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 DALA2024012901224Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 407: CORROSION LEVEL 2. FLOOR SUPPORTS (UPPER/LOWER SURFACE) BTW STA 160-200 ON X=44.5 (1 EA) AND X=55 (1 EA) AT PAXSDR DALA2024012901223Stringer Splice · corrodedCORROSION ON PREVIOUS REPAIR SPLICE AT STA Y=908 BTW LONG 26L AND LONG 27L IN AFT CARGO COMPARTMENT. SUMMARY OF NRC 00647: CORORSION LEVEL 2. SPLICE OF STA Y=908 BTW LONG 26L AND LONG 27L WAS REPLACED PER B717-200 DGW 9971183 REV 'J'. (LP #0174281)SDR DALA2024012901222Doubler · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN. SUMMARY OF NRC 00395: CORROSION LEVEL 2. PREVIOUS REPAIR DOUBLER BTW STA 844-859 AND LONGERONS 28L-28R AT EXTERNAL FUSSELAGE SKIN WAS REPLACED PER B717 SRM 5SDR DALA2024012901221Floor Support · corrodedCORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00413: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 148-200 BTW X=-5 TO X=-9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACED PER B717-200 SRM 5SDR DALA2024020301509Door Frame · damagedRAMP REPORTS DAMAGE TO AFT CARGO DOOR CUTOUT. FOUND DAMAGE OUT OF LIMITS. REMOVED DAMAGE PER B717 SRM 53-20-15-2R REPAIR 10 OPTION 2. FABRICATED, TREATED, & PAINTED REPAIR PARTS PER B717 SRM 53-20-15-2R-10 OPTION 2. INSTALLED PARTS -11 & -13 PER B717 SRM 53-20SDR DALA2024012901220Angle · corrodedCORROSION WAS FOUND ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH, PAX CABIN. SUMMARY OF NRC 00611: CORROSION LEVEL 2. CUSP ANGLE ON LH/LOWER CUSP ANGLE BTW STA Y=180 AND X=56 LH WAS REPAIRED PER B717 SRM 53-00-55-2R-3. (LP #0173416)SDR DALA2024013101411Skin · damagedFASTENER HOLES AND COUNTERSINKS ARE ELONGATED OUT OF LIMITS ON 1/4 FASTENERS ROW AT VERT STAB FIX LE. ALSO, ON VERT STAB REMOVABLE LE STA ZFS=52.267 REF SERVICE GENERAL DRAWING SG95550001. SUMMARY OF NRC 00538: FASTENER HOLES AND COUNTERSINKS AT VERT STAB FIX SDR DALA2024012901219Fitting · crackedCRACK ON VERTICAL FITTING ON AFT PRESSURE BULKHEAD STA 1053 LONGERON #1 (ABOVE DOOR CUT OUT) AT PAX CABIN. SUMMARY OF NRC 00522: SPRING OF THE ARM ASSEMBLY WAS REMOVED AND INSTALLED PER B717-200 AMM 53-52-02-020-801 AND 53-52-02- 420-801, VERTICAL FITTING ON ASDR DALA2024012901218Pan · crackedCRACK ON INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR. SUMMARY OF NRC 00069: INTERNAL PAN FWD EDGE BTW BEAM #2 AND BEAM #4 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201. (LP #0171673)SDR DALA2024012601171Cusp Web · corrodedCORROSION ON DOUBLER OF LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB. SUMMARY OF NRC 00477: CORROSION LEVEL 2. DOUBLER OF REPAIR ON LH CUSP WEB UPPER BTW STA Y=389 TO Y=408 AT PAX CAB WAS REPLACED PER B-717-200 SRM 53-00-55-2R. (LP #0171752)SDR DALA2024012601170Floor Support · crackedCRACK ON FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00170: FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1) WAS REPAIRED PER B717-200 SRM 51-70-11- 2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 201. (LP #0171182SDR DALA2024012501109Finger Doubler · corrodedCORROSION ON FINGER DOUBLER STA 944, 972, 1001, AND 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00194: CORROSION LEVEL 2. FINGER DOUBLER BTW STA 944 AND STA 1004 BTW STRG 26L/27L AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-02-SDR DALA2024012501108Cusp Web · corrodedCORROSION ON ANGLE CUSP BTW STA