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 DALA2019061303544Seat Track · corrodedCORROSION ON F.O. LOWER OUTBOARD SEAT TRACK. NRC 00559: CORROSION LEVEL 2, SEAT TRACK WAS REPLACED PER B717-200 SRM 51-41-01-0G.SDR DALA2019061303542Frame · crackedCRACK ON FRAME, LONG 17LH STA 1037 (CPAX). NRC 00402: FRAME STA 1037 AT LONG 17LH WAS REPAIRED B717-200 SRM 53-20-07-2R-4. (LP #1120245)SDR DALA2019061303543Frame Angle · crackedCRACK ON CLIP FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00398: FRAME LONG 16RH STA 1022 AT FWD FACE OF BULKHEAD WAS REPLACED PER B717-200 SRM 51-41-05-0G AND DWG #9912243 REV. JS. (LP #1120252)SDR HALA2019061200292Smoke Detector · faultedCGO AFT SMOKE DETECTOR FAULT DISPLAYED. PER FLT CREW. // RESET C/B S29, 30, 31 AND PERFORMED TEST ON CARGO SMOKE. MSG EXTINGUISHED.SDR DALA2019061203520Frame · crackedCRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN (CPAX). NRC 00242: CRACK ON RING PAN UPPER AFT CORNER STA Y:832 RH SIDE AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 56-20-02 REPAIR 1. (LP #1118572)SDR DALA2019061203519Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 (CPAX). NRC 00432: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=7 WAS REMOVED PER B717-200 SRM 51-10- 04 PAR 26. REMAINING THICKNESS OF 0.003" IS OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG.SDR DALA2019061203518Access Panel · corrodedEXCESSIVE CORROSION ON FUEL ACCESS PLATES #520PB AND #520DT.(AI). NRC 00667: CORROSION ON FUEL TANK ACCESS DOORS #520DT AND 520PB OF LH WING WAS REMOVED PER B717-200 SRM 51-10-04-0G PAR 26 AND 57-10-01-2R REPAIR 2 PAR. 5. REMAINING THICKNESS WAS OUT OF LIMITS SDR DALA2019061103517Frame Angle · crackedCRACK ON CLIP FRAME LONG 5LH STA 1022 AT FWD FACE OF BULKHEAD (CPAX). NRC 00393: FRAME CLIP LONG 5LH STA 1022 WAS REPAIRED PER B717-200 SRM 53-00-06-2R-2. (LP #1117079)SDR DALA2019061103499Cusp Web · corrodedRH CORROSION CUSP MEMBRANE BTW STA Y=936 TO Y=942 AT CPAX IN REFERENCE NRC #341 IS OUT OF LIMITS. NRC 00613: CORROSION LEVEL 2, CUSP MEMBRANE BTW STA Y=936 TO Y=942 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 215.SDR DALA2019061103498Access Door · corrodedCORROSION ON FUEL TANK ACCESS DOOR #520CT AND #620CT OF WING LEFT -RIGHT. (AI) (AD). NRC 00609: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND #620CT WERE REPLACED AND PART NUMBER WAS VERIFIED PER B717-200 IPC 57-22-01-01 ITEM 065.SDR DALA2019061103497Longeron · crackedCRACK ON LONGERON 5LH STA 1022 (CPAX). NRC 00387: SECTION LONGERON 5LH FROM STA 986 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1116805)SDR DALA2019061103496Floorbeam · corrodedCORROSION ON FLOOR SUPPORT AT STA 148 FROM X=-31/-44 (CPIL). NRC 00560: LEVEL CORROSION 2, FLOOR SUPPORT AT STA 148 FROM X=-31/-44 WAS REPLACED PER B717-200 SRM 51-41-02-0G. ORIGINAL THICKNESS WAS 0.040" REMAINING THICKNESS IS 0.019", THEREFORE IT IS OUT OF