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 UPS06846053Shear Tie · corrodedINSPECTION TYPE:C3 HEAVY CORROSION ON SHEAR TIE AT STA 1480 L34L TO 33L. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1480 L34L TO L33L IAW DWG 5640233, AND SRM 53-4-1, 51-1-8, AND SRM 51-1-20D.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Main, StructureSDR UPS06846052Shear Tie · corrodedINSPECTION TYPE:C3 EXFOLIATION CORROSION ON SHEAR TIE AT STA 1380 L32L TO L35R. REMOVED DAMAGE SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1380 L32L TO L35R IAW DWG 5755075, AND SRM 51-1-8, AND SRM 51-1-20D.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS06846024Shear Tie · corrodedINSPECTION TYPE:CC3 SHEAR TIE AT STA 1420 L36L TO L32L HAS EXFOLIATION CORROSION. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1420 L36L TO L32L IAW DWG5640230, AND SRM 53-4-1, 53-4-1 FIG 51, AND SRM 51-1-21.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS06846023Shear Tie · corrodedINSPECTION TYPE:C3 D-PIT STA 1440 L36L TO L33L SHEARTIE HAS HEAVY CORROSION REMOVED CORRODED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1440 L36L TO 33L IAW DWG 5640231,AND SRM 53-4-1, 51-3-2,AND SRM 51-1-21Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS06846020Shear Tie · corrodedINSPECTION TYPE:C3 EXFOLIATION CORROSION ON SHEARTIE AT STA 1400 BETWEEN L35L AND L34R. REMOVED CORRODED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1400 L35L TO L34R IAW DWG 5640229, AND SRM 53-4-1, 51-3-2,AND SRM 51-1-21Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS06846019Shear Tie · crackedINSPECTION TYPE:C3 SHEARTIE AT STA 1394 L36R-33R CORRODED AND CRACKED REMOVED DAMAGED SHEARTIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEARTIE AT STA 1394 L33R-L36R IAW SRM 53-4-1 FIG 51, DWG 5641014, SRM 51-1-8, AND51-1-20D.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Internal Mounting StructureSDR UPS06845979Longeron · crackedINSPECTION TYPE:C3 LONGERON 34R CRACKED AT STA 1420. REMOVED LONG 34R IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONG 34R AT STA 1420 IAW DWG 3645937, SRM 51-1-8, AND SRM 51-1-20D.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06846091Repair · misrepairedINSPECTION TYPE:C3 DURING REPAIR SURVEY OF THE PRESSURIZED FUSELAGE, FOUND "A" PIT FWD AND AFT LWR DOOR CORNER REPAIRS NOT PER THE SRM REPAIRS. CUT OUT FUSELAGE SKIN AT L28R FWD AND AFT SIDE OF "A" PIT DOOR CUT OUT IAW SAA EA008-5320-01-A0008, FABRICATED AND Jan 5, 2006 · N718UP · Doug DC871F · Aircraft StructuresSDR UPS06846090Repair · damagedINSPECTION TYPE:C3 DURING REPAIR SURVEY OF THE PRESSURIZED FUSELAGE, FOUND 3 CATEGORY "D" REPAIRS AT STA 1742 BETWEEN L13R TO L17R EXTERNAL DOUBLERS. REMOVED 3 OLD REPAIR DOUBLERS IAW SRM 21-1-20D. CUT OUT DAMAGED AREA IAW EA 008-5330-01-A0018. FABRICATED AJan 5, 2006 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846075Fitting · crackedINSPECTION TYPE:C1 CRACKED FRAME FITTING BELOW DOOR STOP FITTING IN AFT CARGO COMPT STA 1180 AFT SIDE OF FRAME L27L. REMOVED AND REPLACED FITTING AT STA 1180, L27L IAW EO DC8-5350-7876-A, AND