Boeing 717-200
Service difficulty reports · 18,756
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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 DALA2024082408420Cusp Web · corrodedAIRCRAFT 9510, CORROSION ON CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP MEMBRANE (WEB) RH STA Y=389 TO Y=370 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP 0518607)SDR DALA2024082408419Frame · crackedAIRCRAFT 9527, CRACKS ON FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN. CORRECTIVE ACTION: FRAME STA Y=1037 AT INTERSECTION WITH LONGERONS 17L, 13L AND 12L ON PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCESDR DALA2024082408418Fuel Cell · corrodedAIRCRAFT 9546, CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. CORRECTIVE ACTION: LOWER SKIN OF THE CENTRAL TANK APPROX. STA. Y=748 AND STA XCW=-25 AND Z=-29 WAS REPAIRED PER SDR DALA2024082308415Cusp Web · crackedAIRCRAFT 9510, CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX. CORRECTIVE ACTION: CRACK ON LH CUSP WEB AT STA Y=219, Y=657, Y=719 AT CABIN PAX WERE REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP 0516683)SDR DALA2024082308414Cusp Web · crackedAIRCRAFT 9527, CRACK CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB MEMBRANE UNDER SEAT TRACK STA Y 660 X=-44 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R-2 AND SRM 51-41-02-0G. (LP 0516434)SDR DALA2024082308413Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CUSP WEB STA Y=715 X=44 AT PASSENGER CABIN (CPAX) REPAIRED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 51-70-10-2R-2 FIG. 201. (LP 0516174)SDR DALA2024082308412Skin · damagedAIRCRAFT 9550, LIGHTNING STRIKES ON SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE. CORRECTIVE ACTION: SKIN STA Y=256, 229 AND BTW RH LONGERONS 15/16 AT EXTERNAL FUSELAGE WAS REPAIRED PER. PRI 619580-14 REV. 4 AND ER/A 619580-14AD REV. ORISDR DALA2024082308411Window Frame · crackedAIRCRAFT 9527, CRACK ON RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX. CORRECTIVE ACTION: RH WINDOWS RING PAN ON STA Y=737 UPPER FWD CORNER AND STA Y=889 LOWER FWD CORNER AT CPAX WERE REPAIRED PER B717-200 SRM 56-20-0SDR DALA2024082208364Cusp Web · crackedAIRCRAFT 9527, CRACK ON CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: CORROSION LEVEL 2, CUSP WEB STA Y=813 X=54 AT LH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM. 53-00-55-2R PROCEDURE 4 FIG. 205. (LP 0514941)SDR DALA2024082208363Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=446 TO STA Y=465 AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. FIGURE 210. (LP 0514913)SDR DALA2024082208362Pan · crackedAIRCRAFT 9550, INITIAL INSPECTION: CRACK ON INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INNER PAN AFT SIDE ON BEAM NBR 3, NBR 4 AND NBR 5 AT AFT CARGO COMPARTMENT DOOR. WAS REPAIRED PER PRI 619298-14 REV.SDR DALA2024082208361Floorbeam · corrodedAIRCRAFT 9510, CORROSION ON FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 AT PAX CABIN STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2, FLOOR SUPPORT, STA Y=200 BTW X=8 TO X=15 AND STA Y=180 BTW -X=9 TO -X=42 WERE FABRICATED PER DWG SDR DALA2024082208360Pan · crackedAIRCRAFT 9527, INITIAL INSPECTION: CRACK ON LH RING PAN (FWD/UPPER) STA Y= 484, (FWD/LOWER) STA Y=636, (AFT/UPPER) STA