LISDR DALA2019061103495Skin · dentedDENTS ON FUSELAGE SKIN AT STA 427 BETWEEN LONGERON 27L AND 29L. ACCOMPLISHED PERMANENT REPAIR REF PRI #578768-14, REV. 1 AND ER/A #578768 -14 REV. ORIGINAL. REQUIRED INSPECTION COMPLETE QC1981. (LP #1116346)SDR DALA2019061103494Longeron · crackedCRACK ON LONGERON 3RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00394: SECTION OF LONGERON 3RH FROM STA 1010 TO 1053 WAS REPLACED PER B717-200 SRM 53-00-05-2R. (LP #1115922)SDR DALA201906113493Longeron · crackedCRACK ON LONGERON 5RH STA 1022 AT AFT FACE OF BULKHEAD (CPAX). NRC 00395: SECTION OF LONGERON 5RH BTW STA 1010 TO 1053 WAS REPAIRED PER SRM 53-00-05-2R. (LP #1115229)SDR DALA201906113492Longeron · crackedCRACK ON LONGERON 6LH STA 1022 (CPAX). NRC 00386: SECTION LONGERON WAS REPLACED PER B717-200 SRM 53-00-05-2R-2. (ET) HFEC INSPECTION WAS PERFORMED ON LONGERON 6LH STA 1022 (CPAX) ON TRIM OUT. NO CRACKS WERE FOUND PER B717 NDT SPM PART 6. 06-10-01.001. (EQ. NORSDR DALA201906113491Cusp Web · corrodedCORROSION CUSP MEMBRANE BTW STA Y=559 TO Y=562 AT CPAX IN REFERENCE NRC #338 IS OUT OF LIMITS. NRC 00612: CUSP MEMBRANE BTW STA Y=559 TO Y=562 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114952)SDR DALA201906113490Cusp Web · crackedCRACK AT CUSP WEB STA 660 RH X=-44/-60 (FUS). NRC 00366: CRACK AT CUSP WEB STA 660 RH X=-44/-60 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #1114893)SDR DALA201906113489Skin · dentedDENT ON FUSELAGE SKIN AT STA 524 TO 527 1" BELOW LONG 26L LAP SEAM. PER B717 SRM 53-01-01-1A-3 CONDITION 5 DENT IS OUT OF LIMITS. REMOVED DAMAGE 1" X 3" PER B717 SRM 53-03-01-2R-1 FIG. 110 SHEET 3. FUSELAGE SKIN MISDRILLED AT STA 520 ON LONG 26L, REMOVED DAMAGSDR DALA2023031702018Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702014Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 503 AND LONGERON 19. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702013Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 465 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702012Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 446 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702011Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 332 AND LONGERON 20. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702010Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 313 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR DALA2023031702009Unknown · unknownAIRCRAFT 9577, FOUND EVIDENCE OF LIGHTENING STRIKE ON RH FUSELAGE AT STATION 256 AND LONGERON 21. CORRECTIVE ACTION: REMOVED FASTENER WIP 715288. REPAIRED PER B717 SRM 53-02-01-2R PROCEDURE 1. TEMPORARY REPAIR REQUIRES VISUAL INSPECTION AT 3000 CYCLES, PERMANESDR HALA2019061000286Eec · malfunctionedATB - ENG L SYS FAIL ENROUTE FOLLOWED BY REV L FAULT. PERFORMED EEC1 RTS TEST. TEST FAILED. EEC BOX FAULT. REMOVED & REPLACED EEC1 PER AMM 73-21-01. RTS TEST PASSED. PERFORMED