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 DALA2016053104212Pan · crackedCRACK ON AFT/UPPER CORNER BETWEEN BS 851 TO 870 AT LT RING PAN. PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016053104211Cusp Web · crackedCRACKED LT CUSP WEB BETWEEN BS 587 TO 589, X=45. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 221.SDR DALA2016053104210Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO BS 655 IN CPAX, SM, ZONE: 201 CARD: 10. ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 636 TO 655 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016053104209Pan · crackedCRACK ON FWD, UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775. ON FWD/UPPER CORNER AT LT RING PAN BETWEEN BS 756 TO 775 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202.SDR DALA2016053104207Pan · crackedCRACK ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832. ON AFT, UPPER CORNER AT LT RING PAN BETWEEN BS 813 TO 832 WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, CRACK LENGTH, L= 0.235".SDR DALA2016053104206Pan · crackedCRACK ON FWD, LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927. ON FWD / LOWER CORNER AT LT RING PAN BETWEEN BS 908 TO 927 WAS REPAIRED IAW SRM 50-20-02, REPAIR 1, FIG 202, CRACK LENGTH 0.198".SDR DALA2016053104205Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 617 TO 636. THE PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR, FIG 202.SDR DALA2016053104208Attach Angle · crackedAFT SIDE, BS 1022 AT LONGERON 7R ATTACH ANGLE CRACKED FROM FASTENER INTO RADIOUS. REMOVED DAMAGE ON AFT SIDE, BS 1022 LONGERON 7R ATTACH ANGLE. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 51-70-11, 51-41-02, 51-41-05.SDR DALA2016053004204Doubler · dentedDENTS ON PREVIOUS REPAIR ON LOWER SKIN AT L1 DOOR. REPLACED IAW SRM VOL 1 52-10-01, FIG 4 AND 51-30-02, VOL II.SDR DALA2016053004203Skin · wornWORN EXTERNAL SKIN AT EDGE BETWEEN BEAMS 1 AND 3 AT AFT CARGO COMPARTMENT DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-00-01, REPAIR 8, FIG 204.SDR DALA2016053004202Pan · crackedCRACK ON FWD PAN BS 370 BETWEEN BEAMS 2 AND 3 AT FWD CARGO COMPARTMENT DOOR. PAN WAS REPAIRED IAW SRM 52-30-02, FIG.201, 51-41-02, 51-41-04, 51-41-01, 51-10-04 PAR 15.SDR DALA2016052904201Intercostal · crackedCRACKED INTERCOSTAL X=0, BS 636 TO 617 AT CEILING AREA OF FWD CARGO COMPARTMENT. INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00, FIG 201.SDR DALA2016052904200Frame · crackedCRACKED FRAME BS 689, LONGERON 26L AT KEEL BEAM AREA. THE FRAME WAS REPARED IAW SRM 53-00-00, REPAIR 1, FIG 201.SDR DALA2016052904199Frame · crackedCRACK ON FRAME BS 674, LONGERON 25L AT UNDER WING BARREL KEEL BEAMS. THE FRAME WAS REPAIRED IAW SRM 53-00-00, REPAIR 1, FIG 201.SDR DALA2016052904198Cusp Web · crackedCRACKED CUSP WEB BETWEEN X=54 AND X=60 BETWEEN BS 851 AND 870. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.SDR DALA2016052904197Beam · crackedCRACK ON NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE L1 DOOR. NR 1 BEAM WAS REPAIRED IAW SRM 51-41-02, 51-41-01, SRM 52-10-02, FIG 202, SHEET 8, 51-20-09, 51-41-03, AND 51-10-04, PAR 15.SDR DALA2016052904196Doubler · corrodedCORROSION ON DOUBLER ATTACH INNER FUSELAGE SKIN AND CUSP WEB BETWEEN X=54 TO X=60 BS 579 TO 598, RT SIDE. CORROSION WAS REMOVED, AREA WAS MEASURED. ORIGINAL THICKNESS: 0.080" REMAINING THICKNESS: 0.041" THEREFORE ITS OUT OF LIMITS AND DOUBLER WAS REPLACED ISDR DALA2016052804194Skin · gougedGOUGES ON EXTERNAL SKIN BETWEEN BS 408-420 BETWEEN BEAM 2 AND LOWER EDGE AT FWD CARGO COMPARTMENT DOOR. SKIN WAS REPAIRED IAW SRM 52-00-01, FIG 202.SDR DALA2016052704193Cusp Web · corrodedCORROSION ON CUSP WEB BS 245 TO 249, RT SIDE IN REF CARD 59, ZONE 200. CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 244 TO BS 249 RT SIDE IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 215, REPAIR 4, SRM 53-20-51, FIG 1 ITEM SDR DALA2016052704192Cusp Web · corrodedAWR EXCESSIVE CORROSION ON RT CUSP WEB BETWEEN BS 408 AND BS 427 IN REF CARD 59, ZONE 200. CARD 96, ZONE 200. DUE TO EXCESSIVE CORROSION ON CUSP WEB BS 408 AND STA 427 IN REF CARD 59, ZONE 200 AREA WAS REPAIRED IAW SRM 53-00-55, FIG 203, REPAIR 4, DWG 9930538SDR DALA2016052704185Light · inoperativeEIGHT EMERGENCY LIGHTS INOPERATIVE. LIGHTS WERE REPLACED IAW 33-52-00.SDR DALA2016052604191Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW=10, XCW=50 AT LT MLG WHEEL WELL. SM, MLG. CORROSION ON WING BOX SKIN WAS ATTENDED WITH ER/A 545162-14, REV ORIGINAL AND SRM 51-41-03, 51-41-01, 51-41-05, 51-10-04 PAR 14, 21, 26. OLYMPUS NDT 3DL, SONOSDR DALA2016052604183Retainer · damagedAFT CARGO DOOR AND SEAL RETAINER DAMAGED ON LOWER/ AFT CORNER, 2 AREAS, MARKED. REPAIRED DAMAGE TO AFT LOWER CARGO DOOR AFT LOWER CORNER BY BLENDING OUT DAMAGE AND INSTALLING DOUBLER IAW B717 SRM 52-30-02 REPAIR 8 FIG 201. REMOVED AND REPLACED AFT LOWER CORNERSDR DALA2016052604182Doubler · damagedPREVIOUS REPAIR DOUBLER WORN AND BENT, INNER PAN AND OUTER PAN BS 954 BETWEEN BEAM 1 AND 2 AT AFT CARGO COMPARTMENT DOOR. REPAIR DOUBLER WAS FABRICATE AND REPLACED IAW SRM 52-30-02, REPAIR 4, FIG 201.SDR DALA2016052604181Cusp Web · corrodedAT BS 446 RT CUSP WEB CORRODED ON BOTTOM SIDE. REMOVED CUSP WEB, RT WEB OUT OF LIMITS MATERIAL IS 100 PERCENT IN SEVERAL LOCATIONS, REMOVED CUSP TEE AT BS 446-484, CUSP TEE IS OUT OF LIMITS 100 PERCENT MATERIAL LOSS AT SEVERAL LOCATIONS, FABRICATED REPAIR PIESDR DALA2016052604180Cusp Web · crackedCRACKED RT CUPS WEB BETWEEN X=54 TO X=60, BS 368 TO 375. CUSP WEB WAS REPAIRED IAW SRM 53-00-05, FIG 214 AND 51-41-05, 51-41-02, 