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 HALA2022012500029None · noneC CHECK MAJOR REPAIR - DURING ROUTINE MAINTENANCE TASKS, A CRACK IN THE FUSELAGE AT STATION 1022 AT LONGERON L-14L, AND WAS FOUND ON BOTH THE SKIN (PN 5936436-101) AND ON THE FINGER DOUBLER (PN 5936436-39) BELOW. A 3.8 INCH X 1.1 INCH SECTION WAS CUT OUT OF TSDR HALA2022012500028None · noneC CHECK MAJOR REPAIR - CRACK IN LH FUSELAGE FRAME GUSSET AT STA 1022, L-7L // REPAIRED PER SR#3-5198890164SDR DALA2022012500495None · noneCRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R. SUMMARY OF NRC 00057: CRACK ON FUSELAGE SKIN STA Y=1133 AND ABOVE LONGERON 2R WAS REPAIRED PER ETI-17-22-001 REV. 3 AND ER/A 596558-14AD SECTION I. PERMANENT REPAIR REPAIR APPROVAL IS LIMITED TO 60,000 FSDR HALA2022012500030None · noneA CHECK MAJOR REPAIR - THRU BLEND ON RT WING LOWER SKIN AT XRS 535, RS AND REAR SPAR CAP BLEND NEAR XRS 534 // REPAIRED PER E105-488206-PERMSDR DALA2022012000391None · noneTHE EMERGENCY LIGHTS BATTERY PACK AT B5-119 WAS INOPERATIVE FOR ROW 20DC EMERGENCY PATH LIGHTS. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT B5-119. THE EMERGENCY LIGHTS OPERATIONAL CHECK WAS NORMAL REF B717 AMM 33-51-04. (LP #5363034)SDR DALA2022012000390None · noneA FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY EXIT SIGN AT L1 DOOR IS FLICKERING. MAINTENANCE REPLACED THE B5-235 BATTERY PACK. OPERATIONAL CHECK IS GOOD. (LP #8380198)SDR DALA2022030301343None · noneTHE FUSELAGE INTERCOSTAL WAS FOUND CRACKED AT BEND STA 1212 STA 1225, WHICH AFFECTED THE TAILCONE DEPLOYMENT CABLE ATTACH POINT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. A TEMPORARY REPAIR WASSDR DALA2022011700299None · noneCORROSION ON PAN BTW STA Y=954 TO Y=994 AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 00008: CORROSION LEVEL 2, PAN BTW STA Y=954 TO Y= 994 AT AFT CARGO DOOR JAMB WAS REPAIRED PER B717 SRM 53-20-15-2R REPAIR 7. (LP #2088850)SDR HALA2022011800015Bracket · looseEMER EQ - COCKPIT EMERGENCY EXIT WINDOW FO SIDE WILL NOT CLOSE // FOUND F/O LOWER TRACK SUPPORT BRACKET AFT BOLT LOOSE. REIINSTALLED NEW BOLT, OP HECK GOOD OK FOR SERVOCE, PER AMM 56-12-30.SDR DALA2022011700298None · noneCRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L. SUMMARY OF NRC 00056: CRACK ON FUSELAGE SKIN STA Y=1022 BTW LONGERON 7L AND 8L WAS REPAIRED PER B717-200 SRM 53-03-01-2R, REPAIR 1 STEP 6 PAR G, FIG 20. REQUIRES VISUAL REPETITIVE (8,000 CYCLES) INSPECTSDR HALA2022011800016Cable · inoperativeEMER EQ - LFT MAIN CABIN DOOR EMER SLIDE ARMING CABLE INOP // REMOVED AND REPLACED 1L DOOR EMERG SLIDE ARMING CABLE. SECURE OK TO CONTINUE.SDR DALA2022011800324Longeron · corrodedCORROSION AT LONGERON 30 BETWEEN STA 904 AND STA 927. SUMMARY SEE NRC 088-0008:5331-2001/007 00377: REPLACED LONGERON 30 BETWEEN STA 904 AND STA 927 PER B717 SRM 51-40-02. CORROSION LEVEL:2 . (LP #2086514)SDR DALA2022011400280None · noneCORROSION STA 927 TO 946 AT LONGERON 30 AND SPLICE. SUMMARY