Pratt & Whitney JT8D-17

Service difficulty reports · 1,680

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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 engine_model_key = 'JT8D17'
  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.

SDR DALA1024319868Floor Panel · gougedDURING H-CHECK, FOUND FLIGHT DECK FLOOR PANEL NR 14 WITH GOUGE AND 2 EA DENTS. REPLACED FLOOR PANEL IAW SRM 51-10-4 AND DWG 9957827.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1024329868Floor Panel · chafedDURING M-CHECK FOUND MAIN CABIN FLOOR PANEL NR18 HAT CHANNELS WITH WORN AREA FROM CHAFING ON FASTENERS. REPLACED FLOOR PANELS IAW ERA 485767-14 & DWG 9923433.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1024339868Floor Panel · damagedDURING M-CHECK FOUND FLOOR PANEL NR70 WITH L/E FASTENER HOLES DOUBLE DRILLED. REPLACED FLOOR PANEL SKIN IAW ERA 900-5-1 AND DWG 9957927.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1024349868Floor Panel · corrodedDURING M-CHECK FOUND CORROSION ON MAIN CABIN FLOOR PANEL NR 59 TOP AND BOTTOM SURFACE AROUND FASTENER HOLES. REPAIRED IAW SRM 53-23-0, SRM 51-10-4, SRM 51-10-3, SRM 51-30-2, ERA 485773-14 AND DWG 9957919.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1024239868Vane · gougedDURING M-CHECK FOUND GOUGE IN LT WING INBD FIXED VANE L/E. REPAIRED IAW SRM 51-70-2, SRM 05-10-02 PAGE 226.Sep 24, 2010 · N777NC · Doug DC951 · Trailing Edge FlapsSDR DALA1024249868Pressure Panel · damagedDURING M-CHECK, FOUND NOSE WHEEL WELL PRESSURE PANEL BS 40 LT OTBD END 2 EA FASTENER HOLES WITH SHORT EDGE MARGIN. REPAIRED IAW SRM 51-30-02, SRM 51-30-05 & DWG 560953001.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Main, BulkheadSDR DALA1024259868Floor Panel · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR PANEL NR 50 TOP AND BOTTOM SURFACE AROUND FASTENER HOLES. REPAIRED IAW SRM 51-10-2, SRM 51-10-4, SRM 51-10-3 & ERA 485766-14.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1024269868Skin · misrepairedDURING M-CHECK, FOUND DOUBLE DRILLED HOLES IN DOUBLER AT BS 681 BETWEEN LONGERON 27 AND LONGERON 28. REPAIRED IAW SRM 54-01 FIG 2, SRM 53-33-0 FIG 3, SRM 51-10-3, SRM 51-30-2 AND SPM 06-10-01.001.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1024279868Skin · misrepairedDURING M-CHECK FOUND DOUBLE DRILLED HOLES IN DOUBLER AT BS 692 BETWEEN LONGERON 27 AND LONGERON 28. REPAIRED IAW SRM 54-01 FIG 2, SRM 53-33-0 FIGURE 3, SRM 51-10-3, SRM 51-30-2 AND SPM 06-10-01.001.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1024289868Floorbeam · crackedDURING M-CHECK, FOUND CRACK IN E & E COMPARTMENT FLOORBEAM LT ATTACH ANGLE AT BS 180 BL 0. REPAIRED IAW SRM 51-30-2, DWG 9923484 REV 4E ITEM 21, SRM 51-30-5.