Y=851, (FWD/LOWER) STA Y= 851, (FWD/LOWER) STA Y=870, (FWD/LOWER) STA Y=908, (FWD/LOWER) STA Y=927, (FWD/UPPER/LOWER) STA Y= 946 AT CABIN PAXSDR DALA2024082208359Web · corrodedAIRCRAFT 9527, CORROSION ON RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX. CORRECTIVE ACTION: CORROSION LEVEL 2: RH WEB BTW STA Y=448 TO STA Y=503 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 210. (LP 0514363)SDR DALA2024082208358Pan · crackedAIRCRAFT 9550, CRACK INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. CORRECTIVE ACTION: INNER PAN NEAR TO AFT STOP FITTING AND BEAM NBR 01. WAS REPAIRED PER PRI 619304-14 REV. 3 AND ERA 619304-14 REV ORIGINAL SECTION I PERMANENT REPAIR ASSOCIATED ER/A 14-6SDR DALA2024082208357Longeron · crackedAIRCRAFT 9527, CRACK ON LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: LONGERON 4R STA Y=1152 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R. PROCEDURE 2. REPAIR 2 FIG. 201. (LP 0514325)SDR DALA2024082108332Structure · ground damageAIRCRAFT 9527, FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER. CORRECTIVE ACTION: PERMANENT REPAIR ON FWD CARGO DOOR SURROUND AFT SIDE HIT BY BELT LOADER WAS PERFORMED PER B717-200 SRM 53-20-15-2R, REPAIR 11, OPTION 1. PERFORMED VISUAL INSPECTION ON PERMASDR DALA2024082108331Cusp Web · corrodedAIRCRAFT 9510, INITIAL INSPECTION: CORROSION ON LH REPAIR DOUBLER OF CUSP WEB STA Y=841, Y=866 AT PAX CABIN. CORRECTIVE ACTION: CORROSION LEVEL 2-LH CUSP WEB STA Y=866 AT PAX CABIN WAS REPAIR PER B717-200 SRM-53-00-55-2R-4 FIG. 214, LH CUSP WEB STA Y=841 WAS ASDR DALA2024082108330Web · crackedAIRCRAFT 9527, INITIAL INSPECTION: SEVERAL CRACKS BELOW INBD WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX. CORRECTIVE ACTION: WEB RH APPROX BTW STA Y=715 TO STA Y=737 AT CPAX WAS REPAIRED PER B717-200 SRM 57-70-10-2R-2, PAR. 4 AND B717-200 SRM 51-41-02-0G.SDR DALA2024082008300Angle · crackedAIRCRAFT 9550, INITIAL INSPECTION: CRACKS ON ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE. CORRECTIVE ACTION: ANGLE OF CANTED KEEL STRUCTURE ON STA Y=716 AND PROJECT LONG 27L AT LOWER CTR FUSELAGE WAS REPAIRED PER PRI SDR HALA20240820042Trim Switch · damagedATB - CAPTAIN SIDE PITCH TRIM SWITCH DOES NOT CENTER LEFT SIDE OF SWITCH SAGS DOWN. REPLACED CAPT PRIMARY TRIM SWITCH PER AMM 27-41-01. OPS CHK OK.SDR DALA2024081908281Splice · cracked-AD- FOUND 2 CRACK INDICATIONS ON LEFT SIDE OF VERTICAL STAB BELOW SPLICE AT STA 2F552.267 WHILE PERFORMING BHEC PER AA 5530-01048 STEP 8 REF AD2018-10-08. HOLES ARE MARKED. AFTER SEPARATION OF LAYERS CONFRIMED CRACK INDICATIONS FROM FWD FLANGE LAYER REF AA553SDR HALA20240819041Windshield · crackedCAPTAIN SIDE WINDSHIELD CRACKED IN FLIGHT. REMOVED AND INSTALLED NEW CAPTAIN SIDE WINDSHIELD PER AMM 56-11-02 UP TO STEP E (7).(B) NEED TO CONTINUOUS FROM E.