Douglas DC-8-62

Service difficulty reports · 2,778

Newest first. General aviation reporting is voluntary.

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 = 'DC862'
  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 RRXA002207Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 1460, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS AND FILLERS AND INSTALLED IAW EO NR May 1, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002305Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON LWR AFT LOBE OF FLOORBEAM AT FS 900 AND XCW 47 RT, 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 53-2-0, 51-1-2Apr 28, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000989Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT FRAME AFT PRESSURE BULKHEAD FRAME Z + 18 X + 2 TO -2 TOP ANGLE OF FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRIApr 28, 2000 · N994CF · Doug DC862 · Fuselage Main, BulkheadSDR RRXA000988Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT FRAME AFT PRESSURE BULKHEAD FRAME BOTTOM ANGLE ON FRAME & TOP ANGLE AT Z + 30 X -2 TO +4, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILApr 28, 2000 · N994CF · Doug DC862 · Fuselage Main, BulkheadSDR RRXA000987Bulkhead · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK ON AFT PRESSURE BULKHEAD FRAME TOP ANGLE ON FR & BOTTOM OF FRAME Z + 43 X + 2 TO -2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FAApr 28, 2000 · N994CF · Doug DC862 · Fuselage Main, BulkheadSDR RRXA002474Frame · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE INTERIOR ANGULAR FRAME AT STA 1586 BETWEEN L19R AND L24R, 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 51-1Apr 27, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002370Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AT STA 255 RT AND RBL 52.5 INCHES, 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 EO NR 00-Apr 27, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002268Channel · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL AT STA 580 XCW 60 INCHES LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC-8 SRM 51-1-20D AND EO NR 00-047Apr 27, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002239Skin · damagedDURING A MAINTENANCE VISIT FOUND ATTACH SCREWS PULLING THROUGH SKIN AT LT WING O/B SLOT L/E VANE AT STA XFS 508.000 34 INCHES TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABApr 27, 2000 · N995CF · Doug DC862 · Leading Edge DevicesSDR RRXA002197Plate · damagedDURING A MAINTENANCE VISIT FOUND AN ELONGATED SCREW HOLE ON THE NR 4 MAIN FUEL TANK LAND PANEL 505D, DAMAGE HAS EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 00Apr 27, 2000 · N995CF · Doug DC862 · Fuel StorageSDR RRXA002495Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND A HOLE DRILLED THROUGH RADIUS IN WEB ON THE LONGITUDINAL FLOORBEAM AT STA 230 RT AND RBL 45.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLApr 26, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002269Longeron · crackedDURING A MAINTENANCE VISIT FOUND A HOLE DRILLED IN THE FRAME AT STA 1570 AND L16L TO L17L, 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 EO NR Apr 26, 2000 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA002263Frame · misdrilledDURING A MAINTENANCE VISIT FOUND DRILLED HOLES IN THE FRAME AT STA 1400 LT AND L21L TO L19L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24Apr 26, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002261Frame · tool damageDURING A MAINTENANCE VISIT FOUND TOOLING MARK AT STA 1280 LT AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED TOOLING MARKS SMOOTH IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.Apr 26, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002255Vane · damagedDURING A MAINTENANCE VISIT FOUND SCREW HOLE ELONGATED ON LEFT I/B FLAP NR 1, 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 EO NR 00-047 WITH APApr 26, 2000 · N995CF · Doug DC862 · Trailing Edge FlapsSDR RRXA002192Skin · crackedDURING A MAINTENANCE VISIT FOUND A POSSIBLE CRACK EMANATING FROM RIVET HOLE ON THE LT WING UPPER SURFACE AT STA 22.250 AT CENTER SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTApr 26, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002401Support Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER KEEL BEAM CENTER PANEL SUPPORT CLIP AT STA 890 AND L36L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAApr 25, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA2212Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 600, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS/FILLERS AND INSTALLED IAW Apr 25, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002221Support Fitting · crackedDURING A MAINTENANCE VISIT FOUND A WORN AND CRACKED MAIN CARGO DOOR CUTOUT UPPER SUPPORT, 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 EO NR 0Apr 25, 2000 · N995CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA002201Support Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER KEEL BEAM PANEL SUPPORT CLIP AT STA 880 AND L36L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SUPPORT CLIPApr 25, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR IXXA0000017Fan · defectiveEN ROUTE FROM FJR TO NKW, THE FLIGHT CREW NOTICED SMOKE INTO THE COCKPIT WHEN THE LEFT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO NKW FOR AN UNEVENFUL LANDING. MAINTENANCE INSPECTED THE FApr 25, 2000 · N728PL · Doug DC862 · Air Distribution FanSDR RRXA002272Panel · crackedDURING A MAINTENANCE VISIT FOUND CRACKED WELDS ON THE CUSP PANEL 1380 TO 1420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.Apr 24, 2000 · N995CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA002318Web · crackedDURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE MEMBRANE AT THE L1 DOOR AREA STA 270 - 225 LT AND L21L DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MEMBRAApr 22, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002262Frame · misdrilledDURING A MAINTENANCE VISIT FOUND DRILLED HOLES IN THE FRAME AT STA 1380 AND L21L TO L19L, 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 EO NR 0Apr 22, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002500Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEADING