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 DALA2017071405424Lens · missingMID CABIN EXIT SIGN LENS MISSING. REPLACED EXIT SIGN LENS. CHECKED GOOD.SDR DALA2017071405422Antenna · erodedL/E OF FWD TCAS ANTENNA ERODED. REPLACED THE TCAS ANTENNA IAW AMM 34-46-03.SDR DALA2017071405421Pan · crackedCRACKED FWD/LOWER CORNER OF RH WINDOW RING PAN BS 636. REPAIRED IAW SRM 56-20-02-2R-1.SDR DALA2017071405420Pan · crackedCRACKED FWD/UPPER CORNER OF RH WINDOW RING PAN BS 737. REPAIRED IAW SRM 56-20-02-2R-1.SDR DALA2017071405419Pan · crackedCRACKED AFT/UPPER CORNER OF THE LT WINDOW RING PAN ON BS 927, 870, 851, AND 832. REPAIRED IAW SRM 56-20-02-2R-1.SDR HALA2017071200183Engine · damagedLEFT ENGINE HAD SEVERE DAMAGE.SDR DALA2017071305389Lens · missingEMERGENCY LIGHT LENS MISSING. INSTALLED THE LIGHT LENS.SDR DALA2017071305388Cover · unsecureEMERGENCY EXIT LIGHT COVER UNSECURE AT ROW 1. INSTALLED THE LIGHT COVER.SDR DALA2017071205387Cargo Track · corrodedCORROSION ON THE RT CARGO TRACK BETWEEN BS 895 & 954, BS 994 & 1022 IN THE AFT CARGO BAY. THE SECTION OF CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-40-08.SDR DALA2017071205367Skin · corrodedCORROSION ON CTR FUEL TANK SKIN STA Y=742 BTW X=-20 TO X=-60 AT RT WHEELWELL SLANT PANEL AREA AMDS 5300-2003. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205366Skin · corrodedCORROSION ON CENTRAL FUEL TANK SKIN BELOW SLANT PANEL STA Y=742 BTW X=18 TO X=25 LT WHEEL WELL AMDS 0593-2002. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205365Skin · corrodedCORROSION ON CENTER FUEL TANK UPPER SKIN FROM Y=737 TO Y=756, X=22 TO X=60, ALSO Y=705-710, X=-56 TO X=-60 AT CABIN PAX WING BOX AREA AMDS 5300-2008. REPAIR WAS ACCOMPLISHED PER ETI 17-17-087 REV 04 AND ER/A 559506-14 REV ORIGINAL.SDR DALA2017071205364Spar · crackedDURING REMOVAL OF OUTBD FLIGHT SPOILER LOCKED TOOL ONE CRACK WAS MADE TO RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355. RT WING AFT SPAR MEMBRANE BTW STA XRS=350 AND XRS=355 WAS REPAIRED PER ETI -17-17-097 REV 2 AND ER/A 559526-14 REV ORIG.SDR DALA2017071205363Skin · crackedSKIN CRACK AT FASTENER AT STA 1095, 4" ABOVE L14R ABOVE RT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.SDR DALA2017071205362Fastener · looseFOUND NUMEROUS LOOSE FASTENERS ON VERTICAL STABILIZER REMOVABLE LEADING EDGE AT STA ZFS 52. REPAIRED REF PRI 560042-14 REV 0 AND ER/A 560042-14 REV A.SDR DALA2017071205361Skin · cracked2 SKIN CRACKS AT FASTENERS AT STA 1095, 4" ABOVE L14R ABOVE LT PYLON. REPAIRED SKIN REF PRI 560007-14 REV 0 AND 1 AND ER/A 560007-14 REV ORIGINAL.SDR DALA2017071205360Fastener · looseVERTICAL STAB LEADING EDGE LOWER FASTENERS ARE LOOSE AT STA ZFS 52. COMPLIED WITH PRI 560026-14 REV 0 AND REV 1. REPAIRED REF ER/A 560026-14 REV ORIG.SDR DALA2017071105332Cowling · crackedCRACK ON FIXED COWL APRON HINGE, LATCH ASSEMBLY AFT OF LOWER FAN COWL DOOR ENGINE LT. CRACK ON FIXED COWL WAS REPAIRED PER SRM 54-00-00 REP 1 HINGE, GUSSET, AND CLIP WERE REMOVED AND REINSTALLED PER SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2017071005295Angle · crackedCRACKED ANGLES ON UPPER BEAM FWD & AFT ENDS, AT THE AFT LT OVERWING EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735, REV G.SDR DALA2017071005294Bellcrank · wornWEAR ON BELLCRANK AT THE RT SLAT DRIVE MECHANISM. THE BELLCRANK WAS REPAIRED IAW ETI-17-17-075, REV 1, AND ER/A 559492-14, REV ORIG.SDR DALA2017071005293Fitting · corrodedCORROSION ON FWD STAIRWAY DOOR MECHANISM FITTING. THE DAMAGED FITTING WAS REPLACED IAW AMM 20-50-01-201.SDR DALA2017071005292Angle · crackedCRACKED ANGLE ON THE UPPER BEAM AFT END AT THE FWD RT OVERWING EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-05, 51-41-02, AND DWG 9957735, REV G.SDR DALA2017071005291Skin · corrodedCORROSION ON RT WING UPPER SKIN XRS 375. ONE INCH FROM FRONT SPAR. THE SKIN WAS REPAIRED IAW ETI-17-17-094, REV 1, AND ER/A 559516-14, REV ORIG.SDR DALA2017071005331Door Sill · corrodedCORROSION ALONG THRESHOLD SILL FROM STA 370 TO 427. REPAIRED PER SRM 53-20-15-2R PROCEDURE 6.SDR DALA2017070905290Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BELOW OF LONGERON 14L IN THE PAX CABIN. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-05, AND DWG 9912243, REV JS.SDR DALA2017070905289Cargo Track · corrodedCORROSION OUT OF LIMITS ON THE RT CARGO TRACK BETWEEN BS 892 & 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51-01-7, AND 51-41-01.SDR DALA2017070905288Access Panel · damagedELONGATE HOLES ON THE FUEL ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION II.SDR DALA2017070905287Cargo Track · corrodedCORROSION OUT OF LIMITS ON THE LT CARGO TRACK BETWEEN BS 813 - 1022 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51-01-7, AND 51-41-01.SDR DALA2017070905286Access Panel · damagedHOLES ELONGATED AT FUEL ACCESS PANEL 520GB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, PAR 5, REPAIR 2, CONDITION II.SDR DALA2017070905285Strap · crackedCRACKED STRAP ON FRONT OF DOOR FRAME WEB BS 200 LONGERON 18L. THE STRAP WAS REPLACED IAW SRM 51-41-08, AND SRM 51-41-05.SDR DALA2017070905284Frame Angle · crackedCRACKED FRAME ANGLE BS 1022, LONGERON 14L. FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9912243, REV JB.SDR DALA2017070805283Skin · crackedCRACK ON FUSELAGE SKIN BS 1076 BETWEEN LONGERONS 15 - 13L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2017070805282Skin · crackedCRACK ON FUSELAGE SKIN BS 1087 BETWEEN LONGERONS 13 - 15L. REPAIRED IAW ETI-17-17-082, REV 2, AND ER/A 559501-14, REV ORIG.SDR DALA2017070805281Longeron · crackedCRACKED LONGERON 2R, BS 1133 IN THE AFT ACCESSORIES BAU AREA. A REPAIR SPLICE WAS INSTALLED SRM 53-00-05-2R.SDR DALA2017070805280Intercostal · crackedCRACK ON INTERCOSTAL IN THE CEILING AREA BETWEEN BS 617 - 636, BL 0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R-1.SDR DALA2021122908130Skin · crackedTWO CRACKS WERE NOTED ON THE FUSELAGE SKIN, BETWEEN 1076 AND 1087, L-14L. ER/A 559501-14 SECTION I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION FOR SECTION II IS REQUIRED. ACCOMPLISH ER/A 559501-14 SECTION II INSPECTION AT C-CHECK INTERVALS FROM SECTION I, NOT TOSDR DALA2017070705279Frame · crackedCRACKED FRAME ANGLE BS 1022, LONGERON 14R. THE DAMAGE WAS REMOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-00-06-2R, AND DWG 9912243, REV JB.SDR DALA2017070705278Frame · corrodedCORROSION ON FRAME ANGLE BS 927 BETWEEN LONGERONS 29L AND 29R. REPAIRED IAW SRM 53-00-06-2R, FIG 201, AND 53-20-07-01.SDR DALA2017070705277Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 620MB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01-2R, PROCEDURE 2, REPAIR 2, FIGURE 201, SHEET 1.SDR DALA2017070705276Skin · corrodedCORROSION ON WING BOX UPPER SKIN BETWEEN BS 737 - 751 RBL 22 - 60. REPAIRED IAW ETI-17-17-079, REV 1 AND ER/A 559498-14, REV ORIGINAL.SDR DALA2017070705275Panel · out of limitsSEVERAL COUNTERSINK OUT OF LIMITS ON REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE AT VERTICAL STABILIZER (EHV) WAS REPAIRED IAW DRAWING SG95550001, REV ORIGINAL, AND JIC CARD 5530-01048-03.SDR DALA2017070605217Battery Pack · inoperativeLOWER LT & RT AFT OVERWING EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.SDR DALA2017070605216Floor Panel · crackedCRACK FLOOR PANEL 121NF. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-00-00-2R.SDR DALA2017070505188Battery Pack · inoperativeWHILE PERFORMING A SERVICE CHECK, FOUND FIRST CLASS OVERHEAD CEILING LIGHTS, EMERGENCY LIGHTS INOPERATIVE. INSTALLED A NEW BATTERY IAW AMM 33-51 OPS CHECKED OK. OK FOR SERVICE.SDR DALA2017070505187Skin · debondedDISBONDED AREAS AT DENTS 6, 7, AND 18 ON RT WING AFT MOVABLE FLAP VAN. REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND OPN 1031 CARD 2000-8149-02.SDR HALA2017070400179Unknown · odorPOTENTIAL BURNED ELECTRICAL WIRE ODOR AT ROWS 18 AND 19. INSPECTED SURROUNDING AREA ROWS 17-19 FOR POSSIBLE ELECTRICAL BURNING ODOR. NO ODOR NOTED.SDR DALA2017070505214Seat Track · corrodedCORROSION ON RT SEAT TRACK RBL 22 BTW BS 822 & 937. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R, REPAIR 5.SDR DALA2017070505186Frame · crackedCRACKED FRAME ANGLE, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2017070505185Frame · crackedCRACKED FRAME ANGLE BETWEEN LONGERONS 3R &3L, BS 1168. A NEW FRAME ANGLE WAS INSTALLED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2017070505181Pan · crackedCRACKED PAN LOWER AREA INTERNAL STRUCTURE BS 408 FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02-2R PROCEDURE 1, REPAIR 1, FIG 201.
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