N8079U, cancelled Sep 6, 2001

Service difficulty reports · 84

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N8079U' AND deregistration_id = 'N8079U-2001-09-06'
  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 99T64R545EWAPin Boss · corrodedDURING D-CHECK. LT MAIN GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102. REF: EMERY WORNov 19, 1999 · N8079U · Doug DC871 · Landing Gear Retraction/Extension SystemSDR 99T64R533EWAFastener · missingFOUND DURING D-CHECK. RT WING L/E ABOVE NR PYLON. ONE LOOSE FASTENER WITH SKIN WASHER, ONE FASTENER MISSING. (EO). TIGHTENED THE LOOSE FASTENER. INSTALLED NAS1670L4 JO-BOLT IN OPEN HOLE. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8Nov 13, 1999 · N8079U · Doug DC871 · Wing Miscellaneous StructureSDR 2000T74R547EWMetal Strip · crackedDURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS .75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRACK. STOP DRILLED AND NDT TO CONFIRM CRACK. STOP DRILLED - BROKEN SHARP EDGES. TREATED, PRIMED AND FILLED STOP DRILL HOLES WITH SEALER PERNov 12, 1999 · N8079U · Doug DC871 · Nacelle/Pylon StructureSDR 99T64R535EWAFastener · missingFOUND DURING D-CHECK. RT MAIN LANDING GEAR FITTING MISSING FASTENER AFT SIDE. (EO). LEFT THE SHEARED SHANK IN THE HOLE, FILLED HOLE WITH PR1422B 1/2 SEAL. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-174 WITH APPROVED 8110-3 DATED 11-11-99. REF: EMENov 11, 1999 · N8079U · Doug DC871 · Main Landing Gear Attach SectionSDR 99T64R539EWADoor · missingDURING D-CHECK. FABRICATED AND INSTALLED DIVIDER WALL BETWEEN C AND D PITS. (EO). FABRICATED A NEW DOOR USING DRAWING 99-174-2. TREATED AND PRIMED PER EO 999-174 WITH APPROVED 8110-3 DATED 11-8-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)Nov 10, 1999 · N8079U · Doug DC871 · Fixed Inner DoorsSDR 99T64R534EWAPin Boss · corrodedFOUND DURING D-CHECK. RT MAIN LANDING GEAR SHOCK STRUT ASSY RETRACT PIN BOSS CORRODED. (EO). BLENDED OUT CORROSION. FABRICATED NEW BUSHING AND CAD PLATED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-15-99. INSTALLED BUSHING AND PIN IAW DC-8 SB 32-102. Nov 9, 1999 · N8079U · Doug DC871 · Landing Gear Retraction/Extension SystemSDR 99T64R504EWADrain Plug · missingFOUND DURING D-CHECK. C-PIT DOOR MISSING DRAIN PLUG. FABRICATED FILLER. TREATED AND PRIMED. INSTALLED FILLERS AND DRAIN PLUG PER EO 99-174 WITH APPROVED 8110-3 DATED 11-02-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Nov 8, 1999 · N8079U · Doug DC871 · Cargo/Baggage DoorsSDR 99T64R444EWABulkhead · damagedFOUND DURING D-CHECK. 'A' PIT AFT BULKHEAD BOTTOM NEEDS TO BE TRIMMED STA 440. (EO). FABRICATED NEW DOOR USING DRAWING NR 99-174-1. TREATED AND PRIMED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)Nov 4, 1999 · N8079U · Doug DC871 · Fuselage Main, BulkheadSDR RRXA991790Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 660 TO STA 750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONNov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor PanelSDR RRXA991789Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 750 TO STA 860. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONNov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor PanelSDR RRXA991788Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 40 TO STA 80 AND BETWEEN BL 56L TO BL 68L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor PanelSDR RRXA991787Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1240 TO STA 1348 AND BETWEEN BL 48L TO BL 62L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL Nov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor PanelSDR RRXA991786Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 346. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONNov 3, 1999 · N8079U · Doug DC871F · Fuselage Floor PanelSDR 99T64R537EWAPanel · brokenFOUND DURING D-CHECK. STA 1660 SIDE RAIL PANEL BROKEN STA 1650 - STA 1700. (EO). FABRICATED NEW SIDE RAIL PANEL PER EO 99-174 WITH APPROVED 8110-3 DATED 10-20-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)Nov 3, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR RRXA991779Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA=-69 BETWEEN BL=0 TO BL=45L AND WL-9.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED DER Nov 2, 1999 · N8079U · Doug DC871F · Fuselage Main, FrameSDR 99T64R532EWAVane · damagedFOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 5 VANE INBOARD UPPER END HAS ELONGATED HOLE. DRILLED AND REAMED HOLE TO .75 INCH DIAMETER. TREATED AND PRIMED. FABRICATED PLUG AND INSTALLED, DRILLED PLUG TO CORRECT HOLE SIZE PER EO 99-174 WITH APPROVED 8110-3 Oct 27, 1999 · N8079U · Doug DC871 · Trailing Edge FlapsSDR 99T64R518EWASkin · damagedFOUND DURING D-CHECK. LEFT WING OUTBOARD FLAP VANE INBOARD END UPPER SURFACE HAS IMPROPER REPAIR OF ELONGATED HOLE. DRILLED AND REAMED HOLE TO .375 INCH DIAMETER. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WOct 27, 1999 · N8079U · Doug DC871 · Trailing Edge FlapsSDR 99T64R452EWAActuator Crank · crackedFOUND DURING D-CHECK. RIGHT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRACK ON FLAP ACTUATOR ASSEMBLY IAW DC-8 OHM 27-28-7. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 26, 1999 · N8079U · Doug DC871 · Trailing Edge FlapsSDR 99T64R451EWAActuator Crank · crackedFOUND DURING D-CHECK. LT WING FLAP ACTUATOR ASSY STA 340 FOUND CRANK TO BE CRACKED. REMOVED AND REPLACED CRANK ON FLAP ACTUATOR ASSY IAW DC-8 OHM 27-28-7. REF: EMERY WORLDWIDE A/L. RRXA. (X)Oct 26, 1999 · N8079U · Doug DC871 · Trailing Edge FlapsSDR 99T64R503EWASkin · damagedFOUND DURING D-CHECK. RIGHT OUTBOARD FLAP NR 6 VANE INBOARD END TOP SIDE HAS HOLE ELONGATED. DRILLED AND REAMED HOLE TO .375 INCH. FABRICATED PLUG AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 25, 1999 · N8079U · Doug DC871 · Trailing Edge FlapsSDR RRXA991780Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 980 TO STA 995 AND LONGERON 35 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SOct 22, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous StructureSDR 99T64R536EWASkin · damagedRIGHT INBOARD LEADING EDGE TOP MOUNT HOLES DAMAGED OR ELONGATED, 7 EACH. DRILLED, PRIMED AND INSTALLED IAW EO NR 99-174 WITH APPROVED 8110-3 DATED 9-14-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 22, 1999 · N8079U · Doug DC871 · Wing, Plate/SkinSDR 99T64R538EWAKick Plate · crackedFOUND DURING D-CHECK. AFT LOWER CARGO RACKS AND DENTS. (EO). STRAIGHTEN DENTS. NDT VERIFIED NO CRACKS, STOP DRILLED CRACKS AND WELDED IAW EO 99-174 WITH APPROVED 8110-3 DATED 10-11-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R513EWAThrust Reverser · damagedFOUND DURING D-CHECK. RT FAN REV DAMAGED ON LOWER VERTICAL SURFACE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST MIXED WITH MICRO BALLOONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99.Oct 18, 1999 · N8079U · Doug DC871 · Engine Thrust ReverserSDR 99T64R512EWACowl · damagedFOUND DURING D-CHECK. HOLE ON INSIDE OF LT FORWARD OF LT FORWARD COWL NR 1 ENGINE. CUT OUT DAMAGED AREA, FILLED WITH LY5052 02 RESIN AND HY5052 02 RESIN CATALYST AND MIRCO BALLONS. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10Oct 18, 1999 · N8079U · Doug DC871 · Engine Cowling SystemSDR 99T64R508WKick Plate · damagedFOUND DURING D-CHECK. TYPE ONE EMERGENCY EXIT DOOR LEFT SIDE. KICK PLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICK PLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R434EWAStiffener · brokenLEFT WHEELWELL FORWARD WEBBING FRAME BROKEN. (EO). WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND. ACCEPTABLE TO RETURN TO SERVICE PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-24-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R432EWAStiffener · brokenRIGHT WHEELWELL FORWARD WEBBING STIFFENER BROKEN. (EO). WELDED NEW SECTION OF TUBING IAW MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 18, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R514EWALine · chafedFOUND DURING D-CHECK. FIRE RETARDANT LINE CHAFED FORWARD OF TOMBSTONE NR 3 PYLON. BLENDED CHAFE SMOOTH FILLED CHAFE WITH WELD, NDT WELD NO FLAWS FOUND PER EO 99-174 WITH APPROVED 8110-3 DATED 10-7-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 15, 1999 · N8079U · Doug DC871 · Extinguishing SystemSDR 99T64R510EWAKick Plate · damagedFOUND DURING C-CHECK. TYPE ONE EMERGENCY DOOR RIGHT FORWARD KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAVE BEEN STOPPED, WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED 10-14Oct 14, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R509EWAKick Plate · damagedFOUND DURING D-CHECK. TYPE ONE EMERGENCY DOOR AFT RIGHT SIDE KICKPLATE DAMAGED. (EO). STOP DRILLED CRACK, NDT TO ASSURE CRACKS HAD BEEN STOPPED. WELDED KICKPLATE AND NDT TO ASSURE NO FLAWS IN WELD, NONE NOTED. PER EO 99-174 WITH APPROVED 8110-3 DATED 10-Oct 14, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R507EWAKick Plate · gougedFOUND DURING D-CHECK. B-PIT DOOR KICK PLATE GOUGED/SCRATCHED. (EO). FABRICATED NEW KICK PLATE. WELDED ACCORDING TO MIL-STD-2219, NDT WELD TO ASSURE NO FLAWS IN WELD. NONE NOTED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-20-99. REF: EMERYOct 12, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R454EWASkin · damagedFOUND DURING D-CHECK. RT MID LEADING EDGE TWO DOUBLER LOWER EXTERIOR TO EVALUATE DAMAGE STA XFS 416.500 - XS 435.289. (EO). REMOVED AND REPLACED THE OUTBOARD EXTERNAL SKIN WITH NEW SKIN SAME SIZE. SHAPE AND MATERIAL AS THE ORIGINAL PER EO 99-174 WITH APROVEOct 12, 1999 · N8079U · Doug DC871 · Wing, Plate/SkinSDR RRXA991785Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERCOSTAL BETWEEN STA 520 TO STA 540 AND LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 Oct 8, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous StructureSDR 99T64R515EWAThrust Reverser · lightning strikeFOUND DURING D-CHECK. THREE LIGHTNING STRIKES, RIGHT FAN REV. TRAILING EDGE OUTER SECTION MIDDLE AND BOTTOM NR 4 ENGINE. (EO). BLENDED THE EDGE OF THE LIGHTNING STRIKES, SMOOTH, ALODINED AND FINISHED PER FACTORY SPECS. IT IS ACCEPTABLE TO RETURN TO SERVICOct 8, 1999 · N8079U · Doug DC871 · Engine Thrust ReverserSDR 99T64R453EWASkin · damagedFOUND DURING D-CHECK, LT MID-WIND LEADING EDGE OUTBOARD END SLOT VANE STA 520.168, HOLES WORN AND ELONGATED. (EO). FABRICATED REPAIR STRAP 12 INCHES BY 2.25 INCHES. TREATED AND PRIMED. INSTALLED CONICAL WASHERS AND INSTALLED REPAIR STRAP PER EO 99-174 WITHOct 8, 1999 · N8079U · Doug DC871 · Wing, Plate/SkinSDR 99T64R445EWABushing Mount · crackedFOUND DURING D-CHECK. AFT PASSENGER DOOR (L2) HAS CRACK AT UPPER HINGE BUSHING AREA STA 1600. REMOVED CRACK SECTION BY CUT OUT. FABRICATED REPAIR DOUBLERS. TREATED, PRIMED, AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-01-99. REF: EMERY WORLOct 7, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99664R428EWASkin · damagedEXTERIOR RT LIGHTING STRIKE STA 250 RT BETWEEN L21R - L22R. (EO). BLENDED ROUGH AREAS SMOOTH, REAMED HOLES AND INSTALLED MS20470AD8 RIVET. TREATED AND PRIMED PER EO 99-174 WITH APPROVED 8110-3 DATED 9-16-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)Oct 7, 1999 · N8079U · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA991781Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1280 AND LONGERON 35 LEFT, 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 51-1-21. CORROSION DOct 6, 1999 · N8079U · Doug DC871F · Fuselage Main, FrameSDR 99T64R500EWACover · gougedFOUND DURING D-CHECK. 