SEE NRC 088-0008:5331-2001/011 00381: REMOVED CORROSION AND CHECKED LIMITS STA 927 TO 946 LONGERON 30 PER B717 SRM 53-00-00. REPLACED SPLICED PER B717 SRM 53-20-05-2R. (LP #2085655)SDR 2022FA0000020Spoiler · corrodedSPOILER WAS FOUND DISBONDED BETEEN HONEYCOMB CORE AND SKIN.SDR DALA2022011300257None · noneMAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS, FROM ROW 15-19, WERE INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AT STA 645 WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #8121299)SDR DALA2022011300256None · noneTHE IDG FEEDER HARNESS IS ROUTED TOO CLOSE TO THE #2 ENGINE FUEL LINE, AS INDICATED IN WORK CARD 0571-9202. THERE MUST BE A 0.39" MIN DISTANCE. SUMMARY SEE NRC 110-0001:0571-9202/010 00370: ROUTED IDG FEEDER HARNESS AS PER AMDS CARD 0571-9202. (LP #2083609)SDR DALA2022011200239None · noneTHE KEVLAR CABLE FOR THE TAIL CONE EMERGENCY EXIT RELEASE IS WORN TO LIMITS. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE TAILCONE JETTISON KEVLAR CABLE REF B717 AMM 53-52SDR 2022F00005Spoiler · corrodedSPOILER WAS FOUND DISBONDED BETWEEN HONEYCOMB CORE AND SKIN.SDR DALA2022010700123Floor Support · corrodedMAIN CABIN FLOOR SUPPORT UNDER FLOOR PANEL 221AF FOUND CORRODED. MAINTENANCE REPLACED SUPPORT PER BOEING DWG 9936534, AND B717 SRM 51-40-02. (LP #2076902)SDR DALA2022010600093None · noneTHE RIGHT HAND GALLEY CABIN EMERGENCY EXIT SIGN LIGHT HAS BROKEN WIRES. -M- SUMMARY SEE NRC 001-0010:2500-2647/113 00431: REPAIRED WIRES PER REF B717 SWPM 20-10-03. OPERATIONAL CHECK WAS GOOD. (LP #2076170)SDR DALA2022010600092None · noneFWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. REMOVED EXSITING RIVETS AND CUT OUT DAMAGE FOR REPAIR PER B717 SRM 53-20-15-2R PRC. 11. FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53- 20-15-2R PROC 11 OPTION 2 AND INSTALLED CONICAL SEALS. RII COMPSDR DALA2022010600094None · noneCAPT WINDSHIELD SHOWED SPARKS TOP LEFT. MAINTENANCE FOUND CAPT WINDSHIELD TEMP SENSOR WIRES TOUCHING SPRING. ADJUSTED WIRES. CAPTS WINDSHIELD HEAT CHECKS GOOD. A/C OK FOR SERVICE. (LP #8297415)SDR DALA2022010600091None · noneAFT CARGO. FLOOR BOARD SUPPORT/FORMER CORRODED AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER. (M) FLOOR BOARD SUPPORT/FORMER AT STA 973 STRINGERS 29 AND 30 ATTACH POINTS, 6 INCHES FWD OF ANTENNA DOUBLER FOUND CRACK, FOUND TO BE SDR DALA2022010400050None · noneFLOOR BEAM CRACKED AT STATION Y=737 RH OVERWING FRAME ATTACH POINT. REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072760)SDR DALA2022010400049None · noneFLOOR BEAM CRACKED AT STATION Y=737 LH OVERWING FRAME ATTACH POINT. MAINTENANCE REPLACED FLOOR BEAM PER B717 SRM 51-40-02. (LP #2072758)SDR DALA2022010400048None · noneTAIL SLIDE IS INPROPERLY PACKED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE SLIDE PER AMDS 5352-4002. (LP #2072354)SDR DALA2022010300010None · noneHIDDEN DAMAGE DURING THE DOUBLER REMOVE PROCESS. WEB DAMAGE WAS FOUND ON LEFT HAND SIDE, LOCATED ON INTECECTION