Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  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 UPS99829233Bulkhead Angle · crackedINSPECTION TYPE-C, MAIN CABIN AT STA 176 AND L9R CORNER OF PRESS BULK ANGLE CRACKED. REMOVED EXISTING ANGLE -24 AND DYEPENED, INSPECTED AERA TO FIND END CRACK. STOP DRILLED CRACK, FOUND PREVIOUSLY REPAIRED, REINSTALLED ANGLE.Mar 23, 1999 · N805UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS99829231Fitting · corrodedINSPECTION TYPE-C1, AFT PIT LONG TIE FITTING AT STA 1510 LONG 29L HAS BLEND OUT OF LIMITS. REMOVED SPLICE FITTING, FABRICATED REPAIR STRAP IAW REO 06413, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED STRAP AND SPLICE IAW DC-8 SRM 51-1-20D.Mar 23, 1999 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829230Fitting · crackedINSPECTION TYPE-C, FWD PIT STA 340 AT L27R INTERNAL TORQUE BOX CRACKED FITTING. REMOVED ANGLE SWITCH AND STRIKER IAW DC-8 SRM 51-3-0, DRILLED FITTING IAW DC-8 SRM 51-1-20D, ALODINED AND PRIMED IAW DC08 SRM 51-1-8, INSTALLED IAW DC-8 SRM 51-1-20D.Mar 23, 1999 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829227Angle · corrodedINSPECTION TYPE-C, FWD PIT STA 347 INTERIOR OF C1 DOOR FWD TORQUE BOX FORMED ANGLE CORRODED AT L35L. REMOVED ANGLE IAW DC-8 SRM 51-1-24, OUT OF LIMITS IAW DCF-8 SRM 53-20, FABBED NEW ANGLE IAW DAC DWG 9754020, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLMar 23, 1999 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL99804002Linkage · brokenLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. UNABLE TO VERIFY NOSE WHEEL ALIGNED, LEFT GEAR DOWN AND RETURNED FOR LANDING. FOUND GROUND SHIFT MECHANISM BROKEN. REMOVED AND REPLACED LINKAGE PER MM 32-23-1. CYCLED HANDLE WITH NO DEFECTS NOTED.Mar 23, 1999 · N804DH · Doug DC873F · Landing Gear Retraction/Extension SystemSDR UPS99829249Fitting · crakcedINSPECTION TYPE-C/CK, INTERCOSTAL END FITTING STA 857, LONGERON 18L IS CRACKED. REMOVED CRACKED END FITTING IAW DC8 SRM 51-1-20D. MATERIAL ID FOR NEW FITTING 7075-T651 IAW DAC DWG 4750423 PO 265699, FABRICATED NEW END FITTING IAW DAC DWG 4750423. ALODINED AMar 22, 1999 · N805UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829248Longeron · corrodedINSPECTION TYPE-C/CK, LONGERON 25 RIGHT HAS REPAIR AT FS 1560-1590 CORRODED BULGED. REMOVED PREVIOUS REPAIR ANGLE IAW DC8 SRM 51-1-21, CORROSION WAS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED DAMGED SECTION OF LONGERON AND SPLCIED IN NEW SECTION IMar 22, 1999 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99829247Longeron · corrodedINSPECTION TYPE-C/CK, LONGERON 33 RIGHT CORRODED AT STA 1650-1660. REMOVED EXISTING LONG SECTION, REPLACED WITH NEW SECTION (P/N 575777 8-1).Mar 22, 1999 · N805UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL9980745CTr Cowl · crackedAT C CHECK, NR3 ENG I/B T/R FAN COWL FWD MATING FLANGE HAS CRACK AT 12 O'CLOCK. CUT OUT DAMAGED AREA. FABRICATED REAPIR ANGLE 3.5 BY 3.5 FT AND FILLER 3 BY 1.5 PER EO18R78310191. N/R 1160.Mar 22, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980719CSupport · crackedAT C-CHECK, RT MLG STA 950 AND XCW 46 FITTING SUPPORT CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-21.Mar 22, 