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 DALA2016060704393Channel · crackedCRACKS ON CHANNEL OF FLOOR PANEL NR 222 X. CHANNEL WAS REPAIRED IAW SRM 53-20-50, FIG 201. HFEC INSPECTION WAS PERFORMED, NO CRACKS WERE FOUND AFTER STOP DRILL IAW NDT SPM 06-10-001.SDR DALA2016060704392Skin · damagedDAMAGE ON LT SIDE OF RUDDER SKIN PANEL, LOWER SECTION. SM, CARD 5, ZONE 370. DAMAGED AREA WAS REPAIRED IAW SRM 51-70-13 R1.SDR DALA2016060604391Skin · crackedVERTICAL STAB L/E FWD OF RAM AIR SCOOP COMMON TO PANEL 370AL LOWER LT SIDE SKIN IS CRACKED AND UPPER AREA IS HEAVILY ERODED. REPLACED DOUBLER, PN 5910242-121, SKIN, ON VERT SLAB DORSAL FIN FWD OF RAM AIR SCOOP COMMON TO PANEL 370 AL IAW SRM 51-41-02, PG 1 PARSDR DALA2016060604390Door · wornMAINTENANCE DISCOVERED THAT THE AFT CABIN BULKHEAD EMERGENCY ESCAPE DOOR WAS WORN AND DAMAGED ON THE LOWER INBD SIDE. THE DAMAGE AREA WAS REPAIRED IAW SRM 52-10-02. REPAIR 15 AND 16.SDR DALA2016060604389Cusp Web · crackedCRACKED LT CUSP WEB BS 813 AND 825. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 226.SDR DALA2016060604388Cusp Web · crackedCRACKED LT CUSP WEB BS 674-676, X 44 TO 46. CUSP WEB WAS REPLACED IAW SRM 53-00-55, FIG 223,SDR DALA2016060604387Stiffener · crackedCRACKED STIFFENER ON AFT PRESSURE BULKHEAD BETWEEN LONGERONS 7RT AND 8 RT AT PASSENGER CABIN. STIFFENER WAS REPLACED IAW SRM 51-41-05 DWG 9915558, REV BA CRACK L= 0.750".SDR DALA2016060604386Stiffener · crackedAFT ACCY CANTED FRAME BS 1200 INSIDE LT VENT BOX, VERTICAL STIFFENER CRACKED. REPLACED IAW DWG ORNRC 67775-0300-0036. FABRICATED NEW VERTICAL STIFFENER, INSTALLED IAW SRM 51-41-02, PARA 4.SDR DALA2016060604385Floorbeam · crackedCRACKED FLOORBEAM BS 737 AND X -50. FLOORBEAM WAS REPLACED IAW 51-41-02 AND 51-41-05.SDR DALA2016060604375Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS FOR THE FWD OVERWING HATCH WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016060604374Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA2016060504373Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT SECTION OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.SDR DALA2016060504384Frame · crackedCRACKED FRAME BS 1037 AT INTERSECTION WITH LONG 17RT. RT AFT LAV AREA. FRAME ON STA Y=1037, RT WAS REPAIRED IAW SRM 53-20-07, FIG 201.SDR DALA2016060504383Cusp Web · damagedCORROSION ON RT CUPS WEB, UPPER AND LOWER SURFACE, X 54 TO X 60, BS 436 TO 465, 503 TO 522, 522 TO 579. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 203, 51-41-02, AND 51-41-05 FROM BS Y=436 TO Y=465 AREA WAS REINSPECTED AND NO CORROSION WAS FOUND. RII CSDR DALA2016060504382Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14, REV. ORIGINAL.SDR DALA2016060904469Support · crackedLOWER FUSELAGE UNDER WING KEEL BEAM LT BS 674 CRACKED KEEL BEAM SUPPORT. REPAIRED KEEL BEAM SUPPORT IAW ER/A 545683-14MA.SDR DALA2016060904468Cusp Web · corrodedCORRODED CRACKS, AND MISSING FASTENERS AT FLOOR SUPPORT ON LT CUSP WEB BETWEEN BS 148-331. REPLACED CORRODED FLOOR SUPPORT AND SUB FLOOR IAW SRM 51-41-02. INSTALLED MISSING FASTNERS IAW SRM 51-41-02. REPAIRED LT CRACKED CUSP WEB IAW SRM 53-00-55, REPAIR 4.SDR DALA2016060404381Skin · crackedCRACKED EXTERNAL SKIN AROUND OF HOLD OPEN LOCK HOUSING AT MAIN L1 DOOR. EXTERNAL SKIN WAS REPAIRED IAW SRM 52-10-01, REP 4, FIG 201. LENGTH