Douglas DC-8-73F

Service difficulty reports · 15,471

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 = '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 DHL200080377CAngle · crackedAT C-CHECK, NR 4 MAIN TANK LWR AFT ANGLE CRACKED 1 INCH APPROX XRS 255 (INTERIOR). REMOVED FITTING IAW SRM 51-1-21A PG 4, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-21 PG 6 & 51-1-20D PG 9 & 10. N/R 1350Feb 24, 2000 · N803DH · Doug DC873F · Wing Miscellaneous StructureSDR DHL200080366CSeat Track · deterioratedAT C-CHECK, MAIN CARGO NR 2 LT SEAT TRACK FLANGE DETERIORATED FS 1080 TO FS 1160. REMOVED SEAT TRACK FLANGE, FABRICATED AND INSTALLED NEW SEAT TRACK AND FLANGE IAW SRM 51-1-21 PG 7. N/R 5574Feb 24, 2000 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR DHL200080364CFitting · crackedAT C-CHECK, AFT FUSELAGE SECTION 32 RT LONGERON SPLICE AFT FITTING CRACKED BETWEEN STA 1690 AND STA 1702. REMOVED AND REPLACED FITTING IAW SRM 51-1-8 PG 12. N/R 5484Feb 24, 2000 · N803DH · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003399Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME CAP AT STA 1000 AND L31R-L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 9755885.Feb 23, 2000 · N831AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000562Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE FLOORBEAM AT STA 70 AND LONGERON RBL 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW DC-8 SRM 51-1-20D AND SK 831-235. (CORROSION DAMAGE RFeb 23, 2000 · N831AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000561Seat Track · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 530 AND 590 AND LONGERON RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM 51-1-8. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SEAT TRACK SECTION AND INSTALLED IAW DFeb 23, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000533Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN BETWEEN STA 55 TO STA 70 AND LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DAC DWG 561386Feb 23, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000531Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 280 AND LONGERON 30 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIGURE 2D.Feb 23, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR DHL2000803117Seat Track · deterioratedAT C-CHECK, MAIN CARGO NR 1 RT SEAT TRACK FLANGE DETERIORATED FS 960 TO FS 1100. REMOVED DETERIORATED FLANGE AND TRACK, FABRICATED AND INSTALLED FLANGE AND TRACK IAW SRM 53-2-3 PG 49 & 50. REF: N/R 5573.Feb 23, 2000 · N803DH · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003797Cover · misdrilledDURING A MAINTENANCE VISIT FOUND MISSDRILLED HOLES TO D-PIT INNER THRESHOLD COVER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. WELDED EXTRA HOLES IAW E.O. 00-016 WITH APPROVED 8110-3 DATED 02/18/00Feb 22, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003796Sill · damagedDURING A MAINTENANCE VISIT FOUND MISSING NUT PLATE TO B-PIT DOOR LWR SILL HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. WELDED BAMAGE AND INSTALLED NUT PLATES IAW E.O. 00-016 WITH APPROVED 8110-3 DATED 02/18Feb 22, 2000 · N792FT · Doug DC873F · Fuselage Main, StructureSDR RRXA003397Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBOARD AT STA 1420 AND X=0 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3 AND 51-1-26.Feb 22, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA002932Insert · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TRACK INSERT BETWEEN FS 760 - 980 AND X-+30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0. (CORROSIONFeb 22, 2000 · N792FT · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000664Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE FLOORBEAM ATTACH FITTING AT STA 70 BBL 55, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20 AND DAC DWG 4888829.Feb 22, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA000663Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE END FITTING AT STA 1140 AND LONGERON 33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG NR 475Feb 22, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000534Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 300 AND LONGERON 32 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755826. CORROSION DAFeb 22, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA003409Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK BETWEEN STA'S 300-320 AND RBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DFeb 21, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000659Angle · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LT HORIZONTAL STAB L/E FORMER ANGLE AT STA XFS 47, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ANGLE AND INSTALLED IAW DC-8 SRM 53-2-0, 51-2-20D ANDFeb 21, 2000 · N831AL · Doug DC873F · Horizontal Stabilizer StructureSDR RRXA000529Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 1660 TO STA 1665. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION IAW DAC DWG 2772660. CFeb 21, 2000 · N831AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000654Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE MAIN CABIN FLOORBEAM TIE FITTING AT STA 680 AND BL 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG NR 5Feb 20, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000653Web · crackedDURING A MAINTENANCE VISIT, FOUND 3 CRACKS TO THE MAIN DECK 9G NET SUB FLOOR PANELS AT STA 70 AND LBL 5 TO RBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLFeb 20, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA003790Web · damagedDURING A MAINTENANCE VISIT FOUND BROKEN OUT DAMAGE TO MAIN CARGO DOOR WEB FRAME AT STA. 270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 & E.O. 00-016 WITH APPFeb 19, 2000 · N792FT · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000719Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/E RIB AFT UPPER END STA XFS 741.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED CRACK IAW DC-8 SRM 57-2-0 FIG 2.Feb 19, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000658Clip · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE RIGHT WING L/E RIB CLIP AT STA XOLDI 6.225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW SRM 51-1-20D AND DAC DWG NR 5769589.Feb 19, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA000656Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LEFT WING L/E RIBS AFT FASTENERS AT STA XFS 741.250, 747.500. 753.750 AND 760.