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1024299868Frame · damagedDURING M-CHECK, AFTER REMOVAL OF CANTED FRAME FOUND MISDRILLED HOLES IN WEB AT BS 1245. REPAIRED IAW SRM 51-30-2, SRM 51-30-5 AND DWG 9911858.Sep 24, 2010 · N777NC · Doug DC951 · Fuselage Main, FrameSDR DALA1023679868Bolt · crackedDURING M-CHECK FOUND CRACK IN RT WING WEB OTBD OF RT BOTTLE BOLT. REPAIRED IAW SRM 57-21-00, SRM 51-30-2, SRM 51-30-5 PAGE 226.Sep 23, 2010 · N777NC · Doug DC951 · Wing Main, Frame StructureSDR DALA1023689868Floor Panel · mismanufacturedDURING M-CHECK FOUND MAIN CABIN FLOOR PANEL NR 74 HAS 11 DOUBLE DRILLED HOLES. REPAIRED IAW SRM 51-70-4 FIG 1, SRM 51-10-4, SRM 51-10-3 & SRM 51-70-7 FIG 1.Sep 23, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1023699868Floor Panel · crackedDURING M-CHECK FOUND CRACKS IN RIBS OF MAIN CABIN FLOOR PANEL NR 60B. REPAIRED IAW SRM 53-22-01-801.Sep 23, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1023719886Vane · chafedDURING M-CHECK FOUND RT WING INBD FIXED VANE CHAFED ON INBD AND OTBD ENDS. REPAIRED IAW SRM 57-50-9 &1-70-02.Sep 23, 2010 · N600TR · Doug DC951 · Trailing Edge FlapsSDR DALA1023729886Seat Track · corrodedDURING M-CHECK FOUND CORROSION ON SEAT TRACK AT BS 200-304 LBL 22. REPAIRED IAW SRM 51-30-1 & SRM 51-30-5.Sep 23, 2010 · N600TR · Doug DC951 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1023739886Floor Panel · corrodedDURING M-CHECK FOUND CORROSION ON TOP AND BOTTOM OF MAIN CABIN FLOOR PANEL NR101 AT BS 1136. REPAIRED IAW SRM 51-70-4 FIGURE 1.Sep 23, 2010 · N600TR · Doug DC951 · Fuselage Floor PanelSDR DALA1023749886Channel · crackedDURING M-CHECK FOUND CRACKS IN HAT CHANNELS IN MAIN CABIN FLOOR PANEL NR18. REPAIRED IAW SRM 53-22-01-801-663A & SRM 51-90-0.Sep 23, 2010 · N600TR · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1023759886Floor Panel · damagedDURING M-CHECK FOUND DAMAGE TO PREVIOUS REPAIR ON MAIN CABIN FLOOR PANEL NR 102A. REPAIRED IAW SRM 51-30-2 & SRM 53-01.Sep 23, 2010 · N600TR · Doug DC951 · Fuselage Floor PanelSDR DALA1023769886Attach Bracket · crackedDURING M-CHECK FOUND CRACK IN INSIDE ACCESS HOLE RIB ATTACH BRACKET OTBD OF NR 4 HINGE ON RT WING FLAP. REPAIRED IAW SRM 51-10-4, SRM 51-10-2, SRM 51-30-1, 51-30-2 & 51-20-0.Sep 23, 2010 · N600TR · Doug DC951 · Wing, Control Surface Attach FittingsSDR FDEA201009233660Nose Cowl · damagedDAMAGE BOTTOM NR 3 NOSE COWL. REMOVED AND REPLACED NR 3 ENGINE NOSE COWL IAW MM 71-10-021-4. REFERENCE NON-ROUTINE N00917 WORK ORDER 00049152.Sep 23, 2010 · N204FE · Boeing 7272S2F · Nacelle/Pylon, Main FrameSDR DALA1023639868Floor Panel · damagedDURING M-CHECK, FOUND AFT END OF MAIN CABIN FLOOR PANEL NR73 DAMAGED. R & R FLOOR PANEL PN 9957921-18.Sep 22, 2010 · N777NC · Doug DC951 · Fuselage Floor PanelSDR DALA1023509859Battery Pack · inoperativeDURING MX CHECK FOUND EMERGENCY EXIT LIGHT AT ROW 25 CEILING INOP, REPLACED BATTERIES AND TESTS OK.Sep 20, 2010 · N768NC · Doug DC951 · Emergency LightingSDR FDEA201009203664Seat Track · damagedMAIN CABIN SEAT TRACK AT BS 680-700, LBL 62.5 HAS DAMAGED SCALLOPS. CUT OUT DAMAGED AREA BS 656 TO 728 LBL 62.5, FABRICATED NEW SECTION, SPLICE REPAIR, ANGLES, AND FILLERS IAW SRM 53-10-5 FIG 1. INSTALLED REPAIR IAW SRM 53-10-5 FIG 1.Sep 20, 2010 · N204FE · Boeing 7272S2F · Fuselage, Seat/Cargo Attach FittingsSDR DALA1023179869Frame Splice · crackedDURING L-CHECK, FOUND CRACK IN AFT ACCESSORY COMPARTMENT RT CANTED FRAME SPLICE AT BS 1243, STRINGER 10. REPAIRED IAW SRM 53-13-4 FIG 3, SRM 51-30-5, SRM 51-30-4 PAGE 9, SRM 51-10-2 & SRM 