CRACK = 0.270", RII COMPLETED.SDR DALA2016060404380Longeron · corrodedCORROSION ON LONGERON TERMINAL 24 RT, BETWEEN BS 927 TO 946 AT AFT CARGO COMPARTMENT. LONGERON END WAS REPLACED IAW DWG 5911494, REV CZ AND SRM 51-41-05, PAR 8, UT, WAS ACCOMPLISHED ORIGINAL THICKNESS 0.050" REMAINING THICKNESS 0.025 THEREFORE IT IS OUT OF LSDR DALA2016060404379Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND ELONGATED HOLE OF COUNTERSINK OF FUEL ACCESS DOOR 141AR. CARD 44, ZONE 000. CORROSION SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE 141AR WERE REMOVED AND MEASURED, AND FOUND OUT OF LIMITS WITH 5 HOLES 0.700", 0.662", 0SDR DALA2016060404378Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 952. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 205, RII COMPLETED BY INSPECTION.SDR DALA2016060404377Spar · crackedAT THE LEFT HORIZONTAL STABILIZER AFT SPAR, BOTH ELEVATOR CONTROL TAB FITTING CLOSEOUTS ARE CRACKED, MARKED CA016 AND CA017. REPLACED LT OTBD AND INBD ELEVATOR CONTROL TAB FITTING CLOSEOUTS IAW SRM 51-45-05, PARA 10.SDR DALA2016060304372Lanyard · disconnectedF/A DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A DISCONNECTED LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR PARTSDR DALA2016060304371Floor Panel · damagedDAMAGED PASSENGER CABIN FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 546511-14.SDR DALA2016060304321Skin · wornWEAR ON EXTERNAL SKIN APPROXIMATELY STATION 170, LOWER EDGE AT MAIN ENTRANCE DOOR. EXTERNAL SKIN, LOWER EDGE, WAS REPAIRED IAW SRM 52-10-01, FIG 201, REP 2 HFEC INSPECTION WAS PERFORMED AND NO CRACKS WERE FOUND. PERFORM INSPECT DECAL CONDITION EVERY "C" CHECSDR DALA2016060304320Attach Angle · crackedCRACK ON ANGLE TO ATTACH LT AFT ENGINE PYLON SUPPORT BULKHEAD, BS Y=1022 BETWEEN LONGERONS 6 TO 7L ALSO LONGERONS 16 TO 17L. ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-10-14, PAR. 21 AND 15.SDR DALA2016060304319Pan · crackedCRACK ON INNER PAN APPROXIMATELY BS 200, AFT EDGE, BETWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. INNER PAN WAS REPAIRED IAW SRM 52-10-02, REP 2, FIG 201. LENGTH OF CRACKS: 1.800", 2.400".SDR DALA2016060304318Beam · crackedCRACK ON BEAM NR 1, FWD EDGE AT MAIN ENTRANCE DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. LENGTH OF CRACK = 0.800".SDR DALA2016060304317Stiffener · damagedLEFT HORIZONTAL STABILIZER AFT SPAR STIFFENERS DAMAGED, TWO DENTED AND ONE TORN CORNER, REMOVED THE STIFFENERS IAW SRM 51-40-08.SDR DALA2016060304316Cusp Web · corrodedCRACK ON LT CUSP WEB BETWEEN X 50 TO X 54, BS 674 - 680. CUSP WEB REPAIRED IAW SRM 53-00-55, FIG 226.SDR DALA2016060204315Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 940. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215.SDR DALA2016060204314Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BETWEEN X-54/60, BS 794 TO 813, CARD 111, ZONE 200. RT CUSP WEB WAS REPAIRED BETWEEN BS 794-813 IAW SRM 53-00-55, FIG 216.SDR DALA2016060204313Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620DT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620DT WAS REMOVED AND WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .680 IN, 0.680 IN AND 0.665 IN, IAW SRM 57-10-01SDR DALA2016060204312Access Panel · corrodedCORROSION AND COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS DOOR 620AT