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 DALA2017070505180Fitting · crackedCRACKED LOWER FITTING INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPLACED IAW SRM 51-41-01, AND 51-41-05.SDR DALA2017070505179Skin · delaminatedDELAMINATION WAS FOUND BELOW DENTS NR 3 & 12 OF RT WING FLAP FORWARD MOVEABLE VANE LOWER SURFACE. REPAIRED SRM 57-53-01, FIG 201, REP 1.SDR DALA2017070405178Panel · corrodedSEVERAL COUNTERSINKS OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER. REPAIRED IAW SERVICE GENERAL REPAIR DRAWING SG 95550001 REV ORIGINAL.SDR DALA2017070405177Frame · crackedCRACK ON LT FORMER BS 694, LONGERON 26L. THE FRAME WAS REPAIRED IAW SRM 51-70-11, REP 1.SDR DALA2017070305155Intercostal · crackedCRACKED INTERCOSTAL BETWEEN BEAMS 4 AND 5, BS 181, FWD PASSENGER DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9955763, REV M.SDR DALA2017070305175Rub Strip · corrodedCORROSION ON RUBSTRIP OF FUEL ACCESS DOOR 520JB I. NEW RUB STRIP 520JB WAS REPLACED PER B717-200 SRM 57-10-01-2R REP 3 PAR 6. (LP #0098256)SDR DALA2017070305154Access Panel · corrodedCORROSION ON SETTLEMENT AREA AT FUEL ACCESS PANEL. THE FUEL ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.SDR DALA2017070305153Access Panel · corrodedCORROSION ON COUNTERSINK HOLES ON FUEL ACCESS PANEL. REPLACED THE ACCESS PANEL IAW SRM 57-10-01, PAR 5, CONDITION II.SDR DALA2017070205123Unknown · malfunctionedAFT EXIT SIGN ILLUMINATED WHILE EMERG LIGHT SWITCH IN ARM POSITION. PERFORMED EMERGENCY LIGHTS TEST PER AMM 33-51. CYCLED EMERGENCY LIGHTS SWITCH SEVERAL TIMES. AFT EXIT SIGN DID NOT ILLUMINATE IN THE ARMED POSITION. SYSTEM CHECKS GOOD. A/C OK FOR SVC.SDR DALA2017070205124Lens · missingSTANDBY DIFFUSER LENS IS MISSING AT ROW 27. INSTALLED SERVICEABLE LENS COVER ON EMERGENCY LIGHT AT ROW 27, OPS CK NORMAL.SDR DALA2017070205119Power Supply · inoperativeOVERWING EMERGENCY EVACUATION LIGHTS ARE INOPERATIVE. R&R OVERWING EMERGENCY EVAC BATTERY POWER SUPPLY PER MM 33-51. OPS CHK GOOD. OK FOR SVC.SDR DALA2017070205118Battery · dischargedFOUND EMERG LIGHTS ALONG WALKWAY IN 48 SEC OUT. REPLACED BATTERY AND POWER SUPPLY PER AMM 33-51.SDR DALA2017070205114Skin · damagedLOOSE FASTENERS ON LT/RT SIDE AT VERTICAL STABILIZER LEADING EDGE STRUCTURE (REPAIR DOUBLER) AND REMOVABLE LEADING EDGE, STA ZFS=52.267. SEVERAL COUNTERSINK ON REMOVABLE LEADING EDGE STRUCTURE WERE MEASURED ABOVE 0.540" WERE LIMIT IS 0.517" AND ABOVE 0.420" WESDR DALA2017070205113Beam · crackedCRACKED BEAM NR 4 FWD EDGE ON R1 DOOR (PTAS). BEAM NR 4 WAS REPLACED PER SRM VOL II 51-30-02 AND 51-30-05.SDR DALA2017070205112Doubler · damagedWEAR AND NICKS ON PREVIOUS REPAIR DOUBLERS STA 907 LT/LWR ALSO STA 909 LT/UPPER AT PASSENGER CABIN RING PANS AREA. REPAIR DOUBLERS WERE REPLACED PER SRM 56-20-02 REPAIR 1 FIGURE 202.SDR DALA2017070105111Pan · crackedCRACK ON RT RING PAN (FWD UPPER CORNER) STA Y=756 AT PAX CABIN (CPAX). RING PAN WAS REPAIRED PER SRM 56-20-02-2R-1 REPAIR 1.SDR HALA201707050175Unknown · malfunctionedATB- UNABLE RNP, MAP SHIFT. BITE CHECKED MMR