Boeing 757-2Q8
Service difficulty reports · 2,798
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 = '7572Q8' 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 = '7572Q8' 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 DALA2015120907514Deck Plate · corrodedCORROSION ON MAIN CABIN DECK PLATE AT BS 1680, BL-0 TO LBL-54 AND BETWEEN BS 1700-1710, LBL-51. REMOVED CORROSION ON DECK PLATE BS 1681, BL0 TO LBL 54 AND STA 1700-1710 AT LBL 51 IAW SRM 51-10-02, PARA 15 AND 53-60- 51 ALLOW. DAMAGE 2, PARA 2, STEP C. BLENDESDR DALA2015120907477Hinge · damagedUPON REMOVAL OF CORROSION ON NR 100-124, FOUND ELONGATED, DAMAGED FASTENER HOLE, FWD-RT POSITION AT BS 1120, CENTER MLG DOOR HINGE ATTACH FITTING. R & R DAMAGED CENTER MLG DOOR HINGE ATTACH SUPPORT FITTING AT BS 1120 IAW SRM 51-40-02 PARA 9, PG 10 & DWGS 144NSDR DALA2015120807513Frame · corrodedLOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24, CORROSION AROUND NUTPLATES. REMOVED CORROSION ON LOWER WTB FAIRING FRAME T-CAP BS 1040, RBL 9-24 IAW SRM 53-00-71. ALLOW-DAMAGE 1, FIG 101 DETAIL IX FOUND TO BE OUT OF LIMITS IAW SRM 53-00-71. ALLOW-DAMAGE, 1SDR IXXA20151230119Skin · dentedAFT OF REAR L4 DOOR DENTS, SCRAPES & DAMAGE IN SKIN. BLENDED SCRAPE AT STRINGER 15L, FS 1715, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. TWO EACH DENTS AT FS 1708, STRINGER 15L - 17L. REPAIRED IAW SRM 53-00-01 REPAIR 3 FIG 201.SDR DALA2015120407482Frame · damagedFWD CARGO RT FRAME DENTED AND GOUGED ON UPPER FLANGE AT BS 700 BETWEEN STR 23R-25R. TRIMMED OUT 3 DAMMAGED SECTIONS AND PERMANTLY REPAIRED IAW SRM.SDR DALA2015120407473Frame · dentedFWD CARGO BS 660, STR 23L-25L, FRAME DENTED SEVERAL PLACES. REJECTED DUE TO INCOMPLETE WORK, NO OPEN HOLE OR NEW STR CLIPS DOCUMENTED REF SRM 53-00-07, REPAIR 5, DETAIL III. COMPLIED WITH SRM 53-00-07, REPAIR 5, DETAIL III, HFEC OPEN HOLE INSPECTION PERFORMEDSDR DALA2015120307371Frame · dentedAFT CARGO BS 1520 BETWEEN STR 25L-26L TOP OF FRAME HAS DENT, GOUGE. FRAME AT BS 1520 BETWEEN STR 25L AND 26L HAS 2 EACH DENTS ON TOP OF FRAME, LOWER DENT MEASURES .63"W X .95"L, UPPER DENT MEASURES .85" W X .95" L, BOTH DENTS ARE OUT OF LIMITS REF SRM 53-00-0SDR DALA2015120307370Strap · misrepairedCABIN FLOOR STRUCTURE BS 365-377, LBL 25, FLOOR BEAM STABILIZATION STRAP HAS IMPROPER PREVIOUS REPAIR INSTALLED AT BS 365 AND STRAP IS CRACKED ABOVE REPAIR AT BS 375.5. FLOORBEAM STABILIZATION STRAP AT BS 365-377, LBL 25 HAS IMPROPER PREVIOUS REPAIR INSTALLED SDR DALA2015120307369Frame · dentedAFT CARGO, BS 1540, STR 25L TOP OF FRAME HAS DENT. FRAME AT BS 1540, STR 25L HAS A DENTS ON TOP OF FRAME, LWR DENT MEASURES .95" W X 1.23" L , UPPER DENT MEASURES .76" W X 1.0" L BOTH DENTS ARE OUT OF LIMITS REF SRM 53-00-07, PG 101. ALLOWABLE DAMAGE 1, FIGSDR FOTR20151202002Skin · corrodedLEFT SIDE OF FUSELAGE HAS AREAS OF CORROSION BS 1620 TO BS 1655 JUST BELOW STRINGER 26L.SDR FOTR20151202001Skin · corrodedLEFT SIDE OF FUSELAGE SKIN HAS CORROSION BS 1520 TO BS 1590 JUST BELOW STR 26L.SDR FDEA201512013836Fire Warning · false activationMAIN CARGO FIRE WARNING ILLUMINATED AT APPROX 100 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF ACCOMPLISHED & QRH CONSULTED. CRASH & FIRE RESCUE