Douglas DC-8-62F

Service difficulty reports · 1,163

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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 = 'DC862F'
  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 IXXA07SMN120SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-36 CRACKED AT STATION 1100.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERNAL DOUBLER. INSTALLED NEWFeb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA07SMN116SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 798.000 AND LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING N/P IAW SRM 51-1-20D, AND SRM 51-3-1.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN115SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER PANEL CORRODED, BETWEEN STATION XE 65.158 AND XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARFeb 23, 2007 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA07SMN114SLongeron · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT LONGERON 30 RIGHT HAS IMPROPER REPAIR AT STATION 460.000. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT AND SPLICES. CLEANED,TREAFeb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA07SMN113SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME CRACKED AT STATION 759.000, LONGERON 18 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACFeb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN112SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING, INBOARD FLAP LOWER PANEL HAS A NON STANDARD REPAIR, AT STATION XW 3.000 TO XW 50.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH Feb 23, 2007 · N71CX · Doug DC862F · Trailing Edge FlapsSDR IXXA07SMN110SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER PANEL HAS CORROSION, STATION XE 221.000 AND XE 272.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDFeb 23, 2007 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN109SFitting · brokenDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT FITTING BROKEN, BETWEEN STATION 440.000 AND STATION 460.000, L-31L. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN108SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR AT STATION WX 84.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. FABRICATED NW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOFeb 23, 2007 · N71CX · Doug DC862F · Trailing Edge FlapsSDR IXXA07SMN107SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND TAIL CONE LOWER SKIN CORRODED STATION XFS 1813.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMEDFeb 23, 2007 · N71CX · Doug DC862F · Aerodynamic FairingsSDR IXXA07SMN111SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND. ELEVATOR UPPER SKIN CORRODED AT STATION XE65.158. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEFeb 23, 2007 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA070003OLine · leakingDURING CLIMB FROM FHAW, THE CREW NOTICED THE HYDRAULIC QUANTITY BEGAN DECREASING. THE CREW RAN THE HYDRAULIC LOSS OF QUANTITY CHECK LIST AND RETURNED TO FHAW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER THREE ENGINE HYJan 10, 2007 · N41CX · Doug DC862F · Hydraulic System, MainSDR IXXA06SMN436SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS422.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATEDDec 13, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN435SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD AILERON SKIN DENTED AT STATION XA694.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. BONDED REPAIR PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDDec 13, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN434SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING FITTING CRACKED AT STATION XW408.000, STRINGER 58. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED HEAT TREATMENT FROM AL7075-T651 TO AL 7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSIDec 13, 2006 · N799AL · Doug DC862F · Wing, Attach FittingsSDR IXXA06SMN433SDoubler · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND INTERNAL DOUBLER CORRODED BETWEEN STATION 1460.000 AND STATION 1480.000 AND BETWEEN LONGERON 33 RIGHT AND LONGERON 33 LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED INNER DOUBLER. FABRICATED NEW DOUBLER. CLEDec 13, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN432SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN INTERNAL SURFACE CORRODED FROM STATION XE195 2190 TO STATION XE221.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFDec 13, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN431SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN INTERNAL SURFACE CORRODED FROM STATION XE272.000 TO STATION XZ297.2347. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATEDec 13, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN430SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FITTING CRACKED AT STATION 1610.000. LONGERON 17 LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-8B DC8 SRM 51-1-20D, DC8 SRM 51-1-21, AND DC8 SRM 51-3-1.Dec 13, 2006 · N799AL · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA06SMN429SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE219.919 TO STATION XE221.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED PANEL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREADec 13, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN428SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT STATION XE77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW Dec 13, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN427SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT STATION XE28.843. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW Dec 13, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA060614OLanding Gear · out of adjustDURING CLIMB-OUT OF KCOF WHILE PERFORMING THE GEAR UPLATCH CHECK THE DOOR NOT LATCH LIGHT ILLUMINATED. THE CREW FOLLOWED PROCEDURES AND RETURNED TO KCOF AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND ADJUSTED THE MAIN GEAR FOLLOW UP MECHDec 11, 2006 · N41CX · Doug DC862F · Main Landing GearSDR IXXA06SMN426SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD LEADING EDGE UPPER SLANT PANEL CORRODED FROM STATION XFS7.000 TO STATION XW751.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION Nov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN425SPanel · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING INBOARD LEADING EDGE SLANT PANEL UPPER CAP CORRODED AT STATION XFS7.000 TO STATION XFS195.000. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED SLANT PANEL UPPER CAP. CLEANED, TREATED AND PRIMED AREA. INSTANov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN424SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP CORRODED ON LOWER ANGLE BETWEEN STATION XN24.000 AND STAXN32.