51-10-04 AND 51-40-08 TRIMOUT WAS ACCOMPLISHED.SDR DALA2016052604179Floor Support · corrodedCORROSION ON FLOOR SUPPORT X=44 BETWEEN BS 1022 TO 1060 AT LT PAX CABIN. FLOOR SUPPORT WAS REPLACED IAW DWG: 9981474, REV: L.SDR DALA2016052604184Pin · unsecureL1 DOOR SLIDE LOWER INFLATION CABLE PIN FOUND UNSECURED. INSTALLED PASSENGER ENTRY DOOR SLIDE.SDR DALA2016052504148Battery Pack · inoperativeDURING SERVICE CHECK, FOUND AFT CABIN CEILING EMERGENCY LIGHTS INOPERATIVE. R & R CABIN EMERGENCY POWER SUPPLY BATTERY PACK.SDR DALA2016103107958Seat Track · corrodedCORROSION ON SEAT TRACK X 44 AT BS 609. THE SEAT TRACK WAS REPAIRED IAW SRM 51-10-04 AND 53-20-52 FIG.201.SDR DALA2016103107957Web · corrodedVERTICAL WEB AFT OF L1 DOOR FRAME IS CORRODED ABOVE FLOOR BS 190. COMPLIED WITH ERA 54677-14 REV ORIGINAL.SDR DALA2016052404176Cusp Web · crackedCUSP WEB CRACKED AT APPROXIMATELY BS 670 RT. R & R RT CUSP WEB AT BS 670 IAW DWG 9910151, REV CH.SDR DALA2016052404175Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS=10 TO XCW=50 AT RT MLG WELL CORROSION ON WING SKIN WAS ATTENDED WITH ER/A NR 545162-14, REV ORIGINAL 546475-14, REV ORIGINAL AND SRM 51-10-04, 51-41-03, 51-70-10, 51-70-11 AND 51-41-05.SDR DALA2016052604149Control Valve · malfunctionedDURING SLAT EXTENSION SLAT DISAGREE MSG ENUNCIATED AND ACFT ROLLED TO THE RT. FLIGHT CREW DECLARED AN EMERGENCY, FOLLOWED QRH PROCEDURES NO SLATS NO FLAP LANDING. MAINTENANCE R & R SLAT CONTROL VALVE.SDR HALA2016052200204Control Handle · contaminatedUPON GEAR EXTENSION, ALL GEAR UNSAFE, RED, LIGHTS ILLUMINATED. GEAR HANDLE WAS FOUND TO BE STICKY AND TIGHT. SUSPECT GEAR HANDLE WAS NOT MOVED TO THE FULL DOWN AND LOCKED POSITION DURING GEAR EXTENTION. INSPECTED AND CHECKED RIGGING BETWEEN GEAR CONTROL HANSDR DALA2016052904195Intercostal · crackedINTERCOSTAL CRACKED ON FWD SIDE OF BS 636, FLOORBEAM BL0. REPAIRED CRACK IN INTERCOSTAL IAW SRM 53-00-00, REPAIR 1, FIG 201 AND SRM 51-41-05, PARA 10.SDR DALA2016052404177Intercostal · corrodedLOWER FUSELAGE, AFT CARGO BILGE, BETWEEN BS 1028-1037-L30, CORROSION. REMOVED INTERCOSTAL REINSTALLED INTERCOSTAL IAW SRM 51-40-2. REMOVED STR, FABRICATED NEW STR 717, SRM 52-20-05. INSTALLED STR IAW 717 SRM 51-40-2.SDR DALA2016052104174Skin · crackedBS 1022 ABOVE LONGERON 14R EXTERNAL SKIN CRACKED, HFEC VERIFIED. REPAIRED THE SKIN IAW ERA NR 545671-14.SDR HALA2016052000203Unknown · smokeWHILE DEPLANING, SMOKE APPEARED IN THE CABIN-TURNED OFF PACK, SMOKE DISAPPEARED. F/A DEPLOYED TAIL SLIDE. FERRY FLIGHT REQUIRED THIS ACFT HAS BEEN INSPECTED AND IS SAFE FOR INTENDED FLIGHT. REMOVED TAIL CONE TO ACCOMPLISED INSPECTION REMOVED IAW AMM 53-52-0SDR HALA201605200203Unknown · smokeF/A REPORTED SMOKE IN CABIN.SDR DALA2016052004043Cargo Track · corrodedCORROSION ON RT TIE TRACK