED LIGHT ASSY CKS GOOD.SDR DALA2018070304341Light · inoperativeEMERGENCY ESCAPE PATH LIGHT INOP AT 22CDE. R&R ASSY PER AMM 33-51, OPS NML.SDR DALA2018070304339Access Panel · damagedFOUND DAMAGED ACCESS PANEL ON LT ELEVATOR INBD. MANUFACTURED NEW ACCESS PANEL PER DRAWING 5910412. TREATED AND PAINTED PER SRM 51-22-01-0G. OKAY FOR SVC.
Back to Boeing 717-200