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA AND FABRICATED REPAIR Nov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN423SDoubler · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING NR 2 STUB WING SLOT DOUBLER HAS ELONGATED HOLES AT STATION XS 250.000. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FNov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN422SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND THE RUDDER SKIN CRACKED AT STATION 2R 219.000 LEFT SIDE. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. BONDED NEW SKIN AND INTERNAL DOUBLER WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. APPLIED SEALANNov 17, 2006 · N799AL · Doug DC862F · Rudder, Plate/SkinSDR IXXA06SMN421SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE HAS A NON STANDARD REPAIR AT STATION XOLDI6.224. REMOVED EXISTING NON-STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRNov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN420SAngle · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP CORRODED ON LOWER ANGLE BETWEEN STATION XN24.000 AND STATION XN32.000. DC8. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA AND FABRICATNov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN419SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LEFT WING NUMBER 2 STUB WING HAS A NON STANDARD REPAIR AT STATION XS 250.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVANov 17, 2006 · N799AL · Doug DC862F · Leading Edge DevicesSDR IXXA06SMN417SAngle · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER TRAILING EDGE ANGLE CRACKED AT STATION XE29.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. STOP DRILLED CRACKED ENDS AND FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED ARENov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer StructureSDR IXXA06SMN416SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR AT STATION XS430.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMNov 17, 2006 · N799AL · Doug DC862F · Standard Practices/StructuresSDR IXXA06SMN415SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SLOT CENTRAL LEADING EDGE HAS A NON STANDARD REPAIR AT STATION XOLDI6.224. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE RENov 17, 2006 · N799AL · Doug DC862F · Standard Practices/StructuresSDR IXXA06SMN414SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LONGERON 34 RIGHT CORRODED FROM STATION 1190.000 TO STATION 1200.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRINov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA06SMN413SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE221.000 TO STATION XE270.979. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS. CLEANED, TNov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN412SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN CORRODED FROM STATION XE221.000 TO STATION XE270.979. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND STIFFENERS CLEANED, TREATNov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN411SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN CORRODED FROM STATION XE272.000 TO STATION XE301.656. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND STIFFENERS. CLEANED, TREATED AND PRNov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN410SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CORRODED FROM STATION XE29.812 TO STATION XE52.825. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN. INSTALLED NEW Nov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN409SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER UPPER SKIN DELAMINATED FROM STATION XE77.000 TO STATION XE147.906. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYINov 17, 2006 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN408SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF430.000. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. BONDED REQUIRED PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS AS NEEDED. INSTALLENov 17, 2006 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA06SMN407SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 4 STUB WING UPPER SKIN CORRODED AT STATION XF520.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVED. FABRICATED RENov 17, 2006 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA06SMN406SAccess Door · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT CENTER TANK NUMBER 505 G ACCESS DOOR CORRODED. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. ANov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN405SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER LEADING EDGE SKIN CRACKED AT STATION XA615.000. REMOVED DAMAGED LEADING EDGE. FABRICATED NEW LEADING EDGE. CLEANED, TREATED AND PRIMED AREA AND INTERNAL SURFACE OF NEW LEADING EDGE. APPLINov 17, 2006 · N799AL · Doug DC862F · AileronsSDR IXXA06SMN404SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD SERVICE DOOR UPPER FORWARD CORNER CRACKED AT STATION 225.000 LONGERON 11 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTENov 17, 2006 · N799AL · Doug DC862F · Service DoorsSDR IXXA06SMN400SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 PYLON RIGHT UPPER SKIN CRACKED AT STATION YN210.000. REMOVED LEFT SKIN. REMOVED RIGHT SIDE STRAP AND HINGE HALVES FROM RIGHT SIDE AND ATTACHING PARTS FROM PYLON STRUCTURE AS NEEDED. FABRICATED REPAIR PARTS. Nov 17, 2006 · N799AL · Doug DC862F · Nacelle/Pylon, Plate/SkinSDR IXXA06SMN399SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 2 PYLON RIGHT UPPER SKIN CRACKED AT STATION YN210.000. REMOVED LEFT SKIN. REMOVED RIGHT SIDE STRAP AND HINGE HALVES FROM RIGHT SIDE AND ATTACHING PARTS FROM PYLON STRUCTURE AS NEEDED. FABRICATED REPAIR PARTS. Nov 17, 2006 · N799AL · Doug DC862F · Nacelle/Pylon, Plate/SkinSDR IXXA06SMN386SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 PYLON LEFT UPPER SKIN CRACKED AT STATION YN225.000. REMOVED LEFT PANEL. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SERVICE BULLETIN NUMBER 54-70 DNov 17, 2006 · N799AL · Doug DC862F · Nacelle/Pylon, Plate/SkinSDR IXXA06SMN403SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE TAIL CONE EXTERIOR LOWER SKIN DAMAGED AT STATION 1730.000. REMOVED FASTENERS. FABRICATED REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER. APPLIED SEALANT TO FAYING SURFACES. INSTALLNov 17, 2006 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA06SMN385SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 4 PYLON RIGHT UPPER SKIN CRACKED AT STATION YN225.000. REMOVED LEFT SKIN. REMOVED RIGHT SIDE STRAP AND HINGE HALVES FROM RIGHT SIDE AND ATTACHING PARTS FROM PYLON STRUCTURE AS NEEDED. FABRICATED REPAIR PARTS. Nov 17, 2006 · N799AL · Doug DC862F · Nacelle/Pylon, Plate/Skin
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