NR 1 AND 2, ADIRU NR 1 AND 2, AND VIA NR 1 AND 2, ALL TESTS PASSED AND NO FAULTS NOTED, RESET VIA NR 1 AND 2 IAW MM 31-43-00 - RTS TESTS PASS - MAP BACK TO NORMAL POS - A/C CHECK OK - OK FOR SVCSDR DALA2017070105110Longeron · crackedCRACKED LONG 6 RT ON STA 1022. AT PASSENGER CABIN AREA. LONG 6 RT ON STA 1022. WAS REPAIRED PER SRM 53-00-05-2R-2-, FIG 201.SDR DALA2017070105109Longeron · crackedCRACKED LONGERON 6 LT ON STA 1022 AT PASSENGER CABIN AREA. LONGERON WAS REPAIRED PER SRM 53-00-05-2R-2, FIG 201.SDR DALA201706301Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK, THE LT OTBD SPOILER FOUND DELAMINATED.SDR DALA2017070305156Access Panel · damagedELONGATE HOLES ON FUEL TANK ACCESS PANEL 620DB. THE ACCESS PANEL WAS OUT OF LIMITS FOR EXCESSIVE DAMAGES IAW SRM 57-10-01 AND WAS REPLACED.SDR DALA2017063005108Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 620CT AND 620FT. FUEL TANK ACCESS 620CT AND 620FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005107Skin · corrodedCORROSION ON SETTLEMENT AREA ON FUEL TANK ACCESS 520CT AND 520DT. FUEL TANK ACCESS 520CT AND 520DT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WERE REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005106Access Panel · corrodedCORROSION ON COUNTERSINK AREA ON FUEL TANK ACCESS 520FT. FUEL TANK ACCESS 520FT OUT OF LIMITS FOR EXCESSIVE DAMAGES PER SRM 57-10-01 AND WAS REPLACED. THE EFFECTIVITY WAS VERIFIED PER IPC 57-22-01-01.SDR DALA2017063005080Skin · crackedCRACK ON FUSELAGE SKIN Y=1087 BTW LONG 13L-14L. FUSELAGE SKIN WAS REPAIRED PER ETI -17-17-072 REV 2 AND ER/A 558145-14 REV ORIG.SDR DALA2017063005079Frame · crackedCRACK ON RT FORMERS Y=715 , Y= 694 AT UNDERWING CANTED KEEL , INTERNAL STRUCTURE. FRAMES WERE REPAIRED PER SRM 51-70-11-2R. HFEC INSPECTION WAS PERFORMED AND 01 CRACK OF 0.4" ON RT FORMER Y=694 AT UNDERWING CANTED KEEL, INTERNAL STRUCTURE AND 01 CRACK OF 0.5" SDR DALA2017063005078Attach Angle · corrodedCORROSION ON ANGLE THAT ATTACH FUSELAGE TO CUSP ANGLE BTW LONGS 18L-19L, BTW STA Y=889-908. ANGLE WAS REPLACED PER SRM 53-20-51-01 AND DWG 9910151 ITEM -117. MEASURED (UT) WAS ACCOMPLISHED PER NDT SPM 04-00-07 PAR 5 FIG 3 SHEET 1 AND 2. THE ORIGINAL THICKNESS SDR DALA2017062905077Door Frame · crackedCRACKED DOOR JAMB WEB STA Y=207 LONG 15L AT PAX CABIN. CRACKED DOOR JAMB WAS REPAIRED PER SRM 53-10-15-2R-1.SDR DALA2017062905051Pan · crackedCRACKED LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA. LT UPPER RING PAN STA 926 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR1 FIG 201.SDR DALA2017062905050Pan · crackedCRACKED LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 928 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905049Pan · crackedCRACKED LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 890 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905048Pan · crackedCRACKED LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA. LT UPPER RING PANS STA 869 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REPAIR 1 FIG 201.SDR DALA2017062905047Pan · crackedCRACKED LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA. LT LWR/UPPER RING PANS STA 831 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062905046Pan · crackedCRACKED LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA. LT LWR RING PAN STA 637 AT PASSENGER CABIN AREA WAS REPAIRED PER SRM 56-20-02 REP 1 FIG 201.SDR DALA2017062905044Skin · crackedCRACKED SKIN BTW BEAM NR 1-2 AT HOUSING AREA FWD CARGO COMPARTMENT DOOR (C1). SKIN WAS REPAIRED PER SRM 52-30-01-2R-1, FIG 201.SDR DALA2017062905043Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE UPPER LWR SURFACE BTW X=-54 TO X=-60 AND STAY=552 TO STAY=553 AT CAB PAX RT SIDE. DAMAGE WAS REMOVED PER SRM 53-00-55-2R REPAIR 4. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS WERE FOUND PER NDTSPM PART 6, 06-10-01.0SDR DALA2017062805023Pan · crackedCRACKED LT LOWER RING PAN BS 618. THE RING PAN WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, FIGURE 201.SDR DALA2017062805022Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 140 AND RBL 50. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.SDR DALA2017062805021Skin · crackedCRACK ON EXTERNAL SKIN, BS 1087 BETWEEN LONGERONS 13 AND 14R. THE SKIN WAS REPAIRED IAW ETI -17-17-074, REV ORIGINAL AND ER/A 558173-14, REV ORIGINAL,SDR DALA2017062805020Beam · crackedCRACKED NR 1 BEAM FWD EDGE AT FWD PASSENGER DOORWAY. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 202.SDR DALA2017062805019Skin · damagedPROTUBERANCE ON LOWER SKIN FOR THE RT WING AFT FLAP MOVEABLE VANE. THE SKIN WAS REPAIRED IAW SRM 57-53-01.SDR DALA2017062705000Skin · damagedVERTICAL STAB LE, ZFS 52 SEAM HAS MANY LOOSE FASTENERS AND MANY AREAS OF FASTENER & LARGE AREA WASHER WEAR. COMPLIED WITH PRI 559680-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559680-14, REV ORIG.SDR DALA2017062705018Floor Panel · brokenBROKEN FLOOR PANEL 211ANF. THE FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R, REP 3 AND REPLACED.SDR DALA2017062704999Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN BS 160 TO 200, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2017062704997Beam · crackedCRACKED NR 1 BEAM, AFT EDGE AT FWD PASSENGER DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 201.SDR DALA2017062704996Beam · crackedCRACK ON FWD LOWER CORNER RETAINER AT THE FWD RT SERVICE DOOR. THE NR 4 BEAM WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2017062604956Former · crackedCRACK ON FORMER BS 694, RBL 34. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R, 51-70-11, 51-41-02-0G, AND 51-41-05-0G.SDR DALA2017062604955Cusp Web · corrodedCORROSION ON RT CUSP WEB BS 549 TO 553 BETWEEN RBL 54 TO 60 IN THE PAX CABIN. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.SDR DALA2017070305157Sign · brokenFIRST CLASS EXIT SIGN BROKEN. REPAIRED THE SIGN. OPS CHECKED GOOD. OK FOR SERVICE.SDR DALA2017062605017Floor Support · corrodedCORROSION AND CRACKED FLOOR PANEL 221AG. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9957828, REV Y.
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