Boeing 717-200
Service difficulty reports · 18,752
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 ASAA2025110261561Socket · failedSEVERAL EMERGENCY LIGHTS INOPERATIVE AT ROW 17. GROUNDED - YES. REMOVED AND REPLACED BATTERY AND POWER SUPPLY AT ROW 17. CONDITION SAME 5742. 11/02/2025. NS 23-51-03. REPAIRED SOCKET AND CONNECTOR P1-6738 PER SWPM 20-31-01. OPS CHECK GOOD. ACFT OK TO CONTINUE SDR DALA2025110708144Sign · damagedSHIP 9526 FORWARD CENTER OVERHEAD EXIT SIGN DAMAGED. CORRECTIVE ACTION: R/R FWD ISLE EMERGENCY LIGHT SIGN IAW B717 AMM 33-51. OPS CHECK GOOD. (7608370)SDR DALA2025110708137Light · inoperativeRT OVERWING EMERGENCY EXIT LIGHT NOT OPERATIONAL. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT PER B717 AMM 33-51. (8143300)SDR DALA2025110708135Slide · unpackedIN REF. TO AMDS 5211-4001: EMERGENCY SLIDE PACK WAS FOUND UNFOLDED, DOOR L1 WAS REPLACED UNDER AMDS 97-2561-9-0003 AND AMDS 2561- 9004 (1281137)SDR DALA2025110708147Girt Bar · detachedSHIP 9504 DOOR 1R GIRT BAR DETACHED FROM SLIDE MECHANISM. CORRECTIVE ACTION: RESECURED PER B717 AMM 25-61. A/C OK FOR SERVICE. (7954750)SDR DALA2025110708139Skin · crackedCRACK SKIN INSIDE OF ACCESS PANEL 370BL FWD /UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN. CORRECTIVE ACTION: UPPER CORNER AT VERTICAL STABILIZER DORSAL FIN WAS REPAIRED PER B717 SRM 55-30-01 (1278507)SDR DALA2025103107965Vane · puncturedINSPECTION: PUNCTURE ON FWD MOVABLE VANE LOWER SURFACE AT LT WING. FWD MOVABLE VANE LOWER SURFACE AT LH WING WAS REPAIRED IAW SRM 57-53-01 (1277612).SDR DALA2025103107964Longeron · crackedCRACKED LONGERON 2R AT BS 1133. LONGERON 2R REPAIRED IAW SRM 53-00-05. (1277454)SDR DALA2025110708148Latch · dirtySHIP 9575 1L DOOR GRIT BAR VERY DIFFICULT TO ARM SLIDE. CORRECTIVE ACTION: FOUND BOTH 1L DOOR RETENTION LATCHES STICKY AND DIRTY. CLEANED AND VERIFIED NORMAL OPERATION REF B717 AMM 25-61. (7816646)SDR DALA2025103107968Hinge Fitting · excess playRT WING FLAP O/B HINGE HAS EXCESSIVE PLAY. REPAIRED PER ERA/PRI 629650-14 REV. A (1274899).SDR DALA2025103107966None · noneMONITOR LOG FOR ER/A 619015-14AD REV A SECTION II. COMPLY WITH SECTION II OF ER/A 619015-14AD (1275112)SDR DALA2025103107963Wire · brokenBROKEN WIRES ON ESCAPE SLIDE LANYARD ASSEMBLY (2 EA) AT R1 & L1 DOOR. LANYARDS ASSEMBLIES AT L1 DOOR AND R1 DOOR WERE REPLACED & VERIFIED IAW AIPC 25-61-01-01 TEM 95 & AIPC 25-61-03 (1275291).SDR DALA2026020900908Skin · damagedERA 630089-14, SECTION I, ISSUED FOR BIRD STRIKE DAMAGE TO RT HORIZONTAL STAB LEADING EDGE INBD STRUCTURE. REPAIRED IAW ER/A 630089-14. (1269533)SDR DALA2025103107961Fuel Cell · leakingFUEL LEAK FOUND DURING