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 DHL2001806538Floor Support · crackedC-CHECK - FWD. CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 1/2 INCH AT STA 420.000, L33L-L-34L. REMOVED FASTENERS IAW SRM 51-1-21 FIG 1. FABRICATED DOUBLER WITH STEEL IAW SRM 53-2-3 FIG 10. TREATED AND PRIMED IAW SRM 51-1-8 PAGE 12-13. INSTALLED DOUBLMar 9, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835507Floor Support · corrodedINSPECTION TYPE: C2, MAIN CARGO FLOOR SUPPORT AT STA 1684 LT SIDE AFT OF PANEL F210 CORRODED AROUND HOLES REMOVED SUPPORT FABBED NEW SUPPORT .Mar 9, 2001 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835501Frame · corrodedINSPECTION TYPE: C2, FRAME AT FS -67 HAS CORROSION AT CUSP AREA. REMOVED ''Z'' ANGLES AND INTERCOSTAL TO GET ACCESS TO FRAME CUT OFF DAMAGED SECTION OF FRAME IAW REO-G07891 FABED -17 FRAME SECTION IAW DAC DW G 5613784 FABED -27 -25 SPLICES IAW REO G07891 HEATMar 9, 2001 · N808UP · Doug DC873F · Fuselage Main, FrameSDR DHL2001806527Floor Panel · crackedC-CHECK - FLIGHT COMPARTMENT 683 FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG. 10. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 FIG 10. STATUS-CLOSED.Mar 9, 2001 · N806DH · Doug DC873F · Fuselage Floor PanelSDR DHL2001806523Floor Support · crackedC-CHECK - FWD. CARGO COMPARTMENT - FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 380 L-31R. REMOVED CRACKED ANGLE AT STA 380 L-31R IAW SRM 51-1-8 PAGE 21. FABRICATED ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8, PAGE 12, 13. INSTALLMar 9, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806511Floor Support · crackedC-CHECK-AFT-CARGO BAY FLOOR SUPPORT ANGLE CRACKED 1/4AT STA.1380 L-31RT TO L-32RT. PERFORMED STOP HOLE, FABRICATED DOUBLER AND INSTALLED IAW.SRM.53-2-0 FIG.1B STATUS CLOSEDMar 9, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835411Floorbeam · damagedINSPECTION TYPE: C2, MAIN CABIN STA 880 PRESSURE DECK FLOORBEAM ON TRACK G RBL 65 IS OUT OF LI MITS AND HAS BARE METAL. REPAIRED AREA IAW TSRM STD-5310-001Mar 9, 2001 · N808UP · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2001806582Angle · crackedC-CHECK - AFT BULKHEAD LINING SUPPORT ANGLE LOWER PART AT STA 1766.000 CRACKED 1 INCH. REMOVED CRACKED LINING SUPPORTING ANGLE IAW SRM 53-2-5 PAGE 6A. FABRICATED NEW SUPPORTING ANGLE IAW SRM 53-2-5 PAGE 6A. TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED Mar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806530Floor Support · crackedC-CHECK - FLIGHT CABIN 1/2 INCH CRACK ON 680 FLOOR MIDDLE PART IN RT ANGLE AT STA - 12.000. REMOVED FASTNERS IAQ SRM 51-1-21 PAGE 1. REMOVED DETERIORATED ANGLE IAW SRM 53-2-3 FIG 10. FABRICATED NEW ANGLE IAW 53-7-3 FIG 10 CLEANED, TREATED AND PRIMED IAW Mar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806526Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE AT STA 100.000 NEAR L-33R SHOWS CRACK OF 3 INCH. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 51-1-8C. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806525Rib · crackedC-CHECK - TAIL CONE LOWER INTERNAL PART RIB CRACKED 2 INCHES AT STA 1910.000. REMOVED RIVETS IAW SRM 51-1-21 PAGE 1. PERFORMED STOP HOLE IAW SRM 53-3-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLERMar 8, 2001 · N806DH · Doug DC873F · Fuselage Main, StructureSDR DHL2001806518Support Bracket · crackedC-CHECK - FWD. CARGO. COMPARTMENT LINING SUPPORT ANGLE AT STA 220 L-33L SHOWS CRACK OF 1/2 INCH. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 2E/2F FIG 1B. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGE 1-2. INSTALLED DOUBLER IAW SRM 53-2Mar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806507Floor Support · crackedFWD CARGO COMPT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA. 120 L-33RH.PERFORMED STOP HOLE,FABRICATED REINFORCING ANGLE AND INSTALLED IAW.SRM 53-20-0 FIG.1B STATUS CLOSEDMar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806504Support · crackedFWD.CARGO BAY SIDE WALL SUPPORT ANGLE CRACKED 2 INCHES AT STA.180 L-32 RT. CORRECTIVE ACTION. PERFORMED STOP HOLE AND FABRICATED SUPPORT ANGLE (STEEL 301 1/2 H 0.032) IAW SRM 53-2-0 FIG 18 AND INSTALLED IAW SRM 53-2-0 FIG 10 STATUS CLOSED.Mar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806514Floor Support · crackedFWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 180. L-31LT. PERFORMED STOP-HOLE TO ANGLE CRACKED IAW SRM 53-2-0 PAGE 2E/2F FIG . R/R FASTENERS IAW SRM 51-1-21 PAGE 1. CONDITIONED AND INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 11. INSTALLED FMar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806501Angle · deterioratedFLIGHT CABIN 1/2 INCH CRACK ON 680 FLOOR MIDDLE PART IN LT ANGLE AT STA-12.000. REMOVED FASTNERS IAW SRM 51-1-21, REMOVED DETERIORATED ANGLE IAW SRM 53-2-3. FABRICATED NEW ANGLE IAW SRM 52-3-3. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW ANGMar 8, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806539Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 3 INCH STA 420, L-30LT TO L-31LT. FABRICATED REINFORCING ANGLE IAW SRM 53-2-3 FIG 10 AND INSTALLED REINFORCING ANGLE IAW SRM 51-1-21 PAGE21. STATUS-CLOSED.Mar 7, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806532Support Bracket · crackedC-CHECK - FWD. CARGO COMPT SIDE WALL SUPPORT ANGLE CRACKED 1 INCH AT STA 160 L-31RT. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. FABRICATED DOUBLER ANGLE IAW SRM 53-7-0 FIG 1B. TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER ANGLE IAW SRM 53-2-0 FIMar 7, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806508Fairing · crackedC-CHECK.- LT WING TO FUSELAGE FAIRING SUPPORT ANGLE CRACKED 3/4 INCH AT STA. 640 L-21LT. TO L-22 LT. REMOVED FAIRING SUPPORT ANGLE IAW SRM.51-1-21 PAGE 1 FABRICATED ANGLE IAW. SRM 53-2-0 FIG 1B CLEANED,TREATED & PRIMED IAW SRM 51-1-8B INSTALLED ANGLE IAW.SRM Mar 7, 2001 · N806DH · Doug DC873F · Aerodynamic FairingsSDR DHL2001806505Angle · brokenAFT CARGO-TUBING SUPPORT ANGLE BROKEN STA.1460 LT. REMOVED DAMAGED ANGLE (STA.1460 LT) IAW.SRM 51-1-21 PAGE1 FABRICATED NEW ANGLE IAW.SRM 53-2-0 PAGE 12 CLEANED,TREATED & PRIMED IAW-SRM 51-1-88 INSTALLED NEW ANGLE IAW-SRM51-1-21 PAGE1 STATUS CLOSEDMar 7, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806515Bolt · misinstalledNR 1 ENGINE FUEL LINE BOLTS AT RT SIDE OF PYLON SHOW SAFETY IMPROPER. SAFETIED PROPERLY NR 1 ENGINE FUEL LINE BOLTS (PYLON RT. SIDE) IAW CFMI MM 70-00-40, PAGE 201, PARA 4. STATUS-CLOSED.Mar 7, 2001 · N806DH · Doug DC873F · Aircraft Fuel Distribution SystemSDR DHL2001806541Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 2 INCHES AT STA 500, L-33L TO L-34L. PERFORMED STOP HOLE. FABRICATED DOUBLER AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSEDMar 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806540Floor Support · crackedC-CHECK - FWD CARGO COMPT. FLOOR SUPPORT ANGLE CRACKED 2 INCH AT STA 460, L-31LT TO L-32LT. PERFORMED STOP HOLE AND FABRICATED DOUBLER AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806537Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT PLATE CRACKED 1 INCH STA 420 - 440, L-33R TO L-34R. FABRICATED DOUBLER IAW SRM 53-2-3 PAGE 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 530203 PAGE 1, SRM 51-1-21 PAGE 1. STATUS-CLMar 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835500Bulkhead · crackedINSPECTION TYPE: C2, LT AFT PRESSURE BULKHEAD CRACKED STA 1766, 11LT REPAIRED AREA IAW DAC DWG SRO 8530007Mar 6, 2001 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR UPS01835499Bulkhead · crackedINSPECTION TYPE: C2, RT AFT PRESSURE BULKHEAD CRACKED AT STA 1766, 11RT REPAIRED AREA IAW DAC DWG SRO 8530007Mar 6, 2001 · N808UP · Doug DC873F · Fuselage Main, BulkheadSDR DHL2001806519Floor Panel · brokenC-CHECK - AFT CARGO COMPARTMENT - LOWER RT FLOOR PANEL BROKEN 2 INCH. REMOVED DAMAGED FLOOR PANEL IAW SRM 51-3-0. FABRICATED NEW FLOOR PANEL IAW SRM 53-2-3 FIG 10. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B PAGE 12-13. INSTALLED FLOOR PANEL IAW SRM 51-3-Mar 6, 2001 · N806DH · Doug DC873F · Fuselage Floor PanelSDR DHL2001806502Floor Support · crackedFWD CARGO COMPT - FLOOR SUPPORT ANGLE CRACKED 3 INCH AT STA 260, L-33 RT.PERFORMED STOP HOLE, FABRICATED DOUBLER (STEEL 301 1/4 H 0.040 INCH) AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 6, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835412Fitting · crackedINSPECTION TYPE:C2 LT MLG WW CRACKED IN VERT LEG OF TRAPEZOIDAL FITTING FS 902 LONG 24 LT. STOP DRILLED CRACK IAW UPS EO DC8-5340-0748 2B CRACK CONDITION REPAI R PREVIOUSLYCOMPLIED WITH IAW UPS EO DC8-5340-0748 NO FURTHER ACTION REQUIRED AT THIS TIMEMar 6, 2001 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835405Attach Angle · crackedINSPECTION TYPE:C2, KEELBEAM AREA BETWEEN MLG DOORS STA 830, LT ATTACH ANGLE CRACKED. FABED AND INSTALLED NEW ATTACH ANGLE IAW DAC DWG 4645535 AND DC8 SRM 51-1-20DMar 6, 2001 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835196Door · malfunctionedINSPECTION TYPE:N/A, RT MLG DOOR OPENING IN FLT. ACCOMPLISHED GEAR SWING AND UPLATCH CHECK PER M/M 32-31-04. ALL LIGHTS AND INDICATIONS NORMAL.Mar 6, 2001 · N874UP · Doug DC873F · Landing Gear Door Retract SectionSDR UPS01835197Hydraulic System · leakingINSPECTION TYPE:N/A, HYD QTY LOSS IN FLT.Mar 6, 2001 · N874UP · Doug DC873F · Hydraulic Power SystemSDR DHL2001806639Fitting · crackedC-CHECK, LT WING VERIFY POSSIBLE CRACK ON FITTING FROM O/B FLAP STA 406.000. PERFORMED HFEC INSPECTION IAW DC-8 NON-DESTRUCTIVE TESTING STANDARD PRACTICE MANUAL PART 6.Mar 5, 2001 · N806DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001806587Skin · crackedC-CHECK - FUSELAGE NOSE SECTION EXTERNAL SKIN CRACKED 1 INCH AT FS -40.0 L-32 RT. PERFORMED STOP HOLE. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B PAGE 77/78. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.Mar 5, 2001 · N806DH · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01835502Fitting · crackedINSPECTION TYPE: C2, AFT LWR CARGO PIT FS 1180 IN CEILING. FLOORBEAM END FITTING IS CRACKED. REMOVED INTERCOSTAL AND FLOORBOARD TO GAIN ACCESS TO FASTENERS & REMOVED CRACKED FITTING LOCATED NEW FITTING PN 3754922-501 DIAW DC8 SRM 51-1-21 & 51-3-0Mar 5, 2001 · N808UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835498Frame · corrodedINSPECTION TYPE: C2, AFT CARGO PIT AT FS 1140 ABOVE LONG 36 FRAME IS CORRODED. FABBED ALODINED & PRIMED & INSTALLED -7 REPAIR ANGLE, FILLER, -3 BACK- UP ANGLE & -5 FRAME CAP IAW REO G07893 DC8 SRM 51-1-8 51-1-20DMar 5, 2001 · N808UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835495Frame · corrodedINSPECTION TYPE: C2, AFT LWR CARGO PIT AT FS 1060 ABOVE LONG 33 RT - 36 FRAME IS CORRODED UND ER AND AROUND NUTPLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-2-0 REMOVED FRAME CAP GUSSET & CLIP FOUND GUSSET DAMAGED, OUT OF LIMITS IAW 53-2-0 REC'Mar 5, 2001 · N808UP · Doug DC873F · Fuselage Main, FrameSDR UPS01835308Fitting · crackedINSPECTION TYPE:C2, 3, STA 1140 RT FWD SIDE LONG 34R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Mar 5, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001806625Skin · dentedC-CHECK - RT OUTBD AILERON UPPER SKIN SURFACE DENTED BETWEEN STA XRS 640-660. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. REMOVED DAMAGED SKIN IAW DHL EO O10313, EO 2411, EO 2001078. CLEANED, TREATED, AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW SKIN (ALCMar 4, 2001 · N806DH · Doug DC873F · AileronsSDR DHL2001806610Skin · deformedC-CHECK - ENTRY DOOR FWD UPPER CORNER DEFORMED FS 60.000. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. CUT OUT DEFORMED SKIN IAW EO DHL 010325, ED 2388, EO 2001047. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER AND DOUBLER (ALCLAD 7075Mar 4, 2001 · N806DH · Doug DC873F · Passenger/Crew DoorsSDR DHL2001806500Support Bracket · crackedC-CHECK - FWD CARGO COMPT SIDE WALL SUPPORT ANGLE CRACKED 1/2 INCH AT STATION 180 L-31 RT. CORRECTIVE ACTION: PERFORMED STOP HOLE, FABRICATED REINFORCING ANGLE (STEEL 301, 1/2 H, 0.032 INCH) AND INSTALLED IAW SRM 53-2-0, FIG. 1B. STATUS - CLOSEDMar 4, 2001 · N806DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835319Splice · crackedINSPECTION TYPE:C2, 3, STA 1040 - 1060 LONG 35R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750545 AND SRM 51-1-20D.Mar 2, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835309Skin · corrodedINSPECTION TYPE:C2, 3, LT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 178. REPAIRED SKIN IAW SRM 55-2-1 FIG 4.Mar 2, 2001 · N811UP · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR UPS01835114Microphone · inoperativeINSPECTION TYPE:N/A PREFLIGHT- FE O2 MIC INOP. *S/D* FOUND WIRE AT CONNECTOR R50-299 BROKEN. REPAIRED, OPS CHECK OK.Mar 1, 2001 · N814UP · Doug DC873F · Communications SystemSDR UPS01835332Seat Track · corrodedINSPECTION TYPE, C2, 3, STA 585 - 595 LBL 60 SEAT TRACK IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01835312Fitting · corrodedINSPECTION TYPE:C2, 3 STA 1220 BANANA FITTING IS CORRODED BEYOND LIMITS AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 3755847, AND SRM 51-1-20D.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835311Intercostal · corrodedINSPECTION TYPE:C2, 3, STA 1240 - 1260 LONG 33R INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 9754949, AND SRM 51-1-20D.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835310Fitting · crackedINSPECTION TYPE:C2, 3, STA 1240 LONG 35L INTERCOSTAL FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758495, AND SRM 51-1-20D.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835307Fitting · crackedINSPECTION TYPE:C2, 3, STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841, AND SRM 53-2-0 FIG 2G.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01835306Longeron · corrodedINSPECTION TYPE:C2, 3, STA 1308 LONG 33L IS CORRODED BEYOND LIMITS ON OUTBOARD UPPER FLANGE. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 811-942.Feb 28, 2001 · N811UP · Doug DC873F · Fuselage Main, Longeron/Stringer
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