Douglas DC-8-71F

Service difficulty reports · 8,938

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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"

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SDR IXXA0100055SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON FORWARD PIT LONGERON 36 BETWEEN FUSELAGE STATION 590 AND 610. REPAIR ACCOMPLISHED REMOVAL OF LONGERON SECTION, FABRICATION AND INSTALLATION OF A NEW LONGERON SECTION AND SPLICE IN ACCORDANCE WITH DOMay 17, 2001 · N822BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0100032Web · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE VERTICAL WEB IN THE RIGHT WHEEL WELL AT FUSELAGE STATION 860, RIB LINE 14. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED WEB, FABRICATION AND INSTALLATION OA NEW WEB IN ACCORDANCE WITH DOUGLAS DRAWING 565May 17, 2001 · N820BX · Doug DC871F · Fuselage Structure (General)SDR UPS01835920Seat · looseINSPECTION TYPE:N/A PILOT REPORT-CAPT SEAT LOOSE. *S/D* REMOVED AND REPLACED CAPTS SEAT, OPS CHECK GOOD IAW MM 25-11-01.May 17, 2001 · N729UP · Doug DC871F · Flight Compartment EquipmentSDR IXXA0100063SFrame · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED IN THE TAIL CONE FRAME AT FUSELAGE STATION 1992 LEFT SIDE BEHIND THE CROSS BRACE. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR ANGLES IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND May 12, 2001 · N822BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0100059SHinge Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING AILERON MECHANISM AREA LOWER SUPPORT HINGE FITTING "L" ANGLE. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF NEW REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS SMay 11, 2001 · N822BX · Doug DC871F · Wing, Attach FittingsSDR RRXA010046Doubler · corrodedDURING FCD A53-4R2 INSPECTION OF LWR FUSELAGE CORROSION. MX DISCOVERED CORROSION BEYOND LIMITS. REMOVED CORROSION , FABRICATED NEW FINGER DOUBLER AND INSTALLED PER EO 01-143 WITH APPROVED 8110-3 DATED 5/12/01.May 10, 2001 · N8076U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS01835836Engine · flamed outINSPECTION TYPE:N/A NR 4 ENGINE FLAME-OUT IN FLT. REMOVED AND REPLACED NR 4 ENG FUEL FILTER. INSPECTED INTAKE AND EXHAUST FOR FOD. NONE FOUND. MANUALLY ROTATED FAN. ROTATES FREELY. INSPECTED CHIP DETECTORS. NO DEFECTS FOUND SUMPED NR 3 AND NR 4 AND NR 4May 10, 2001 · N705UP · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA0100024Warning Light · false activationEN ROUTE FROM BDL TO IND, THE LOWER FORWARD CARGO COMPARTMENT FIRE WARNING LIGHT ILLUMINATED. THE FORWARD LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEM WAS PREVIOUSLY ON DEFERRAL IN ACCORDANCE WITH THE COMPANY APPROVED MEL 26-10. THE FLIGHT CREW FOLLOWED COMMay 9, 2001 · N821BX · Doug DC871F · Fire DetectionSDR IXXA0100058SDoubler · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING LEADING EDGE INTERIOR DOUBLER AT THE LIFT TRANSDUCER, STATION 380. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW DOUBLER IN ACCORDANCE WITH DOUGMay 8, 2001 · N822BX · Doug DC871F · Wing Main, Frame StructureSDR RRXA011044Wheel · vibrationAT ROTATION NOSE GEAR VIBRATION FELT AND METALLIC SOUND HEARD. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL ASSY IAW DC8 MM 32-41-10. OPS CHECKS GOOD.May 8, 2001 · N8085U · Doug DC871F · Wheel/Ski/FloatSDR IXXA0100057SRib · misdrilledDURING ROUTINE C-CHECK INSPECTION, MISDRILLED HOLES WERE DETECTED IN THE RIGHT WING LEADING EDGE RIB AT WING STATION 763, ACCESS PANEL 517B. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW REPAIR DOUBLER IN ACCORDANCE WITHMay 4, 2001 · N822BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA0100056SDoor Frame · damagedDURING ROUTINE C-CHECK INSPECTION, ON THE LEFT HAND AFT OVERWING EMERGENCY EXIT DOOR FRAME BOTTOM SIDE FORWARD DOOR KEEPER STOP WAS FOUND DAMAGED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED KEEPER, FABRICATION AND INSTALLATION OF NEW CLIP IN ACCORDANCE WITH DOUGLMay 4, 2001 · N822BX · Doug DC871F · Emergency ExitsSDR IXXA0100062SSkin · gougedDURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED IN THE A-PIT BASKET EXTERNAL DOOR PLATING RIGHT HAND AFT CORNER. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDMay 3, 2001 · N822BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA0100064SDoor Frame · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE C-PIT BASKET DOOR FORWARD CENTER DOOR PAN FRAME. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION OF DOOR PAN AND SPLICE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUMay 3, 2001 · N822BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA0100061SSpar Cap · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE VERTICAL STABILIZER REAR SPAR LEFT HAND CAP AT STATION ZR 265. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP. FABRICATION AND INSTALLATION OF NEW CAP IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAMay 3, 2001 · N822BX · Doug DC871F · Vertical Stabilizer, Spar/RibSDR IXXA0100060SSkin · gougedDURING ROUTINE C-CHECK INSPECTION, A GOUGE WAS DETECTED ON THE LEFT ELEVATOR UPPER SKIN AT STATION XE 176. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 55-DC8-3046May 3, 2001 · N822BX · Doug DC871F · Elevator, Plate/SkinSDR IXXA0100053SRib · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT HAND LEADING EDGE HORIZONTAL STABILIZER INBOARD SIDE INTERIOR PANEL 16TH RIB. REPAIR ACCOMPLISHED STOP DRILLED CRACK, FABRICATION AND INSTALLATION REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCMay 3, 2001 · N822BX · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR IXXA0100054SRib · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT HAND LEADING EDGE HORIZONTAL STABILIZER INBOARD SIDE INTERIOR PANEL 2ND RIB. REPAIR ACCOMPLISHED STOP DRILLED CRACK, FABRICATION AND INSTALLATION REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTMay 3, 2001 · N822BX · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS01835797Buss · openBTB-FOR SMOKE IN COCKPIT DUCT OVERHEAT LIGHT ON. SMOKE IN COCKPIT LEFT PACK TEMP GAUGE PEGGED FULL HOT. LEFT PACK WAS NEVER TURNED ON. SUSPECT LOSE OF NR 1 BUS OPENING LEFT PACK VALVE, RUN BOTH PACKS NO DEFECTS NOTED.May 3, 2001 · N706UP · Doug DC871F · Air Conditioning SystemSDR IXXA0100023Warning System · malfunctionedEN ROUTE FROM SJC TO TOL, THE LANDING GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE GEAR DOOR WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCMay 3, 2001 · N826BX · Doug DC871F · Landing Gear Position and WarningSDR IXXA0100065SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, A DENT WAS FOUND AT FUSELAGE STATION Y+1400.000 BETWEEN LONGERONS 26R AND 27R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF DOUBLER AND FILLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAMay 2, 2001 · N822BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA010045Frame · corrodedCOMPLY WITH FCD A53-4R1 INSPECTION FOR LOWER FUSELAGE CORROSION. INSPECTED LOWER FUSELAGE FOR CORROSION. FOUND CORROSION AT STA 100 L36 LEVEL 2 CORROSION. BLENDED CORROSION, BEYOND LIMITS. AIRCRAFT FERRIED TO TENNESSEE TECHNICAL SERVICES, LLC. INSPECTED TMay 2, 2001 · N8091U · Doug DC871F · Fuselage Main, FrameSDR UPS01835786Engine · flamed outNR 1 ENGINE FLAMEOUT IN CRUISE FLT THEN RESTARTED. ACCOMPLISHED TROUBLESHOOTING PROCEDURES: VISUAL INSP, ROTATION OF FAN, INSPECTED MAGNETIC CHIP