INSPECTION OF THE LT WING AFT LOWER SKIN DOUBLER XRS=164. : COMPLIED WITH PRI 629418-14AD (1268439).SDR DALA2025103107969Fuel Cell · leakingFUEL LEAK FOUND DURING INSPECTION OF RT WING AFT LOWER SKIN XRS=164. RT WING AFT LOWER SKIN DOUBLER XRS=164, & RT WING REAR SPAR LOWER CAP. COMPLIED WITH PRI 629419-14AD (1268436).SDR DALA2025102407794Rib · damagedHOUR GLASS PANEL LOWER WING RIB, UPPER ROW, FWD FASTENER HOLE DAMAGED. REPAIRED PER PRI 630032-14 REV. 0, 1 AND 2 AND ER/A 630032-14 REV ORIGINAL. (1267567)SDR DALA2025102407795Access Panel · damagedFOUND FASTENER HOLE OUT OF ROUND AT TANK PLATE 520HB. REPAIRED REF ERA 629530-14 REV O (1265545)SDR DALA2025102407792Doubler · not reportedEXISTING REPAIRS FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED DOUBLER INSPECTION PER ERA 625837-14 AD (7976471)SDR DALA2025102407797Warning Message · false activationATO- DURING TAKEOFF ROLL THE CREW REPORTED A STAB OUT OF TRIM AURAL WARNING AND ABORTED TAKEOFF. MAINTENANCE PERFORMED STABILIZER SYSTEM TESTS AND RETURNED TO SERVICE.(7843690)SDR DALA2025102407790Spar Cap · noneRH WING / REAR SPAR / LOWER CAP / AFT FLANGE / XRS = 164 / CRITICAL HOLE INSPECTION. PRI 629860-14AD REQUIRES ACCOMPLISHMENT WHILE IN BHM. ACCOMPLISH PRI 629860-14AD WHILE IN BHM OCT-2025 MAINTENANCE VISIT. (1263856)SDR DALA2025102407793Roller · faultedRETURNED TO ATLANTA DUE TO A LEFT GEAR UNSAFE INDICATION. PERFORMED TROUBLE SHOOT PER B717 FIM 32-60. REPLACED EMERGENCY RELEASE ROLLER FOR LEFT GEAR. TEST GOOD.(7707462)SDR DALA2025102207717Seal · fodDIVERTED TO BOS DUE TO R1 GALLEY DOOR HIGH PITCH SQUEAL. CLEANED DEBRIS & LUBED DOOR SEAL, PRESSURIZED AIRCRAFT. NO DEFECTS NOTED.(7584826)SDR DALA2025102207715Cable · twistedSHIP 9520 DURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. CORRECTIVE ACTION: PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER B717-200 AMM 53-52-01-830-802 ONLSDR DALA2025102207714Cable · twistedDURING SSE WAS FOUND TWISTED PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT. PULL CABLE OF TAIL CONE RELEASE SISTEM AT AFTER ACCESSORY COMPARTMENT WAS INSTALLED CORRECTLY PER AMM 53-52-01-830-802 ONLY STEP E. (1) (S). (1262180)SDR DALA2025102207719Sensor · faultedRETURNED TO AGS DUE TO A LEFT GEAR UNSAFE INDICATION. MAINTENANCE REPLACED THE LEFT DOOR UP AND LATCHED SENSOR. CYCLED GEAR OPS CHECK NORMAL.