EDGE LT WING AT XFS 566, 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 51-1-21 AND EO NR 00Apr 21, 2000 · N995CF · Doug DC862 · Leading Edge DevicesSDR RRXA002475Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE FRAME AT FS 620 AND L7L, 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 51-1-20 AND EO NR 00-047 WITH APPROVEDApr 21, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002404Channel · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL AT STA 225 RT AND RBL 55.5 - 62 INCH, 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 51-2-0 AND 51-1Apr 21, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002317Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM ON LWR CUSP AT STA 225 AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW GUSSET IAW DC-8 SRM 51-1-21 AND 51-1-4.Apr 21, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002248Intercostal · crackedDURING A MAINTENANCE VISIT FOUND GOUGED/CRACKED OUT HOLES ON INTERCOSTAL BETWEEN STA 1420 - 1400 RT AND BETWEEN L2R-L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IApr 21, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002654Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT STA 1739 BETWEEN L32R AND L28R, 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 DC-8 SRM 53-2-0 AND EO Apr 20, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002389Web · crackedDURING A MAINTENANCE VISIT FOUND A 4 INCH CRACK LT WING I/B FLAP FILLER WEB AT FUSELAGE AT STA 980, 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 51-1-21 ANApr 20, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002382Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 270 - 280, 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-Apr 20, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002356Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE ON THE CIRCUMFERENTIAL FRAME GILLINER AT STA 1140 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRApr 20, 2000 · N995CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA002320Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING BELOW SKIN ON THE RIGHT L/E CENTER SECTION O/B NR 3 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 DC-8 SRApr 20, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002499Threshold · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, DISTORTED EDGES AND ELONGATED HOLES TO A FASTENER AT L2 DOOR INNER THRESHOLD PANEL, 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 Apr 19, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002325Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AT FS 1280 TO 1300 AND L9R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51-1-21 AND 51-1-4Apr 19, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002312Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL AT FS 1320 - 1340 AND L5L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51-1-Apr 19, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002276Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN I/B SLOT LEADING EDGE VANE AT STA XS 250.000, 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 SRApr 19, 2000 · N995CF · Doug DC862 · Leading Edge DevicesSDR RRXA002220Web · crackedDURING A MAINTENANCE VISIT FOUND CRACKS IN 5 PLACES AND MULTIPLE DISTORTIONS TO THE CABIN FLOOR CUSP LINE WEB AT STA 320 TO 270 RT CUSP AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATEApr 19, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002219Web · crackedDURING A MAINTENANCE VISIT FOUND MULTIPLE HOLE ELONGATION WITH DISTORTION AND CRACKS IN 4 PLACES TO THE CABIN FLOOR CUSP WEB AT STA 270 TO 235 RT AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. Apr 19, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002195Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE RIGHT I/B STUB WING LWR SURFACE BETWEEN LWR RIB AT XFS 233 AND XFS 240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAApr 19, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002321Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS LOOSE AND PULLING BELOW SKIN ON THE RIGHT I/B SLOT DOOR LEADING EDGE, 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 SRMApr 18, 2000 · N995CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA002277Skin · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN LT WING I/B SLOT LEADING EDGE VANE AT STA XS 220.000, 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-Apr 18, 2000 · N995CF · Doug DC862 · Leading Edge DevicesSDR RRXA002241Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON THE NR 1 STUB WING MOUNTING SHIM AT LWR FRONT SPAR CAP AT STA XW 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM IAW DC-8 SRApr 18, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002216Skin · chafedDURING A MAINTENANCE VISIT FOUND CHAFING TO THE L1 DOOR SKIN AT EXTERIOR DOOR HANDLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 4-17Apr 18, 2000 · N995CF · Doug DC862 · Passenger/Crew DoorsSDR RRXA002199Plate · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED LWR FRONT SPAR CAP ON THE NR 4 STUB WING I/B MOUNT SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED EDGES SMOOTH AND RETURNED TO SERVICE IAW EO NR Apr 18, 2000 · N995CF · Doug DC862 · Wing Miscellaneous StructureSDR RRXA000916Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL AREAS DRILLED IN THE CABIN L/H FLOOR BEAM ATTACH FITTING AT FS 580 AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM.Apr 14, 2000 · N994CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA002465Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 540 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 AND EOApr 13, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002419Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES IN THE INTERCOSTAL AT FS 798 - 822 AND L5L, 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 51-1-4 AND 51-1-21.Apr 13, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002400Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 680, 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 EO NR 00-04Apr 13, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor Beam
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