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 RRXA000933Intercostal · misdrilledDURING A MAINTENANCE VISIT, FOUND SEVERAL MISDRILLED HOLES IN THE UPPER CARGO COMPT. FLOORBEAM INTERCOSTAL AT STA 520 TO 500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. HOLES IN IFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001518Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES IN THE CABIN FLOORBEAM AT STA 857 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED DOUBLER FRFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA001517Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES IN THE CABIN FLOORBEAM AT STA 857 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED DOUBLER FRFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000914Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN MAIN CABIN ANGLE AT STA 1040 AND LONGERON -1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM. RECEIVED AND INSTALLED IAW DC-8 SRM.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000913Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED SUB-FLOOR UNDER L/H ELEC. CENTER AT STA 225 LT. RBL 24 -28 Z AXIS 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM. STOP DRILLED CRACK, FABRICATED REPAIR.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000903Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE CABIN UPPER CARGO COMPT. SEAT TRACK C7-R2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000885Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACKED ATTACH ANGLES AT FS 420 TO 440, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000884Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE UPPER CARGO BAY. FLOORBEAM INTERCOSTALS AT FS 440 TO 420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES ARE WITHIN ALLOWABLE LIMFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000883Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACKED ATTACH ANGLES AT FS 600 TO 580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000882Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE UPPER CARGO BAY. FLOORBEAM INTERCOSTALS AT FS 600 TO 580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES ARE WITHIN ALLOWABLE LIMIFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000881Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACKED ATTACH ANGLES AT FS 620 TO 600, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8.Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000880Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE UPPER CARGO BAY. FLOORBEAM INTERCOSTALS FLOORBEAM TO FLOORBEAM AT STA 620 TO 600, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000868Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ACCESS PANEL NR 62 FWD MOST COMPTARTMENT, RT SIDE BOTTOM ANGLE OF FWD BULKHEAD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000817Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE FUSE STRUCTURE AFT UPPER CARGO COMPT OF FLOORBEAM AT STA 1440, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED STFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000816Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT TOP OF FLOORBEAM AT STA 1380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES WITH AD RIVET MATERIAL, FABFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000809Angle · looseDURING A MAINTENANCE VISIT, FOUND MISSING AND LOOSE BOLTS IN THE FLOORBEAM ATTACH ANGLE AT STA 400 AND LBL 63, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. REPLACED BOLTS, FABRICATED ANGLE, FILLER, TRFeb 24, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000740Floorboard · wornDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE CABIN COCKPIT FLOOR PANEL AT STA 148 TO 168, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FLOOR PANEL SKIN IAW DC-8 SRM 53-2-3Feb 24, 2000 · N994CF · Doug DC862 · Fuselage Floor PanelSDR RRXA000724Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE AT STA XE 99 TO XE 123, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW STAB PANEL IFeb 24, 2000 · N994CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA000723Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE AT STA XE 219 TO XE 245, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRFeb 24, 2000 · N994CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA000722Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE BETWEEN STA XE245 TO XE270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IFeb 24, 2000 · N994CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA000721Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TAIL RT HORIZ STAB REAR SPAR UPPER SURFACE INSIDE AT STA XE52.825 -XE.75.672, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW RT STABFeb 24, 2000 · N994CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA002396Bracket · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE ATTACH ANGLE BRACKET ON THE RT LEADING EDGE CENTER SECTION O/B SLOT DOOR PANEL AT STA XFS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRFeb 23, 2000 · N995CF · Doug DC862 · Wing Miscellaneous StructureSDR RRXA001705Intercostal · misdrilledDURING A MAINTENANCE VISIT, FOUND A HOLE DRILLED IN RADIUS OF INTERCOSTAL IN THE CABIN UPPER CARGO COMPT. AT FS 1280 TO 1300 AND LONG. 14L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOFeb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001702Plate · damagedDURING A MAINTENANCE VISIT, FOUND A TEMP. REPAIR AT EXT. AIR RECEPTICLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW DOOR FROM 2024-T3 AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-4Feb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001650Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT. TOP OF FLOORBEAM AT STA 1260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED Feb 23, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000869Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER IN CABIN STA 188 TO 208 AND RBL 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 2024-T3 AND INSTALLED Feb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000846Frame · crackedDURING A MAINTENANCE VISIT, FOUND THE FUSELAGE STRUCTURE FWD OF LT W/W PANEL SUPPORT FRAME