STA 674 AND STGR 18LH. SUMMARY OF NRC 00175: WEB ON STA 674 LH WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2071146)SDR DALA2022010300009None · noneREF NRC 276 "WEAR MARKS ON OUTSIDE OF MATING SURFACE TO SLANT PANEL". SMOOTHED 3EA AREAS AND LOWEST READING WAS .092. ORIG MATL THICKNESS IS .125. REMOVED INBOARD SLANT PANEL BRACKET FOR FOM. ROUTED TO SHOP. COMPLIED WITH PRI 596194 -14 REV 0, REV,1, REV 2, RESDR DALA2023030701656None · noneERA 586819-14AD INSTALLED A REPAIR STRAP COMMON TO RH SPAR CAP O N VERTIAL STABILIZER, ERA REVISION A IS CURRENT. ACCOMPLISH ERA 586819-14AD REV A SECTION II AT 4600 CYCLES AFTER SECTION I, THEN 2400 CYCLE INTERVALS THEREAFTER. ASSOCIATED AA 5530-01048 ADDED FSDR DALA2021123008160None · noneTHE R1 DOOR FWD GIRT BAR FITTING IS CORRODED. THE AFT FITTING IS CORRODED AND BENT. SUMMARY SEE NRC 070-0023:5310-2005/003 00274: CLEANED AND CHECKED LIMITS. CORROSION LEVEL 2. REPLACED FLOOR FITTINGS REF BOEING DWG 9936534 AND B717 SRM 51-40-02. (LP #2068598)SDR DALA2024031103213Skin · damagedRH FUSELAGE WINDOW BELT WINDOW #12 AT STA 446-465 HAD A LIGHTNING STRIKE. FOLLOW ON ACTION REQUIRED. ERA 596251-14 ISSUED. FOLLOW ON ACTION REQUIRED SECT I TBA DURING C-CHK VISIT IN MSP DEC2021. SECT II HFEC INSPECTIONS TBA AT EVERY 24 MONTH INTERVALS AFTER SESDR DALA2021122808083Cover · missing(LOG 8380514) DURING INSPECTION FOUND CEILING LIGHT COVER OVER ROW 1DEF MISSING. REPLACED LIGHT COVER PER B717 AMM 33-51.SDR DALA2021122808084None · none(LOG 2066142) DURING INSPECTION FOUND FWD ELECTRONIC BAY, DRAIN MAST BASE SHOW SIGNS OF CORROSION. REPAIRED REF B717 SRM 53-01-01 AND B717 DRW # 9923686 .SDR DALA2021122708042None · none(LOG 2065059) DURING INSPECTION FOUND FWD CARGO DOOR JAMB HAS SEVERAL AREAS WITH SURFACE CORROSION. REPAIRED FWD CARGO DOOR JAMB PER B717 SRM 53-20-15-2R PROCEDURE 6.SDR HALA2021122700202Door · damagedEMER EQ - DOOR - FOUND DENT/GOUGE BELOW LEADING EDGE OF 1R SERVICE DOOR. // EDDY CURRENT SHOWS NO CRACK. #8089 12/24/21. BLEND GOUGE PER SRM 53-01-01-1A-1. MEASURED BLEND: ADJ 0.024, MIN REM:0.017; M66 SUBMITTED. 12/24/2021 MECH:015816. #5178. REMEASURED BLENDSDR HALA2021122700201Cover · abnormalEMER EQ - SLIDE - FORWARD SERVICE DOOR GIRT BAR DISCONNECTED FROM EMERGENCY SLIDE // RESECURED FWD SVC DOOR COVER. FOUND SLIDE COVER DISENGAGED. SECURITY CHK GOOD. OK FOR SVCSDR DALA2021122708041Control Unit · inoperativeSHIP 9544 -DIV- TO RDU WITH A RIGHT ENGINE SPURIOUS FIRE INDICATION. CORRECTIVE ACTION: REPLACED #2 VIA, FDCU AND PERFORMED ENGINE DUCT LEAK CHECKS AND ALL RETURN TO SERVICE CHECKS.SDR DALA2021122308001None · noneSHIP 9563 -DIV/INFLT SHUTDN- TO MSY DUE TO RIGHT ENGINE FIRE WARNING. CREW PULLED FIRE HANDLE AND DISCHARGED BOTH BOTTLES. CORRECTIVE ACTION: MAINTENANCE REPLACED NUMBER 1 AND 2 FIRE BOTTLES PER B717 AMM 26-21 AND REPLACED RIGHT ENGINE FDCU PER B717 AMM 26-11.SDR DALA2021122308000None · none(LOG 2061219) DURING INSPECTION FOUND CRACKS ON HOLE #6 AND HOLE #7 BELOW STATION ZFS=52.267, ON RH SIDE VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP. RH SIDE VERTICAL STABILIZER LEADING EDGE FRONT SPAR CAP WAS REPAIRED PER ER/A 534685-14AD REV B SECTION IVSDR DALA2021122908129None · none**THIS LOG REPLACES LOG 2010626.