DETECTORS, SUMPED FUEL TANK AND INSPECTED NR 1 ENGINE FUEL FILTER, NO CONTAMINATES NOTED. REF AMM 71-00-00 AND AMay 2, 2001 · N709UP · Doug DC871F · Powerplant SystemSDR RRXA011041Fire Loop · failedENGINE NR 1 ON TAKEOFF INTERMITTENT FIRE WARNING. AS PER QRH, ENG WAS SHUT DOWN AND FIRE LOOP TESTED. IT DID NOT RESET. DISCHARGED BOTTLE NR 1, WAITED 30 SEC, FIRE LOOP TESTED. IT DID NOT RESET, DISCHARGED BOTTLE NR 2, WAITED 30 SEC, LOOP DID NOT TEST. ALApr 30, 2001 · N801GP · Doug DC871F · Fire DetectionSDR RRXA011040Restrictor Valve · failedON/BEFORE LANDING, WITH LANDING GEAR HANDLE PLACED DOWN, DOORS WARNING LIGHT ON, LANDING GEAR UNSAFE LT MLG GREEN LIGHT NOT ILLUM. ALT DOOR LT LIGHT ON LT GEAR WOULD NOT EXTEND. RAN EMERGENCY CHECKLIST AND PERFORMED EMERGENCY LEFT GEAR UP LANDING. REMOVED AApr 26, 2001 · N8076U · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0100022Sensing Element · shortedEN ROUTE FROM TOL TO LAX, THE NUMBER TWO ENGINE FIRE WARNING SHORT CIRCUIT LIGHT ILLUMINATED INTERMITTENTLY. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE FIRE Apr 26, 2001 · N827BX · Doug DC871F · Fire DetectionSDR UPS01835706Extinguisher · leakingINSPECTION TYPE:N/A PORTABLE FIRE EXTINGUISHER LEAKING NEEDS RECHARGE. REMOVED AND REPLACED FIRE EXTINGUISHER IN COURIER AREA.Apr 24, 2001 · N713UP · Doug DC871F · Fire Bottle, PortableSDR UPS01835789Stringer · crackedINSPECTION TYPE:C1,3 RIGHT WING STRINGER 58 IS CRACKED AT XRS 172. REPAIRED STRINGER I.A.W. SRM. 57-2-2 FIG. 3DApr 24, 2001 · N707UP · Doug DC871F · Wing, Longeron/StringerSDR IXXA0100017Uplock Sensor · dirtyEN ROUTE FROM SJC TO TOL, THE LANDING GEAR UNSAFE AND DOOR WARNING LIGHTS ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING INDICATING LIGHTS EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTApr 24, 2001 · N826BX · Doug DC871F · Landing Gear Position and WarningSDR UPS01835655Smoke Detector · false indicationSMOKE DETECTOR INOP. DEF M213526 M213526 4/20 PIT 33 SMOKE DETECTOR 2ND FROM FRONT S/N 6631 FALSE WARNING REPLACED SMOKE DETER S/N OFF 6631 ON 3094 REPLACED CM, PRECAUTIONALY OPS. CHECK O.K.Apr 21, 2001 · N709UP · Doug DC871F · Smoke DetectionSDR UPS01835788Skin · crackedINSPECTION TYPE:C1,3 RIGHT WING LOWER SKIN IS CRACKED AT XRS 172 BETWEEN STRINGERS 56 & 58. REPAIRED SKIN I.A.W. 8110-3 DH SK 707-212Apr 20, 2001 · N707UP · Doug DC871F · Wing, Plate/SkinSDR UPS01835657Seal · failedINSPECTION TYPE:N/A COULD NOT MAINTAIN CABIN PRESSURE WITH BOTH PACKS ***SUPPLEMENTAL MRR*** SEALED R2 DOOR AND R1 WINDOW PRESS CHECKED GOOD IAW 21-31-00Apr 20, 2001 · N798UP · Doug DC871F · Passenger/Crew DoorsSDR UPS01835627A/C Pack · smokeLT PACK TRIP LIGHT CAME ON IN FLIGHT FOLLOWED BY A STRONG SMELL OF ELECTRICAL SMOKE. SMOKE SMELL WENT AWAY AFTER PERFORMING SMOKE OF UNKNOWN ORIGIN CHECKLIST. PERFORMED OPERATIONAL CHECK PER MM 21-60-00 ON TEMP CONTROL ON LEFT PACK SYSTEM CHECK NORMAL NO LEAApr 20, 2001 · N730UP · Doug DC871F · Cabin Cooling SystemSDR RRXA011038Warning Light · false indicationON T/O BOTH PACK TRIP LIGHTS ON. RESET ALL PACK CB'S ALSO GND RELAY CB'S. ON RETURN TO MSY FLAPS STAYED DOWN, THEN SUDDENLY CAME UP AT THAT TIME, PUSHED RESET BUTTON, PACKS RESET. INSPECTED BOTH PACKS GROUND OPERATED, OPS CHECKS GOOD. INSPECTED FLAPS. GRApr 19, 2001 · N996GE · Doug DC871F · Cabin Cooling SystemSDR RRXA011037Altimeter · defectiveF/O''S ALTIMETER STICKS AT 700 TO THOUSANDS OF FEET PER CLIMBOUT AND LEVEL FLIGHT. ON LANDING ALTIMETER STUCK AT 43,000 FT. VSI STUCK AT 1000 FPM DESCENT. RII ISOLATED STATIC LEAK TO F/O''S STATIC MANIFOLD. TIGHTENED ALL STATIC LINES AND FITTINGS AT F/O''Apr 18, 2001 · N500MH · Doug DC871F · Altimeter, Barometric/EncoderSDR IXXA0100016Swivel · leakingAFTER TAKEOFF FROM TOL, THE FLIGHT CREW NOTICE A DECLINED IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATING A RUPTURED LEFT AILERON SWIVEL GLAND. MAINTENANCE REPACKED THEApr 18, 2001 · N824BX · Doug DC871F · Hydraulic System, MainSDR RRXA10771Switch · failedDURING A MAINTENANCE VISIT FOUND UNSAFE LIGHT DAMAGE TO LT MLG UNSAFE LIGHT (RED) STAYS ON & NO L/H MLG GREEN LIGHT AFTER SEVERAL GEAR CYLES, GOT GREEN LIGHT ONLY AFTER STEEP BANKS AT LT. SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATEDApr 16, 2001 · N8091U · Doug DC871F · Landing Gear Position and WarningSDR UPS01835590Skin · crackedRT WING STATION 172.000 INBD OF NR 3 ENGINE. SKIN CRACKED RT WING LOWER SURFACE, SKIN CRACKED AT WS 172 AFT OF CENTER SPAR. JUST 8 INCHES I/B OF NR 4 MAIN TANK MID FUEL DRAIN VALVE. AREA (APPROX 7 1/4 INCHES) PERFORMED INTERIM REPAIR OF RT INNER WING AFT BOTApr 13, 2001 · N707UP · Doug DC871F · Wing, Plate/SkinSDR IXXA0100013Uplock · dirtyEN ROUTE FROM BRO TO TOL, THE LANDING GEAR UNSAFE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR,Apr 13, 2001 · N823BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR UPS01835643Skin · crackedINSPECTION TYPE:C2,3 LEFT HORIZONTAL STAB. L/E. SKIN IS CRACKED AND DENTED BEYOND LIMITS XFS 150. REPAIRED SKIN I.A.W. SRM. 55-2-1 FIG. 4Apr 11, 2001 · N797UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS01835562Aileron · lack of lubeAILERONS STIFF. INSPECTED AILERON CONTROL SYSTEM AND FOUND AILERONS IN NEED OF LUBE. LUBRICATED AILERONS IAW 27-10-06 AND PERFORMED AILERON SYS ADJ/TEST IA W MM 27-10-00. AILERONS CHECKED NORMAL OK FOR SERVICEApr 11, 2001 · N748UP · Doug DC871F · Aileron Control SystemSDR UPS01835561Structure · crackedCRACK IN WING STRUCTURE AFT OF LEFT MLG REF DC8-5720-14401-A D213157 COMPLETE AT NEXT C CHECK UPS01835548 VOIDED DUE TO DUPLICATION OF MRRApr 11, 2001 · N702UP · Doug DC871F · Wing Main, Frame StructureSDR UPS01835548Structure · crackedMX INSP-CRACK IN WING STRUCTURE JUST AFT OF LEFT MLG STRUT, MRR FILED AS OPEN.Apr 11, 2001 · N702UP · Doug DC871F · Wing Main, Frame StructureSDR RRXA10728Web · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LEFT WING I/B FLAP WEB AT XCW64 (EO), 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 EO 01-104.Apr 9, 2001 · N996GE · Doug DC871F · Trailing Edge FlapsSDR RRXA10727Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING SKIN AT STA XFS 463 AND STR 63, 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 EO 01-195.Apr 5, 2001 · N997GE · Doug DC871F · Wing, Plate/SkinSDR RRXA10726Stringer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO STR 63 RT WING AT STA XFS 463, 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 57-2-2 FIG 3D.Apr 5, 2001 · N997GE · Doug DC871F · Wing, Longeron/StringerSDR UPS01835680Floorbeam · corrodedINSPECTION TYPE:C2,3 STA. 140 FLOORBEAM IS CORRODED BEYOND LIMITS BETWEEN RBL. 50 AND RBL. 60. REPAIRED FLOORBEAM I.A.W. 8110-3 APPROVED DH SK 779-363Apr 5, 2001 · N797UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS01835594Rib · crackedINSPECTION TYPE:C2,3 LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 327. REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2Apr 4, 2001 · N797UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS01835494Seal · leakingPBE. IN FLIGHT DECK HAS AIR TIGHT SEAL BROKEN. R & R PBE IN FLIGHT DECK AS REQ''''D. OK FOR SERVICE. S/NApr 3, 2001 · N729UP · Doug DC871F · Emergency EquipmentSDR UPS01835771Doubler · crackedINSPECTION TYPE: C2,3. RIGHT WING OB L/E. INTERNAL WRAPAROUND DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-21Apr 2, 2001 · N797UP · Doug DC871F · Wing, Plate/Skin
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