'D' PIT DOOR THRESHOLD PLATE GOUGED/SCRATCHED STA 1420. (EO). REMOVED THE EXISTING D-PIT THRESHOLD PLATE. FABRICATED NEW THRESHOLD, WELDED CURVED PORTIONS AND NDT WELDS. NO FLAWS FOUND AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3Oct 6, 1999 · N8079U · Doug DC871 · Fuselage Miscellaneous StructureSDR 99T64R506EWAFrame · corrodedFOUDN DURING D-CHECK. CORROSION AT STA -67 APPROXIMATELY 45 INCHES LEFT OF CENTER ON SUB-FLOOR FRAME IN COCKPIT. (EO). REMOVED CORROSION. TREATED, PRIMED AND FINISHED PER FACTORY SPECIFICATIONS. FABRICATED REPAIR ANGLE AND INSTALLED PER EO 99-174 WITH APPOct 5, 1999 · N8079U · Doug DC871 · Fuselage Main, FrameSDR 99T64R455EWASkin · lightning strikeFOUND DURING D-CHECK. LIGHTNING STRIKE STA 300 RT BETWEEN L18R - L19R (EO). OPENED LIGHTNING STRIKE HOLE TO .375 INCH. FABRICATED DOUBLER AND INSTALLED PER EO 99-174 WITH APPROVED 8110-3 DATED 10-4-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 4, 1999 · N8079U · Doug DC871 · Wing, Plate/SkinSDR RRXA991783Bolt · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CARGO DOOR T-BOLT BETWEEN STA 280 TO STA 340 AND LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW T-BOLT AND INSTALLED DC-8 SRM 5Oct 3, 1999 · N8079U · Doug DC871F · Cargo/Baggage DoorsSDR 99T64R440EWARib · crackedLEFT WING T/E STA 261 FLAP WELL RIB CRACKED BELOW NR 4 SPOILER. CUT OUT CRACK. TREATED AND PRIMED. FABRICATED REPAIR DOUBLER AND INSTALLED PER EO NR 99-174 WITH APPROVED 8110-3 DATED 9-21-99. REF: EMERY WORLD WIDE A/L, RRXA. (X)Oct 2, 1999 · N8079U · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991784Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 1420 AND LONGERON 36. 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 53-2-0. CORROSION DAMAGEOct 1, 1999 · N8079U · Doug DC871F · Fuselage Main, FrameSDR 99T64R426EWASeat Tracks · wornF/E SEAT AFT TRACK LOCK HOLES WORN TO LIMITS. REMOVED AND REPLACED F/E'S SEAT TRACK IAW DC-8 SRM 51-1-21. REF: EMERY WORLDWIDE A/L. RRXA. (X)Oct 1, 1999 · N8079U · Doug DC871 · Fuselage, Seat/Cargo Attach FittingsSDR 99T64R475EWASkin · damagedFOUND DURING D-CHECK, MID-WING LEADING EDGE SLOT VANE HOLE OVERSIZED AND WORN AT STA XS 520.186. (EO). CLEANED EXISTNG COUNTERSINKS, ALODINED, TREATED AND PRIMED. FABRICATED CONICAL WASHERS AND FILLED THE COUNTERSINKS. FABRICATED REPAIR DOUBLER AND INSTALLSep 28, 1999 · N8079U · Doug DC871 · Wing, Plate/SkinSDR 99T64R429EWAShim · brokenNR 3 STUB WING L/E INBOARD LOWER SPAR CAP SHIM BROKEN OFF XILD .7095. (EO). SMOOTHED REMAINING EDGE OF SHIM. NDT TO ASSURE THAT NO CRACKS EXIST. (NONE FOUND). TREATED AND PRIMED, INSTALLED INBOARD PIECE AS A SHIM USE FACTORY FASTENERS PER EO 99-174 WITH ASep 25, 1999 · N8079U · Doug DC871 · Leading Edge DevicesSDR RRXA991782Finger Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA -25 AND BL 36L AND WL -9. 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-8 SRM 53-3-1.Sep 24, 1999 · N8079U · Doug DC871F · Fuselage Miscellaneous StructureSDR 99T64R467WEARib · crackedFOUND DURING D-CHECK. NR 2 STUB WING LEADING EDGE, 7 INCH CRACK TOP RIB STA 250.089. STOP DRILLED CRACK IAW DC-8 SRM 57-2-0. FABRICATED TWO DOUBLERS IAW DC-8 SRM 57-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20D AND Sep 23, 1999 · N8079U · Doug DC871 · Wing, Rib/Bulkhead
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