CRACKED O/B PANEL 161S AT STA 834, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANGLE DOUBLERS FROFeb 23, 2000 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000834Intercostal · misdrilledDURING A MAINTENANCE VISIT, FOUND HOLES DRILLED IN RADIUS OF INTERCOSTAL CABIN UPPER CARGO COMPT STA 1200 TO 1200 LONG ST 14L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGLE FROMFeb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000833Intercostal · misdrilledDURING A MAINTENANCE VISIT, FOUND HOLES DRILLED IN RADIUS OF INTERCOSTAL IN CABIN UPPER CARGO COMPT STA 1240 TO 1260 AND LONG ST 14L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FRFeb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000832Intercostal · misdrilledDURING A MAINTENANCE VISIT, FOUND HOLES DRILLED IN RADIUS OF INTERCOSTAL AT THE CABIN UPPER CARGO COMPT STA 1270 AND LONGERON ST 19L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR ANGFeb 23, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000732Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING TRAILING EDGE LOWER PANEL BETWEEN O/B FLAP CENTER AND O/B HINGES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW WING T/Feb 23, 2000 · N994CF · Doug DC862 · Trailing Edge FlapsSDR RRXA000726Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LT WING REAR SPAR UPPER PANEL AT STA XRS 624 TO STA XRS 693, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW LT WING REAR SPAR PANEL Feb 23, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002331Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE IN THE MAIN CABIN INTERIOR FRAME AT STA 900 AND L11L, 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 SFeb 22, 2000 · N995CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA001728Web · crackedDURING A MAINTENANCE VISIT, FOUND CRACKED HOLES AND A CRACKED MEMBRANE IN THE CABIN BETWEEN STA 225 TO 270 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED CUSP MEMBRANE & ATTACFeb 22, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001727Floor Support · crackedDURING A MAINTENANCE VISIT FOUND SEVERAL AREAS CRACKED IN THE FLOOR SUPPORT AND ATTACH ANGLE 2 AXIS 0 BETWEEN STA 225 TO 208 AND LBL 14 TO RBL 11, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTFeb 22, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000874Web · chafedDURING A MAINTENANCE VISIT FOUND CHAFFING AT THE LT AFT FILLET WEB AT FUSELAGE STA 920, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR FROM 7075-T6 AND INSTALLED IAW DC-8 SRM 51-1-21Feb 22, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000735Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING FILLET PANEL AT 161P, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REBONDED AND INSTALLED AREA PANEL 161P IAW DC-8 SRM 51-1-9. (CORROSION DAMAGEFeb 22, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA001685Spar · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING REAR SPAR UPPER SURFACE AT STA XRS 162 TO 163, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED -L- ANGLES FROM 7075-T6 5Feb 21, 2000 · N994CF · Doug DC862 · Wing SparSDR RRXA001666Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT. TOP OF FLOORBEAM AT STA 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATED Feb 21, 2000 · N994CF · Doug DC862 · Fuselage Floor PanelSDR RRXA001654Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT. TOP OF FLOORBEAM AT STA 1180, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES, FABRICATEDFeb 21, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000819Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT TOP OF FLOORBEAM AT STA 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES, FABRICATED STRAP DOUBLERS Feb 21, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000813Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT TOP OF FLOORBEAM AT STA 1500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES WITH AD RIVET MATERIAL, FABFeb 21, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000741Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE RT WING T/E LWR PANEL AFT OF FUEL DUMP HINGE PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-3-0. (Feb 21, 2000 · N994CF · Doug DC862 · Trailing Edge FlapsSDR RRXA000739Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING T/E UPPER PANEL AT STA XRS 580 TO XRS 630, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW RT WING T/E PANEL IAW DC-8 SRM Feb 21, 2000 · N994CF · Doug DC862 · Trailing Edge FlapsSDR RRXA000738Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING REAR SPAR UPPER PANEL AT STA XRS 653 TO STA XRS 763, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW LT WING REAR SPAR PAFeb 21, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA000736Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING FILLET PANEL AT 161Q, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW LT WING FILLET 161Q IAW DC-8 SRM 51-1-8. (CORROSIONFeb 21, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA000733Panel · delaminatedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING REAR SPAR UPPER PANEL AT STA 456 TO XRS 519, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW RT WING T/E PANEL IAW DC-8 SRFeb 21, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR IXXA0000008Duct · looseEN ROUTE FROM KWI TO AVB, THE FLIGHT CREW HEARD CREW HEARD A BANG FROM THE TURBO COMPRESSOR BAY ARE FOLLOWED BY LOSS OF CABIN PRESSURIZATION. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES AND DESCENTED TO A SAFE ALTITUDE. THE FLIGHT CONTINUED TO AVB Feb 21, 2000 · N31CX · Doug DC862 · Cabin Pressure Control SystemSDR RRXA001668Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE DOUBLER ATTACHED TO LONGERON IN AFT LOWER CARGO BILGE AT STA 1080 TO 1100 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. REMOVED LOFeb 18, 2000 · N994CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA001657Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT. TOP OF FLOORBEAM AT STA 1120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED EXISTING HOLES, FABRICATED DFeb 18, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor Beam
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