Y=168 AND STA Y=200, AND STA X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY). SUMMARY OF NRC 00245: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=168 AND STA Y=200, AND X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY) WAS REPAIRED PER ERA 614741-1SDR DALA2024012501107Cusp Web · corrodedCORROSION ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN. SUMMARY OF NRC 00510: CORROSION LEVEL 2. AREA ON CUSP WEB (RH) BTW STA Y=610 TO STA Y=660 APROX AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-55-2R. (LP #0170434)SDR DALA2024012501106Frame · crackedCRACK ON LH FRAME STA 1037 LONG 17LH AT PAX CABIN. SUMMARY OF NRC 00294: LH FRAME STA 1037 LONG 17LH AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R. (LP #0170333)SDR DALA2024012601172Light · sparksAFTER TAKEOFF ON RWY 6 IN BHM, AT APPROX 600 FT, CAPTAIN SIDE MAP LIGHT SPARKED AND BEGAN TO SMOKE. THE CIRCUIT BREAKER W29 TRIPPED AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PUSHED C/B IN AND BOTH LIGHT WORKED ON CAPTAIN AND FIRST OFFICER SIDESDR DALA2024012401101Seat Track · corrodedCORROSION ON SEAT TRACK X=-44.5 BTW STA 200-219 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00403: SEAT TRACK SECTION X=-44.5 BTW STA 200-246 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED OFF PER B717-200 SRM 53-20-52-2R PROCEDURE 5. (LP #0169174)SDR DALA2024012401100Skin · damagedCREASES WERE FOUND ON REPAIR SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH PER B717 SRM 53-00-01-02 REPAIR 6 PAR. 7. SUMMARY OF NRC 00270: SKIN SECTION OVER THE FRAME STA 256 BTW LONG 17LH-18LH WAS REPAIRED PER B717-200 SRM 53-00-01-2R REP 6. SPECIFICSDR DALA2024012301009Skin · gougedGOUGE AND DENT ON FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L. SUMMARY OF NRC 00615: FUSELAGE SKIN AT STA 237 BTW LONG 18L-19L WAS PERMANENT REPAIRED PER B717-200 SRM 53-02-01-2R-1 FIG 202. THE PERMANENT REPAIR SPECIFIED MAINTENANCE REQUIREMENTS ARE A VISUAL INSSDR DALA2024012301008Web · crackedWEB CRACKED FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION. SUMMARY OF NRC 00599: WEB FORWARD OF CANTED FRAME 1200 AT 2 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION II. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #0162948)SDR DALA2024012301007Web · crackedWEB CRACKED FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION. SUMMARY OF NRC 00598: WEB FORWARD OF CANTED FRAME 1200 AT 10 O-CLOCK POSITION WAS REPAIRED PER ERA 537343-14MA REV B SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-537343 ADDED FOR AC 9523. (LP #SDR DALA2024012200906Angle · crackedCRACK ON ANGLE STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1. SUMMARY OF NRC 00073: ANGLE (INTERCOSTAL) STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1 WAS MANUFACTURED AND REPLACED PER DWG 9955763 REV K, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #01640SDR DALA2024012200905Web · puncturedPUNCTURES (2 EA) ON WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00415: WEB BTW STA 160-200 AND X=-44.4 TO X=-54 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R. (LP #0163433)SDR DALA2024012200904Web · corrodedCORROSION ON WEB BTW STA Y=200/205 AND L 18L AND L 17L AT DOOR JAMB L1. SUMMARY OF NRC 00304: CORROSION LEVEL 2. CORROSION ON WEB BTW STA Y=200/205 AND L 18L AND L 17L AT DOOR JAMB L1 WAS REPAIRED PER ERA 614628-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOSDR DALA2024012200903Floor Support · corrodedCORROSION AT FLOOR SUPPORT ON X=56 BTW STA Y=160/200 PAX CABIN. SUMMARY OF NRC 00455: CORROSION LEVEL 2. FLOOR SUPPORT ON X=56 BTW STA Y=160 TO Y=200 WAS FABRICATED AND REPLACED PER DWG 9936534 REV BW AND B717-200 SRM 51-41-05-0G PAR 8. (LP #0162459)SDR DALA2024012200902Floor Support · corrodedCORROSION ON FLOOR SUPPORT (UPPER/LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00412: CORROSION LEVEL 2. FLOOR SUPPORT (UPPER/ LOWER SURFACE) BTW STA 148-200 BTW X=5 TO X=9 AT PAX CABIN FLOOR STRUCTURE WAS REPLACEDSDR DALA2024011900810Cusp Web · crackedCRACK ON RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00397: RH CUSP WEB BTW STA 218-237 AND X=-44 TO X=-60 AT PAX CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4. (LP #0161271)SDR DALA2024011900809Web · crackedCRACK ON WEB STA Y=674 X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00311: WEB STA Y=674 X=55 AT PASSENGER CABIN WAS REPAIRED PER ERA 614715-14 REV ORIGINAL SECTION I PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 24-MONTHS FROM 14JAN24 ONLY. ADDITIONAL ENGSDR DALA2024011900811Lens · missingCABIN EMERGENCY LIGHT LENS MISSING AT 2B. MAINTENANCE FOUND STAND-BY OVERHEAD EMERGENCY LIGHT COVER MISSING AT ROW 2. INSTALLED THE LIGHT COVER AS REQUIRED REF B717 AMM 33-51. AIRCRAFT IS OK FOR SERVICE. (LP #0160810)SDR DALA2024011900808Cusp Web · corrodedCORROSION ON CUSP WEB (UPPER AREA) BTW STA 579-598, 609-617, 658-678, AND 720-756 AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00560: CORROSION LEVEL 2. CORROSION ON CUSP WEB (UPPER AREA) BTW STA 579-598, 609-617, 658-678, AND 720-756 AT CABIN FLOOR STRUCTURE WAS SDR DALA2024011900807Web · crackedCARCK ON WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX. SUMMARY OF NRC 00342: WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0161024)SDR DALA2024011900806Cusp Web · crackedCRACKS ON CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN. SUMMARY OF NRC 00376: CUSP WEB (BELOW) BTW STA Y=715 TO STA Y=728 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 51-41-02-0G AND 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0160778)SDR DALA2024011900805Floorbeam · corrodedCORROSION ON FLOOR SUPPORTS AT W1 AREA STA 200 BTW X=7 AND X=-44 IN REF TO NRC 00401. SUMMARY OF NRC 00539: CORROSION LEVEL 2. FLOOR SUPPORTS WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0160759)SDR DALA2024011800752Battery Pack · no testDURING SERVICE CHECK FOUND AFT OVER WING (RT/LT) EMERGENCY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY AT STA 726 AND STA 803 IAW B717 AMM 33-51-03. PERFORMED OPERATIONAL CHECK IAW B717 AMM 33-51-03. OPERATIONAL CHSDR DALA2024012601173Pseu · faultedSHIP 9547 -MISC/DE- DURING THE DEPARTURE CLIMBOUT FROM QRO, THE MLG "UNSAFE" LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE UP POSITION. THE FLIGHT CREW COMPLIED WITH THE QRH, WHICH HAD THEM CYCLE THE LANDING GEAR. THE UP AND LOCKED GEAR POSITION INDICSDR DALA2024011800751Cusp Web · corrodedCORROSION ON RH CUSP WEB LOWER SURFACE BTW STA Y=435 TO Y=465 PAX CABIN. SUMMARY OF NRC 00558: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=435 TO Y=465 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0159555)SDR DALA2024011700680Web · crackedCRACKS ON WEBS AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT. SUMMARY OF NRC 00238: WEB AT 11 O'CLOCK POSITION