Douglas DC-8-62

Service difficulty reports · 2,778

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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 = 'DC862'
  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 RRXA991563Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB PAN SKIN BETWEEN STA 1240 AND STA 1280, AND BETWEEN LONGERONS 31 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATJul 9, 1999 · N993CF · Doug DC862 · Fuselage Main, Plate/SkinSDR RRXA991561Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AT DOOR JAMB TORQUE BOX FITTING AT STA 490, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING Jul 8, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R334ARTube · missingFLT 2823 - CABIN SMOKE DETECTOR LINES AND END FITTINGS NOT INSTALLED. FABRICATED AND INSTALLED SMOKE DETECTOR TUBES AND FITTINGS IAW AS ELEVEN DWG AS 11045 WITH APPROVED FAA FORM 8110-3 DATED APRIL 27, 1999 APPROVED BY FAA ATLANTA CERTIFICATION OFFICE LETTER Jul 8, 1999 · N1808E · Doug DC862 · Smoke DetectionSDR 99T64R350ARSpar · crackedRIGHT WING LOWER FORWARD TANG OF FRONT SPAR OUTBOARD OF STATION XFS 515, 3 HOLES CRACKED. REMOVED NUT CHANNEL IAW DC-8 SRM 51-1-21. REAMED HOLES, EDDY CURRENT HOLES, NO DEFECTS. INSTALLED BUSHING IAW BOEING MESSAGE XXX-MEM-99-0007RR. (M)Jul 7, 1999 · N1808E · Doug DC862 · Wing SparSDR 99T64R370ARDuct · wornNR 2 ENGINE STARTER SUPPLY DUCT BADLY WORN. WELDED DUCT IAW BOEING MESSAGE M7200-99-05-0359. (M)Jul 7, 1999 · N1808E · Doug DC862 · Engine Start Valves/ControlsSDR 99T64R343ARGuide · brokenRIGHT WING INBOARD LEADING EDGE OUTBOARD END HAS CABLE GUIDE (PHENOLIC BLOCK) BROKEN. APPLIED EPOXO 88 TWO PART EPOXY WITH AN ADDITIONAL 4 FASTENERS PER EO 99-061. (M)Jul 7, 1999 · N1808E · Doug DC862 · Leading Edge Slat Control SystemSDR RRXA991562Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO DOOR JAMB TORQUE BOW FITTING AT STA 500, BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALJul 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R386ARFitting · damagedNR 2579 - REMOVE FLAP CANOE FITTING AT STATION XF340, HOLE ELONGATED. REMOVED FLAP CANOE FITTING AT STATINO XF340 IAW DC-8 MM 27-51-12. REPLACED FLAP CANOE FITTING IAW DC-8 MM 27-51-12, SB27-260 R2 AND BOEING MESSAGE M-72-99-04220. (M)Jul 7, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR T64R387ARCover · puncturedARROW AIR - NR 2073, LEFT HORIZ STABILIZER T/E OUTBOARD DAMPER WELL HOLE PUNCHED THROUGH. REMOVED DAMPER WELL COVER IAW DC-8 SRM 51-1-21, WELDED HOLE PER EO 99-061 AND REINSTALLED IAW DC-8 SRM 51-1-21. (M)Jul 5, 1999 · N1808E · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR RRXA991546Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 36 AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3648359. (CORROSION DAMAGJul 2, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA991545Intercostal · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO INTERCOSTAL BETWEEN STA 1240 AND STA 1280, AT WL 4 RIGHT, AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTJul 2, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA990701Wheel · failedCLO - FLT 627 - INBOURND TO CALI, MESSAGE THAT MLG TIRE HAD SEPARATED FROM AIRCRAFT ON TAKEOFF FROM QUITO, ECUADOR. AIRCRAFT LANDED IN CALI WITHOUT INCIDENT. INSPECTION FOUND NR 2 MLG OUTBOARD WHEEL HALF BEAD HAD SEPARATED AND TIRE EJECTED. INCURRED DAMAGE Jun 27, 1999 · N1804 · Doug DC862 · Wheel/Ski/FloatSDR 99T64R283ARDuct · crackedNR 3050 - NR 3 TURBO COMPRESSOR OIL COOLING DUCT CRACKED. WELDED CRACK IAW BOEING MESSAGE M-7200-99-05081. ARROW AIR (M)Jun 25, 1999 · N1808E · Doug DC862 · Engine Oil CoolerSDR 99T64R258ARDuct · crackedNR 0161 - CSD OIL COOLER DUCT CRACKED AT FORWARD MOUNTING FLANGE ENG S/N 670982 NR 4 POSITION. WELDED CRACK IAW BOEING ENGINEERING MESSAGE M-7200-99-05081 WITH APPROVED FAA FORM 8110-3 DATED 6-21-99. REF: ARROW AIR, ARWA. (X)Jun 25, 1999 · N1808E · Doug DC862 · Engine Oil CoolerSDR 99T64R367ARPanel · corrodedRIGHT OUTBOARD INBOARD SLOT PANEL HAS CORROSION XS 442.185. REMOVED CORROSION AND BLENDED AREA IAW EO 