SRM 51-1-21, 51-1-20D. FAB`D AND INSTALLED REPAIR DOUBLER IAW EO DJan 5, 2006 · N852UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06845982Skin · crackedINSPECTION TYPE:C3 REPAIR SURVEY OF THE PRESS FUSELAGE AREA FOUND FUSELAGE EXTERIOR SKIN EXISTING DOUBLER HAS SHORT ED FASTENER AT STA 1750 L14L. REMOVED EXISTING DOUBLER IAW SRM 51-1-20D AND FOUND 2 INCH CRACK IN SKIN, CUT OUT DAMAGED AREA IAW SRM 53-02-01 FJan 5, 2006 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06845981Fitting · crackedINSPECTION TYPE:C3 L10R END FITTING CRACKED IN 60 COMPT STA 1769. REMOVED AND REPLACED LONGERON END FITTING AT STA 1769 L10R IAW 51-3-2, AND SRM 51-1-20D.Jan 5, 2006 · N718UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846123Door Seal · crackedINSPECTION TYPE:C1 LT AFT EMERGENCY EXIT AFT SEAL CRACKED AT 2 PLACES 6" BELOW UPPER CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-02 -00 FIG 009A AND DWG 5755980.Jan 4, 2006 · N702UP · Doug DC871F · Emergency ExitsSDR UPS06846082Spar Cap · crackedINSPECTION TYPE:C3 NDT FOUND CRACK ON LM LWR SPAR CAP AT LBL41.5- 47 ON VERTICAL LEG. FS 857. REPAIRED LM LWR SPAR CAP IAW SRO 8570009.Jan 4, 2006 · N718UP · Doug DC871F · Flight Compartment WindowsSDR IXXA0600002OO-Ring · failedDURING FLIGHT 817 FROM KMCO TO RATL AFTER TAKEOFF A LOSS OF HYDRAULICS OCCURED. RAN LOSS OF HYDRAULIC EMERGENCY CHECK LIST. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO RETURN TO DEPARTURE STATION KMCO AND LANDED WITHOUT INCIDENT. FOUND RIGHT AILERON CYLINDJan 4, 2006 · N829BX · Doug DC871F · Hydraulic System, MainSDR UPS06845983Cusp Web · corrodedINSPECTION TYPE:C3 RT CUSP EXTRUSION AT L21R BETWEEN STA 1020-1040, FOUND CORROSION BEYOND LIMITS IAW SRM 53-4-1 FIG 26A. CUT OUT DAMAGED AREA IAW SRM 51-3-0, FABRICATED AND INSTALLED 4 EA SPLICES, AND CUSP DOUBLER IAW DWG J060296, SRM 51-1-26 SRM 53-02-05-0,Jan 3, 2006 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06845963Finger Doubler · corrodedINSPECTION TYPE:C3 MAIN CABIN SUBFLOOR STA 880 LBL3, FINGER DOUBLER BULGING AND POSSILBLE CORROSION UNDER DOUBLER. REMOVED FINGER DOUBLER IAW SRM 51-1-21, NO CORROSION NOTED UNDER FINGER DOUBLER, FABRICATED AND INSTALLED FINGER DOUBLER IAW DWG 5645332, AND SJan 3, 2006 · N718UP · Doug DC871F · Fuselage Main, StructureSDR UPS06845942Fitting · crackedINSPECTION TYPE:C3 FRAME ATTACH FITTING CRACKED AT FS 781, L18R FWD SIDE REMOVED AND REPLACED FITTING AT FS 781, L18R IAW SRM 51-3-2, AND SRM 51-1-20AJan 3, 2006 · N718UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06845941Channel · crackedINSPECTION TYPE:C3 INSIDE NR 60 HOLE, STA 1926 5TH SUPPORT CHANNEL RT CORNER CRACKED 1/2" LONG. STOP DRILLED CRACK IAW SRM 51-1-20, FABRICATED AND INSTALLED REPAIR DOUBLER AT STA 1926 5TH SUPORT CHANNEL IAW SRM 53-5-1, AND SRM 51-1-20D.Jan 3, 2006 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06845917Doubler · corrodedINSPECTION TYPE:C3 A-PIT UNDER DOOR STA 300, L33R-L34R DOUBLER HAS EXFOLIATION CORROSION. REMOVED CORRODED DOUBLER IAW SRM 51-1-21, FABRICATED AND INSTALLED DOUBLER AT A-PIT STA 300 L33R-L34R IAW