(7707452)SDR DALA2025102207716Door Frame · crackedSHIP 9520 CRACK OF 0.350IN LENGTH WAS FOUND ON LH OVERWING FRAME STA Y=737 IN REFRENECE TO CARD 5310-01439-01B / JOB 068-0003, STEP 4. LEFT OVERWING FRAME STA Y=737 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (1258141)SDR DALA2025102207713Seal · leakingDURING STATIC LEAK CHECK, WATER LEAKS WERE FOUND ON INSIDE OF FWD AND AFT LT OVERWING EMERGENCY EXIT DOORS. EXIT DOOR JAMB FILLER FWD AND AFT LT WERE REPLACED PER AMM 53-12-01 AND STATIC LEAK CHECK WAS PERFORMED PER AMM 52-21-01-790-801 AND NOT LEAKS WERE FOSDR DALA2025102207712Fuel Tank · corrodedEXFOLIATION ON LOWER SKIN OF CENTER FUEL TANK ON STA Y= 756 AND X= 43 AT LEFT MLG WHEEL WELL. LEFT MLG WHEEL WELL WAS REPAIRED PER ER/A 629799-14AD REV. (1258160)SDR DALA2025102207718Battery Pack · inoperativeCREW REPORT EXIT SIGN F/C INOP (EMERRGENCY LIGHT). FOUND BATTERY PACK B5-259 INOP, REPLACED BATTERY PACK. OPS CHEC K GOOD, IAW B717AMM 33-51. (7585679)SDR DALA2025102207711Release Mech · out of positionIN REFERENCE AMDS 5352-4002 DURING INSTALL TAILCONE SLIDE WAS FOUND TAILCONE RELEASE MECHANIS CAM OUT POSITION. TAILCONE RELEASE MECHANISM CAM WAS ADJUSTED PER AMM 53-52-03 (1257600)SDR DALA2025101707597None · noneSHIP 9544 REPETITIVE INSPECTIONS WITHIN FORTY-SIX HUNDRED (4,600) FLIGHT CYCLES UPON ER/A 617313-14. CORRECTIVE ACTION: C/W REPAIRED PER ERA 617313 (1255743).SDR DALA2025101707596Not Reported · not reportedSHIP 9544 ACCOMPLISH ER/A 617313-14 REV A. CORRECTIVE ACTION: REPARIED PER ER/A 14-617313. (1255302)SDR DALA2025101707595Spar Cap · crackedSHIP 9506 CRACK WAS FOUND ON HOLE 6 HRS AT STA ZFS=51.267 APROX. FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE. CORRECTIVE ACTION: REPAIR ON FRONT SPAR CAP FORWARD FLANGE VERTICAL STABILIZER LH SIDE WAS PERFORMED PER PRI 606161-14 (1254228)SDR DALA2025101707598Idg · faultedSHIP 9547-MISC/DE- ON DESCENT THE CREW RECEIVED A "RT GEN OFF" MESSAGE WITH THE APU ON MEL. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL RTS TESTS.(7586116)SDR DALA2025101707594Skin · damagedFASTENERS (45 EA) ON VERTICAL STAB LEADING EDGE PREVIOUS REPAIR STA ZFS =52. CORRECTIVE ACTION: VERTICAL STAB LEADING EDGE REPAIR STA ZFS =52 WERE REMOVE AND INSTALL PER CARD 5530-01048-02 AND DVI WAS PERFORMED ON RH/LH VERTICAL STAB LEADING EDGE STRUCTURE SPLSDR DALA2025101707599Oil System · leakingSHIP 9547 OIL FUMES PRESAENT IN COCKPIT AND FORWARS GALLEY WITH APU RUNNING AND LEFT PACK IN AUTO. COCKPIT SMELLED OF FRESH OIL & GALLEY SMELLED OF BURNED POPCORN. CORRECTIVE ACTION: CLEAN AND BURN OUT THE PNEMATIC HIGH PRSSEURE DUCTING PER B717 AMM 21-51. OPESDR HALA20251015052Accumulator · blownBRAKE PRESSURE LOW PULLING UP TO THE GATE. FOUND LT BRAKE ACCUMULATOR BLOWN. REMOVED AND REPLACED LT BRAKE ACCUMULATOR IAW AMM 32-44-01, OPS & LEAK CHECKED GOOD. OK FOR SERVICE.SDR DALA2025101707593Skin · wornSHIP 9528 LEADING EDGE UPPER SKIN PANEL / FASTENERS WORN ALONG OUTER