99-061. (M)Jun 24, 1999 · N1808E · Doug DC862 · Leading Edge DevicesSDR ARWA990602Engine · failedSJU - FLT 601 - CLIMBING-OUT THROUGH 16000 FT AT 1302Z, NR 4 ENGINE LOUD BANG ALL PARAMETERS ERRATIC. COMPLETED APPROPRIATE CHECK LISTS. DUMPED FUEL TO MAX LANDING WEIGHT. RETURNED TO TJSJ WITHOUT INCIDENT. CUASE OF FAILURE CONTINUES. REMOVAL AND REPLACEMEJun 22, 1999 · N802BN · Doug DC862 · Engine (Turbine/Turboprop)SDR IXXA9900011Compressor · defectiveEN ROUTE FROM WRI TO COF, AN ODOR WAS SENSED IN THE COCKPIT ACCOMPANIED BY A LOUD NOISE EMITTING FROM THE NUMBER THREE TURBO COMPRESSOR. THE FLIGHT CREW SECURED THE TURBO COMPRESSOR AND THE ODOR SUBSIDED. MAINTENANCE PLACED THE TURBO COMPRESSOR ON DEFERRAL AJun 21, 1999 · N21CX · Doug DC862 · Cabin Compressor SystemSDR RRXA991530Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INNER SKIN BETWEEN STA 480 AND STA 580, AND BETWEEN LONGERONS 34 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEJun 19, 1999 · N993CF · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R243ARAccess Door · crackedNR 1066 - ACCESS DOOR STA 1380 BENT AND CRACKED (PLEXIGLASS CRACKED). FABRICATED NEW ACCESS DOOR PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-10-99. REF: ARROW AIR, ARWA. (X)Jun 17, 1999 · N1808E · Doug DC862 · Accessory Compartment DoorsSDR 99T64R341ARAngle · misinstalledMAIN CARGO DOOR UPPER JAM INSTALLATION Z ANGLE INCORRECTLY INSTALLED STATION 450. DOES NOT EFFECT THE INTEGRITY OF THE DOOR. NO CORRECTIVE MEASUREMENTS NECESSARY IAW DWG AS11048. (M)Jun 15, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R241ARFrame · crackedNR 0762 - 6 INCH CRACK IN NR 3 PYLON CAP FORMER (HORSE COLLAR) FORWARD SECTION STA YN161. FABRICATED REPLACMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR - ARWA. (X)Jun 15, 1999 · N1808E · Doug DC862 · Nacelle/Pylon, Frame/Spar/RibSDR RRXA991542Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DJun 12, 1999 · N993CF · Doug DC862 · Fuselage Main, FrameSDR 99T64R383ARSkin · gougedNR 0907 D-PIT DOOR CUTOUT - SKIN FORWARD LOWER EDGE GOUGED. CUT OUT DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS, AND INSTALLED PER EO 99-048 AND 99-061 WITH APPROVED FAA FORM 8110-3 DATED JUNE 14, 1999. REF: ARROW AIR, ARWA. (X)Jun 9, 1999 · N1808E · Doug DC862 · Fuselage Main, Plate/SkinSDR 99T64R252ARSkin · damagedNR 2392 - LEFT INBOARD FLAP WEDGE, DAMAGED SKIN LOWER STA XW 47. FABRICATED NEW LOWER SKIN LEFT INBOARD FLAP WEDGE PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X)Jun 9, 1999 · N1808E · Doug DC862 · Trailing Edge FlapsSDR 99T64R349ARDuct · chafedHEAVY CHAF MARK NR 3 ENGINE STARTER DUCT 10 OCL POS. FABRICATED DOUBLERS AND WELDED ON DUCT IAW BOEING MESSAGE M-7200-99-04226. (M)Jun 7, 1999 · N1808E · Doug DC862 · Engine Start Valves/ControlsSDR 99T64R346ARAngle · damagedCLEAN INSPECT REPAIR AS NECESSARY ALL SIDE RAIL SYSTEM. CUT OUT DAMAGED AREAS FABRICATED ANGLE TIERNAY AND INSTALLED PER AS 11040. (M)Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R337ARBeam · mismanufacturedMAIN CARGO DOOR JAM AFT JAM AFT BEAM INBOARD LEAG TO SHORT. FABRICATED DOUBLER SHIM/SPACER IAW EO DWG AS 11042. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED IAW EO AS11042 AND DC-8 SRM 51-1-21 WITH APPROVED FAA FORM 8110-3 DATED MAY 12, 1999. (M)Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991559Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 RIGHT, AT STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 5754184. (CORROSIJun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA991558Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME AT STA 1250 AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME IAW DC8 SRM 53-4-1, FIGURE 52. (CORROSIONJun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, FrameSDR RRXA991557Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 34 LEFT, BETWEEN STA 1240 AND STA 1260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA991555Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1240 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8 SRM 53-2-0, FIGURE 2Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991554Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DCJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991553Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 33 LEFT AND 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-2Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991552Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1220, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991551Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DCJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991550Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1200, BETWEEN LONGERONS 35 LEFT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC8Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991547Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO LONGERON 35 RIGHT AT STA 1280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DAC DRAWING 3646937. (CORROSIONJun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA991544Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE AT STA 1235, BETWEEN LONGERONS 33 RIGHT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ENW SHEAR TIE Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991543Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO SHEAR TIE BETWEEN STA 1220 AND STA 1240, AND BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLEJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991538Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FRAME ATTACHMENT ANGLE AT STA 580, BETWEEN LONGERONS 33 LEFT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991537Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 560, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRMJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991534Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 34 RIGHT AT STA 580. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC8 SRM 53-1-20 FIGURE 1. (CORROSIJun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR RRXA991532Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 540, BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRMJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991531Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO FITTING AT STA 500, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755827. (CORROSION DAMJun 7, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA991529Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION TO LONGERON 32 RIGHT, BETWEEN STA 460 TO STA 600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON 32 RIGHT BY CLAD PLATING AND INSTALLED IAW DC8 SRM 51-1-21Jun 7, 1999 · N993CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR 99T64R336ARBeam · shortFLT 2851 - MAIN CARGO DOOR FORWARD JAMB - FORWARD BEAM INBOARD LEG TOO SHORT. FABRICATED DOUBLER SHIMS IAW EO DWG AS11042, TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW EO DWG AS11042 AND DC-8 SRM 51-1-21. WITH APPROVED FAA FORM 8110-3 DATED MAY 1Jun 7, 1999 · N1808E · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R265ARSpar · corrodedNR 2841 - LT WING REAR SPAR HAS 4 EACH AREAS OF CORROSION BETWEEN XRS 139-172. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)Jun 7, 1999 · N1808E · Doug DC862 · Wing SparSDR RRXA991536Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, TO ATTACHMENT ANGLE AT STA 500, LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT ANGLE IAW DC8 SRM 5-1-20Jun 6, 1999 · N993CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 99T64R345ARSpar · corrodedLT WING AFT SPAR HAS 7 EACH AREAS OF CORROSION AT XRS 190. REMOVED CORROSION, FABRICATED SPECIAL WASHERS AND DOUBLERS AND INSTALLED PER EO 99-061. (M)Jun 4, 1999 · N1808E · Doug DC862 · Wing SparSDR 99T64R368ARDoor · corrodedFORWARD RIGHT O/W EXIT DOOR CORROSION WINDOW FRAME INTERNAL STATION 730. REMOVED CORROSION FILLED WITH HYSOL EA 9309NA. FAIRED TO ORIGINAL THICKNESS. TREATED AND FINISHED IAW DC-8 SRM 51-1-8 PER EO NR 99-061. (M)Jun 3, 1999 · N1808E · Doug DC862 · Emergency Exits
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