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 RRXA002337Attach Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME ATTACH ANGLE TO FWD RT OVERWING EXIT DOOR AT FS 717 - 740 AND L19R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FITTING Mar 13, 2000 · N995CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA002304Skin · tornDURING A MAINTENANCE VISIT FOUND FUSELAGE SKIN TORN AWAY BY GROUND PNEUMATIC CONNECTOR DOOR CUTOUT, 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 AMar 13, 2000 · N995CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA002481Floor Support · gougedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT FLOORBEAM SUPPORT AROUND BOLT HEADS AND A DEEP GOUGE AT FS 960 XCW 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DMar 10, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002403Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE LONGITUDINAL FLOORBEAM AT STA 270 - 225 AND RBL 10, 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 SMar 10, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002385Panel · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE C PIT DOOR FILLET PANEL, 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 51-1-4.Mar 10, 2000 · N995CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA002373Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE IN THE MAIN CABIN INTERIOR AT STA 1586 AND L31L, 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 51-3-Mar 10, 2000 · N995CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA002384Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED DOOR SCUFF PLATE ATTACH ANGLE AT STA 1140 AND L34R, 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 51-Mar 9, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002357Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT SCREW HOLES ON THE RT O/B HORIZONTAL STAB LEADING EDGE I/B AT STA XFS 185 TO 187, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAMar 9, 2000 · N995CF · Doug DC862 · Horizontal Stabilizer StructureSDR RRXA002336Tie Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL FRAME TIE AT FS 760 AND L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED GUSSET IAW DC-8 SRM 51-1-21 AND 51-1-4.Mar 9, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002334Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES IN THE INTERCOSTAL AT FS 900 - 920 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW DC-8 SRM 53-2-0 AND 51-1-21.Mar 9, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002323Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE AT STA 1420 LEFT ABOVE L21L, 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 51-1-8.Mar 9, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002314Web · damagedDURING A MAINTENANCE VISIT FOUND A JAGGED METAL PIECE OF MEMBRANE AT STA 1000 - 1020 AT L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW DC-8 SRM 51-1-21, 51-1-4 ANDMar 9, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002418Intercostal · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE INTERCOSTAL AT FS 560 - 580 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 51-1-4 AND 51-1-21.Mar 8, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002414Intercostal · damagedDURING A MAINTENANCE VISIT FOUND A CUTOUT WITH NO REPAIR ON THE INTERCOSTAL BETWEEN STA 320 - 340 RT AND RBL 10 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAWMar 8, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002310Web · tornDURING A MAINTENANCE VISIT FOUND HOLES TORN OUT BETWEEN STA 560 - 580 XCW 12 INCHES LEFT AT CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB IAW DC-8 SRM 51-1-21 ANDMar 8, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002303Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT WING RIGHT O/B LEADING EDGE O/B EDGE UPPER AND LWR SKIN INTERIOR AT XFS 710, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND Mar 8, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002280Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON SKIN LEFT WING O/B LEADING EDGE O/B SECTION AT STA XW 761.695 24 INCHES FWD OF FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED Mar 8, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002218Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE FINGER DOUBLER COCKPIT SUBFLOOR AT STA 148 TO 144 AND L20L, 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 DMar 8, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001701Skin · crackedDURING A MAINTENANCE VISIT, FOUND A 2.5 INCH CRACK TO THE RT WING UPPER SKIN AT STA 960 AND XCW 69.5 , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED DOUBLERS FROM Mar 8, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA000995Frame · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK IN THE CABIN AT STA 520 AND L6L TO L7L, 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 REPAIR ANGLE IAW DC-8 Mar 8, 2000 · N994CF · Doug DC862 · Fuselage Main, FrameSDR RRXA000871Web · crackedDURING A MAINTENANCE VISIT FOUND CRACKED AND GOUGED RT WING I/B TE FLAP WELL FWD WEB AT FUS. STA 980 RT WING STA XW5. EO, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER FROM 7075-T6Mar 8, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000811Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND SEVERAL MISDRILLED HOLES CUSP TO CUSP AT STA 1580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED AND DISCREPANT HOLES, FABRICATED STRAP DOUBLER FROMMar 8, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000810Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND SEVERAL MISDRILLED HOLES CUSP TO CUSP AT STA 1560, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES, FABRICATED STRAP DOUBLER FROM 7075-T6 AND INMar 7, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002332Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOORBEAM TO FRAME ATTACH ANGLE AT STA 1586 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 NEW ANGLE IAW DC-8 SRM 51-3-Mar 6, 2000 · N995CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA002316Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL AT FS 640 - 660 AND L14R, 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, 53-2-0, 51-1-4 AMar 6, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002315Intercostal · misdrilledDURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL AT FS 700 - 717 AND L5R, 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, 51-1-4 ANMar 6, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA001687Vane · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE RT WING IB FLAP O/B FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW I/B FLAP OB FLAP VANE IAW DC-8 MM 27-51-14.Mar 6, 2000 · N994CF · Doug DC862 · Trailing Edge FlapsSDR RRXA000808Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM AT STA 1480 AT LONGERON 21 X + 12 Z O, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED L ANGLE, STRAP DOUBLER & FILLER FROM 7Mar 6, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000737Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AT LT WING O/B AILERON I/B HINGED PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW LEFT WING AILERON HINGE PANEL IAW DC-8 SRM 51-3Mar 6, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002335Intercostal · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT FS 798 TO 830 AND L5R, 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, 51-1-4 AND 51-1Mar 3, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002333Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK APPROX 2.5 INCHES LENGTH AT THE RT W/W LONGERON 24 STA 879, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 53-2-3,Mar 3, 2000 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA002322Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN RADIUS OF SUPPORT ANGLE ON RT BETWEEN STA 920 AND 902 LONGERON 24, 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 Mar 3, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002273Intercostal · damagedDURING A MAINTENANCE VISIT FOUND A HOLE TO THE INTERCOSTAL AT FS 340 - 360 AND L5R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAAW DC-8 SRM 51-1-4 AND 51-1-21.Mar 3, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002193Skin · dentedDURING A MAINTENANCE VISIT FOUND THE SKIN DENTED AT RIGHT WING O/B LEADING EDGE AT STA XFS 685, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED RIVETS AND DENT FILLER IAW DC-8 SRM 57-2-1.Mar 3, 2000 · N995CF · Doug DC862 · Wing, Plate/SkinSDR RRXA000814Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND NUMEROUS DRILLED HOLES IN THE AFT LWR CARGO COMPT TOP OF FLOORBEAM AT STA 1480, 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, FABMar 3, 2000 · N994CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA002398Finger Doubler · damagedDURING A MAINTENANCE VISIT FOUND A RIVET PULLED THROUGH THE FINGER DOUBLER ON THE LT HORIZ STAB REAR SPAR ACCESS AT STA 221, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED Mar 2, 2000 · N995CF · Doug DC862 · Horizontal Stabilizer StructureSDR RRXA002330Rivet · looseDURING A MAINTENANCE VISIT FOUND LOOSE RIVETS ON LWR DOOR RETAINERS RT FWD EXIT OPENING OVERWING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0.Mar 2, 2000 · N995CF · Doug DC862 · Emergency ExitsSDR RRXA002309Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL SUPPORT AT STA 600 XCW 6 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 NEW ANGLE IAW DC-8 SRM 51-1-21, 51-1-Mar 2, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002275Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED LWR RIB ON THE LEFT WING O/B LEADING EDGE I/B SEGMENT AT STA 603.750, 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 Mar 1, 2000 · N995CF · Doug DC862 · Leading Edge DevicesSDR RRXA002271Frame · damagedDURING A MAINTENANCE VISIT FOUND A HOLE IN THE FRAME AT FS 320 AND L14R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED GUSSET IAW DC-8 SRM 51-1-21A, 53-2-0, 51-1-4 AND 51-1-21.Mar 1, 2000 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA002227Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1220 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 DOUBLERS IAW DC-8 SRM 51-1-20D AND EO Mar 1, 2000 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA000918Web · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK IN THE FUSELAGE STRUCTURE, R-1 DOOR JAM LIGHTING HOLE AT STA 348 TO 354 R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PANEL FROM 2024-T3 ANDMar 1, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA000856Web · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN THE R-1 DOOR FWD LIGHTING HOLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK, FABRICATED DOUBLER FROM 7075-T6 AND INSTALLED IAW DC-8 SRM Mar 1, 2000 · N994CF · Doug DC862 · Passenger/Crew DoorsSDR RRXA000727Panel · delaminatedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LT WING REAR SPAR UPPER PANEL AT STA XRS 589 TO STA XRS 530, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW WING REAR SPAR PANEL IAWMar 1, 2000 · N994CF · Doug DC862 · Wing, Plate/SkinSDR RRXA002307Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT AT STA 500 XCW 6 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 NEW ANGLE IAW DC-8 SRM 51-1-21 AND 51-1-4Feb 29, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002306Floor Support · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT AT STA 500 XCW 6 INCHES RT, 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 51-1-21 AND 51-1-4Feb 29, 2000 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA002217Skin · damagedDURING A MAINTENANCE VISIT FOUND A BROKEN PIECE TOP OF L1 DOOR , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4.Feb 29, 2000 · N995CF · Doug DC862 · Cargo/Baggage DoorsSDR RRXA000924Attach Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE FLOORBEAM ATTACH FITTING AT STA 798 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED FITTING FROM 7075-T6 AND INSTALLED PER DOUGLAS DWG #Feb 29, 2000 · N994CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA000922Attach Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE FLOORBEAM ATTACH FITTING AT STA 781 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED ATTACH FITTING IAW DC-8 SRM 51-3-0 AND 51-1-20D.Feb 29, 2000 · N994CF · Doug DC862 · Fuselage Main, Attach FittingsSDR RRXA000872Web · crackedDURING A MAINTENANCE VISIT FOUND A GOUGED & CRACKED I/B TE FLAP WELL WEB ON THE RT WING STA XW5 STA. 1020 TO 980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW WEB FROM 2024-T3 AND INSTAFeb 29, 2000 · N994CF · Doug DC862 · Fuselage Miscellaneous Structure
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