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 RRXA000262Transducer · inoperativeON LANDING ANTI-SKID FAILED. FOUND RFO TRANSDUCER TO BE INOP. REMOVED AND REPLACED RFO TRANSDUCER IAW DC-8 MM CH 32-43. PERFORMED SPIN UP ANTI-SKID, OPS CHECKS GOOD, NO DEFECTS NOTED.Apr 18, 2000 · N831AL · Doug DC873F · Brake Anti-Skid SectionSDR DHL200080499CAngle · corrodedMAIN CARGO AFT SIDE FLOOR LOWER PART SUPPORT ANGLE SHOWS CORROSION AT STA 1734 L-25R (LEVEL 1). REMOVED DAMAGED FLOOR SUPPORT ANGLE PER SRM 51-3-0. CLEANED, TREATED AND PRIMED EFFECTED AREA PER SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-3-0.Apr 17, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832442Fitting · corrodedINSPECTION TYPE:C2 2 EE FITTING (P/N 3755842-503) HEAVILY CORRODED AT STA 1200 L32L - L33L. REMOVED FITTING CORRODED, RECEIVED NEW FITTING AND FABRICATED REPAIR ANGLES, ALODINED, PRIMED AND INSTALLED NEW FITTING.Apr 17, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL200080403CAngle · crackedFWD BAGGAGE COMPARTMENT FRAME REINFORCING ANGLE CRACKED 3 INCHES AT STA 220 FROM L-33 TO L 34 RT. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 2. STOP DRILLED IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51Apr 17, 2000 · N804DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001948Boss · corrodedDURING A MAINTENANCE VISIT FOUND THE MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEEDED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-05Apr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Attach SectionSDR RRXA001813Strut · corrodedDURING A MAINTENANCE VISIT MLG STRUT ASSY RETRACT PIN BOSS AND RETRACT PIN NEED REWORK PER MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED, REWORKED AND INSTALLED RETRACT PIN IAW EWA MA-AIApr 15, 2000 · N961R · Doug DC873F · Main Landing Gear Strut/Axle/TruckSDR RRXA001947Outflow Valve · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RETANGULAR OUTFLOW VALVE (SUGAR SCOOP) IN THE AFT ACCESSORY COMPT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IApr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow ValveSDR RRXA001946Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN THE LWR PIT C ON WEB AT STA 1200 BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 53-Apr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001945Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLEDApr 14, 2000 · N961R · Doug DC873F · Cargo/Baggage DoorsSDR RRXA001812Outflow Valve · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT ACCESSORY COMPT RETANGULAR OUTFLOW VALVE BETWEEN STA 1670 TO 1690, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND BLENDED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVIApr 14, 2000 · N961R · Doug DC873F · Pressure Regulator/Outflow ValveSDR RRXA001811Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN LWR PIT C ON WEB AT STA 1200 AND BETWEEN L34R AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RETURNED TO SERVICE IAWApr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001810Web · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AREA BETWEEN STA 1120 TO 1160 AND BETWEEN L26L TO ''C'' PIT DOOR SILL L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. AREA IS ACCEPTABLE AND RETApr 14, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832505Frame · corrodedINSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1220 - 1230 CROSS SLIDE AFT TORQUE BOX UPPER WEB CORRODED FROM LONG 33L - 34-R UNDERSIDE OF WEB. REMOVE FITTING, DOOR GUIDE AND GUIDE SPLICE. REMOVE CORROSION, ALODINE & PRIME. INSTALL NEW FITTING AND REINSTALL DOApr 14, 2000 · N818UP · Doug DC873F · Fuselage Main, FrameSDR UPS00832324Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY LIGHT DISARM DOES NOT WORK. RELAMPED EMERGENCY LIGHT SOCKET.Apr 14, 2000 · N814UP · Doug DC873F · Emergency LightingSDR RRXA002135Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL IN THE UPPER CARGO COMPT. AT FS 798 TO 822 AND L5L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA002040Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "L" ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D.Apr 13, 2000 · N961R · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA002019Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE C PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001944Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D AND 53-2-0. (Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001914Spar Cap · damagedDURING A MAINTENANCE VISIT FOUND GOUGED HOLES AND ELONGATED UPPER SPAR CAP ON RT WING FRONT SPAR AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 EO NR 00-055 WApr 13, 2000 · N961R · Doug DC873F · Wing SparSDR RRXA001885Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE C'' PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED ANApr 13, 2000 · N961R · Doug DC873F · Fuselage Main, FrameSDR RRXA001809Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L ANGLE AT STA 1120 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-20D AND 53-2-0.Apr 13, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001778Spar Cap · damagedDURING A MAINTENANCE VISIT, FOUND GOUGED AND ELONGATED HOLES IN THE RT WING UPPER SPAR CAP AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES & RE-COUNTER SUNK AND INSTALLApr 13, 2000 · N961R · Doug DC873F · Wing SparSDR UPS00832453Attach Angle · crackedINSPECTION TYPE:C2, AFT LOWER CARGO PIT CROSS SLIDE. DOOR RT FWD LWR ANGLE CRACKED. FABRICATE REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-8.Apr 13, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001921Skin · crackedDURING A MAINTENANCE VISIT FOUND DENTED AND CRACKED THE LEFT O/B STUB WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW EO NR 00-055 WITH APPROVED 8110-3 DATED 3-Apr 12, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001902Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, RIVETS PULLING THROUGH AND RIVET HEADS SHEARING OFF ON THE RT FLAP SCISSORS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANELApr 12, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR RRXA001785Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACKED AND DENTED LT OB STUB WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW E.O. 00-055 WITH APPROVApr 12, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR RRXA001766Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE, RIVETS PULLING THROUGH & RIVET HEADS SHEARING OFF FROM THE RT FLAP SCISSORS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW Apr 12, 2000 · N961R · Doug DC873F · Trailing Edge FlapsSDR UPS00832504Fitting · corrodedINSPECTION TYPE:C2, AFT LWR CARGO PIT AT FS 1200 BETWEEN L33R -L34R CROSS SLIDE DOOR 5TH FROM FWD LATCH FITTING CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED FITTING IAW DC 8 SRM 53-2-0 & 51-1-20D.Apr 12, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832444Skin · bentINSPECTION TYPE:C2, L-1 DOOR SKIN BENT LWR RT CORNER ACROSS BOTTOM OF DOOR. STRAIGHTENED DOOR SKIN EDGE IAW DC8 SRM 52-2-2. FOUND TO BE OUT OF LIMITS AND OIL-CANNED IAW DC8 SRM 52-2-2 PAGE 3. REMOVED LWR L-1 DOOR SEAL FOR ACCESS, ROUTED OUT DAMAGED AREA, FAApr 12, 2000 · N818UP · Doug DC873F · Passenger/Crew DoorsSDR RRXA002021Hinge · crackedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE FWD SIDE OF C-PIT CROSS SLIDE SILL GUARD HINGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NApr 11, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001901Door · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING FLYING DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DOOR IAW DC-8 SRM 51-3-0 AND MM 52-10-0.Apr 11, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA001899Door · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT FUEL DUMP CHUTE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DOOR IAW DC-8 SRM 51-1-3 AND 28-30-4. CORROSION DAMAGE RApr 11, 2000 · N961R · Doug DC873F · Fuel Dump SystemSDR RRXA001887Hinge · crackedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE FWD SIDE OF C-PIT CROSS SLIDE SILL GUARD HINGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NApr 11, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001765Door · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING MLG DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW DOOR IAW DC-8 SRM 51-3-0 AND DC-8 MM 52-10-0.Apr 11, 2000 · N961R · Doug DC873F · Landing Gear DoorsSDR RRXA001763Door · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT FUEL DUMP CHUTE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW CHUTE IAW DC-8 SRM 51-1-3 AND 28-30-4.Apr 11, 2000 · N961R · Doug DC873F · Wing, Plate/SkinSDR DHL2000804122Seat Track · brokenMAIN CARGO NR 1 LT TRACK LUG BROKEN AT SEVERAL POINTS FROM STA 1670.000 TO 1700.00. REMOVED DAMAGED TRACK PER SRM 51-3-0 PAGE 1. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED NEW TRACK PER SRM 51-3-0.Apr 11, 2000 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832488Angle · crackedINSPECTION TYPE:C2, ANGLE ON TOP OF WING BOX SKIN STA 847 - 857 RBL 27 IS CRACKED. REMOVED AND REPLACED ANGLE (P/N 4648710-2) IAW DC8 SRM 51-1-20D.Apr 11, 2000 · N818UP · Doug DC873F · Fuselage Main, StructureSDR RRXA003729Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO PANEL 161A SCREW HOLES AT STA 640-660 X-20 TO -40 Z-53 TO -73, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0Apr 10, 2000 · N961R · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA001951Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND LARGE TORN AREA IN THE FWD ACCESSORY COMPT CENTER OVERHEAD CEILING PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DApr 10, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001918Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER ON COCKPIT PRESSURE DECK APPROX 14 INCHES LEFT OF CENTER AT STA 45 TO STA 52, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRIApr 10, 2000 · N961R · Doug DC873F · Fuselage Main, BulkheadSDR RRXA001905Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE TO THE RT SIDE OF THE TAIL CONE INSIDE STA 1940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4 AND 51-1-21.Apr 10, 2000 · N961R · Doug DC873F · Aerodynamic FairingsSDR RRXA001816Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED AND TORN CENTER OVERHEAD CEILING PANEL IN THE FWD ACCESSORY COMPT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC-8 SApr 10, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001782Finger Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE BELOW FINGER DOUBLER ON COCKPIT PRESSURE DECK APPROX. 14 INCHES LEFT OF CENTER AT STA 45 TO 52, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABApr 10, 2000 · N961R · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA001769Frame · damagedDURING A MAINTENANCE VISIT, FOUND A HOLE TO THE RT. SIDE TAIL CONE INSIDE STA 1940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4.Apr 10, 2000 · N961R · Doug DC873F · Aerodynamic FairingsSDR RRXA000618Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LONGERON AT STA 665 AND LONGERON 31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED AND INSTALLED IAW DEE HOWARD AIRCRAFT MAINTENANCE SK 837-451.Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000617Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RT CENTER L/E LOWER SKIN AROUND O/B FUEL CAP AND EVIDENCE OF CRACK 8-18 INCHES FWD OF FRONT SPAR AT STA 385 TO 391.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-Apr 10, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL200080498CCargo Track · corrodedMAIN CARGO COMPT NR 1 LT TRACK FLOOR SUPPORT FLANGE SHOWS CORROSION FROM STA 860.00 TO 880.00. REMOVED DAMAGED TRACK PER SRM 53-2-3. CLEANED, TREATED AND PRIMED PER SRM 53-2-3. INSTALLED NEW TRACK PER SRM 53-2-3.Apr 10, 2000 · N804DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR UPS00832490Stringer · corrodedINSPECTION TYPE:C2, FWD LWR PIT AT STA 280 BETWEEN STR 35R TO 36R LWR PART OF TORQUE BOX STR 36R CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED Z-FITTING FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED LONGERON SECTION, SPLICESApr 10, 2000 · N818UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS00832489Pan · crackedINSPECTION TYPE:C2, FWD SERVICE DOOR AFT LWR DOOR PAN CRACKED. REMOVED AND REPLACED PAN IAW DAC DWG 5615700.Apr 10, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS00832443Fitting · corrodedINSPECTION TYPE:C2, RT CUSP AT STA 8, CUST TO FRAME FITTING HAS CORROSION. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-3-2 & 51-1-20D.Apr 10, 2000 · N818UP · Doug DC873F · Fuselage Miscellaneous Structure
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