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 DHL2001801549Hinge · brokenL/H MAIN LANDING GEAR INBD DOOR CNTR HINGE BROKEN.REMOVED AND REPLACED L/H MLG I/B DOOR CTR HINGE PER SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21-29Oct 14, 2001 · N801DH · Doug DC873F · Landing Gear DoorsSDR DHL2001801558FittingFWD CARGO COMPT FITTING CRACKED AT L/H UPPER SECTION STA 300.000 L-27L.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TERATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Oct 13, 2001 · N801DH · Doug DC873F · Buffet/GalleysSDR UPS01837042Skin · crackedINSPECTION TYPE:N/A CRACKS RT WING INBOARD OF INBOARD FUELING CAP (MARKED LOWER WING) BETWEEN NR 3 & 4 PYLON LWR WING) 28 INCHES FROM L/E & 3 INCHES FROM ACCESS PNL 1206. HFEC VERIFIED CRACK-CRACK TERMINUS CENTER PUNCH MARKED EP QC 70100 10-13-01. COMPLIED WOct 13, 2001 · N803UP · Doug DC873F · Wing, Plate/SkinSDR DHL2001806017Smoke Detector · inoperativeNR 1 SMOKE DETECTOR NOT SECURE AND NR 5 SMOKE DETECTOR INOP. RESECURED SMOKE DETECTOR IAW 26-15-05, RELAMPED SMOKE DETECTOR IAW 26-15-5.Oct 13, 2001 · N806DH · Doug DC873F · Smoke DetectionSDR DHL2001801561Skin · crackedLEFT WING T/E PANEL UPPER SKIN SHOWS CRACKS (1.5 - 0.5 IN) NEAR REAR SPAR XRS 162.000. CUT OUT DAMAGED SKIN AND FABRICATED FILLER AND DOUBLER PER SRM 57-2-0 FIG 2A AND SRM 57-2-0 FIG 2A. INSTALLED FILLER AND DOUBLER PER SRM 51-1-21 FIG 33 AND DACO TR 51-96.Oct 12, 2001 · N801DH · Doug DC873F · Wing, Plate/SkinSDR UPS01837145Frame · corrodedINSPECTION TYPE:C23 STA 1240 FRAME IS CORRODED BEYOND LIMITS LONG 35R-36. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 836-901, BY INSTALLING A REPAIR STRAP IAW DH SK 836-901.Oct 12, 2001 · N836UP · Doug DC873F · Fuselage Main, FrameSDR DHL2001801568Fitting · crackedWING CNTR SECTION (MAIN CARGO COMT)FITTING CRACKED 1 IN AT STA 798.000,XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-120D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Oct 11, 2001 · N801DH · Doug DC873F · Aircraft StructuresSDR DHL2001801559FittingCENTER WING (MAIN CARGO COMPT)FITTING CRACKED 1 IN AT STA 759.000, XCW 23L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Oct 11, 2001 · N801DH · Doug DC873F · Wing, Center BoxSDR DHL2001801557FittingCENTER WING FITTING CRACKED AT STA 717.XCW 23 L/H.REMOVED CRACKED FITTING PER SRM 51-1-20D.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PERSRM 51-1-20D PG 9.Oct 11, 2001 · N801DH · Doug DC873F · Wing, Center BoxSDR DHL2001801554FittingC- BELLY DOOR LWR T BOLT # 6 SHOWS CRACKED FITTING.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 4.CLEANED TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20D PG 9.Oct 10, 2001 · N801DH · Doug DC873F · Cargo/Baggage DoorsSDR DHL2001801534Seat Track · wornMAIN CARGO SEAT NR 2 LT TRACK LUG WORN STA 320.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED NEW SPLICES AND TRACK PER SRM 53-2-3 PG 49-50.Oct 10, 2001 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001801532Skin · dentedLEFT WING I/B FLAP UPPER SKIN DENTED 1 INCH AT XW 115.000. REMOVED DAMAGED SKIN FROM LEFT I/B FLAP PER SRM 57-2-0 PG 1-2. FABRICATED NEW SKIN PER SRM 57-2-0 PG 1-2. INSTALLED NEW SKIN PER SRM 53-2-0 PG 1-2.Oct 10, 2001 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001801531Skin · dentedRIGHT I/B FLAP L/E UPPER SKIN SURFACE DENTED STA XW 115. REMOVED DAMAGED SKIN FROM RIGHT I/B FLAP PER SRM 57-2-0 PG 1. FABRICATED NEW SKIN PER SRM 57-7-1 PG 1. INSTALLED NEW SKIN PER SRM 57-2-0 PG 1-2.Oct 10, 2001 · N801DH · Doug DC873F · Trailing Edge FlapsSDR DHL2001801530Skin · dentedLT EXHAUST GATE SHOWS 2 DENTS 1 AND 2 IN ON UPPER SKIN. REMOVED DAMAGED SKIN FROM EXHAUST GATE PER SRM 57-2-0 PG 1-2. FABRICATED NEW SKIN PER SRM 57-71 PG 4. INSTALLED NEW SKIN PER SRM 57-2-0 PG 1-2.Oct 10, 2001 · N801DH · Doug DC873F · Wing, Plate/SkinSDR DHL2001801528Skin · crackedFWD PASSENGER DOOR INNER SKIN UPPER PART CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B.Oct 10, 2001 · N801DH · Doug DC873F · Passenger/Crew DoorsSDR DHL2001801527Skin · dentedVERTICAL STABILIZER LEFT OUTER SKIN DENTED 3 INCHES AT 2 R 159.961. REMOVED DAMAGED SKIN FROM VERTICAL STABILIZER AND FABRICATED NEW ONE PER SRM 55-2-0 PG 1-2 AND SRM 55-51 FIG 1. INSTALLED NEW SKIN PER SRM 55-2-0 PG 1-2.Oct 10, 2001 · N801DH · Doug DC873F · Vertical Stabilizer, Plate/SkinSDR UPS01837108Fitting · crackedINSPECTION TYPE:C23 RIGHT WING STRINGER 64 SPLICE FITTING IS CRACKED AT APPROX XRS 510. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3644046 AND SRM 51-1-20D.Oct 10, 2001 · N836UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS01837003Control Unit · failedINSPECTION TYPE:NA DEPLOYED REVERSERS IN FLIGHT (280 KIAS) TO MEET CROSSING RESTRICTION, NR 2 WOULD NOT STOW. RAN CHECKLISTS THROUGH INFLIGHT SHUTDOWN. SLOWING THROUGH 200 KIAS, REVERSER STOWED. THREE ENGINE LANDING. INFLIGHT WINDMILLING. REMOVED NR 2 ENGIOct 10, 2001 · N803UP · Doug DC873F · Hydraulic System, MainSDR DHL2001804020Window · lack of lube1) CAPT'S SLIDING WINDOW WILL NOT OPEN.2) ADJUSTED SLIDING WINDOWS IAW MM 56-10-2 CHECKED OPERATION OKSTATUS: CLOSEDOct 10, 2001 · N804DH · Doug DC873F · Flight Compartment WindowsSDR DHL2001801529Rib · crackedRT WING CNTR L/E INTERIOR RIB CRACKED .5 INCH (LWR) AT XFS 385.000. STOP DRILLED CRACK PER SRM 57-2-1 PAR 7. FABRICATED REINFORCING ANGLE PER SRM 57-2-1 PAR 7. INSTALLED REINFORCING ANGLE PER SRM 57-2-1 PAR 7.Oct 9, 2001 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001804019Window · malfunctioned1) CAPTAINS SLIDING WINDOW WILL NOT OPEN.2) LUBRICATED CAPTAIN'S SLIDING WINDOW I.A.W. MAINTENANCE MANUAL 56-20 OPS. CHECK O.K.STATUS: CLOSEDOct 9, 2001 · N804DH · Doug DC873F · Flight Compartment WindowsSDR UPS01837144Finger Doubler · corrodedINSPECTION TYPE:C23 STA 70-120 LONG 31R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21.Oct 6, 2001 · N836UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01837141Frame · crackedINSPECTION TYPE:C23 STA 55 RT SIDE FRAME IS CRACKED ABOVE FITTING AT CUSP. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.Oct 6, 2001 · N836UP · Doug DC873F · Fuselage Main, FrameSDR DHL2001801535Support · crackedFWD CARGO COMPT B-2 DOOR SUPPORT FRAME CRACKED 1.5 INCH BETWEEN STA 520.000 TO 560.000. REMOVED DAMAGED AREA PER SRM 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE PER SRM 53-2-0 FIG 1B. INSTALLED REINFORCING ANGLE PER SRM 53-2-0 FIG 1B.Oct 6, 2001 · N801DH · Doug DC873F · Fuselage Main, StructureSDR DHL2001801507Rib · crackedFWD CARGO LWR COMPT TRACK SUPPORT RIB CRACKED 1 INCH AT STA 90 L-34 R. STOP DRILLED CRACK PER SRM 53-2-0 FIG 1B. FABRICATED DOUBLER PER SRM 53-2-0 FIG 1B. INSTALLED DOUBLER PER SRM 53-2-0 FIG 1B.Oct 6, 2001 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01837109Angle · crackedINSPECTION TYPE:C23 LEFT HORIZONTAL STAB T/E UPPER ANGLE IS CRACKED AT XE 29. REPAIRED ANGLE IAW SRM 55-2-0 FIG 2.Oct 6, 2001 · N836UP · Doug DC873F · Horizontal Stabilizer StructureSDR UPS01837110Rib · crackedINSPECTION TYPE:C23 RIGHT HORIZONTAL STAB LOWER RIB IS CRACKED AT XFS 135. REPAIRED RIB IAW SRM 55-2-0 FIG 2.Oct 5, 2001 · N836UP · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS01837148Seat Track · corrodedINSPECTION TYPE:C23 SEAT TRACK STA 1020-1040 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A.Oct 5, 2001 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01837147Seat Track · corrodedINSPECTION TYPE:C23 SEAT TRACK STA 1400-1540 RBL 60 IS CORRODED BEYOND LIMITS. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 14.Oct 5, 2001 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01837146Frame · corrodedINSPECTION TYPE:C23 STA 12 FRAME AND WEB ARE CORRODED BEYOND LIMITS AT RBL 48. REPAIRED FRAME BY INSTALLING FILLER AND ANGLE DOUBLER IAW 8110-3 APPROVED DH SK 836-869, AND REPAIRED WEB IAW SR08530026.Oct 5, 2001 · N836UP · Doug DC873F · Fuselage Main, FrameSDR UPS01837143Seat Track · corrodedINSPECTION TYPE:C23 SEAT TRACK IS CORRODED BEYOND LIMITS STA 1130-1150 AT LBL 60. REPAIRED SEAT TRACK IAW SRM 53-2-3 FIG 8A, AND DC8-53B-003-501.Oct 5, 2001 · N836UP · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS01837135Fitting · crackedINSPECTION TYPE:C23 LEFT HORIZONTAL STAB LOWER FLANGE FITTING AT FRONT SPAR IS CRACKED AT XFS 47. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D.Oct 5, 2001 · N836UP · Doug DC873F · Horizontal Stabilizer StructureSDR DHL2001801540Intercostal · crackedBELLY DOOR-SUPPORT TRACK INTERCOSTAL CRACKED 2 INCHES. STOP DRILLED CRACK PER SRM 53-2-0 FIG 18. FABRICATED DOUBLER PER SRM 53-2-0 FIG 18. INSTALLED DOUBLER PER SRM 53-2-0 FIG 18.Oct 5, 2001 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001801538Seat Track · wornMAIN CARGO SEAT TRACK NR 2 LUG WORN STA 960.000. CUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED TRACK AND SPLICES PER SRM 53-2-3 PG 49-50.Oct 5, 2001 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001801519Rib · crackedRIGHT WING CENTER LEADING EDGE INTERIOR RIB CRACKED .5 INCH AT XFS 304. STOP DRILLED CRACK PER SRM 57-2-0 PG 1-2. FABRICATED REINFORCING ANGLE PER SRM 57-2-0 PG 1-2. INSTALLED ANGLE PER SRM 57-2-0 PG 1-2.Oct 5, 2001 · N801DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001801563Longeron · crackedAFT BULKHEAD LONGERON 17 R STA 1766.000 NEAR TO JOINT FITTING CRACKED 3 INCHES. REMOVED CRACKED LONGERON PER SRM 51-1-21 PG 1. INSTALLED NEW LONGERON PER SRM 51-1-21 PG 1.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS01837140Angle · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB ANGLE IS CRACKED AT XS 472.099. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5770170, AND SRM 51-1-20D, 51-1-21.Oct 4, 2001 · N836UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS01837134Rib · crackedINSPECTION TYPE:C23 LEFT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/BulkheadSDR DHL2001801537Fitting · crackedAFT BULK HEAD JOINT FITTING CRACKED 1 1/2 IN STA 1966.000 L17R.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20 PG 9.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage Structure (General)SDR DHL2001801533Seat Track · wornMAIN CARGO SEAT TRACK NR 2 LT TRACK LUG WORN AT STA 1600.000. CUT OUT DAMAGED AREA PER SRM 53-2-3 PG 49-50. FABRICATED SPLICES PER SRM 53-2-3 PG 49-50. INSTALLED NEW SPLICES AND TRACK PER SRM 53-2-3 PG 49-50.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL2001801508Angle · crackedFLT CABIN - ANGLE BROKEN AT STA 8.000, RBL-10. REMOVED BROKEN ANGLE PER SRM 53-2-0 FIG 1B. FABRICATED ANGLE PER SRM 53-2-0 FIG 1B. INSTALLED NEW ANGLE PER SRM 51-1-21 PG 7.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001801503Floor Support · crackedFWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .5 INCH AT STA 272.000, L33R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED ANGLE PER SRM 53020-0 PG 2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL2001801502Floor Support · crackedFWD CARGO COMPT-FLOOR SUPPORT ANGLE CRACKED .5 INCH AT STA 350.000 L-33R. STOP DRILLED CRACK PER SRM 53-2-0 PG 2E-2F. FABRICATED SUPPORT ANGLE PER SRM 53-2-0 PG2E-2F. INSTALLED ANGLE PER SRM 53-2-0 PG 2E-2F.Oct 4, 2001 · N801DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01837132Splice · crackedINSPECTION TYPE:C23 STA 440 - 460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.Oct 4, 2001 · N836UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01837120Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 404. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01837119Clip · crackedINSPECTION TYPE:C23 RIGHT WING L/E INTERCOSTAL ATTACH CLIP IS CRACKED AT XOLDI 6.225. REMOVED, FABRICATED, AND REPLACED CLIP IAW DWG 5769589, AND SRM 51-1-21.Oct 4, 2001 · N836UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS01837118Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E LOWER RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01837117Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 491.193. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01837116Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XS 497.491. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS01837115Rib · crackedINSPECTION TYPE:C23 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 366.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 4, 2001 · N836UP · Doug DC873F · Wing, Rib/Bulkhead
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