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLFeb 19, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000655Flange · chafedDURING A MAINTENANCE VISIT, FOUND CHAFE DAMAGE TO THE RIGHT O/B SLOT VANE O/B END FLANGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FLANGE AND INSTALLED IAW DC-8 SRM 51-1-21 AND DAC DWG NR 576994Feb 19, 2000 · N831AL · Doug DC873F · Aileron TabsSDR RRXA000526Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 27 RIGHT BETWEEN STA 8 TO STA 70. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DWG 3648666. CFeb 19, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA003396Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN DECK FLOOR BOARD BETWEEN STA'S 1200 TO 1220 AND X32 Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53Feb 18, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000690Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E RIBS AT STA'S XFS 366.500, 360.250, 354.000, 347.750, 341.500 AND 322.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AFeb 18, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000648Skin · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RT WING L/E SKIN DOUBLER AT STA XFS 570.3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, PRIMED AND SEALED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D, Feb 18, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA000647Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK AT THE LT WING L/E RIBS AT STA XFS 722.5, 728.75 AND 735.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2Feb 18, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000522Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA 1150 BETWEEN LONGERONS 34 RIGHT TO 35 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DCFeb 18, 2000 · N831AL · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS00831745Eadi · failedINSPECTION TYPE:N/A DIVERSION, CAPT EADI FAILED SMOKE IN COCKPIT. CARGO SMOKE DETECTORS BOTH ILLUMINATED AT FL 330 SMOKE IN COCKPIT. REMOVED AND REPLACED CAPT EADI, OPS CHECKS GOOD.Feb 18, 2000 · N802UP · Doug DC873F · Integrated Flight SystemSDR DHL200080381CFloorbeam · crackedAT C-CHECK, MAIN CARGO UPPER FLANGE OF THE FLOORBEAM SHOWS 8 INCH CRACK BETWEEN LBL 41 AND LBL 48 AT FS 240. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO NR 011802. N/R 5193Feb 18, 2000 · N803DH · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000717Door Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NUT PLATE MOUNTING POINT ON A-PIT DOOR FRAME (AFT SIDE) AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW SUPPORT FRAME IAW DC-8 Feb 17, 2000 · N831AL · Doug DC873F · Fuselage Main, StructureSDR RRXA000689Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E UPPER RIBS AT STA'S XFS 422.750, 416.500, 379, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED RIBS, REPAIRED AND INSTALLED IAW DC-8 SFeb 17, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000186Inverter#2 IGNITION C/B TRIPPED IN FLIGHT UNABLE TO RESET *** CORECTIVE ACTION *** R/R IGNITION STATIC INVERTER AND BATTERY BUS BLOCKING RECTIFER START SYSTEM AND TACHS FUNCTION NORMAL NO DEFECTS FOUND ON GROUND RUNFeb 17, 2000 · N795FT · Doug DC873F · DC Rectifier/ConverterSDR RRXA000185Skin · damagedFOUND BREAK IN AIRCRAFT SKIN BETWEEN RIVITS LEFT SIDE OF AIRCRAFT APPROXIMATELY MID POINT BETWEEN MAIN CARGO DOOR AFT EDGE AND WING. *** CORRECTIVE ACTION *** DETERMINED AREA IN QUESTION TO BE LOCATED AT FUELAGE STA 440 (APPROX) AND LONGERON NR 3 (APPROX)Feb 17, 2000 · N2674U · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000527Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 28 LEFT BETWEEN STA 350 TO 360. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DWG 9754913. CORFeb 17, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000521Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 130 TO 140 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DC-Feb 17, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000520Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERNAL SKIN SECTION AT STA 512 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA DER ENGINEERING Feb 17, 2000 · N831AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000519Floorboard · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1580 TO STA 1680 AND BL 26 RIGHT. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FOUND TO BE IN LIMITS IAW DC-8 SRM 53-2-0 FIGURE 1. CORROSION DAMAGE RECORDED IN EWA CORROSION PFeb 17, 2000 · N831AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000657Clip · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE LT WING L/E INTERCOSTAL ATTACH CLIP AT STA XOLDI 6.225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-21 AND DAC DWG 357Feb 16, 2000 · N831AL · Doug DC873F · Wing Miscellaneous StructureSDR RRXA003788Threshold · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO CABIN R1 DOOR TRESHOLD AFT I/B CORNER AT STA. 190, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. WELDED CRACKED SECTION, NDT INSP PER ASTM E1417, NO DEFECTS NOTED. IFeb 15, 2000 · N792FT · Doug DC873F · Fuselage Main, StructureSDR RRXA003408Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CABIN FLOOR BEAM AT FS 879.3 AND RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D AND 51-1-Feb 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA003407Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/E UPPER SKIN AT STA XFS 854, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0 AND 57-2-1, FIG 38.Feb 15, 2000 · N831AL · Doug DC873F · Wing, Plate/SkinSDR RRXA003394Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON STIFFNER AT STA 55 TO 70 AND RBL -48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0, FIG 18 AND 51-1-20D.Feb 15, 2000 · N831AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000688Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT O/B L/E UPPER RIBS, AT STA'S XFS 603.750, 610.000, 616.250 AND 622.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, REPAIRED AND INSTALLED IAW DFeb 15, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000687Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT THE LT O/B CENTER L/E UPPER RIB AT FASTENER END AT STA'S XFS 635.000, 641.250, 653.750, 660.000 AND 672.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED, RFeb 15, 2000 · N831AL · Doug DC873F · Wing, Rib/BulkheadSDR RRXA000516Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 21 RIGHT BETWEEN STA 1280 TO 1400. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DAC DWG J060296. CORROSION DAMAFeb 15, 2000 · N831AL · Doug DC873F · Fuselage Main, Longeron/Stringer
Back to Douglas DC-8-73F