51-10-3 PAGE 125.Sep 17, 2010 · N778NC · Doug DC951 · Fuselage Main, FrameSDR DALA1023029869Pan · crackedDURING L-CHECK FOUND CRACK IN FWD CARGO DOOR COMPARTMENT DOOR PAN AT AFT END. REPAIRED IAW SRM 53-05 FIGURE 44, SRM 51-30-5, SRM 51-30-42 & SRM 51-30-02.Sep 16, 2010 · N778NC · Doug DC951 · Cargo/Baggage DoorsSDR DALA1023039886Keelbeam · crackedDURING H-CHECK, FOUND CRACK IN LT KEEL AREA ON OTBD END OF FRAME AT BS 753. REPAIRED IAW SRM 53-13-3 FIG 2, SRM 51-30-5 & SRM 51-20-0 PAGE 117.Sep 16, 2010 · N600TR · Doug DC951 · Fuselage Main, KeelSDR DALA1023049886Keelbeam · crackedDURING H-CHECK, FOUND CRACK IN LT KEEL AREA BS 734 OTBD END OF FRAME. REPAIRED IAW SRP DCP-A-51-72-01-801-663A, SRM 51-30-2 & SRM 51-30-5.Sep 16, 2010 · N600TR · Doug DC951 · Fuselage Main, KeelSDR DALA1023059886Floor Panel · corrodedDURING H-CHECK FOUND CORROSION AND CRACK IN FLOOR PANEL NR 20. REPLACED IAW SRM 51-10-4, SRM 51-30-2, PAGE 244.Sep 16, 2010 · N600TR · Doug DC951 · Fuselage Floor PanelSDR DALA1023069868Floor Panel · crackedDURING M-CHECK FOUND CRACK IN CABIN FLOOR PANEL NR 20. REPAIRED IAW SRM 51-10-4.Sep 16, 2010 · N777NC · Airbus A330223 · Fuselage Floor PanelSDR DALA1023079868Floor Support · crackedDURING M-CHECK FOUND 2 EA CRACKS IN END OF HAT CHANNELS ON MAIN CABIN FLOOR PANEL NR29. REPAIRED IAW SRM 51-90-0 PAGE 243.Sep 16, 2010 · N777NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1023089868Floor Support · crackedDURING M-CHECK FOUND CRACK IN END OF HAT CHANNELS ON MAIN CABIN FLOOR PANEL NR 54. REPAIRED IAW SRM 53-22-01-801-663A.Sep 16, 2010 · N777NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1023099868Floor Support · crackedDURING M-CHECK FOUND 2EA CRACKS ON END OF HAT CHANNELS ON MAIN CABIN FLOOR PANEL 60C.Sep 16, 2010 · N777NC · Doug DC951 · Fuselage Miscellaneous StructureSDR FDEA201009163511Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 950E BETWEEN STRINGERS 29R AND 28R. FABRICATED NEW STUB FRAME FROM 7075 0 .040" DIM 22" X 5" IAW SRM 51-10-3 AND 51-20-1 FIG 7 REV 103. REMOVED SHEAR TIE AT BS 950E BETWEEN STR 29R AND 28R IAW SRM 51-30-2 AND REINSTALLED SHEAR Sep 16, 2010 · N204FE · Boeing 7272S2F · Fuselage Internal Mounting StructureSDR DALA1022879868Longeron · crackedDURING M-CHECK, FOUND CRACK IN AFT CARGO COMPARTMENT LONGERON AT BS 1088 L29L. REPAIRED IAW SRM 51-01/53-3 FIG 18, PAGE 241.Sep 15, 2010 · N777NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR DALA1022889868Intercostal · damagedDURING M-CHECK, FOUND INTERCOSTAL WITH ELONGATED FASTENER HOLES AT BS 237-BS 256, BL 0. REPAIRED IAW SRM 51-30-2, SRM 51-10-4, 51-30-5.Sep 15, 2010 · N777NC · Doug DC951 · Fuselage Miscellaneous StructureSDR DALA1022909869Frame Splice · crackedDURING M-CHECK, FOUND CRACK IN AFT ACCESSORY COMPARTMENT LT SIDE FRAME SPLICE AT BS 1243 STRINGER 9. REPAIRED IAW SRM 51-10-2, SRM 51-10-4, SRM 51-30-5.Sep 15, 2010 · N778NC · Doug DC951 · Fuselage Main, FrameSDR DALA1022919869Frame · crackedDURING M-CHECK, FOUND CRACK IN AFT ACCESSORY COMPARTMENT RT SIDE FRAME FASTENER HOLE AT BS 1275, STRINGER 9. REPAIRED IAW SRM 51-30-05.Sep 15, 2010 · N778NC · Doug DC951 · Fuselage