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 RRXA000306Angle · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING LEADING EDGE INTERNAL ANGLE CRACKED AT XW 230. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-4.Oct 17, 1999 · N605AL · Doug DC873F · Leading Edge DevicesSDR 20000424AP021Angle · crackedFOUND DURING D-CHECK, NR 3 RT STUB WING HAS CRACK INSIDE L/E DOUBLER. REMOVED CRACKED ANGLE. FABRICTED NEW ANGLE, TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-20D. (M)Oct 17, 1999 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR 20000522AP025Seat Track · wornFOUND DURING D-CHECK, UPPER CARGO COMPARTMENT SEAT TRACK NR 6 XCW 25 RIGHT STATION 500-510. CUT OUT WORN SECTION OF TRACK. INSTALLED NEW TRACK AND SPLICES IAW DC-8 SRM 53-2-3, 51-1-8 AND 51-3-0. (M)Oct 16, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA000314Seat Track · damagedDURING A MAINTENANCE VISIT FOUND UPPER CARGO SEAT TRACK DAMAGED BETWEEN STA 500 TO STA 510 AND BL 25 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2Oct 16, 1999 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR 20000424AP029Finger Doubler · corrodedFOUND DURING D-CHECK, WHEEL WELL PRESS PANEL HAS CORROSION AROUND RIVETS AND PANEL STATION 902 TO 920 RBL 20 INCH. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FINGER DOUBLER REPAIR. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-4 AND 51-1Oct 16, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000206Finger Doubler · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WHEEL WELL PRESSURE PANEL AROUND RIVETS FROM STA 902 TO STA 920 RBL 20.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLERSOct 16, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR DHL99804007Dir Gyro · failedF/O COMPASS DRIFTS (HSI) EXCESS + - 30 DEGREES OR MORE. REPLACED NR 1 DG PER MM 34-21-1, SYSTEM CHECKED GOOD.Oct 16, 1999 · N804DH · Doug DC873F · Directional Gyro and Indicating SystemSDR 99T64R465EWAFloorbeam · corrodedFOUND DURING D-CHECK, UPPE CARGO COMPT STATION 1120 XCW 50 LEFT FLOORBEAM SEAT TRACK MOUNT POINT, AREA OF CORROSION. (M)Oct 15, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000193Skin · corrodedDURING A MAINTENANACE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN AT BETWEEN STA 980 TO 1120. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-1.Oct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 99T64R456EWASkin · corrodedFOUND DURING D-CHECK, FUSELAGE CORRODED AROUND NUT PLATE HOLES FOR WING FILLET ATTACH UPPER STATION 980 TO 1120. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 53-2-1. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8, 51-1-21 ANOct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 20000424AP027Longeron · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT LONGERON 9 STATION 1300-1340 LT SURFACE CORROSION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. CUTOUT DAMAGED AREA. FABRICATED DOUBLER PARTS IAW DC-8 SRM 53-2-2. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-2. Oct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR 20000424AP025Floorboard · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT FLOOR PANEL 580-840 AREA OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 53-2-0 AND 51-1-21. (M)Oct 14, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR 20000424AP022Floorbeam · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT FLOORBEAM EXFOLIATED STATION 1500 XCW 50 LEFT. REMOVED CORROSION IAW DC-8 SRM 51-18-8. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-2-0 AND 51-1-8 AND 51-3-0. (M)Oct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000215Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1500 XCW 50 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER AND INSTALLED IAW DC-8 SRM 51-2-0, 51-1-8 AND 51-3-0. (CORROSOct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000212Floorboard · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER CARGO COMPARTMENT FLOOR PANEL BETWEEN STA 580 TO STA 840. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SOct 14, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000210Longeron · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON NR 9 BETWEEN STA 1300 TO STA 1340 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-2 & 51-1-8. (COOct 14, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR DHL99802002Oxygen Sys · leakingLOST O2 PRESSURE FROM 1600 TO 200 PSI. SERVICED AND LEAK CHECKED CREW O2 PER MM 35-10-00. OK FOR SERVICE.Oct 14, 1999 · N802DH · Doug DC873F · Crew Oxygen SystemSDR RRXA000265Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 880 TO STA 1100 AND BL 45R, 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.Oct 13, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR UPS99830964Battery Pack · dischargedEMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT. OPS CHECK NORMAL PER DC8 DC8 MM 33-50-01.Oct 13, 1999 · N802UP · Doug DC873F · Emergency LightingSDR UPS99830903Battery Pack · dischargedEMERGENCY LIGHT VERY DIM. REPLACED EMERGENCY LIGHT BATTERY PACK AND RELAY UNIT. OPS CK NORMAL PER MM 33-50-01.Oct 13, 1999 · N802UP · Doug DC873F · Emergency LightingSDR RRXA000273Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN PANEL 262 BETWEEN STA 960 TO STA 1000 AND LEFT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW FAA DER APPROVEOct 12, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR 20000522AP012Web · corrodedFOUND DURING D-CHECK, RIGHT LONGERON AND FUSELAGE WEB ATTACHMENT CORROSION EXIST FROM STATION 879 TO 960. BLENDED OUT CORROSION. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-186 WITH APPROVED 8110-3 DATED 10/11/99. (M)Oct 12, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830877Pack · failedNR 1 BUS PWR FAIL LIGHT ILLUMINATED ON BLOCK IN. COCKPIT FILLED W/PACK SMOKE EVEN THOUGH PACK WAS OFF. COULD STILL HEAR FAN OPERATING AND COOLING DOORS OPEN. TROUBLESHOT SYSTEM PER MM 24-20-00. RECONNECTED NR 3 GENERATOR, RAN ENGINE, SYSTEM OPS CHECKS GOODOct 12, 1999 · N806UP · Doug DC873F · Air Distribution SystemSDR 20000424AP030Finger Doubler · corrodedFOUND DURING D-CHECK, FINGER DOUBLER CORRODED AND RIVET CORRODED STATION 857 TO 902 CENTER OF AIRCRAFT 10 INCHES BELOW CABIN FLOOR. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED FINGER DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AOct 11, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000216Floorbeam · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM AT STA. 1220 XCW 51 R/H. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.///// CORRECTIVE ACTION ///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC-8Oct 11, 1999 · N605AL · Doug DC873F · Fuselage Main, Floor BeamSDR RRXA000205Finger Doubler · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE FROM FS 857 TO FS 902 AT BL 0.0 BELOW CABIN FLOOR. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC-8 SRM 51-1-8, 51-1Oct 11, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000251Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 1540 BL-R 40 AND WL-15, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGLE IAW DC-8 SRM 51-1-21.Oct 10, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000522AP023Angle · corrodedFOUND DURING D-CHECK, D PIT STATION1540 BULKHEAD FRAME UPPER ANGLE CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED ANGLE IAW DC-8 SRM 51-1-5. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Oct 10, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830876Smoke Curtian · unsecuredINSPECTION TYPE:N/A, SMOKE CURTAIN NOT ATTACHED TO FLOOR NEAR ENTRY DOOR. SECURED SMOKE CURTAIN TO FLOOR AS REQUIRED. OK FOR SERVICE.Oct 10, 1999 · N808UP · Doug DC873F · Emergency EquipmentSDR RRXA003426Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING FILLET PANEL 261C LT TOP FWD CORNER ATTACH ANGLE AT STA 960-990, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 5-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8Oct 9, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003425Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON BACK SIDE OF WING FILLET PANEL 161F AT STA 880-920, 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 51-1-24.Oct 9, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003424Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WING FILLET PANEL 261E RUB STRIP AT STA 960-980 AND XCW 69, 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 53-2Oct 9, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830918Longeron · corrodedINSPECTION TYPE:C1 LONGERON 32R, FWD OF FS 1766 IS CORRODED OUT OF LIMITS UNDER THE SPLICE FITTING. CUT OUT DAMAGED SECTION OF THE LONGERON AND SPLICED IN A NEW SECTION IAW SRM 53-2-2 FIG 10.Oct 9, 1999 · N814UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99830917Fitting · crackedINSPECTION TYPE:C1 FS 1230 FRAME ATTACH FITTING AT LONGERON 35L IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Oct 9, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830875Floor · misinstalledINSPECTION TYPE:N/A, EVACUATION SLIDE GIRT BAR COULD NOT BE INSTALLED BECAUSE OF FLOOR PANEL RAISED TO HIGH. REINSTALLED FLOOR PANEL TO BE FLUSH WITH FLOOR, OPS CHECK GOOD.Oct 9, 1999 · N808UP · Doug DC873F · Fuselage Floor PanelSDR RRXA003423Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH ANGLE IN FRONT OF WING LENS ON WING FILLET PANEL 261A AT STA 640-660 AND XCW 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND IOct 8, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003422Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND SCREW HOLES INSIDE AND OUTSIDE OF THE RT WING FILLET PANEL 262B, 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 SRMOct 8, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA000280Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 360 AND BETWEEN LONGERONS 32 LEFT TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL.Oct 8, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000278Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 260 TO STA 280 AND BETWEEN LONGERONS 32 LEFT TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL ANDOct 8, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000277Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 260 TO STA 280 AND BETWEEN LONGERONS 32 LEFT TO 32 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL ANDOct 8, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR RRXA000272Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 55 TO STA 62 AND BL 48L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FLOOR PANEL AND INSTALLED IAW DC-8 SRM 51-1-9.Oct 8, 1999 · N605AL · Doug DC873F · Fuselage Floor PanelSDR 20000424AP026Skin · crackedFOUND DURING D-CHECK, LEFT AFT OVERWING EXIT DOOR FOUND CRACK IN DOOR UNDER BOTTOM PLATE THAT WAS REMOVED FOR CORROSION. STOP DRILLED CRACK IAW DC-8 SRM 52-20-0. FABRICATED DOUBLER. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21D. (M)Oct 8, 1999 · N605AL · Doug DC873F · Emergency ExitsSDR RRXA000276Channel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO U-CHANNEL AT STA 98 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW U-CHANNEL AND INSTALLED IAW DC-8 SRM 51-1-4.Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000250Door Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER AFT CARGO DOOR JAMB (FRAME) AT STA 1540 AND LONGERON 33 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Main, StructureSDR 20000609AP008Door Frame · corrodedFOUND DURING D-CHECK, STATION 1540 BULKHEAD DOOR FRAME HAS CORROSION BLISTER 30 INCHES ABOVE L33R. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21. (M)Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR 20000424AP028Frame · corrodedFOUND DURING D-CHECK, UPPER CARGO COMPT LIGHT SURFACE CORROSION STATION 1200 LONGERON 9-10 LEFT. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-21, 53-2-0 AND 51-1-4. (M)Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000208Frame · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER CARGO COMPARTMENT LIGHT AT STA 1200 BETWEEN LONGERON NR 9 & 10 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE,TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLERS AND INSTALLED IAW DC-8Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR RRXA000207Angle · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO WING PRESSURE PANEL ATTACH ANGLE FROM STA 960 TO STA 980 AT RIGHT BUTT LINE8.0. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ATTACH ANGLE Oct 7, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830916Bulkhead Chord · crackedINSPECTION TYPE:C1 ACCOMPLISH APPENDIX C OF EO DC8-5310-10158-A, FS 70 BLKHD LWR CHORD AT LONGERON 33L IS CRACKED AND CORRODED. REPAIRED FS 70 BLKHD LWR CHORD AT LONGERON 33L IAW EO DC8-5310-10158-A APPX C.Oct 7, 1999 · N814UP · Doug DC873F · Fuselage Main, BulkheadSDR RRXA003420Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT INBOARD FLAP FAIRING PLATE AT XRS 172, 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, 51-1-4, 51-3-0Oct 6, 1999 · N605AL · Doug DC873F · Wing, Plate/Skin
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