FROM BS 994 TO 1022 AT AFT CARGO COMPARTMENT, C2. TIE TRACK FROM BS 994 TO 1022 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. ORIGINAL THICKNESS IS 0.090" MINIMUN REMAINING IS 0.0SDR DALA2016052004042Cargo Track · corrodedCORROSION ON RT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. RT TIE TRACK FROM BS 813 TO 889 WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-01, 51-41-02, 51-40-08, 51-10-04 PAR 15, 21, AND 37. OLYMPUS 38 DL PLUS SONOPEN V260SM 25AUG16 AMX-PNSDR DALA2016062404926Skin · damagedDAMAGE TO VERTICAL STABILIZER RT SKATE ANGLE AND SKIN BETWEEN L2R AND L4R, BETWEEN STA 1103 AND 1145. ACCOMPLISHED HFEC INSPECTION OF CRACK IAW NDT/SPM 06-10-01.001, MARKED THE END OF THE CRACK END AND VERIFIED AFT CRACK EXTENDS INTO CENTER OF A RIVET HOLE OTSDR DALA2016062404915Skin · puncturedFUSELAGE SKIN PUNCTURED BETWEEN CANTED STA 1103 AND 1131 BETWEEN L6R AND L7R. CUTOUT DAMAGED SKIN. ACCOMPLISHED HFEC INSPECTION OF CUTOUT IAW NDT/SPM 06-10-01.001. NO CRACKS NOTED. INSTALLED DOUBLER IAW INSTRUCTIONS OF ER/A 547090-14, SECTION III. ASSOCIASDR DALA2016052404178Stiffener · crackedAFT ACCY RT SIDE FRAMES 1178.225 & 1200 HAVE 2 EA SUPPORT STIFFENERS CRACKED. CAN BE SEEN INSIDE RT VENT BOX. R & R CRACKED STIFFENERS IAW SRM 51-41-02, SECTION 4.SDR DALA2016051904045Skin · gougedLT FUSELAGE GOUGE / DENT 3" X 8" BS 1159, STR 19-20L .0625" DEEP. BLENDED IAW SRM 53-01-01. ACCOMPLISHED HFEC IAW NDT/SPM 06-10-01.001, NO CRACKS NOTED. ACCOMPLISHED INTERNAL GVI, NO DAMAGE NOTED. ACCOMPLISHED UT INSPECTION IAW NDT/SPM 04-00-03. ALODINE AND SDR DALA2016052004039Cargo Track · corrodedCORROSION ON LT TIE TRACK FROM BS 813 TO 889 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 813 TO 889 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, AND CIC APPLIED IAW SRM 53-20-51, FIG 1, ITEM 3, 51-40-08, 51-10-04, PAR 15, 21, 37, 5SDR DALA2016052004038Cargo Track · corrodedCORROSION ON LT TIE TRACK FROM BS 908 TO 1022 AT AFT CARGO COMPARTMENT. C2, SM. LT TIE TRACK FROM BS 908 TO 1022 WAS REPLACED, DRILLED, ADJUSTED, TREATED, PAINTED, INSTALLED, CIC APPLIED, AND REPAIR PARTS WERE INSTALLED IAW SRM 53-20-51, FIG 1, ITEM 9, 51-40-SDR DALA2016062404927Skin · damagedDENT AND GOUGES IN RT VERTICAL STABILIZER SKIN APPROXIMATELY 12" ABOVE FUSELAGE BETWEEN CS 1103 AND CS 1131. BLEND AREA OF PAINT FOR HFEC. REF SRM 53-01-01. ACCOMPLISHED HFEC INSPECTION OF BLENDED AREA IAW NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINE ANDSDR DALA2016062404925Skin · gougedMULTIPLE GOUGES AND DENTS AT L-3R BETWEEN FS 1095 AND FS 1144. ACCOMPLISHED HFEC OF BLENDED AREA IAW NDTSPM 06-10-01.001. NO CRACKS NOTED. ASSOCIATED ER/A 00-547136 ADDED FOR AC 9562. REPAIRED IAW ER/A 547291-14AD, REV A. ER/A MATCHES ALL PRIS. CLOSED LO
Back to Boeing 717-200