PERIMETER. CORRECTIVE ACTION: REPAIRED PER ER/A 620349-14 (1245364).SDR DALA2025101707592None · noneSHIP 9520 DTA ER/A 629799-14 SECTION II MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 10-OCT-25. CORRECTIVE ACTION: REPAIRED PER DTA ER/A 629799-14 (1250137)SDR DALA2025101707591Service Panel · corrodedSHIP 9506 CORROSION ON LOWER AREA OF LAVATORY SERVICE PANEL BTW TRAY-PANEL AND PREVIOUS REAPAIR INTERNAL FILLER. CORRECTIVE ACTION: REPAIRED PER ER/A 542102- 14 REV. (1245325)SDR DALA2025101707590Fuel Cell · leakingFUEL LEAK FOUND DURING INSPECTION OF THE L/H WING AFT LWR SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: REPAIRED PER ER/A 14-621176. (1243963).SDR HALA20251010051Battery Pack · inoperativeCENTER EXIT SIGN INOP. REPLACED EMERGENCY BATTERY AND POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD.SDR DALA2025101407521Vane · dentedDISBOND OF 2.300IN X 3.100IN. ON DENT LOCATED AT LH AFT MOVABLE FLAP VANE, LOWER SURFACE. REPAIRED PER B717-200 SRM 57-53-01-2R (1239681)SDR DALA2025100807355Door · openATB- PERFORMED AN AIR TURN BACK DUE TO A NOSE GEAR AREA VIBRATION. MAINTENANCE CLOSED THE NOSE GEAR DOORS, CONFIRMED THE SECURITY AND CONDITION OF THE DOORS AND SURROUNDING AREA AND RETURNED TO SERVICE.(7585642)SDR DALA2025101407519None · noneDTA ER/A 542233-14 REV D REPAIR MONITOR LOG REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS AFTER 04-OCT-25. C/W ER/A 542233-14. (1245089)SDR DALA2025101407522Sensor · faultedON THE GROUND ON APU POWER WHEN RT PACK TURNED ON, DID NOT COME ON. SMELLED SMOKE & THEN GOT PACK R FLO DISAG. TURNED SWITCH OFF AND SMELL WENT AWAY. R & R RT AIRFLOW SENSOR REF AMM 21-52. OPS CHK NML NO FAULTS, GOOD AIRFLOW. MEL/PLAC REMOVED. REVERSED M PRSDR DALA2025101407520Spar · corrodedWORKING PRI 629584-14 REV 0, REV1, REV 2, REV 3, AND ERA 629584- 14AD REV ORIG. LT REAR SPAR XRS 179 CORROSION. ACCOMPLISHED PRI 629584-14AD REV 3 LT WING REAR SPAR XRS 179 REPAIR. SFAR 88 AND CDCCL REQUIREMENTS C.W. (1232961)SDR DALA2025100807327Sealant · not reportedWORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717 51-24-00 & DWG'S. C/W STEP 19 OF ERA 629612-14AD (1239562)SDR DALA2025100807326Skin · leakingWORKING PRI 629612-14, RH WING LOWER SKIN XRS 164 FUEL SEEP. C/W SECTION I LEAK EVALUATION OF ERA 629612-14AD (1231435)SDR DALA2025092907060Release Cable · tornINITIAL INSPECTION: TORN CABLE OF RELEASE MECHANISM OF TAIL CONE AT AFT ACCESORIES COMPARTMENT. CORRECTIVE ACTION: CABLE ASSY RELEASE HANLDE P/N: 3913359-545 OF RELEASE MECHANISM OF TAIL CONE WAS REPLACED PER B717-200 AMM 20-00-02 AND ADJUSTED WAS PERFORMED PE
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