DRWG 3754065 AND SRM 51-1-20D.Jan 3, 2006 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846083Keelbeam · crackedINSPECTION TYPE:C3 KEEL BEAM UPPER WEB (SEC STRUCTURE) CRACKED AT BOTH RIB NOTCHES, LT W /W STA.960-980 VIEW FROM ACCESS HOLE WITH MIRROR. REMOVED AND REPLACED WEB IAW DWG 3651959.Jan 2, 2006 · N718UP · Doug DC871F · Fuselage Main, KeelSDR UPS06845980Fitting · crackedINSPECTION TYPE:C3 MAIN CABIN FRAME ATTACH FITTING CRACKED 2" LONG AT STA 781 L18R AFT SIDE. REMOVED FRAME ATTACH FITTING IAW SRM 51-1-20D. FABRCATED AND INSTALLED ATTACH FRAME FITTING AT STA 781 L18R IAW DWG 3750025, AND SRM 51-3-0, 51-1-8.Jan 2, 2006 · N718UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846092Skin · corrodedINSPECTION TYPE:C3 FWD ACCESSORY COMPT STA 670 BETWEEN L36 TO L35L FUSELAGE SKIN HAS HEAVY CORROSION. REMOVED CORRODED SKIN AT STA 610-779 L31L-L31R IAW SAA EA 008-5320-01-A0019, FABBED AND INSTALLED -1, -2, -3 DOUBLERS, -4. -5, -6, -7, AND -8 STRAPS, AND SKIDec 31, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06845962Longeron · crackedINSPECTION TYPE:C3 CRACK IN LOWER RADIUS OF L24R, RT W/W STA 880. STOP DRILLED CRACK IAW SRM 53-02-02, FABRICATED AND INSTALLED REPAIR ANGLES -23, AND -24 IAW DPS 7.00-1 SRM 53-02-02,51-3-2 51-1-8, AND SRM 51-1-20D.Dec 30, 2005 · N718UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS06845919Rib · crackedINSPECTION TYPE:C3, LEFT WING O/B LEADING EDGE HAS CRACKED UPPER RIB AT STA XFS 868. STOP DRILLED CRACK IAW SRM 57-02-00, FABRICATED REPAIR ANGLES AND INSTALLED ANGLES AT LEFT WING LEADING EDGE AT STA XFS 868 IAW SRM 57-02-00, 57-03-00, AND SRM 51-1-20.Dec 30, 2005 · N718UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06846043Skin · corrodedINSPECTION TYPE:C3 REMOVE AND REPLACE LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R. REMOVED AND REPLACED LWR BELLY SKIN FROM STA 1350 TO 1490, L31L TO L31R IAW SRM 51-1-21, AND SRM 51-1-20D.Dec 29, 2005 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06845918Rib · crackedINSPECTION TYPE:C3, RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 796. STOP DRILLED CRACK IAW SRM 57-03-01-0, FABRICATED REPAIR ANGLES AND INSTALLED REPAIR ANGLES AT RIGHT O/B LEADING EDGE STA XFS 796 IAW SRM 57-02-00-0, 51-1-8 AND SRM 51-1-20.Dec 29, 2005 · N718UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06845916Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 802. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE IAW SRM 57-03--01-0, AND INSTALLED REPAIR ANGLE AT RIGHT OUTBOARD LEADING EDGE WING STA XFS 802 IAW SRM 51-1-20D.Dec 29, 2005 · N718UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS06845961Skin · crackedINSPECTION TYPE:C3 R-1 DOOR FWD UPPER CORNER CRACKED 1/4" LONG. CUT OUT DAMAGED AREA IAW SRM 53-02-00, FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER AT R-1 DOOR UPPER FWD CORNER IAW SRM 53-2-0 FIG 14, 51-1-8, AND SRM 51-1-20D.Dec 27, 2005 · N718UP · Doug DC871F · Passenger/Crew DoorsSDR IXXA0500215ORadio · malfunctionedON FLIGHT 362 FROM KTOL TO KEWR NR 1 HF CONTINOUSLY ATTEMPTED TO TUNE ON ALL FREQUENCES