1999 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980718CFrame · crackedAT C-CHECK FOUND RT WING FLAP WELL AT STA 90.00 UPPER FRAME FOR L/E FLAP CONTOUR CRACKED. FABRICATED NEW COVER PANEL RT WING O/B FLAP L/E STA 90.00 IAW DC-8 SRM 51-1-7.Mar 22, 1999 · N807DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL9980715CAngle · crackedAT C-CHECK, LT HORIZONTAL STABILIZEER L/E INTERIOR AREA AT STA FS 60 VERTICAL ANGLE IS CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PER SRM 51-1-8, 2 X 6.Mar 22, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer StructureSDR DHL9980714CSkin · crackedAT C-CHECK, LT HORIZ STAB L/E I/B SECTION I/B INTERIOR LOWER AREA AT APPROX STA FS 53.75 HAS CRACK DAMAGE ON SURFACE AT FASTENER HOLE POINT. STOP DRILLED CRACK, FABRICATED ANGLE REPAIR 6 X 1 X 1 AND 5 X 1 X 1 PER SRM 51-1-8.Mar 22, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9980710CSkin · crackedAT C-CHECK, RT WING T/E PANEL LOWER WS 90 DELAMINATED WITH CRACK DAMAGE. CLEANED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-9, 4 X 4 .Mar 22, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR UPS99829229Frame · corrodedINSPECTION TYPE-C, CORROSION ON FRAME UNDERSIDE AT STA 1705 BETWEEN L20 AND L21 RT SIDE. REMOVED CORRODED IAW DC-8 SRM 51-1-8 OUT OF LIMITS, REO REC, FABBED DOUBLER ALODINED AND PRIMED IAW DC-8 SRM 51-1-8, INSTALLED IAW REO 06 410.Mar 21, 1999 · N805UP · Doug DC873F · Fuselage Main, FrameSDR UPS99829226Beam · crackedINSPECTION TYPE-C1, RT AFT SERVICE DOOR INTERNAL AFT BOTTOM CORNER NR 6 HORIZ BEAM CRACKED. STOP DRILLED CRACKS, FABBED DOUBLER IAW3 DC-8 SRM 52-2-0 FIG 2, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED WITH HI-LOKS AND RIVETS IAW DC-8 SRM 51-1-20D AND 5Mar 21, 1999 · N805UP · Doug DC873F · Service DoorsSDR DHL9980746CAngle · missingAT C CHECK, COCKPIT FLOOR PANEL 674A HAS MISSING FWD ANGLE. FABRICATED NEW ANGLE 1 BY 1.5 BY 10 PER SRM 51-121, N/R 1036.Mar 21, 1999 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980722CCover · crackedAT C-CHECK, RT HORIZONTAL STAB REAR SPAR AT STA XE 219.9 COVER IS CRACKED. REMOVED COVER, FABRICATED NEW COVER AND INSTALLED PER SRM 51-3-0.Mar 21, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer StructureSDR UPS99829225Skin · damagedINSPECTION TYPE-C1, LT WING LEADING EDGE O/B SLOT, O/B END HAS FASTENERS PULLING THRU SKIN. REPAIRED PER TIMCO REO NR 06403.Mar 20, 1999 · N805UP · Doug DC873F · Wing, Plate/SkinSDR DHL9980725CTr Cowl · crackedAT C-CHECK, NR 4 ENGINE LT T/R HALF CORE COWL FWD INTERIOR AREA AT 10 O'CLOCK FOUND CRACK DAMAGE ON SKIN. CUT OUT DAMAGED SECTION OF SKIN, FABRICATED REPAIR AND INSTALLED PER SRM 51-1-21A, 3 X 3.Mar 19, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980724CTr Cowl · crackedAT C-CHECK, NR 4 ENGINE LT T/R HALF CORE COWL INTERIOR AREA AT 8 O'CLOCK FOUND CRACK ON SURFACE SKIN. CUT OUT DAMAGED SECTION, FABRICATED REPAIR PER CFM MM AND INSTALLED PER SRM 51-1-21A, 5 X 5.Mar 19, 1999 · N807DH · Doug DC873F · Engine Thrust ReverserSDR DHL9980762CSkin · corrodedAT C CHECK, AFT LOWER CARGO COMPT FS 1350 AND LONG 31L/32L AREA WITH BULGING CORROSION. CUT OUT DAMAGED SECTION OF SKIN PER EO 18R5331086. N/R 955Mar 17, 1999 