RESPONDED, NEGATIVE INDICATION. BRIEFED CREW AT BLOCK IN, CARGO FIRE WARNING ALERT EXTINGUISHED AFTER EXITING RUNWAY.SDR DALA2015112907302Frame · dentedTWO DENTS ON FWD CARGO RT FRAME UPPER FLANGE AT BS 660 BETWEEN STRINGERS 22-25R. TRIMMED OUT DAMAGE IAW SRM. INSTALLED PERMANENT REPAIR IAW SRM.SDR FDEA201511273800Panel · corrodedMAIN CABIN AFT 9G SHEAR WEB AT STATION 422.5, RBL 15.5, AREA CORROSION. COMPLIED WITH EA F-5310-T0321795 PT1 FUSELAGE-MAINFRAME-MAIN CABIN SHEAR PANEL CORROSION REPAIR AT STA 422 BETWEEN BL0 AND RBL 24.SDR DALA2015120307372Support Angle · corrodedCORROSION ON FWD CARGO DOOR LOWER SECTION OF FRAME SUPPORT ANGLE, 2ND FROM FWD END. R & R SUPPORT ANGLE AT FWD CARGO DOOR LOWER SECTION OF FRAME IAW DWG 143N6603 AND SRM 51-40-02, ORIGINAL MATERIAL .094", MATERIAL LOSS IS 1" X 1"X.022" FOUND OUT OF LIMITS RESDR DALA2015112607298Floorbeam · corrodedCORROSION ON MAIN CABIN FLOORBEAM UPPER SURFACE AT BS 1640, RBL 46 - 58. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. AREA REPAIRED SRM.SDR DALA2015112507294Frame · dentedDENT ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1400, BETWEEN STR 23L, 25L AND 26L. DENTS ON FRAME AT BS 1400 BETWEEN STR 23L, 25L AND 26L FOUND OUT OF LIMITS REF SRM. PERFORMED FRAME REPAIR BS 1400, STR 23L, 25L AND 26L REF SRM.SDR DALA2015112507292Frame · dentedAFT CARGO BS 1500 BETWEEN STR 23-27L FRAME HAS DENTS. PERFORMED FRAME REPAIR AT BS 1500 STR 23L TO 27L REF SRM.SDR DALA2015112207187Seat Track · corrodedCORROSION ON MAIN CABIN FLOOR SEAT TRACK FLANGE/AROUND FASTENER HOLES AT BS 641, LBL 45.5. ACCOMPLISHED PERMANENT REPAIR ON SEAT TRACK FLANGE, AROUND FASTENER HOLES AT BS 640-780, LBL 45 REF ER/A 538367-14, REV ORIGINAL.SDR DALA2015112207185Skin · damagedAFTER REMOVAL OF ANTENNA MOUNT, FOUND SCRIBE MARKS AT ANTENNA MOUNT AREA, LWR EXT FUSELAGE SKIN BETW BS 1460 -1480, STR 29R-30. ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN ANTENNA MOUNT AREA BS 1459-1480 BETWEEN STR 29R-30, REF ER/A 541036-14, REVISION ORISDR DALA2015112007092Skin · corrodedFUSELAGE EXTERIOR SKIN STA 1464.5-1477.5, RBL 1.5-5, ANTENNA MOUNT LOCATION PITTED AND HAS TOOLING MARKS. BLENDED OUT CORROSION AND TOOLING MARKS ON FUSELAGE EXTERIOR SKIN AND ANTENNA MOUNT AT BS 1464.5-1477.5, RBL 1.5-5 IAW SRM 53-00-01, FIG 101 ORIGINAL MATSDR DALA2015112107153Frame · gougedFUSELAGE BS 1280 STR 11R-14R, FRAME GOUGED IN 2 PLACES. BLENDED 2 EA GOUGES ON FRAME BS 1280/STR 11R-14R IAW SRM 53-00-07, FIG 101, DETAIL II. MECHANICAL MEASUREMENTS OF BLENDED AREAS, AT FRAME BS 1280, STR 14R, NR 1: L=1.55" X W=0.4" X D=.023"; BELOW STR 11SDR DALA2015112007093Skin · dented3 EA PROTRUDING DENTS ON LOWER FUSELAGE SKIN AT APPROXIMATELY BS 666, 1 EA ABOVE S27R AND 2 EA BELOW S27R 3 EA PROTRUDING DENTS ON LOWER FUSELAGE SKIN AT BS 666, 1 EA ABOVE 27R AND 2 BELOW 27R HAVE BEEN REPAIRED BY COMPLYING WITH PRI 539825-14, REV 0 AND ER/A SDR DALA2015112007091Deck Plate · corrodedCORROSION ON MAIN CABIN DECK PLATE AT BS 1680 BL-0 TO RBL=54 AND AT BS 1691 RBL-51. REMOVED CORROSION ON MAIN CABIN DECK PLATE AT BS 1680, BL-0 TO RBL 54 AND BS 1691, RBL-51. REPAIR AREA REF PRI 541027-14, REV 0, ER/A 541027-14, REV A. ACCOMPLISHED PERMANENT SDR DALA2015111907078Frame · corrodedAFT CARGO UNDER FLOOR FRAME BS 1460 HAVE 3 AREAS OF CORROSION AT RT SIDE OF STR S-30 AND OTBD OF STR S-29R. REMOVED CORROSION AT RT SIDE OF STR S-30, OTBD OF STR S-29R AND ACCOMPLISHED A PERMANENT REPAIR REF ER/A 538392-14, REV ORIGINAL AT BS 1460 FRAME.SDR DALA2015121407591Shutoff Valve · corrodedAPU BLEED AIR SHUTOFF VALVE HAS SURFACE CORROSION VIEWED THRU ACCESS DOOR 313AL RLO14. R & R APU BLEED SHUTOFF VALVE IAW AMM 36-11 -10-401. LEAK AND OPS CHECK DUE. PERFORMED OPS AND LEAK CHECK OF APU BLEED SHUT OFF VALVE, OPS AND LEAK CHECK GOOD IN REF TO ASDR DALA2015111707011Frame · dented2 EA DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 600 BETWEEN STR 23L-25L. REPAIRED FWD CARGO LT FRAME UPPER FLANGE AT BS 600 BETWEEN STR 23L AND STR 25L IAW DWG 143N1009 AND SRM 53-00-07, FIG 201, PAGE 201. TRIMOUTS, 2 EA, MEASURE NR 1: 1.54" X 0.94" X 0SDR DALA2015111707010Frame · dentedDENT ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1420, BETWEEN STRINGER 25L AND 26L. REPAIRED FUSELAGE FRAME AT AFT CARGO COMPARTMENT BS 1420 BETWEEN STRINGERS 25L AND 26L IAW SRM 53-00-07, FIG 201, PAGE 201. ORIGINAL MATERIAL 7075-T6 .063", REPAIR AREA ISSDR DALA2015111406982Crease Beam · corrodedCORROSION ON MAIN CABIN RT CREASE BEAM INNER CHORD, BS 1236 TO BS 1290. CORROSION ON MAIN CABIN RT CREASE BEAM INNER CHORD, BS 1236 TO BS 1290 FOUND OUT OF LIMITS IAW SRM 53-60-13. R & R CREASE BEAM ON MAIN CABIN RT BS 1180 TO BS 1290 IAW SRM 51-40-02 AND DWSDR DALA2015111206925Seat Track · corrodedCORROSION ON SEAT TRACK, BS 1276 - 1320, RBL 45.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, PAGE 102, FIG 101. R & R THE SEAT TRACK IAW SRM 53-00-52, REPAIR 3, FIGURE 201.SDR DALA2015111106895Skin · dentedLOWER FUSELAGE- 1EA DENT BETWEEN RIVETS FOR FRAME ON SKIN AT BS 1320 AND 1" ABOVE S-27R. DENT MEASURED 1.0" X 0.9" X 0.012" DEEP, A/Y=75. ACCOMPLISHED PERMANENT REPAIR ON DENT FUSELAGE SKIN FOR FRAME AT BS 1320 & 1" ABOVE S-27R IAW ER/A 539852-14, REV ORIGISDR DALA2015111006892Frame · dentedFWD CARGO BS 660 STR 23-25R, FRAME DENTED 2 PLACES. TRIMMED-OUT 2 EA DENTS ON FRAME AT BS 660, STR 23R-25R, REF SRM 53-00-07, REPAIR 5. TRIMOUT NR 1 MEASURES 1.040" X 2.105" X 0.5" R, TRIMOUT NR 2 MEASURES 1.090" X 1.040" X 0.5"R. ACCOMPLISHED PERMANENT RESDR DALA2015110806834Skin · corrodedCORROSION ON LOWER FUSELAGE SKIN, BS 535 BETWEEN STRINGER 28L AND 28R, ON ANTENNA MOUNTING AREA. REMOVED CORROSION ON LOWER FUSELAGE SKIN BS 535 BETWEEN STR 28L & 28R ON ANTENNA MOUNTING AREA, BLENDOUT MEASURE 6" X 2.5" X .050" MIN REM MATERIAL ACCOMPLISHED PSDR DALA2015110506881Frame · dentedDENT ON FWD CARGO LT FRAME UPPER FLANGE AT BS 740 ABOVE STR 23L. PERFORMED REPAIR TO FRAME AT BS 740 AND STR 23L. REF SRM 53-00-07, FIG 201, REPAIR 5. TRIMOUT OF DENT MEASURE 1.64" X 0.94" X 0.5"R. REPAIR IS PERMANENT CAT "B" WITH THRESHOLD INSPECTION TO SSDR DALA2015110406746Support · corrodedFWD CARGO BS 900 BULKHEAD VERTICAL SUPPORT AT RBL-7.5 HAS CORROSION AT BOTTOM. UPON EVALUATION, FOUND BULKHEAD VERTICAL SUPPORT BS 900, RBL 7.5 TO HAVE AN EXFOLIATION CORROSION MEASURING 3" X 1" X .060" MATERIAL LOSS, ORIGINAL MATERIAL TO BE 0.220". FOUND DASDR DALA2015110306686Frame · dentedTHREE DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 680 BETWEEN STR 23L-25L. FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED FRAME IAW SRM.SDR DALA2015110306685Frame · dentedDENT ON FWD CARGO FRAME UPPER FLANGE AT BS 680 BETWEEN STR 24-25R. REMOVED DAMAGE FABRICATED REPAIR AND INSTALLED IAW SRM.SDR DALA2015110206681Support · gougedL4 DOOR POWER ASSIST BOTTLE CABLE SUPPORT ASSY IS GOUGED. REMOVED AND INSTALLED NEW DOOR POWER ASSIST BOTTLE CABLE SUPPORT ASSY AT L-4 DOOR IAW AMM.SDR DALA2015103106679Frame · corrodedCORROSION ON FWD CARGO DOOR AFT LOWER FRAME. REPAIRED IAW ERA 538381-14, REV ORIGINAL.SDR DALA2015103106678Frame · corrodedCORROSION ON AFT CARGO DOOR AFT LOWER FRAME. ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO DOOR AFT LOWER FRAME IAW ER/A 538385-14, REV ORIGINAL.SDR DALA2015103106677Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK, BS 1280 TO 1320, LBL 24.7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AREA OF SEAT TRACK AND REPAIRED IAW SRM.SDR DALA2015103106676Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK, BS 1350 TO 1320, LBL 24.7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED AREA OF SEAT TRACK AND SPLICED REPAIR IAW SRM.SDR DALA2015103106675Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK, BS 1280 - 1320, LBL 45.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SEAT TRACK AND INSTALLED SPLICE IAW SRM.SDR DALA2015103106674Intercostal · corrodedFWD CARGO BS 720-740 LBL 7.5, INTERCOSTAL LOWER FLANGE AT BELLY SKIN CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R INTERCOSTAL IAW DWG.SDR DALA2015103106673Seat Track · corrodedCORROSION ON MAIN CABIN SEAT TRACK, BS 1327 TO 1320, LBL 45.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED DAMAGED SEAT TRACK AND REPLACED SEAT TRACK AND INSTALLED SPLICE CHANNEL IAW SRM.SDR DALA2015111507006Seat Track · corrodedSEAT TRACK BS 365-400 RBL 25, CORROSION IN SEVERAL SPOTS. FOUND CORROSION DAMAGE ON SEAT TRACK SUPPORT BS 365-400, RBL 25 TO BE OUT OF ALLOWABLE LIMITS. R & R SEAT TRACK SUPPORT. ORIGINAL MATERIAL THICKNESS IS .070 MAX MATERIAL LOSS IS 2" X 1" X .022". MAXSDR DALA2015112207155Floor Support · corrodedCABIN FLOOR STRUCTURE BS 704-714 AND 729-736/RBL 65, CUSP BEAM CORRODED. R & R INNER CUSP CHORD THAT WAS CORRODED BEYOND LIMITS IAW DWG 143N8328 AND SRM 51-40-02 (100 PERCENT MATERIAL LOSS X 2" X 1".SDR DALA2015102806579Girt Bar · obstructedRAM-1 1R DOOR HARD TO ARM. DURING DOOR INSPECTION WITH BUSTLE REMOVED, FOUND SLIDE SURVIVAL PACK GREEN ROPE CHORD ON FWD SIDE OF SLIDE HAD COME OUT FROM STOWED POSITION AND WRAPPED AROUND GIRT BAR MECHANISM AND GIRT BAR SLIDER CAUSING INTERFERENCE WITH GIRT BSDR DALA2015102406489Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED BS 365 - 418, RBL 45. REMOVED ALL CORROSION IAW SRM 53-00-52, FIG 101 AND FOUND AREAS OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02, PAGE 7, PAR 8 & DWG 141N5130, REV E.SDR DALA2015102406488Seat Track · corrodedMAIN CABIN, CORROSION ON SEAT TRACK SUPPORT BETWEEN BS 365 & 418, RBL 24. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02, PAGES 7, 21, DETAIL II & DWGS 141N5130, 141N5131, REV A.
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