WITH THE SAME RESULTS. THEN HF RADIO NR 2 WAS KEYED TO TUNE, THE AUTOPILOT KICKED OFF CAUSING THE AIRCRAFT TO YAW AND PITCH. DUE TO INTENDED FLIGHT PLAN, CREW ELECTED TO Dec 27, 2005 · N828BX · Doug DC871F · HF Communications SystemSDR IXXA0500196OEngine · flamed outDURING FLIGHT FROM KLRD TO KLRD LEVELING AT 17000 FT NR 1 ENGINE FLAMED OUT. ACCOMPLISHED FLAMEOUT CHECK LIST ENGINE STARTED NORMALLY. AFTER WARM UP PERIOD THROTTLE WAS ADVANCED WITH NO RESPONSE FROM ENGINE. THE ENGINE SHUTDOWN. OIL PRESSURE WENT TO 0 AT TDec 21, 2005 · N820BX · Doug DC871F · Engine (Turbine/Turboprop)SDR UPS05845875Battery Pack · inoperativeNO EMERGENCY EXIT LIGHT. INSTALLED NEW EMERGENCY LIGHT BATTERY PACK CHECKED OK PER 33-50-02-2.Dec 15, 2005 · N752UP · Doug DC871F · Emergency LightingSDR UPS05845872Battery Pack · dischargedEMERG LIGHTS BATTERY INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS GOOD REF MM 33-50-01-2.Dec 13, 2005 · N718UP · Doug DC871F · Emergency LightingSDR UPS05845871Battery Beacon · dischargedEMERGENCY EXIT LIGHTS FAIL TEST. DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW AMM 35-50-01-2. OPERATIONAL TEST GOOD. PN OFF 60-1223-5 SN OFF 248 PN ON 5708458-503 SN ON FTL31.Dec 12, 2005 · N730UP · Doug DC871F · Emergency LightingSDR IXXA0500146OMec · inoperativeDURING CLIMB FROM KTOL TO KPHL NR 1 THROTTLE HAS TO BE RETARDED APPROX 4 KNOTS WIDTH TO MAINTAIN CLIMB THRUST, AT CRUISE POWER THROTTLE IS JUST ABOVE IDLE. CREW SHUT DOWN ENGINE PRIOR TO LANDING BECAUSE UNABLE TO RETARD POWER, POSITIVE OIL PRESSURE AND QUANTITDec 8, 2005 · N820BX · Doug DC871F · Fuel Controlling SystemSDR UPS05845876Light · inoperativeFOUND COCKPIT EMERGENCY EXIT LIGHT OVER ENGINEER SEAT INOP. PERFORMED OPS CK OF EMERGENCY LIGHT SYS PER M/M 33-50-02-2, SYS OPS NML.Dec 7, 2005 · N772UP · Doug DC871F · Emergency LightingSDR IXXA0500121OUplock · lack of lubeDURING CLIMB OUT, UNSATISFACTORY UPLATCH CHECK, NOSE GEAR IS EXTENDING DURING UPLATCH CHECK. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITH NO INCIDENT. MAINTENANCE LUBED THE UPLATCH MECHANSIM AND CHECKED OPERATION OF UPLATCH BY GEAR RETRACTION. AN UPLATDec 2, 2005 · N829BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0500120OHsi · inoperativeON CLIMB-OUT FROM KTOL, FO'S ADI/HSI WAS INOP. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET C/B AND GYRO PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.Nov 29, 2005 · N829BX · Doug DC871F · Directional Gyro and Indicating SystemSDR IXXA0500118OBulb · looseDURING A TAKEOFF ROLLOUT AT 110KTS, NR 3 ENGINE OIL PRESSURE LIGHT CAME ON. TAKEOFF WAS REJECTED. OIL PRESSURE AND QUANTITY INDICATED NORMAL BUT LIGHT REMAINED ON UNTIL THE ENGINE WAS SHUTDOWN. CREW RETURNED TO BLOCKS. MAINTENANCE DEFERRED THIS IAW MEL 79-6 (CNov 22, 2005 · N828BX · Doug DC871F · Engine Indicating SystemSDR UPS05845830Battery Pack · inoperativeON PREFLIGHT, FOUND EMERGENCY EXIT LTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CKS GOOD.Nov 21, 2005 · N702UP · Doug DC871F · Emergency LightingSDR UPS05845768Tab · bindingINSPECTION TYPE:N/A ON TAXI OUT, FOUND