AT RT WING. CORROSION AT COUNTERSINK OF FUEL ACCESS PLATE 620 AT WAS REMOVED AND COUNTERSINK WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES 0.661 IN, 0.665 IN, 0.666 IN, IAW ASDR DALA2016060204311Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS DOOR 520DT AT LT WING. CORROSION AT FUEL ACCESS PLATE 520DT ON COUNTERSINK WAS REMOVED, MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES DIAMETER MAX 0.619IN, 0.672IN AND 0.694 IN IAW SRM 57-1SDR DALA2016060104310Skin · damagedFUSELAGE SKIN DAMAGED AT APPROXIMATELY BS 1155 L-20L. COMPLETED REPAIR, REF SRM 53-03-01, FIG 204. CLASS 1, REF NR 27 SUMMERY.SDR DALA2016060104275Lanyard · disconnectedF/A DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE AT DOOR 1L HAD A DISCONNECTED LANYARD. THE LANYARD WAS NOT CONNECTED BETWEEN THE GIRT-BAR AND THE SLIDE RELEASE. THIS WOULD PREVENT PROPER DEPLOYMENT OF THE ESCAPE SLIDE AND IS NOT IN COMPLIANCE WITH 14 CFR, PARTSDR DALA2016060104241Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 503 TO 522. CUSP WEB WAS REMOVED, AND FOUND OUT OF LIMITS. CUSP WEB WAS REPAIRED IAW SRM 51-41-02, SRM 51-10-04 PAR 15, 21, 26, AND 37, SRM 53-00-55.SDR DALA2016060104240Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 636 TO 655. RING PAN WAS REPAIRED IAW SRM 50-20-02. REPAIR 1, FIG 202, TYPE B.SDR DALA2016060104239Pan · crackedCRACKED RT UPPER/FWD CORNER ON RING PAN BETWEEN BS 696 TO 715. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 203, TYPE C.SDR DALA2016060104238Pan · crackedCRACKED RT UPPER, AFT CORNER ON RING PAN BETWEEN BS 832 TO 851. RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIG 202, TYPE B.SDR DALA2016060104237Pan · crackedCRACK ON FWD/LOWER CORNER AT LT RING PAN BETWEEN BS 832 TO 851 IN CPAX, SM, ZONE: 201 CARD: 3. DAMAGE ARE WAS TRIMED OUT IAW SRM 56-20-02, FIG 202. REPAIR PARTS WERE FABRICATED IAW SRM 50-20-02, FIG 202, REPAIR PARTS WERE INSTALLED IAW SRM 51-40-02 AND 51-40-SDR DALA2016060104236Seat Track · crackedCRACKED BEAM BELOW SEAT TRACK X=-54 AT BS 737, PAX CAB, SM, ZONE 140, CARD 6, WB, CARD 6, ZONE 140. BEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05. LONG CRACK: 2.000".SDR DALA2016060104235Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP WEB BETWEEN X=54/60 AND BS 995, CARD 110, ZONE 200. LT CUSP WEB BETWEEN X=54/60, BS Y=995 WAS REPAIRED IAW SRM 53-00-55, FIG 215.SDR 2016F00129Skin · delaminatedDURING ROUTINE MAINTENANCE LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.SDR 2016F00130Skin · delaminatedDURING ROUTINE MAINTENANCE LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.SDR 2016F00131Skin · delaminatedDURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE LOWER AND UPPER SURFACE. SUP: P/N 5940974-1.SDR 2016F00128Skin · delaminatedDURING ROUTINE MAINTANANCE INSPECTION, LT SPOILER FOUND WITH DELAMINATION ALONG THE UPPER AND LOWER SURFACE.SDR DALA2016060104234Stringer · crackedWHILE REMOVING THE RUDDER ACTUATOR FOUND STR FOR RUDDER BRACE AT OTBD END CRACKED. ALSO 3 MOUNTING SCREWS LOOSE AND 1 MISSING FOR BRACE. REPLACED INTERCOASTAL AND SCREWS IAW SRM 51-41-02.SDR DALA2016053104213Frame · crackedCRACK ON FRAME BS 674 - 689, AND BS 715, LONGERON 25RT AT UNDERWING BARREL KEEL BEAMS. FRAME REPAIRED IAW SRM 53-00-00, FIG 201.
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