(8) PERFORMED LEAK CHECK AND PRESSURIZATION CHECK GOOD.PER AMM 56-11-02.NEED TO CONTINUE OPS CHECK ANTISDR DALA2024081908279Beam · crackedCRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR. PTAS. SUMMARY OF NRC 00321: CRACK BEAM #6 MID SECTION JUST BY HARDWARE AREA AT L1 PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9527. SDR DALA2024081908242Nut · corrodedCORROSION ON NUTS INSIDE HOLES #26, #27, #28, AND #30 STA HX 6.625 RIGHT STABILIZER CENTER BOX. SUMMARY OF NRC 00494: NUTS INSIDE HOLES #26, #27, #28, AND #30 STA HX 6.625 RIGHT STABILIZER CENTER BOX WERE REPAIRED PER ER/A 619552-14 PRI REV 1. ASSOCIATED ER/A SDR HALA20240819040Control Unit · faultedAT 1300FT AUTOPILOT DISCONNECTED, AUTO THROTTLES WENT MAX POWER, ALL DU'S WENT BLANK FOR A SECOND. REMOVED AND REPLACED EPCU PER AMM 24-21-02. EPCU OP CK GOOD. PERFORMED VIA 1 &2 EIS OPS TEST PER AMM 31-61-00-720-801. ALSO PERFORMED AFS TEST ON FCC 1&2 PER AMMSDR HALA20240819039Relay · failedAFTER EPCU DOWNLOAD FOUND EMERGENCY POWER RELAY FAULT ( 54 EPR FAILED CLOSED.). REMOVED AND REPLACED EMERGENCY DC POWER RELAY PER AMM 24-34-05. FUNCTIONAL TEST GOOD PER AMM 24-24-00. OK FOR SERVICESDR DALA2024081908280Beam · crackedCRACK ON BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR. SUMMARY OF NRC 00357: BEAM #6 (MID SECTION) AT FWD PASSENGER DOOR WAS REPAIRED PER ER/A 559578-14MA REV ORIGINAL SECTION I PERMANENT. ASSOCIATED ER/A 14-559578 ADDED FOR AC 9510. (LP #0505999)SDR DALA2024081908241Skin · gougedGOUGE ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00704: EXTERNAL SKIN ON STA Y=370 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-00-01-2R PROCEDURE 8 REPAIR 8 PAR 5 FIGURE 204. (LP #0506180)SDR DALA2024081608214Contact · shortedSHIP 9574 -SMKE- AFTER LIGHT TEST, WE NOTICED THAT THE RIGHT APU BUS LIGHT WAS INOPERATIVE. WE TRIED RESETTING THE LIGHT BUT THE BULB AND SOCKET BRIEFLY EMITS SMOKE. MAINTENANCE FOUND THAT THE KORRY SWITCH BRACKET FOR THE APU LIGHT MADE CONTACT AND BURNT UP THSDR DALA2024081608213Battery Pack · inoperativeOVERWING DOOR EMERGENCY LIGHTS ARE INOPERATIVE. T/S OVERWING DOOR EMERGENCY LIGHTS PER B717 FIM 33-50-00 810-801. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6010188SDR DALA2024081608212Frame · crackedCRACK ON WEB AND CRACK ON FRAME OF AFT ACCESSORY COMPARTMENT FROM STA 1178 CANT BTW LONG 1 TO LONG 3RH TO 3LH, APPROXIMATELY. SUMMARY OF NRC 00219: WEB AND FRAME OF AFT ACCESSORY COMPARTMENT FROM STA 1178 CANT BTW LONG 1 TO LONG 3RH TO 3LH WERE REPAIRED PER PRSDR DALA2024101490280Skin · cracked-AD- PD: FASTENER HOLE CRACKS CA: **LIMITED RELEASE** REPAIRED PER BOEING DWG 59360610 REV AC & ER/A 620349-14AD SECTION 1, REV ORIGINAL **NOTE: ER/A 620349-14AD, REV ORIGINAL.SDR DALA2024081608211Cusp Web · crackedCRACK ON CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00515: CUSP WEB STA Y=436 X=44 AT PASSENGER CABIN (CPAX) WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #0504361)SDR DALA2024081608210Pan · crackedCRACK ON INNER PAN WAS FOUND ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00674: INNER PAN ON BEAM 4 FWD EDGE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 619393-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 619393-14 REV 3. ASSDR DALA2024081608208Cusp Web · crackedCRACK ON INBD CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX. SUMMARY OF NRC 00389: CUSP MEMBRANE (WEB) RH BTW STA Y=579 AND STA Y=598 AT CPAX WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 PAR 4 FIGURE 201. MAINTENANCE REQUIREMENTS VISUAL ISDR HALA20240816038Anti-Skid Sys · failed"ANTISKID L FAIL" ON LANDING ROLL OUT LEFT MAIN LANDING GEAR OUTER TIRE POPPED. REMOVED AND REPLACED #1&2 MLG (LH) TIRES PER AMM 32-41-01. AWAITING ANTISKID RESOLUTION.SDR DALA2024081508167Pan · crackedCRACK (3 EA) ON OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00141: OUTER PAN AT BEAM #3, #4, AND #5 INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 619498-14 REV ORIGINAL. ASSOCIATED ESDR DALA2024081608209Static Wick · damagedDURING LIGHTRING STRIKE INSPECTION FOUND LH ELEVATOR O/B STATIC DISCHARGER CONDUCTIVE DOUBLER DAMAGED. COMPLETED TEMP REPAIR PER ENGINEEREING CONCURRENCE EMAIL TOPP 40-60-05 PAR X.B.2 LH ELEVATOR O/B STATIC DISCHANGER CONDUCTIVE REPAIR BY ERA 618920-14 REV ORISDR DALA2024081508166Frame · corrodedCORROSION ON FRAME STA Y=1022 BTW LONGERON 28R/L30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00833; CORROSION LEVEL 2. CORROSION ON FRAME STA Y=1022 BTW LONGERON 28R/L30 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 3, PAR 5, FIGURE 20SDR DALA2024081508165Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LHSDR DALA2024081508164Skin · crackedCORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LH MLG WHEEL WELL. SUMMARY OF NRC 00384: CORROSION LEVEL 2. CORROSION ON UPPER SKIN OF CENTRAL FUEL TANK STA Y=748, X=55 APPROX AND Z=-10 IN THE FRONT WALL ON LHSDR DALA2024081508163Skin · crackedCORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE AT RH CANTED KEEL. SUMMARY OF NRC 00492: CORROSION LEVEL 2. CORROSION ON LOWER SKIN OF CENTER FUEL TANK BTW STA APROX Y=696 AND ON STA Y=655 INTERNAL STRUCTURE SDR DALA2024081408115Battery Pack · inoperativeFOUND L & R FWD OVERWING EXIT EMERGENCY LIGHTS TO BE INOPERATIVE. ALSO FOUND L & R FWD SERVICE DOOR EXIT EMERGENCY LIGHTS INOPERATIVE. PER B717 WDM 33-51-14, ALL LIGHTS ASSOCIATED WITH BATTERY PACK B5-118. REPLACED EMERGENCY LIGHT BATTERY PACK B5-118 IAW B717 SDR DALA2024081408113Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2). SUMMARY OF NRC 00670: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 TO Y=1061 X=44.5 PAX CABIN (W2) FABRICATED PER DWG 9981474 REV L AND REPLACED PER B717-200 SRM 51-41-05-0G AND 51-4SDR DALA2024081408114Cover · detachedMISSING FWD ''EXIT'' PLACARD/SIGN. MAINTENANCE RE-INSTALLED EXIT SIGN COVER REF B717 AMM 33-51. (LP #6186440)SDR DALA2024081408112Window Frame · crackedCRACK ON LH WINDOW FRAME (RETAINER POLISHED). SUMMARY OF NRC 00623: LH WINDOW FRAME WAS REPAIRED PER PRI 619398-14 REV 2 AND PER ER/A 619398-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-619398.SDR DALA2024081408111Longeron · crackedCRACK ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN. SUMMARY OF NRC 00552: (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON LONGERONS 07L, 06L, 05L, 04L, 03L STA Y=1022 AT PASSENGER CABIN, 1 CRACK WAS CONFIRMED ON LONG 6LH. PER DC-MD/BOEING NDTSSDR DALA2024081308067Skin · corrodedCORROSION ON SKIN UPPER EDGE OF LH AND RH WING REAR SPAR BTW XCW=0 TO XW=60 (THROUGH LH AND RH MLG (SPECIFICALLY XCW=30)). SUMMARY OF NRC 00169: CORROSION LEVEL 2. CORROSION ON SKIN UPPER EDGE OF LH AND RH WING REAR SPAR BTW XCW=0 TO XW=60 WAS REPAIRED PER PRISDR DALA2024081308066Beam · crackedCRACKS ON BEAM #6 BTW STA 180-196 AT FWD PASSENGER DOOR. SUMMARY OF NRC 00117: BEAM #6 ON STA 196 AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 12 PAR 4 FIGURE 201. AND (ET) (HFEC) INSPECTION WAS ACCOMPLISHED ON BEAM #6 ON STA 180 A
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