Mcdonnell Douglas DC-8-71

Service difficulty reports · 341

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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 = 'DC871'
  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 RRXA002826Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER T/E AT LT WING CENTER L/E AT STA XS 442, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-2-0.Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002825Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON THE LT WING CENTER L/E AT STA XFS 366.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002824Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER T/E ON THE LT WING CENTER L/E AT STA 372.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4, 57Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002823Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON THE LT WING CENTER L/E AT STA XFS 360.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002822Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT T/E ON THE LT WING CENTER L/E AT STA XFS 310.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-Jul 27, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA003776Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE AND SCREWS BROKEN OFF FROM THE SEAT TRACK BETWEEN STA 600 TO 820, X=0, Z=0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SEAT Jul 26, 2000 · N811AL · Doug DC871 · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003770Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FILLET PANEL 261B AND ELONGATED SCREW HOLES, 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 51-1-20 Jul 26, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA002820Former · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT BOTTOM T/E OF FORMER AT STA XFS 835, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-2-0.Jul 26, 2000 · N811AL · Doug DC871 · Trailing Edge FlapsSDR RRXA002818Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT O/B L/E OUTER SKIN AT I/B BOTTOM AT STA XFS 710, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 57-2-1Jul 26, 2000 · N811AL · Doug DC871 · Fuselage Main, Plate/SkinSDR RRXA003778Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE "B" PIT FLOOR PANEL AT STA 340-440 AND L27, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PJul 25, 2000 · N811AL · Doug DC871 · Fuselage Floor PanelSDR RRXA003775Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER ANGLE AT STA 857 X=0 TO+25 Z+-21, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLETS IAW DC-8 SRM 53-2-0 FIG 1Jul 25, 2000 · N811AL · Doug DC871 · Fuselage Main, Attach FittingsSDR RRXA002809Longeron · crackedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT LONGERON 24 AT "T" UPPER WEB BETWEEN STA 879-902, ALSO 1/8 INCH CRACK AT RADIUS AT STA 896, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAJul 25, 2000 · N811AL · Doug DC871 · Fuselage Main, Longeron/StringerSDR RRXA002808Spar Cap · chafedDURING A MAINTENANCE VISIT FOUND A CHAFFED AREA ON THE RT WING FRONT LWR. SPAR CAP AT STA XFS 7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#00-196 WITH APPROVED 8110-3 DATJul 25, 2000 · N811AL · Doug DC871 · Wing SparSDR RRXA003767Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING UPPER SURFACE TRAILING EDGE INTERCONNECT PANEL AT STA XRS 693.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALJul 24, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA003824Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ANGLE BRACE AFT SECTION INSIDE ANTENNA COUPLER AT STA. ZR218.010, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND IJul 20, 2000 · N811AL · Doug DC871 · Aircraft StructuresSDR RRXA003772Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING UPPER SKIN AT STA 727 STRINGER 2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DJul 20, 2000 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA003779Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE "D" PIT FLOOR PANEL AT STA 988-1066 AND L33R TO L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAAW DC-8Jul 19, 2000 · N811AL · Doug DC871 · Fuselage Floor PanelSDR RRXA003774Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SUB FLOOR PANEL BETWEEN STA 80 TO 220 BL 0 TO LBL 25 Z=-2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 Jul 19, 2000 · N811AL · Doug DC871 · Fuselage Floor PanelSDR RRXA003771Structure · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H UPPER TRAILING EDGE I/B AILERON PANEL 565G, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PANEL AND INSTALLED IAW DC-8 SRM 51-3Jul 19, 2000 · N811AL · Doug DC871 · AileronsSDR RRXA003310Plug · missingDURING A MAINTENANCE VISIT FOUND BORESCOPE PLUGS NOT INSTALLED ON NR 4 ENGINE AT 12:30, 10:00 AND 9:00 POSITIONS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. INSTALLED AND SAFETIED BORESCOPES PLUGS ON NR 4 ENGINE IAW DFM 56 AND MM 72-42-00.Jul 11, 2000 · N996GE · Doug DC871 · Powerplant SystemSDR RRXA003309Plug · looseDURING A MAINTENANCE VISIT FOUND SAFETY WIRE MISSING ON NR 2 ENGINE BORESCOPE PLUG AT 12:30 POSITION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. TORQUED AND SAFETIED NR 2 ENGINE BORESCOPE PLUG IAW DC-8-71 MM 72-00-41.Jul 11, 2000 · N996GE · Doug DC871 · Powerplant SystemSDR RRXA002913Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT CLIP NUTS AND NUT PLATES ON THE LWR. ANG.E AT STA 70 BULKHEAD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, May 25, 2000 · N811AL · Doug DC871 · Fuselage Main, BulkheadSDR 2000ZZZX183Brace · damagedUPON GEAR EXTENSION INTO MIAMI, HEARD STRANGE NOISE FROM NOSE WHEELWELL AREA. GEAR EXTENDED NORMALLY WITH 3 GREEN INDICATIONS. POST-FLIGHT SIDE BRACE ATTACH LUG FOR RETRACT CYLINDER ATTACHMENT CRACKED. ACFT N NR HK-3785X.Dec 6, 1999 · Doug DC871 · Landing Gear Retraction/Extension SystemSDR 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 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 RRXA991679Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RIGHT O/B L/E O/B SECTION FROM NR 4 PYLON SKIN AT STA XFS 710. CRACK TERMINATES AT FASTENER HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSNov 2, 1999 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA991678Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E OB OF NR 4 PYLON AT STA XFS 710, CRACKED SKIN IN 2 PLACES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 57-2-1 FNov 2, 1999 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991677Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E RIBS AT STA XFS 703.75, XFS 672.5, XFS 566.25, XFS 585, XFS 591.25, XF 603.75, XFS 622.5, XFS 635. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANDNov 2, 1999 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991676Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, CENTER L/E RIBS AT STA XFS 347.75 AND XFS 360.25. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS AND INST IAW DC8 SRM 53-2-0 FIG 1Nov 2, 1999 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991675Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E INNER TRIPPLER CRACKED AT STA XOLI 6.225, 20 FWD OF LWR T/E.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TRIPPER IAW DC8 SRM 57-3-Nov 2, 1999 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA991674Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPPER RIB AT END AT STA XS 442.185. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2.Nov 2, 1999 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991673Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E UPER RIBS AT FWD AT STA XS 484.895, XS 467.323, XFS 366.5, XFS 304, XF 322.75 AND XFS 379. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANov 2, 1999 · N811AL · Doug DC871 · Wing, Rib/BulkheadSDR RRXA991672Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E INNER DOUBLER AT STA XW 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RI DOUBLER IAW MFG DWG 5769769 AND DC8 SRM 51-3-0.Nov 2, 1999 · N811AL · Doug DC871 · Wing, Plate/SkinSDR RRXA991671Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, RT CENTER L/E OB UPPER T-CHORD AT STA XS 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0 FIG 2.Nov 2, 1999 · N811AL · Doug DC871 · Wing SparSDR RRXA991670Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, NR 4 PYLON STUB WING FRAME AT STA XW 454. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND INST REPAIR IAW DC8 SRM 51-1-20 AND DCNov 2, 1999 · N811AL · Doug DC871 · Wing SparSDR 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 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 Reverser
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