Main, FrameSDR DALA1022929883Skin · crackedDURING LINE CHECK, FOUND CRACK IN SKIN 1 INCH AFT OF CANTED FRAME, BS 1292 BETWEEN L14L & L15L. REPAIRED IAW SRM 53-01-01, PAGE 12.Sep 15, 2010 · N671MC · Doug DC951 · Fuselage Main, Plate/SkinSDR DALA1022939874Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN AT THE AFT BULKHEAD EMERGENCY EXIT DOOR WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.Sep 15, 2010 · N783NC · Doug DC951 · Emergency LightingSDR DALA1022949874Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN AT THE MAIN CABIN DOOR WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.Sep 15, 2010 · N783NC · Doug DC951 · Emergency LightingSDR DALA1023109873Line · unsecureMX FOUND THAT THE EMERGENCY EXIT HATCH OVER THE LT WING WOULD NOT OPEN. INVESTIGATION DIVULGED THAT A SNAP FOR THE ESCAPE LINE WAS NOT ENGAGED. FOLLOWING PROPER INSTALLATION OF THE SNAP THE EXIT FUNCTIONED.Sep 15, 2010 · N782NC · Doug DC951 · Emergency ExitsSDR FDEA201009153526Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 400 BETWEEN LBL 45 AND 25 UPPER I BEAM TOP AND BOTTOM SURFACE IS CORRODED. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 3. FABRICATED REPAIR PARTS. INSTALLED REPAIR IAW SRM 53-10-8 FIG 3 AND 51-10-2.Sep 15, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR DALA1022749868Strut · crackedDURING M-CHECK FOUND CRACK IN FWD CARGO LT SIDE STRUT AT BS 256. REPAIRED IAW SRM 51-70-5.Sep 14, 2010 · N777NC · Doug DC951 · Fuselage Main, StructureSDR DALA1022759868Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 1151 BETWEEN LBL 10-20. REPAIRED IAW SRM 51-70-5.Sep 14, 2010 · N777NC · Doug DC951 · Fuselage Main, Floor BeamSDR DALA1022769886Floor Support · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 218 TO BS 313 BL0. REPAIRED IAW SRM 51-30-5, SRM 51-10-4 & SRM 51-30-2.Sep 14, 2010 · N600TR · Doug DC951 · Fuselage Miscellaneous StructureSDR FDEA201009143414Frame Splice · damagedUPON FRAME REMOVAL, FOUND DOUBLE DRILLED HOLES IN FRAME SPLICE, STA 950B, STR 24L. REMOVED PRODUCTION SPLICE/DOUBLER IAW SRM 51-30-2 FORMED NEW DOUBLER IAW SRM 51-20-1 FIG 7 INSTALLED NEW DOUBLER IAW SRM 51-30-2 REV 103.Sep 14, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, FrameSDR DALA1022539869Stringer · crackedDURING L-CHECK, FOUND CRACK IN AFT ACCESSORY COMPARTMENT STRINGER 7R AT BS 1217. REPAIRED IAW SRM 51-30-2, SRM 51-30-05, SRM 51-10-4, SRM 51-10-2 & SRM 51-10-3.Sep 13, 2010 · N778NC · Doug DC951 · Fuselage Main, Longeron/StringerSDR FDEA201009133422Floorbeam · corrodedCORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 344 FROM LBL 10 TO RBL 10. REMOVED DAMAGED AREA 8' SECTION IAW SRM 53-10-8 AND 51-30-2. FABRICATED REPAIR TEE SECTION, ANGLES, AND SHIMS IAW SRM 53-10-8 FIG 9 DETAIL 1. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 5Sep 13, 2010 · N204FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR DALA1022349868Floor Panel · damagedDURING M-CHECK FOUND DAMAGE TO MAIN CABIN FLOOR PANEL NR 28. REPLACED FLOOR PANEL IAW SRM 51-10-4.Sep 12, 2010 · N777NC · Doug DC951 · Fuselage Floor Panel
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