FUNCTIONAL CHECK OK L REV PER AMM 78-30-00-720-801. OPS NORMAL. OK FOR SVC.SDR DALA2019060903462Wire · pinchedON TAXI OUT WHEN CHECKING CONTROLS THE WHEEL BECAME STUCK FULL RIGHT. FOUND WIRING INTERNAL ON DUAL AILERON SERVO PINCHED AND WIRING EXSPOSED. DUAL AILERON SERVO WAS REPLACED PER B717 AMM 22-12. FAILED AILERON RTS TEST. REPLACED THE SERVO A SECOND TIME PER B71SDR DALA2019060903461Battery Pack · inoperativeTHE LEFT ENTRY DOOR EMERGENCY LIGHT WENT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW B717 AMM 33-51-03.SDR DALA2019060903460Charger · inoperativeFOUND AFT WING EMERGENCY EXIT DOOR LOWER LIGHTS INOPERATIVE ON BOTH THE LEFT AND RIGHT SIDES. MAINTENANCE REPLACED THE BATTERY CHARGER B5-119 PER B717 AMM 33-51. NO HELP. NO POWER AT TERMINAL BLOCK 53-388 PIN 1. FOUND NEW BATTERY CHARGER BAD FROM STOCK. REPLACSDR DALA2019060903459Floor Panel · crackedCRACK ON FLOOR PANEL #223GF PAX CABIN. FLOOR PANEL #223GF WAS FABRICATED, REPLACED, AND IDENTIFIED PER B-717-200 SRM 53-20-50-2R-3. (LP #1113427)SDR HALA2019061400298Structure · crackedA 1 INCH CRACK WAS FOUND ON THE LH THRUST REVERSER INTERIOR SURFACE. CLEANED AREA, STOP DRILLED THE CRACK WITH A 0.19 IN. DIAMETER HOLE. PERFORMED A DETAILED VISUAL INSPECTION UNDER SUFFICIENT LIGHTING OF THE DAMAGED AREA. APPLIED CORROSION PROTECT AND PRIMESDR HALA2019060700281Actuator · malfunctionedATB - ON APPROACH, AFTER GEAR EXTENSION "GEAR DOOR OPEN" ALERT CAME ON. RECYCLED THE GEAR AGAIN AND ALERT CAME ON. GEAR WAS DOWN AND 3 GREEN. NORMAL GEAR INDICATION WITH NO ALERT. AIRCRAFT RETURNED TO THE DEPARTING STATION, WHERE AN UNEVENTFUL LANDING WAS MADESDR DALA2019060603431Power Supply · malfunctionedEXIT LIGHT OVER TAILCONE EXIT AND AIRCRAFT RIGHT STANDBY EMERGENCY LIGHT FLICKER INTERMITTENTLY DURING ALL PHASES OF FLIGHT. MAINTENANCE RE-SET AFT POWER PACK AND THE FLICKER CEASED. OPERATIONAL CHECK WAS GOOD REF B717 AMM 33-51. (LP #6285367)SDR DALA2019060603430Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 604. MAINTENACE REINSTALLED THE CABIN SIDEWALL LIGHT LENS, (LT SIDE).SDR DALA2019060503399Beam · crackedCRACKED BEAM #4 FWD EDGE AT FWD GALLEY SERVICE DOOR (R1) (PTAS). NRC 00342: BEAM #4 AT FWD GALLEY SERVICE DOOR WAS REPLACED PER B717-200 SRM 51-41-01-0G , 51-41-02-0G, AND 51-41- 05-0G. (LP #1106564)SDR DALA2019060503400Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS IN THE CABIN ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACKS B5-118 AND B5-230 REF B717 AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6252202 )SDR DALA2019060303372Battery Pack · inoperativeBOTH AFT OVERWING EXIT DOOR SIGNS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK B5-230. OPERATIONAL CHECK IS GOOD REF B717 AMM 33-51. OK FOR SERVICE. (LP #5813918)SDR DALA2019060323371Floorbeam · corrodedCORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 (CPAX). NRC 00433: CORROSION LEVEL 