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9980747CAngle · crackedAT C CHECK, AFT PASSANGER DOOR FWD LOWER CORNER HAS 1.75 CRACK INDICATION UNDER DOUBLER. REMOVED DOUBLER AND FOUND THREE ANGLES CRACKED. FABRICTED DOUBLER ANGLE ANGLE SUPPORT AND SPLICE PER EO DN6 NR 18R5321092 .Mar 17, 1999 · N807DH · Doug DC873F · Passenger/Crew DoorsSDR DHL9980743CFitting · crackedAT C CHECK, CENTER WING TANK, THROUGH LOWER ACCESS PANEL 516A RT SIDE BAY ON STA 46 STR 67 UPPER AREA CRACK ON FITTING APPROX 1 LONG. REMOVED AND FABRICATED FITTING PER DER DRAWING MHA 3123 AND INSTALLED PER SRM 51-120D. N/R 1234Mar 17, 1999 · N807DH · Doug DC873F · Wing Miscellaneous StructureSDR UPS99829130Doubler · corrodedINSPECTION TYPE:C123 STA 1756 AT BLO, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REPAIRED AREA IAW DH SK 808-946.Mar 16, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829143Floorbeam · misdrilledINSPECTION TYPE-C3, FS 1660 FLOORBEAM AT RBL 45 HAS DOUBLE DRILLED HOLES. REPAIRED FLOORBEAM IAW DH SK808-353.Mar 15, 1999 · N808UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS99829110Seat Track · corrodedINSPECTION TYPE:C3 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS, FS 320-340, RBL 24. CUT OUT DAMAGED SECTION, FABRICATED, REPLACED SEAT TRACK FS 290 TO 390, RBL 24, IAW SRM 53-2-3.Mar 15, 1999 · N808UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL9980750CFloor · crackedAT C CHECK, GALLEY FLOOR PANEL HAS SURFACE CORROSION ON UPPER AND LOWER SIDES. ALSO, 2 CHANNEL FRAME ARE CRACKED STA 5- 25. CORROSION REMOVED ON PANEL AND WITHIN LIMITS AND REMOVED CHANNEL AND REPLACED PER SRM 51-1-21, 34.25 BY 4 N/R 647.Mar 15, 1999 · N807DH · Doug DC873F · Fuselage Floor PanelSDR DHL9980749CAngle · crackedAT C CHECK, FWD PASSANGER UPPER DOOR HINGE POCKET HAS GOUGE ON METAL. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE 5 BY 6 AND INSTALLED. N/R 872Mar 15, 1999 · N807DH · Doug DC873F · Passenger/Crew DoorsSDR DHL9980748CHinge · crackedAT C CHECK, LT WING AILERON HINGE NR 6 HAS CRACK ON AILERON MOUNT FLANGE. REMOVED HINGE AND INSTALLED NEW HINGE PER MM 27-10-1. N/R 896Mar 15, 1999 · N807DH · Doug DC873F · AileronsSDR DHL9980731CSkin · crackedAT C-CHECK, RT WING T/E LOWER I/B PANEL HAS CRACK DAMAGE ON SURFACE AT WS 90. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-91.Mar 15, 1999 · N807DH · Doug DC873F · Wing, Plate/SkinSDR DHL9980712CSkin · crackedAT C-CHECK, LT HORIZONTAL STAB L/E I/B SECTION O/B INTERIOR LOWER AREA AT APPROX FS 166 HAS CRACK DAMAGE. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 55-2-0, 1 X 1 X 7 AND 10 X 1 X 6.Mar 15, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9980711CFloor · crackedAT C-CHECK, FLOOR PANEL GALLEY CENTER CHANNEL FRAME IS CRACKED. REMOVED DAMAGED PANEL, FABRICATED NEW AND INSTALLED PER SRM 51-1-21, 25 X 4.Mar 15, 1999 · N807DH · Doug DC873F · Fuselage Floor PanelSDR UPS99829140Doubler · crackedINSPECTION TYPE-C3, FS 1110 AT LONG 21R, THE FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED & REPLACED THE FINGER DOUBLER IAW DWG 5750321 AND SRM 51-1-21.Mar 14, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980753CSkin · corrodedAT C CHECK, AFT FUSELAGE LOWER EXTERIOR