STA Y=1200 AT AFT ACC COMPARTMENT WAS REPAIRED PER ERA 537343-14MA REV B, SECTION I, PERMANENT REPAIR. ASSOCIATED ERA 14-537343 ADDED FOR SDR DALA2024011700679Web · crackedCRACK WAS FOUND ON WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT. SUMMARY OF NRC 00607: WEB BTW STA 182 AND X=-6 AT E/E COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 FIG 201. (LP #0158141)SDR DALA2024011700681Door Frame · crackedRT MAIN GEAR WHEEL WELL DOOR JAMB FWD CHANNEL WAS FOUND CRACKED / DAMAGED. MAINTENANCE CLEANED UP DAMAGE AND INSPECTED PER B717 SRM 53-20-02-2R PROC 3. CRACK IN UPPER CHANNEL AREA MEASURED APPROX. 0.25IN. STOP DRILLED CRACK PER B717 SRM 53-20-02-2R REPAIR 3. CSDR DALA2024011700678Beam · crackedCRACKS ON BEAM #1, STA Y=200 AT PAX CABIN DOOR L1. SUMMARY OF NRC 00595: BEAM #1, STA Y=200 AT PAX CABIN DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7, FIGURE 201. (LP #0158063)SDR DALA2024011600593Unknown · unknownON SERVICE CHECK FOUND A FEW CEILING EMERGENCY LIGHTS OUT. MAINTENACE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AT LOCATION B5-227 PER B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #4369661)SDR DALA2024011600591Web · crackedCRACKS ON WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX. SUMMARY OF NRC 00346: WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 203. (LP #0156605)SDR DALA2024011600590Unknown · unknownCRACK INTERCOSTAL AT X=0, BTWEEN STA Y=1002 TO Y=1022, CABIN FLOOR SUPPORT STRUCTURE. SUMMARY OF NRC 00511: TRIMMED OUT INTERCOSTAL AT X=0, BT STA Y=1002 TO STA Y =1022 WAS REPAIRED PER B717-200 SRM-51-70-11-2R PROCEDURE 1 REPAIR. (LP #0156032)SDR DALA2024011600589Web · crackedCRACK ON WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00312: WEB STA Y=715 X=44 AND X=-44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0155891)SDR DALA2024011600588Door Frame · corrodedSEVERAL SPOTS OF CORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00033: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R REP. 7. (LP #0155777)SDR DALA2024011600587Unknown · unknownELONGATED HOLES AT EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00064: EXTERNAL FUSELAGE SKIN SCUFF PLATE AREA BTWN STA 954/STA 986 OF AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 614841-14 REV SDR DALA2024011500579Unknown · unknownON WALK AROUND FOUND RIGHT REAR EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY REF B717 AMM 33-51. (LP #5049081)SDR DALA2024011500578Unknown · unknownCORROSION ON FLOOR SUPPORTS COORDINATE X=-56, BTW STA Y=200 TO 210, COORDINATE X=-44 BTW STA Y=160 TO 200 AND COORDINATE X=0 TO COORDINATE X=-44, STA Y=200. SUMMARY OF NRC 00686: CORROSION LEVEL 2. FLOOR SUPPORTS COORDINATE X=-56, BTW STA Y=200 TO 210, COORDINSDR DALA2024011600592Skin · damagedFUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L-26R TO L-28R / ELONGATED HOLES & CORROSION TIME LIMITED. REPAIRED FUSELAGE / SKIN / AFT CARGO DOOR CUTOUT, STA Y=954, L- 26R TO L-28R / ELONGATED HOLES & CORROSION PER ERA 614841-14 REV ORIGINAL SECTIONI TISDR DALA2024011500580Unknown · unknownDURING SERVICE CHECK, MAINTENANCE FOUND THE FORWARD OVERWING EXIT LIGHT AND ISLE OVERWING EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED 2 EACH BATTERIES, AT ROWS 18 & 19, IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. ALL LIGHTS ILLUMINATE. AIRCRAFT IS O
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