** DENTS LEFT UPPER FLAP MOVEABLE VANE. SUMMARY OF NRC 00049: LEFT UPPER FLAP MOVEABLE VANE WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL ON REFERENCE OF B-717-200 SRM 57-53-01-2R-1 PAR. 4. PERFORM DECAL INSP CONDSDR DALA2021122007872Battery Pack · false indication(8127554) AFT EMERGENCY LIGHTS ILLUMINATED. R/R AFT EMERGENCY LIGHT BATTERY IAW B717 AMM 33-51.SDR HALA2021122000191Slide · defectiveEMER EQ - UPON ARRIVAL FOUND MED SLIDE PARTIALLY DEPLOYED. // REPLACED L1 DOOR SLIDE PER AMM 25-61-01. SECURITY CHECK GOOD. OK FOR SVC.SDR 2021F00352Spoiler Panel · corrodedSPOILER WAS RECEIVED WITH SKIN AND DOUBLERS INTERNALLY DISBONDED FORM HONEYCOMB CORE DUE TO CORROSION. SPOILER WAS REPAIRED IAW DELTA ERS#562089-14SDR 2021F00351Spoiler Panel · corrodedSPOILER WAS RECEIVED FOR REPAIR AND INSPECTION WAS PERFORED IAW CMM 27-60-02. CORROSION OF HONEYCOMB CORE WAS FOUND INTERNALLY BETWEEN THE SKINS (UPPER/LOWER) AND DOUBLERS. COMPLETE DISASSEMBLY AND REBONDING WAS ACCOMPLISHED IAW DELTA ERA#562089-14.SDR DALA2021121607776None · noneSHIP 9533 - THE FLIGHT CREW DECLARED AN EMERGENCY DUE TO THE "RT GEAR UNSAFE" INDICATION ILLUMINATING SHORTLY AFTER TAKEOFF. ON APPROACH, THE GEAR WAS SELECTED DOWN AND THREE GREEN "DOWN & LOCKED" INDICATIONS ILLUMINATED. CORRECTIVE ACTION: THE AIRCRAFT WAS FESDR DALA2021121607774None · noneCORROSION ON AFT AND FWD DOUBLERS OF FORWARD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00116: CORROSION LEVEL 2, AFT AND FWD DOUBLERS OF FORWARD CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717 SRM 53-20-15-2R REPAIR 6. (LP #2052502)SDR DALA2021121407700None · noneTHE AFT CABIN EXIT IDENTIFIER LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY (B5-119). OPERATIONAL CHECK WAS GOOD. (LP #8120797)SDR DALA2021121607775None · noneAFT CARGO LOWER DOOR JAMB FROM MID DOOR TO FWD END OF JAMB HAS LARGE AREAS OF SURFACE CORROSION.(M) SUMMARY SEE NRC 054-0009 5300-2007/002 00319: CORROSION LEVEL 2. BLENDED OUT CORROSION AND CHECK LIMITS PER B717 SRM 53-00-00-01A. NDT REQUIRED. PERFORMED U/T OSDR DALA2021120907587None · noneSHIP 9521 - THE CREW DECLARED AN EMERGENCY DURING THE APPROACH FOR LANDING IN ATL DUE TO THE LOSS OF LEFT HYDRAULIC SYSTEM FLUID QUANTITY. CORRECTIVE ACTION: MAINTENANCE FOUND THE SOURCE OF THE LEAK AND REPLACED THE DAMAGED SECTION OF A HYDRAULIC LINE NEAR THESDR HALA2021120800183Engine · inoperativeCREW REPORTED THAT INBND TO OGG THEY HAD ENG1 BRG OVHT MSG, PER FCOM PROCEDURES CREW SHUT DOWN AFFECTED ENG // MX TROUBLESHOOTING, FOUND METAL FINDINGS FROM OIL FILTER & FBC STRAINER. HAL PP ENGINEERING HAS DETERMINED THAT AN ENG CHANGE IS REQUIRED. MX CURRENT
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