2, CORROSION ON FLOOR SUPPORT AT STA 200 FROM X=09/13 WAS REMOVED PER B717-200 SRM 51-10-04 PAR 26 DUE TO BEING OUT OF LIMITS PER B-717-200 SRM 53-00-00-1A FIG 103. FLOOR SUPSDR DALA201906031370Threshold · corrodedCORROSION FOUND AT AFT CARGO DOOR THRESHOLD. REPAIRED REF B717 SRM 53-20-15-2R-7-REPAIR 7. (LP #1100474)SDR 2019F00222Skin · delaminatedLARGE DISBOND, SKIN CORROSIONSDR DALA2019060303373Lens · damagedTHRESHOLD LIGHT LENS COVER DAMAGED ABOVE AFTJUMPSEAT. FORWARD TO MEL 33-52-01. PLACARDS INSTALLED. R&R LENS COVER IAW B717 AMM 33-25. OK FOR SERVICE. MCO/PLAC REMOVED. (LP #1099186)SDR DALA2019052703202Access Panel · damagedELONGATED HOLES ON FUEL TANK ACCESS PLATE #520LB ON LT WING (AI). NRC 00365: ACCESS PLATE WAS REWORKED WITH COUNTERSINK BUT THE EXCESSIVE DAMAGE IS OUT OF LIMITS PER SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II. FUEL ACCESS PLATE #520LB WAS REPLACED AND PART NUMBSDR DALA2019052703201Access Panel · corrodedCORROSION ON AREA SETTLEMENT AND COUNTERSUNK AT FUEL TANK ACCESS PLATES #520DB, 520CB, AND 520DT ON LT WING (AI). NRC 00363: CORROSION LEVEL 2, CORROSION ON FUEL TANK ACCESS PLATES #520DB, 520CB, AND 520DT ON LT WING WERE REPLACED AND PART NUMBERS VERIFIED PERSDR DALA2019052703200Access Panel · corrodedCORROSION ON AREA SETTLEMENT AND COUNTERSUNK AT FUEL TANK ACCESS PLATES #620FT, 620LB, AND 620DB ON RT WING (AD). NRC 00368: CORROSION LEVEL 2, CORROSION ON SETTLEMENT AREA AND COUNTERSINK HOLES AT FUEL TANK ACCESS PLATES #620 FT, 620LB, AND 620DB OF RT WING WSDR DALA2019052603199Skin · crackedCRACK AT FUSELAGE SKIN STA 1133 BETWEEN LONG 2/3 RT. (FUS). CRACK WAS REPAIRED PER ETI-17-19-065 R4 AND ER/A 578449-14AD REV. ORIGINAL. ASSOCIATED ER/A 00-578449 ADDED FOR AC 9576. (LP #1091843)SDR DALA2019052603198Seat Track · corrodedCORROSION ON RT TIE TRACK FROM STA Y=813 TO Y=954 AND STA Y=994 TO Y=1028 IN REF AMDS 5314-2001. (CCT). NRC 00253: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER SRM 51-41-01-0G. (LP #1091207)SDR DALA2019052303147Skin · crackedCRACK AT FUSELAGE SKIN STA 1076 BETWEEN LONG 13/14 RT. (FUS). NRC 00128: FUSELAGE SKIN STA 1076 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-063 R2 AND ER/A 578372-14 REV. ORIGINAL. SECTION I. ASSOCIATED ER/A 00-578372 ADDED FOR AC 9576 (LP #1086983)SDR DALA2019052303146Skin · crackedCRACK AT FUSELAGE SKIN STA 1037 BETWEEN LONG 13/14 RT. (FUS). NRC 00127: FUSELAGE SKIN STA 1037 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-064 R3 AND ER/A 578307-14 REV. ORGINAL. ASSOCIATED ER/A 00-578307 ADDED FOR AC 9576. (LP #1086863)SDR DALA2019052303145Skin · crackedCRACK AT FUSELAGE SKIN STA 1022 BETWEEN LONG 13/14 RT. (FUS). NRC 00126: FUSELAGE SKIN STA 1022 BETWEEN LONG 13/14 RT WAS REPAIRED PER ETI-17-19-064 R3 AND ER/A 578307-14 REV. ORGINAL. ASSOCIATED ER/A 00-578307 ADDED FOR AC 9576 (LP #1086861)
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