Douglas DC-8-73F

Service difficulty reports · 15,471

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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 aircraft_model_key = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS99830231Fitting · corrodedINSPECTION TYPE:C1 FS 300 BETWEEN LONGERON 34R AND 35R, THE BATH TUB FITTING HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 1D.Jul 15, 1999 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830230Fitting · crackedINSPECTION TYPE:C1 FS 350 BETWEEN LONGERON 36 AND 35L, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0 FIG 2D.Jul 15, 1999 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830229Skin · crackedINSPECTION TYPE:C1 THE FUSELAGE SKIN AT FS 1660, AFT ENTRY DOOR, AFT UPPER CORNER, HAS 5 CRACKS EXTENDING FROM FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 18.Jul 14, 1999 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830228Shear Tie · crackedINSPECTION TYPE:C1 FS 220, BETWEEN LONGERON 11R AND 12R, THE SHEAR TIE IS CRACKED. CUT OUT DAMAGED LEG, AND REPAIRED THE SHEAR TIE IAW SRM 53-2-0 FIG 2B.Jul 14, 1999 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830212Longeron · corrodedINSPECTION TYPE:C123, LONGERON 23R AT FS 65 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A LONGERON IAW SRM 53-2-2 AND 51-1-20D.Jul 14, 1999 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA991425Support · damagedDURING A MAINTENANCE VISIT, REMOVED AND REPLACED FLAP LINK SUPPORT ASSY AT STA 219.498 LEFT AND RIGHT POSITIONS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED FLAP LINKS SUPPORT ASSYS IAW DC8 M/Jul 14, 1999 · N604AL · Doug DC873F · Trailing Edge Flap ActuatorSDR UPS99830287Skin · corrodedINSPECTION TYPE:C1, A/C COMPT SKIN AT FS 10 BETWEEN LONGERON 34R AND 33R, HAS A GAP THAT LETS PRESSURIZED AIR ESCAPE AND IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW IAW EO DC8-5330-8942-C.Jul 13, 1999 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830244Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN AT FS 418, LONGERON 21L, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK866-417.Jul 13, 1999 · N866UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830227Fitting · crackedINSPECTION TYPE:C1 EXTERNAL, CENTER SECTION KEEL BEAM FITTING AT FS 759 RT IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3758519 AND SRM 51-1-20D.Jul 13, 1999 · N866UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830226Skin · crackedINSPECTION TYPE:C1 RT WING L/E SKIN IS CRACKED AND CORRODED AT XW 485. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-0.Jul 13, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830225Doubler · crackedINSPECTION TYPE:C1 RT WING L/E SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5679300 AND SRM 51-1-21.Jul 13, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830224Skin · crackedINSPECTION TYPE:C1 RT WING L/E LOWER SKIN IS CRACKED AT THE DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jul 13, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830223Skin · crackedINSPECTION TYPE:C1 LT WING L/E SKIN AT THE FWD END OF THE NR 2 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0A FIG 1.Jul 13, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830222Skin · crackedINSPECTION TYPE:C1 LT WING L/E SKIN, ABOVE AT THE FWD END OF THE NR 1 PYLON CUT OUT IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A.Jul 13, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830149Web · crackedINSPECTION TYPE:C2, LT WING, I/B FLAP, I/B SIDE, CLOSE OUT WEB CRACKED SEVERAL PLACES. FABRICATED AND INSTALLED NEW WEB, DOUBLER AND STIFFENERS IAW REO 06611 AND DC8 SRM 51-1-21 & 51-1-14.Jul 13, 1999 · N809UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830148Skin · corrodedINSPECTION TYPE:C2, RT HORZ STAB O/B LEADING EDGE, I/B END, HAS CORROSION AROUND SCREW HOLES. FABBED AND INSTALLED REPAIR FILLED AND DOUBLER IAW DC8 SRM 51-1-21, 51-2 -0, & REO 06610.Jul 13, 1999 · N809UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS99830221Skin · crackedINSPECTION TYPE:C1 LT WING L/E UPPER SKIN IS CRACKED AT XFS 379. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Jul 12, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830220Skin · corrodedINSPECTION TYPE:C1 LT OTBD SLOT VANE HAS EXFOLIATION CORROSION AT THE INBD END. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 2H.Jul 12, 1999 · N866UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830219Skin · crackedINSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 635 US CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Jul 12, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830218Skin · crackedINSPECTION TYPE:C1 LT WING L/E UPPERSKIN AT XFS 710 IS CRACKED AT THE AFT INBD CORNER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.Jul 12, 1999 · N866UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830211Skin · crackedINSPECTION TYPE:C123, LT WING LWR SKIN AT APPROX XRS 438, AND STRINGER 68, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5730-9004.Jul 12, 1999 · N874UP · Doug DC873F · Wing, Plate/SkinSDR RRXA991735Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-1 BETWEEN Y=1000 TO Y=1300 AND X=15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVEJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991729Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=580 TO Y=880. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991728Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 BETWEEN Y=580 TO Y=880 AND X=-15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED Jul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991726Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=280 TO Y=580 AND X=50. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVEDJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991724Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=280 TO Y=580 AND X=-15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVEDJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991715Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-1 BETWEEN Y=1020 TO Y=1040. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991708Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-1 BETWEEN Y=900 TO Y=920. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGIJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991699Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E AT Y=329 AND X=-50. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERINJul 12, 1999 · N791FT · Doug DC873F · Fuselage Floor PanelSDR RRXA991687Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME AT Y=1320 AND LONGERON 27 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED FRAME, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR SUPPORT FRAME IAW Jul 12, 1999 · N791FT · Doug DC873F · Fuselage Main, FrameSDR RRXA991617Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, C PIT FLOORBEAM SUPPORT STRUT AT STA 1160, BL 48 RIGHT, BETWEEN WL 10 RIGHT AND WL 40 RIGHT AND LONGERON 28 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FJul 10, 1999 · N604AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830092Floor · corrodedINSPECTION TYPE:C-2 CORROSION ON MAIN CABIN FLOORBOARD SPLICES (3) STA 1040 X10 TO X17. FABRICATED AND INSTALLED NEW SPLICE IAW DC8 SRM 51-3-0. MAT ID 7075-T 6 .063 PO NR 289791 IAW DC8 SRM 53-7-3, DAC DWG 289791.Jul 9, 1999 · N809UP · Doug DC873F · Fuselage Floor PanelSDR UPS99830091Floor · corrodedINSPECTION TYPE:C3 FLOOR BOARD F88 TO F90 HAS LARGE DOUBLER BULBED BY CORROSION AND EX FOLIATION SHOWING ON UNDERSIDE OF PLANK FABBED AND INSTALLED NEW SECTION AND SPLICES IAW DC8 SRM 53-2-3 FIG 9 AND 51-3-0.Jul 9, 1999 · N809UP · Doug DC873F · Fuselage Floor PanelSDR UPS99830210Rib · crackedINSPECTION TYPE:C123, LT WING L/E RIB AT XFS 428.75 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jul 8, 1999 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830062Switch · looseGEAR UPLATCH CHECK FAILED. FOLLOWED CHECK LIST. CHECK STILL FAILED. BOTH DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHTS ILLUMINATED. BOTH ALTERNATE GEAR (MAIN) DOOR LIGHTS ALSO ILLUMINATED DURING UPLATCH CHECK. MAIN GEAR DOOR LIGHT SWITCH MOVED LEFT DOOR NJul 8, 1999 · N801UP · Doug DC873F · Landing Gear Position and WarningSDR UPS99830209Spar Chord · crackedINSPECTION TYPE:C123, RT WING FWD LWR SPAR CAP, LWR TAG IS CRACKED AT THE FASTENER HOLE AT XFS 17. CUT OUT DAMAGED AREA AND REPAIRED IAW SB 57-30 AND DWG SRO8570012.Jul 7, 1999 · N874UP · Doug DC873F · Wing SparSDR UPS99830208Fitting · corrodedINSPECTION TYPE:C123, FS 1540, AT LONGERON 33L, THE SEAT TRACK ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABERICATED, AND REPLACED FITTING IAW DH SK874-181 AND SRM 51-1-21 AND 51-3-0.Jul 7, 1999 · N874UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830160Skin · crackedINSPECTION TYPE:C2, LEFT WING O/B LEADING EDGE, OUTBOARD END TOP SIDE SKIN IS CRACKED STA 889. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-1 & 51-1-21.Jul 7, 1999 · N809UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830125Rib · crackedINSPECTION TYPE:C2, LEADING EDGE RUDDER RIB CRACKED. FABRICATED AND INSTALLED NEW RIB IAW DC8 SRM 51-1-24, 51-1-22 & 51-1- 21.Jul 7, 1999 · N809UP · Doug DC873F · Rudder, Spar/RibSDR UPS99830012Oxy Bottle · leakedAT TOP OF CLIMB, NOTICED BOTH O2 BOTTLES WERE AT 0. REPLACED O2 BOTTLES AND LEAK CHECKED PER M/M 35-10-00 AND 35-20-00. CHECKED FOR LEAKS AT ALL REGULATORS, NO LEAKS NOTED PER 35-10-00 AND 35-20-00.Jul 7, 1999 · N866UP · Doug DC873F · Crew Oxygen SystemSDR RRXA991173Fireloop · malfunctionedAPROX 1 HR 20 MINS INTO FLT, FIRE WARNING LT AND BELL WENT OFF. INDICATION OF LTS IN NR 3 FIRE HANDLE ON. ALL ENG INDICATIONS NORM. NR 3 ENG SHORT CIRCUIT LT CAME ON FIRED 1ST BOTTLE. FIRE INDICATION AND TEST GOOD. AFTER TALKING TO COMPANY, INDICATION ON Jul 7, 1999 · N795FT · Doug DC873F · Fire DetectionSDR UPS99830126Web · crackedINSPECTION TYPE:C2, RUDDER CTR DAMPER LOWER CLOSEOUT WEB WAS CRACKED. FABBED, INSTALLED AND HEAT TREATED NEW WEB IAW DAC DWG 5656229 AND DC 8 SRM 51-1-20D.Jul 6, 1999 · N809UP · Doug DC873F · Rudder StructureSDR UPS99830090Floorbeam · corrodedINSPECTION TYPE:C-2 FLOORBEAM CORRODED UNDERSIDE AT FS 680 BL 33L TO BL 36L. REPAIRED IAW REO-06602.Jul 6, 1999 · N809UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830207Skin · crackedINSPECTION TYPE:C123, RT INBD AILERON UPPER L/E SKIN IS CRACKED JUST OTBD OF THE POWER CYL ATTACH FITTING. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767A.Jul 5, 1999 · N874UP · Doug DC873F · AileronsSDR UPS99830206Rib · crackedINSPECTION TYPE:C123, LT WING L/E UPPER RIBS CRACKED AT XS 484.895 AND 448.58. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jul 5, 1999 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830205Rib · crackedINSPECTION TYPE:C123, LT WING L/E LWR RIBS ARE CRACKED AT XFS 822.5, 797.5, 791.25, 785.0, 778.75; UPPER RIBS ARE CRACKED AT XFS 727.5, 760.0, 766.25, 785.0, AND 828.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jul 5, 1999 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830204Clip · crackedINSPECTION TYPE:C123, RT WING L/E, ABOVE THE NR 3 PYLON, APPROX STA XFS 267, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.Jul 5, 1999 · N874UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830203Doubler · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.Jul 5, 1999 · N874UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830201Rib · crackedINSPECTION TYPE:C123, LT WING L/E HAS RIBS CRACKED AT XFS 672.5, 660.0, 641.25 AT THE UPPER RIB; AND LOWER RIB AT XFS 603.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.Jul 5, 1999 · N874UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830096Seat Track · gougedINSPECTION TYPE:C2 MAIN CABIN SEAT TRACK I IS GOUGED AT STA 300. BLENDED GOUGED AREA, FOUND TO EXCEED LIMITS IAW DC8 SRM 53-2-3. REPAIRED IAW DC8 SRM 53-2-3. INSTALLED PLUG AND CHANNEL IAW DC8 SRM 51-3-0 AND 53-2-3.Jul 5, 1999 · N809UP · Doug DC873F · Fuselage, Seat/Cargo Attach Fittings
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