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 DALA2017010200004Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE NOTED THAT THE OVERHEAD EMERGENCY LIGHTS FOR BOTH THE AFT OVERWING EXITS WERE INOPERATIVE. MAINTENANCE REPLACED THE APPLICABLE BATTERY PACK AND THE OPERATION OF THE LIGHTS CHECKED GOOD. (LP #9446654)SDR DALA2017010400080Longeron · corrodedALC LONGERON 30 HAS CORROSION IN MULTIPLE AREAS FROM FUSELAGE FRAME STA 986 TO STA 1037. REPAIRED L30 FROM STA 899-1053 IAW SRM 53-20-05 REP 1.SDR DALA2017010200003Rivet · leakingRIGHT WING UPPER SURFACE, LE WING XRS 115.500. RIVET SEEPING FUEL. REPAIRED IAW ER/A PR551844-14, SRM 51-40-02.SDR DALA2017010400046Beam · crackedFWD SERVICE DOOR LOWER HORIZONTAL BEAM JUST UNDER LOWER DOOR HINGE CRACKED. REPLACED LOWER HORIZONTAL BEAM ON FWD SERVICE DOOR IAW SRM 51-41-01-0G, 51-41-02 FIG 13, AND 51-41-05 FIG 2.SDR DALA2017010100002Door Frame · corrodedDOOR FRAME LOWER HALF INCLUDING PAN AND SEAL SPLICES HAS MULTIPLE AREAS OF CORROSION. BLEND AND CHECK LIMITS. REPLACED THE DOOR FRAME IAW SRM 51-41-02.SDR DALA2017010100001Skin · crackedLEFT WING, LWR SURFACE, LE, XOS 332.558 CRACKED. REPAIR IAW SRM 57-40-01 REPAIR 7. FABRICATED AND INSTALLED INTERNAL/EXTERNAL DOUBLERS WITH FILLERS IAW ER/A 551840-14 REV ORIGINAL.SDR 2017FAA123000019Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK L/H O/B SPOILER FOUND DELAMINATED.SDR DALA2017010400079Seat Track · corrodedRT CARGO SEAT TRACK IS CORRODED JUST FWD OF DOOR JAMB FWD LOWER CORNER. BLENDED CORROSION ON LWR RT CARGO SEAT TRACK AFTER EVALUATION OF BLEND FLANGE THICKNESS FOUND TO BE .040 ALLOWABLE MINIMUM FLANGE THICKNESS IS .060 THIS IS OUT OF LIMITS PER SRM 53-20-52 ASDR DALA2017010400042Shear Tie · corrodedCORROSION ON FORWARD SIDE OF ALC FRAME AND SHEAR TIES AT STA 1022.091 BETWEEN LONGERONS 29L AND 29R (MARKED IN RED). BLENDED CORROSION ON SHEAR TIE AT STA 1022 L29L -L29R. NOMINAL THICKNESS .050 REMAINING THICKNESS .038 REPAIRED SHEAR TIE IAW SRM 53-20-06 REPASDR DALA2017010300012Structure · crackedLEFT WING, LE NR 5 SLAT, OTBD L SURFACE CRACKED. REPAIRED IAW SRM 51-41-02 AND 51-41-08.SDR 2017F00016Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK RT INBD SPOILER FOUND DELAMINATED.SDR 2017F00015Skin · delaminatedDURING UNSCHEDULED MAINTENANCE CHECK, RT OTBD SPOILER FOUND DELAMINATED.SDR DALA2017030201694Skin · dentedDENT DAMAGE TO FUSELAGE PANEL 150GL. FOUND DENT DAMAGE TO BE 6.00" LENGTH BY 1.750" WIDTH BY .062" DEEP. REPAIRED IAW ER/A 553960-14 REV ORIGINAL.SDR DALA2017010400081Seat Track · corrodedCORROSION ON THE RIGHT CENTER SEAT TRACK (RBL44.5), FROM STA 197 TO STA 256. REPLACED RIGHT CENTER SEAT TRACK AT RBL 44.5 FROM STA 197-256 IAW AMM 53-22-01-400-800 SEE PARTIAL WS PG 1 AND 2. MATERIAL ID IAW SRM 53-20-52 LOCATED AND DRILLED NEW SEAT TRACK SECTISDR DALA2017010400044Cusp Web · crackedUPPER FUSELAGE, CABIN RT CUSP WEB STA 458-503 BL54 5R CORROSION MARKED "CORROSION". REPLACED CUSP WEB RT STA 389-503 IAW SRM 51-41-02, 51-41-05. WORK COMPLETED ON OUTSIDE REPAIR NON-ROUTINE CARD 74117-0200-0257.SDR DALA2017010300007Seat Track · corrodedCORROSION ON THE RIGHT INBD SEAT TRACK RBL 22, BS 197 TO 256. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5.SDR DALA2017010300006Seat Track · damagedRT OTBD SEAT TRACK, BS 756 - 813 RBL 56 GOUGED AND CORRODED. REPLACED THE SEAT TRACK IAW SRM 53-20-52 (FIG 201) REPAIR 5.SDR DALA2017010500082Cusp Web · corrodedUPPER FUSELAGE, CABIN RT CUSP WEB STA 389-427 BL54.5R CORROSION MARKED "CORROSION". BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS ORG 0.020 REMAINING 0.007" REPLACED CUSP WEB WITH NEW CUSP WEB. NEW CUSP WEB IAW DWG #9430538475 AND 51-41-02, 51-41-05.SDR DALA2017010400043Former · corrodedCORROSION ON FORMER STA 954 L29L-L30. BLENDED CORROSION ON FORMER AT STA 954 IAW SRM 53-00-00 FIG 103 .037 REMAINING OF .063 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103 (6784). REPAIRED OUT OF LIMITS AREA IAW SRM 53-00-06 REPAIR 2.SDR DALA2017010300009Seat Track · corrodedRBL 56 OTBD SEAT TRACK BS 927 - 986, FOUND SEVERAL SPOTS OF CORROSION. BLENDED AREAS OF CORROSION IAW SRM 53-00-00 FIG 103 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-52 FIG 101. REPAIRED IAW SRM 53-20-52 REPAIR 1.SDR DALA2017010300008Seat Track · corrodedRBL 56 OTBD SEAT TRACK BS 870 - 898 FOUND SEVERAL SPOTS OF CORROSION. REPLACED THE SEAT TRACK IAW SRM 53-20-52 (FIG 201) REPAIR 5.SDR DALA2017010400045Cusp Web · crackedRT CUSP WEB CRACK AT STA 318 RBL 44. REPAIRED CRACKED RT CUSP WEB AT STA 318 RBL 44 IAW SRM 53-00-55 FIG 221 .032.SDR HALA2016122600562Control Unit · failedANTI-SKID FAIL ALERT ON LANDING GEAR EXTENSION. DIVERTED. REMOVED AND REPLACED BCU IAW AMM 32-45-01. PERFORMED RTS. RTS PASSED. OK FOR SERVICE.SDR DALA2016122610065Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS FOR THE CATWALK WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD. (LP #9077376)SDR DALA2017010300011Cusp Web · crackedRIGHT CUSP WEB CRACKED AT RBL 54.5, BS 503. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.SDR DALA2017010300005Seat Track · corrodedCORROSION ON THE LEFT INBD SEAT TRACK LBL 22, BS 465 - 503. CUT OUT DAMAGE AND INSTALLED 3 LUG REPAIR IAW SRM 53-20-52 REPAIR 1 FIG 201.SDR DALA2016122410064Frame · corrodedFRAME BS 313 HAS CORROSION AROUND FASTENERS AT ATTACH POINT FOR STR 30. BLENDED CORROSION ON FRAME AT STA 313 STR 30 AND FOUND TO BE OUT OF LIMITS ORG 0.050" REMAINING .039" WITHOUT TOOL TAG 6785 REPAIRED FRAME STA 313 STR 30 IAW B717 SRM 53-00-00 FIG 103 AND SDR DALA2016122410063Cusp Web · corrodedSURFACE CORROSION ON RIGHT SIDE CUSP WEB AT BS 562, 582, 598-617. REPAIRED CUSP WEB IAW SRM 53-00-55 2R-4.SDR DALA2016122410062Cusp Web · corrodedSURFACE CORROSION ON RT CUSP WEB AT BS 598-617. REPAIRED THE CUSP WEB IAW SRM 53-00-55 2R-4.SDR DALA2016122310056Hinge · damagedELONGATED HOLE ON LT WING OUTBOARD FLAP FWD OUTBOARD HINGE IAW NRTC 00456. THE HINGE WAS REMOVED IAW AMM 20-50-01 AND AMM 27-50-01. THE BEARING WAS REPLACED, AND THE HINGE WAS REPAIRED IAW ER/A 552872-14 REV ORIGINALSDR DALA2016122310055Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56, BS 726-826 HAS CORROSION, AND SCRATCHES. REPAIRED IAW SRM 53-20-52-2R-1.SDR DALA2016122310054Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56, BS 608-703 HAS CORROSION. BLENDED CORROSION . REPAIRED IAW SRM 53-20-52 REPAIR 1.SDR DALA2016122310053Seat Track · damagedLEFT OUTBD SEAT TRACK LBL 56 BS 488-581 HAS CORROSION, AND NICKS. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-20-52. REPAIRED IAW SRM 53-20-52 REPAIR 1.SDR DALA2016122210024Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56 BS 1010-1022 CORRODED. BLENDED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-20-52 REPAIR 1.SDR DALA2016122210023Seat Track · corrodedLEFT OTBD SEAT TRACK LBL 56 BS 488 CORRODED OUT OF LIMITS. REPAIRED THE SEAT TRACK IAW SRM 53-20-52-2R-1.SDR DALA2016122210022Support Bracket · crackedUPPER CABIN SEAT TRACK SUPPORT BRACKET AT BS 715 LBL 44 IS CRACKED. REMOVED THE SEAT TRACK SUPPORT BRACKET AND INSTALLED A NEW BRACKET IAW SRM 51-41-05.SDR DALA2016122210021Structure · corrodedFOUND AFTER REMOVAL OF FLOOR SUPPORT AT BS 172 TO 178 SUBFLOOR CORRODED. TRIMMED CORRODED SUBFLOOR IAW SRM 51-70-10 REPAIR 1, FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-70-10 REPAIR 1, AND SRM 53-10-51, INSTALLED THE REPAIR IAW SRM 51-70-10 REPAIR 1.SDR DALA2016122210020Floor Support · corrodedFLOOR SUPPORT HAS CORROSION ON UNDERSIDE. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-05 PG 17 STEP 8 AND SRM 51-41-02 PG 3 PAR F. ORIGINAL .SDR DALA2016122210019Skin · damagedRUDDER LOWER LEFT SIDE EXTERNAL SKIN IS BENT AT EDGE. REPAIRED IAW SRM 51-70-13 FIG 202SDR DALA2016122210018Support Bracket · crackedUPPER CABIN SEAT TRACK SUPPORT BRACKET AT BS 737 RBL 44 IS CRACKED. REPLACED THE SUPPORT BRACKET IAW SRM 51-41-05.SDR DALA2016122210017Seat Track · corrodedUPPER CABIN LEFT INBD SEAT TRACK LBL 22 BS 465 CORRODED OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED A REPAIR IAW SRM 53-20-52 REPAIR 1.SDR DALA2016122610066Floor Support · corrodedMAIN ENTRANCE DOOR THRESHOLD FLOOR SUPPORT BS 160 - 200, LBL 62 CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-02, 51-41-05, 51-41-08, AND DRAWING 52929169.SDR DALA2016122109992Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN STA 1021 BTW LONG 13/14 LT. EXTERNAL FUSELAGE SKIN WAS REPAIRED PER ETI-17-16-183 REV. ORIGINAL AND ER/A 552865-14 REV ORIGINAL SECTION I. PERFORM REPETITIVE EXTERNAL GENERAL VISUAL INSPECTION OF THE REPAIR EVERY C-CHECK OR 24 MOSDR DALA2016122109991Cusp Web · crackedRT CUSP WEB AT STA 679 IS CRACKED. MARKED IN RED. REPAIRED CRACK CUSP WEB AT STA 679 RT IAW 53-00-55 REPAIR NR 4.SDR DALA2016122610067Floor Panel · corrodedFORWARD CARGO FLOOR PANEL CORRODED. BLENDED THE FLOOR PANEL IAW SRM 53-00-00 SHEET 1. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW FLOOR PANEL IAW AMM 25-58-01-350-801 C1 AND C2.SDR DALA2016122109989Seat Track · corrodedUPPER FUSELAGE CABIN RT SEAT TRACK STA 356-456 BL 22R CORRODED AND GOUGED METAL. MARKED. RT INBD SEAT TRACK GOUGED AND CORRODED BLENDED TRACK AT STA 356-395 ORG THICKNESS .100 REMOVED .027 ALLOWED .040, BLENDED STA 405-456 ORG THICKNESS .100 REMOVED .025 ALLOWSDR DALA2016122109987Longeron · damagedLONGERON 29L IS CORRODED FROM STA 930 TO STA 954. CLEANED UP CORROSION ON L29L FS 930-954 IAW SRM 51-10-04 PAR 35. ORIGINAL THICKNESS .125" REMAINING .121 WITHIN ALLOWABLE LIMITS IAW SRM 53-00-00 FIG 103. FOUND ELONGATE HOLE AT 943 REPAIRED LONGERON AT FS 943 SDR DALA2016122009963Engine · making metalTHE FLIGHT CREW RETURNED THE AIRCRAFT TO ATL FOLLOWING THE FAILURE OF THE NR 2 ENGINE. MAINTENANCE FOUND METAL IN TAILPIPE UPON THE AIRCRAFT'S ARRIVAL AND REPLACED THE ENGINE.SDR DALA2016122009962Stiffener · crackedAFT ACCESSORY COMPARTMENT HAS A CRACK ON STIFFENER STA Y=1200 CANT LONG PROJECTION 2L. STIFFENER WAS REPAIRED PER SRM 53-00-00 REPAIR 1 FIG 201 IN REF ORNRC 00394.SDR DALA2016122009961Support · crackedAFT CARGO COMPARTMENT HAS A CRACK ON VERTICAL SUPPORT STA Y=816 LONG 30 (AMDS 5331-2001). CRACK DIMENSION IS .650". CRACK IN VERTICAL SUPPORT WAS STOP DRILLED PER SRM 53-00-00 FIG 201, HFEC WAS ACCOMPLISHED. NO CRACK WERE FOUND AFTER STOP DRILL PER NDT SPM 06-
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