AREA AT STA 1761 ACCESS PANEL N-60 INTERIOR AREA AND LINKAGE HAS LIGHT SURFACE CORROSION. REMOVED CORROSION, AREA OUT OF LIMITS. CUT OUT DAMAGED AREA, AND FABRICATED DOUBLER AND INSTALLED PER EO 18R5311087. N/R 730Mar 14, 1999 · N807DH · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL9980752CDoor · misrepairedAT C CHECK, FWD ENTRY DOOR FWD TOP CORNER PREVIOUS REPAIR FS 25 LONG 10L. REMOVED PREVIOUS REPAIR AND FABRICATED AND INSTALLED DOUBLER PER SRM 53-2-0. N/R 742.Mar 14, 1999 · N807DH · Doug DC873F · Passenger/Crew DoorsSDR DHL9980751CDoor · misrepairedAT C CHECK, UPPER FUS FWD SERVICE DOOR AT FWD TOP CORNER PREVIOUS REPAIR. REMOVED REPAIR AND INSTALLED DOUBLER PER SRM 53-2-0 N/R 741.Mar 14, 1999 · N807DH · Doug DC873F · Service DoorsSDR DHL9980709CAngle · crackedAT C-CHECK, FWD LOWER CARGO COMPT AFT DOOR AFT FRAME ANGLE FLANGE IS CRACKED SEVERAL PLACES. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-3-0, 29 X 3.Mar 14, 1999 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL9980708CPanel · crackedAT C-CHECK, LT I/B AILERON I/B LOWER SURFACE ON ACCESS PANEL HAS CRACKED PLATE. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-21, 5 X 4.Mar 14, 1999 · N807DH · Doug DC873F · AileronsSDR DHL9980707CPanel · crackedAT C-CHECK, VERTICAL STAB T/E AREA STA 195 REAR SPAR METAL COVER CRACKED. STOP DRILLED END OF CRACK, FABRICATED DOUBLER REPAIR 3 X 3 AND INSTALLED PER SRM 51-1-21.Mar 14, 1999 · N807DH · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL9980706CPanel · crackedAT C-CHECK, VERTICAL STABILIZER T/E AT STA 225 REAR SPAR COVER PANEL CRACKED. REMOVED PANEL, STOP DRILLED AND INSTALLED FIBREGLASS REPAIR PER SRM 51-3-0.Mar 14, 1999 · N807DH · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR DHL9980756CLongeron · corrodedAT C CHECK, LOWER FUS EXT FS 190 TO 200 LONG AND 35R BULGING CORROSION. REMOVED LONGERON, FABRICATED NEW SECTION 12 BY 1 FT AND INSTALLED PER SRM 51-120A. N/R 640Mar 13, 1999 · N807DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL9980705CPanel · crackedAT C-CHECK, LT HORIZ STAB REAR SPAR STA XE 270.9 CRACKED ON COVER PANEL. REMOVED AND FABRICATED NEW COVER AND INSTALLED PER SRM 52-3-0.Mar 13, 1999 · N807DH · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR DHL9980702CAngle · crackedAT C-CHECK, LOWER FUS BS 680 AND LONG 32L SUPPORT ANGLE CRACKED. REMOVED AND REPAIRED DAMAGED ANGLE PER SRM 51-1-21.Mar 13, 1999 · N807DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829144Fitting · crackedINSPECTION TYPE-C3, FS 1177 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829142Fitting · crackedINSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829141Fitting · crackedINSPECTION TYPE-C3, FS 1196 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829139Fitting · crackedINSPECTION TYPE-C3, FS 1203 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829138Fitting · crackedINSPECTION TYPE-C3, FS 1210 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99829137Fitting · crackedINSPECTION TYPE-C3, FS 1187 AT LONG 21R, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Mar 12, 1999 · N808UP · Doug DC873F · Fuselage Miscellaneous Structure
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