BINDING IN ELEV COLUMN MOVEMENT. RT ELEV CNTRL TAB BINDING FOUND PLAY (WEAR) BETWEEN DRIVE TUBE & CRANK-CONTROL TAB. NEED TO ACCOMPLISH A TEST OF THE ELEV & TAB PER MM 27-30-00. WORN BOLT HOLE IN CRANK & TORQ TUBE REPANov 13, 2005 · N718UP · Doug DC871F · Elevator Tab Control SystemSDR IXXA0500238SLongeron · corrodedDURING ROUTINE C-CHECK FOUND LONGERON CORRODED AT STATION 1702 LONGERON 28 LEFT. REMOVED DAMAGED, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW COOPESA EO COO-8-53-426-04.Oct 27, 2005 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA05SMN267SSkin · elongatedDURING C CHECK INSPECTION, NR 4 PYLON UPPER PLATING HAS ELONGATED HOLES AT STA YN 254 S. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05471 DATED 10-18-05, SEMAN DWG # ED-4084 DATED 10-11-05 AND EO SEMAN # 20051341 DATED 10-18-05. REMOVED FASTENERS IAW DC8 Oct 26, 2005 · N829BX · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR IXXA05SMN266SSkin · crackedDURING C CHECK INSPECT, LT HORIZ STAB ELEVATOR UPPER SKIN CRACKED ½, XE 200.2379. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4085. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPOct 26, 2005 · N829BX · Doug DC871F · Elevator, Plate/SkinSDR UPS05845646Engine · flamed outNR 4 ENGINE FLAMED OUT IN CRUISE FLIGHT. T/S PER MM 71-00-00-1 FIG 139 SHT 1&2. REPLACED FUEL FILTER ELEMENT, RAN ENG WITH FEED & BOOST PUMP OFF, FUEL PRESS WITHIN LIMITS. ENG OPS NORMAL.Oct 26, 2005 · N706UP · Doug DC871F · Powerplant SystemSDR IXXA0500208SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENTS, REMOVED EXISTING EXTERNAL FUSELAGE DOUBLER AT STATION 1715 LONGERON 26 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW DOUBLER REPAIR AT STATION 1670 TO 1753, LONGEROct 20, 2005 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA05SMN264SSkin · unbondedDURING ROUTINE C CHECK INSPECTION, LT RUDDER TAB SKIN UNBONDED 2 AT STA ZRT 98. REMOVED DAMAGED SKIN, CORE SECTION IAW DC8 SRM 55-2-2 PART 2 PAGE 1. FAB`D REPAIR CORE PLUG (AL. HONEY COMB CORE), REPAIR DOUBLER (ALCLAD 2024 T3 0.012) IAW DC8 SRM 55-2-2 PAR 2 POct 20, 2005 · N829BX · Doug DC871F · Rudder, Plate/SkinSDR UPS05845616Battery Pack · dischargedEMERGENCY BATTERY INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CK GOOD IAW MM 33-10.Oct 18, 2005 · N752UP · Doug DC871F · Emergency LightingSDR UPS05845624Skin · crackedNR 4 PYLON O/B SKIN CRACKED APPROX 1 INCH LONG OB SIDE APPROX 6 INCHES AFT OF FWD BOX BULKHEAD. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5430-23086A. PERMANENT REPAIR WITHIN 10 FLT CYCLIES, D312151 ASSIGNED. ACCOMPLISHED PERMANENT REPAIR PER EO DC8-5430-23086Oct 17, 2005 · N744UP · Doug DC871F · Nacelle/Pylon, Plate/SkinSDR IXXA05SMN261SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, LT OUTER WING, OTBD L/E ACCESS DOOR INTERNAL DOUBLER CORRODED, XFS 847.500. REMOVED CORROSION IAW DC8 SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PG 16. REMOVED CORRODED INTERNAL DOUBLER IAW DC8 SRM 51-1-21Oct 13, 2005 · N829BX · Doug DC871F · Wing, Plate/Skin
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