Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 RRXA10747Skin · damagedDURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO SKIN AT HOLE 62 AND RUDDER POWER PACK LEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND ISTALLED IAW SRM 51-1-4 AND DC-8 SRM 51-1-21.Mar 1, 2001 · N8091U · Doug DC871F · Rudder, Plate/SkinSDR RRXA10746Brace · crackedDURING A MAINTENACE VISIT FOUND CRACK DAMAGE TO HORZ. BRACE AT STA. 1916 AND DOOR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 AMar 1, 2001 · N8091U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA10745Skin · damagedDURING A MAINTENANCE VIST FOUND ELONGATED HOLE DAMAGE TO SKIN AT FWD OF MLG DOORS, DAMAGE ECXEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 51-3-0.Mar 1, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01835187Separator · malfunctionedINSPECTION TYPE:IN FUMES IN C/P DURING ENTIRE FLIGHT, SEEM TO BE COMING FROM EITHER PACK. ON GROUND FOUND R PACK EMITTING ODOR. DER R PACK PER MEL 21-38-1. PERF MAINTENANCE PROCEDURES. M 210419 ASSIGNED PLACARDS INSTALLED. REMOVED AND REPLACED RT WATER SEPMar 1, 2001 · N730UP · Doug DC871F · Humidity Control SystemSDR UPS01835116Landing Gear · failedINSPECTION TYPE:N/A, AFTER TAKEOFF MLG FAILED TO RETRACT. MAINTAINED AIRSPEED BELOW 230 KTS AND CLIMBED TO 15000 FT. PERFORMED GEAR HANDLE JAMMED CHECKLIST ON DESCENT TO PHL BELOW 10000 FT NOSE GEAR POSITION APPEARED. AIRCRAFT FERRY PERMIT DMI CONTROL NR D2Mar 1, 2001 · N701UP · Doug DC871F · Landing Gear Retraction/Extension SystemSDR RRXA10862Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN LT WW AT STA. 857-879 AND LBL 0-68.5, 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 51-3-0 & 53-2-0 FIFeb 28, 2001 · N8091U · Doug DC871F · Wing, Plate/SkinSDR RRXA010687Angle · brokenDURING A MAINTENANCE VISIT FOUND THE "C-PIT" ANGLE BROKEN IN HALF (AFT R/H), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRFeb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010686Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM SUPPORT FITTING AT STA 300 AND RBL -24", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRFeb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA010685Hand Rail · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE RAIL AT STA 90-220 RT, 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 AND DC-8 SRM 51-1-4.Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010684Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GALLEY FLOOR PANEL AT TOP SURFACE PANEL #329, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCFeb 28, 2001 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA010683Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP LINE PANEL AT STA 1540-1620 L/H, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010682Structure · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP RAIL AT STA 210-380 RT, 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.Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA010681Fitting · crackedDURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK INSIDE BATH TUB FITTING LWR HORIZ. SURFACE TO LT LONGERON 24 STA 860, 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 53Feb 28, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA010680Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUEL TANK PANEL LAND 506B AT STA XRS 110 TO 125 S-69 TO S-71, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024Feb 28, 2001 · N8091U · Doug DC871F · Wing, Plate/SkinSDR RRXA10868Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION TO BATH TUBE FITTING AT STA. 1690 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 & 51Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, BulkheadSDR RRXA010679Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING SKIN AT STA 960-980 X+45", 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 & 53-2-0 FIG. 1F.Feb 27, 2001 · N8091U · Doug DC871F · Wing, Plate/SkinSDR RRXA010678Guard · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN 2 PLACES TO THE R-1 DOOR SILL GUARD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/15/01.Feb 27, 2001 · N8091U · Doug DC871F · Emergency ExitsSDR RRXA010677Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FLOOR BEAM AT STA 857 X+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/26/Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Floor BeamSDR RRXA010676Flange · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT FWD TYPE I DOOR FRAME SEAL FLANGE LWR END, DAMAGE EXCEEDED LIMITATIONS IAAW 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 AND DC-8 SRM 53-2-0Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA010675Frame · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE FWD SIDE OF FRAME ON THE R/H FWD TYPE I DOOR FRAME SEAL AT STA 370, 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 51-1-2Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, FrameSDR RRXA010674Floor Panel · misrepairedDURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE MAIN CARGO FLOOR PANEL AT STA 80 TO 340E, 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 AND DC-9 SRM Feb 27, 2001 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA010673Doubler · bentDURING A MAINTENANCE VISIT FOUND A BENT TO THE UPPER FWD CORNER ON THE DOUBLER FOR "A-PIT" CUTOUT AT STA 320-333, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAFeb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010672Doubler · bentDURING A MAINTENANCE VISIT FOUND A BENT UPPER FWD CORNER TO THE DOUBLER FOR "A-PIT" CUTOUT AT STA 292, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DFeb 27, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010013Pressure Switch · inoperativeNR 4 ENGINE LOW OIL PSI LIGHT INOP. TRANSFERRED TO DMI LIST AS CONTROL B-9616122-0962 CAT: B MEL 7906 ATA 7910 DUE DATE 02MAR01 PLACARD INSTALLED. REMOVED AND REPLACED NR 4 ENG LOW OIL PRESS SW, OPS AND LEAK CHECK GOOD IAW DC-8 M/M 79-32-2. (LOW OIL PRESS SFeb 27, 2001 · N8076U · Doug DC871F · Engine Oil PressureSDR IXXA0100008Rod · malfunctionedEN ROUTE FORM LRD TO TOL, WHEN THE LANDING GEAR WAS RETRACTED THE FLIGHT CREW NOTICE A VIBRATION IN THE NOSE OF THE AIRCRAFT. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE VIBRATION REMAINED PRESENT. THE AIRCRAFT RETURN TO LRD FOR AN UNEVENTFUL LANDING. MFeb 27, 2001 · N828BX · Doug DC871F · Landing Gear Door ActuatorSDR UPS01835093Relay · failedINSPECTION TYPE:N/A, CREW PREFLT-MASTER WARNING LIGHT FAILS TO RESET. REMOVED AND REPLACED R2-94 RELAY R2-100.Feb 27, 2001 · N703UP · Doug DC871F · Central WarningSDR UPS01835062Bottle · dischargedINSPECTION TYPE:IN, CABIN DOOR EMERGENCY SLIDE BOTTLE PRESS LOW. REMOVED AND REPLACED CABIN DOOR EMERGENCY SLIDE AS PER MM 25-60-00.Feb 24, 2001 · N779UP · Doug DC871F · Escape SlideSDR RRXA10507Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES ON THE FE'S FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREAIAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Feb 22, 2001 · N8091U · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA010510Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE EDGES OF THE FLOOR PANEL CAPT'S SIDE PANEL #676D, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRFeb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA010509Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL #661 AND CRACKED SCREW HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAFeb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA010508Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PERIMETER TOP & BOTTOM EDGES OF CENTER COCKPIT FLOOR PANEL #677 CHAFF STRIP BROKEN, ELONGATED HOLES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAFeb 22, 2001 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA010506Skin · corrodedDURING A MAINTENANCE VISIT FOUND DISCOLORATION TO THE SKIN ON INSIDE TANK AT LT LWR WING FUEL VENT BOX UPPER SKIN BETWEEN STRINGERS NR 1 & 2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAFeb 22, 2001 · N8091U · Doug DC871F · Wing, Plate/SkinSDR RRXA10807Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED Feb 21, 2001 · N801GP · Doug DC871F · Nacelle/Pylon, Main FrameSDR IXXA0100007Warning Light · illuminatedEN ROUTE FROM TOL TO JFK, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO JFK FOR AN UNEVENTFUL LANDING. THE LANDINFeb 21, 2001 · N826BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA0100006Plate · damagedEN ROUTE FROM SJC TO TOL, AFTER THE LANDING GEAR WAS RETRACTED THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOLLOWING COMPANY PROCEDURES. Feb 21, 2001 · N825BX · Doug DC871F · Landing Gear Position and WarningSDR RRXA10863Door Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ACCESS HOLE 60 DOOR FRAME AT STA. 1793-1766 AND L34L-L34R, 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 & 51Feb 20, 2001 · N8091U · Doug DC871F · Fuselage Main, StructureSDR UPS01835031Battery Pack · dischargedINSPECTION TYPE:IN EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. TESTS OK.Feb 20, 2001 · N703UP · Doug DC871F · Emergency LightingSDR UPS01835018Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CHECK. REPLACED BATTERY PACK.Feb 20, 2001 · N703UP · Doug DC871F · Emergency LightingSDR RRXA010503Skin · brokenDURING A MAINTENANCE VISIT FOUND A BROKEN CORNER OF NR 2 GROUND SPOILER BAY ON LT WING NOT SPOILER, 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 57-2-0 FIG.4.Feb 18, 2001 · N8091U · Doug DC871F · SpoilersSDR RRXA010504Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H I/B FLAP TRACK COVER PANEL BETWEEN STA 960-980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DCFeb 16, 2001 · N8091U · Doug DC871F · Trailing Edge FlapsSDR RRXA010024Screw · unsecureON TAKEOFF A/C FELT UNCOORDINATED. APPLIED SOME RT TRIM, ON CLIMBOUT ON AUTOPILOT A/C STILL UNCOORDINATED. TURNED OFF CHANGE DAMPER. A/C ROLLED SHARPLY RIGHT, CHECKED RUDDER TRIM, INDICATED 5 UNITS RIGHT-WITH 2 1/2 UNITS AILERON. A/C STILL ROLLED LEFT. FOFeb 16, 2001 · N996GE · Doug DC871F · Autopilot Trim IndicatorSDR RRXA10839Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z-7, X-24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEFeb 15, 2001 · N801GP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA10806Drive Link · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H O/B FLAP CENTER DRIVE LINK AT STA. 319, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-0Feb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10805Attach Angle · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. WING REAR SPAR FLAP ATTACH FITTING AT STA. XRS98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8Feb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10802Clip · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACCESS HOLE 505D AND BETWEEN STRINGER 68 & 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AFeb 15, 2001 · N801GP · Doug DC871F · Wing Miscellaneous StructureSDR RRXA10781Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. WING FLAP IN FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITFeb 15, 2001 · N801GP · Doug DC871F · Aileron TabsSDR RRXA10751Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 4 STUB WING I/B LWR. FRONT SPAR L/E SHIM PLATE AT I/B LWR. FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.0Feb 15, 2001 · N8091U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA10750Shim · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 STUB WING I/B LWR. FRONT SPAR L/E SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01Feb 15, 2001 · N8091U · Doug DC871F · Wing Miscellaneous StructureSDR RRXA010502Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE STRESS PANEL ON SHELF (F), DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1Feb 15, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA010501Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM CENTER DOUBLER AT STA XFS 435.789, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-Feb 15, 2001 · N8091U · Doug DC871F · Fuselage Main, Plate/Skin
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