Douglas DC-8-62

Service difficulty reports · 2,778

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC862'
  ORDER BY difficulty_date DESC"

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SDR IXXA201308180280Bleed Valve · malfunctionedCOMPRESSOR STALL AT APPROX 75 KNOTS. SUSPECT NR 1 AND 2 ENGINES. RAN NR 1 AND 2 ENGINES IAW ENGINE RUN HANDBOOK 70.01. FOUND NR 1 ENGINE PRESSURE RATIO BLEED CONTROL VALVE WILL NOT CLOSE ABOVE 64 PERCENT N1. R & R PRESSURE RATIO BLEED CONTROL VALVE IAW MM 75Aug 18, 2013 · N41CX · Doug DC862 · Compressor Bleed ValveSDR IXXA20130202002OLink · inoperativeON CLIMBOUT, AFTER A GOOD UPLATCH CHECK, HEARD A LOUD NOISE IN NOSE GEAR AREA. (SOUNDED LIKE A NOSE GEAR DOOR POPPED OPEN). R & R RT NLG DOOR FORWARD LINK ASSY IAW MM 32-22-1. OPS CHECKS GOOD ON NOSE GEAR SWING.Feb 2, 2013 · N41CX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR IXXA2013020700006Skin · crackedRT WING UPPER SKIN CRACKED AT XRS 22.750 S17. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIGURE 8. TRIMMED OUT CRACK ON RT WING UPPER SKIN IAW SRM 57-2-1. FABRICATED DOUBLER 0.190", FILLER 0.200" IAW SRM 57-2-1. CLEANED, TREATED AND PRIMED FABRICATED PARTS AND Dec 5, 2012 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA2013020700005Panel · damagedRT WING OTBD FLAP LOWER PANEL WITH SEVERAL DENTS AND SCRATCHES XF 415 - 452. PERFORMED MAJOR REPAIR IAW SRM 57-7-1, FIG 4, TR 57-94. REMOVED OTBD FLAP LOWER PANEL IAW SRM 51-3-0. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21. FABRICATED NEW PANEL PLATING 0Nov 23, 2012 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA2013020700004Fitting · corrodedAFTER CARGO COMPARTMENT - INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000, L-32R (AFTER PART). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, NOV 15, 2012, DWG ED-5546 NOV 15, 2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING (Nov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA2013020700003Fitting · corrodedAFTER ACCESSORY COMPARTMENT INTERIOR BATHTUB FITTING CORRODED AT STA 1530.000 L-34R (AFTER PART). PERFORMED MAJOR REPAIR IAW FORM 8110-3 DWG NR ED-5546 NOV 15,2012. REMOVED CORRODED FITTING IAW SRM 51-1-20D, SRM 51-1-21. FABRICATED FITTING AL 7075T651 IAW DWNov 12, 2012 · N41CX · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA2013020700002Skin · corrodedRUDDER SKIN-LT PANEL SHOWS CORROSION FROM STA ZR 140.750 TO STA ZR 150.750. PERFORMED MAJOR REPAIR IAW SRM 55-6-1, FIG 1. REMOVED EXISTING DAMAGED PANEL IAW SRM 51-1-21, SRM 55-1-0. FABRICATED NEW PANEL PLATING 0.016" AND BONDED DOUBLER 0.016" BOTH FROM AL 2Nov 9, 2012 · N41CX · Doug DC862 · Rudder, Plate/SkinSDR IXXA121109SMN026SLongeron · crackedLONGERON 24R, HORIZONTAL LEG CRACKED 2 INCHES AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5 TR 53-123. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-20D.Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA121109SMN025SLongeron · crackedLONGERON 24L, HORIZONTAL LEG CRACKED 1 INCH AT FS 879.375. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 5, TR 53-123.Nov 9, 2012 · N41CX · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA2013020700001Skin · damagedRT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. TRIMMED OUT DAMAGED AREA IAW DWG ED-5545 NOV 14, 2012. FABRICATED DOUBLER 0.071" FILLER 0.063" BONov 6, 2012 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA20120706017OLock · lack of lubeHAD A DOOR NOT LATCH LAMP ON DURING UPLATCH CHECK. UNSATISFACTORY UP LATCH, BOTH ALTERNATE DOOR LIGHTS DID NOT COME ON AFTER RECYCLE OF THE LANDING GEAR. JACKED ACFT IAW MM 7-11-0. PERFORMED OPS CHECK OF MLG IAW MM 32-30-0 FOUND RT MAIN GEAR DOOR LOCK MECHAJul 6, 2012 · N799AL · Doug DC862 · Landing Gear Position and WarningSDR RRXA001532Frame · damagedDURING A MAINT VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT. FS 1340 AND L21R TO L21L, DAMAGE EXCEEDED LIMITATIONS IAW SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EOJan 21, 2008 · N994CF · Doug DC862 · Fuselage Main, FrameSDR IXXA08SMN013SFrame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT CRACK ON FRAME FLANGE AT STATION 240.000 LONGERON 21RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME. FABRICATED FRAME AND SPLICE AND ANGLE PERFORMED HEAT TREATMENT. Jan 15, 2008 · N41CX · Doug DC862 · Fuselage Main, FrameSDR IXXA08SMN012SDoor · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED DAMAGED DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MAINTENANCE MANUAL 32-12-1 PAGE 401, DC8 27-10-0, 27-20-0, 27-40-0Jan 15, 2008 · N41CX · Doug DC862 · Landing Gear DoorsSDR IXXA08SMN011SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) MIDDLE DOOR DELAMINATED SKIN. REMOVED DELAMINATED DOOR. INSTALLED NEW MID DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MM 27-10-0, 27-20-0, 27-40-0, 27Jan 15, 2008 · N41CX · Doug DC862 · Landing Gear DoorsSDR IXXA08SMN010SDoor · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED RIGHT MAIN LANDING GEAR OUTBOARD DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MAINTENANCE MANJan 15, 2008 · N41CX · Doug DC862 · Landing Gear DoorsSDR IXXA08SMN009SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) MIDDLE DOOR, DELAMINATED SKIN. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN CENTER DOOR ON RIGHT MAIN LANDING GEAR FUSELAGE. PERFORMED OPERATIONAL CHECK FOR HYD SYSTEM LEAKS, GOOD IAW DC8 MINATEJan 15, 2008 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA08SMN008SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER DELAMINATED. REMOVED DAMAGED SPOILER. INSTALLED NEW RIGHT SPOILER IAW DC8 MAINTENANCE MANUAL 27-60-1 PAGES 201-207. PERFORMED OPERATIONAL CHECK TO ALL FLIGHT CONTROLS, GOOD IAW DC8 MAINTENJan 15, 2008 · N41CX · Doug DC862 · SpoilersSDR IXXA08SMN004SPanel · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER PANEL DELAMINATED AT STATION XF 219 TO XF 339.000. REMOVED DAMAGED PANEL. INSTALLED NEW PANEL IAW DC8 SRM 51-3-0, 51-3-1.Jan 14, 2008 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA070043OB-Nut · looseDURING CRUISE FROM KBWI NUMBER THREE ENGINE OIL QUANITY SLOWLY DECREASED UNTIL INDICATING ZERO. PRESSURE AND TEMPERATURE REMAINED NORMAL UNTIL THE OIL PRESSURE BEGAN TO FLUCTUATE APPROXIMATELY 15 PSI WITH NR 3 OIL PRESSURE LIGHT COMING ON AND OFF. THE CREW SHAug 23, 2007 · N41CX · Doug DC862 · Turbine Engine Oil SystemSDR IXXA070036OFuel Control · malfunctionedDURING CRUISE FROM WSAP TO RJTY NR 1 ENGINE LOST POWER EPR REDUCED 1.2 AND FUEL FLOW DECREASED 1000 POUNDS PER HOUR. THE CREW PERFORMED THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE ENGINE, THE AIRCRAFT LANDED AT RJTY WITHOUT INCIDENT. MAINTENANCE INSPECTEDAug 1, 2007 · N799AL · Doug DC862 · Fuel Controlling SystemSDR IXXA07SMN106SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "A" DOOR AFT LOWER JAMB CORNER CRACKED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND, AFTER TRIM OUT. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER. CLEANED, TREATED Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, StructureSDR IXXA07SMN105SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STATION XS 515.720 AND XS 520.168. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSFeb 8, 2007 · N71CX · Doug DC862 · Leading Edge DevicesSDR IXXA07SMN104SVane · damagedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HOLES ELONGATED, BETWEEN STATION XOLDI 6.225 AND XS 435.789. REMOVED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. Feb 8, 2007 · N71CX · Doug DC862 · Trailing Edge FlapsSDR IXXA07SMN103SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETWEEN STATION XFS 710.000 AND XFS 716.250. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK Feb 8, 2007 · N71CX · Doug DC862 · Wing, Plate/SkinSDR IXXA07SMN102SSkin · brokenDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP, UPPER SKIN BROKEN AT STATION XCW 64.000. REMOVED DAMAGED PANEL PLATING. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND PANELFeb 8, 2007 · N71CX · Doug DC862 · Trailing Edge FlapsSDR IXXA07SMN101SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR, AT STATION XW 115.000. REMOVED PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND PLATINFeb 8, 2007 · N71CX · Doug DC862 · Trailing Edge FlapsSDR IXXA07SMN100SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING, OUTBORD FLAP UPPER SKIN NON STANDARD REPAIR, AT STATION XF 210.000. REMOVED PANEL PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CFeb 8, 2007 · N71CX · Doug DC862 · Trailing Edge FlapsSDR IXXA07SMN099SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA.. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FAFeb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN098SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME, CRACKED AT STATION 759.000, LONGERON 18 LEFT. REMOVED FASTENERS. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSION FOUND. FABRICATEFeb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA07SMN097SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XOLDI 6.225. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. Feb 8, 2007 · N71CX · Doug DC862 · Leading Edge DevicesSDR IXXA07SMN096SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XS 520.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. Feb 8, 2007 · N71CX · Doug DC862 · Wing, Plate/SkinSDR IXXA07SMN094SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND CORROSION AT STATION XFS 178.750. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGEFeb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN095SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER FITTING ANGLE CRACKED AT STATION XFS 60.000. REMOVED DAMAGED FITTING ANGLE. CLEANED, TREATED AND PRIMED. INSTALLED NEW FITTING ANGLE IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM Feb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Attach FittingsSDR IXXA07SMN093SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR, AND REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSFeb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN092SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FOUND. FABRICATED NEWFeb 8, 2007 · N71CX · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN091SPanel · misrepairedDURING ROUTINE C CHECK INSPECTION, LEFT WING OUTBORD AILERON LOWER PANEL NON STANDARD REPAIR, BETWEEN STATION XA 650.000 AND XA 693.000. REMOVED SKIN WITH EXISTING NON STANDAR REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSFeb 8, 2007 · N71CX · Doug DC862 · SpoilersSDR IXXA07SMN090SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED SKIN WITH EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AFeb 8, 2007 · N71CX · Doug DC862 · Standard Practices/StructuresSDR IXXA07SMN089SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT UPPER SKIN CORRODED AT STATION 1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA Feb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA07SMN088SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SKIN CORRODED AT STATION XFS1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED ARFeb 8, 2007 · N71CX · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA070004OFiber Optic Gyro · precessesAPPROXIMATELY 1.5 HOURS AFTER TAKEOFF FROM WSAP THE NR 2 COMPASS STARTED PROCESSING AT THE RATE OF 60° TO 70° PER HOUR, DG MODE PROCESSING AT THE RATE OF 25° PER HOUR. THE CREW ELECTED TO RETURN TO WASP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AND CLEJan 26, 2007 · N799AL · Doug DC862 · Directional Gyro and Indicating SystemSDR IXXA06SMN418SFitting · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CORRODED AT STATION 530.000 RBL 45. REMOVED CORRODED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING FROM 7075-T651 TO 7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED, TRNov 17, 2006 · N799AL · Doug DC862 · Fuselage Main, Attach FittingsSDR IXXA06SMN373SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CORRODED AT STATION XE127.960. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN PANEL. FABRICATED NEW SKIN PANEL AND FINGER DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREANov 10, 2006 · N799AL · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR IXXA06SMN355SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD STUB WING UPPER SKIN CORRODED AT STATION XFS246.000 REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER FILLERS AND STRAP. TREATED REPAIR AREA AND REPANov 10, 2006 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA06SMN350SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER FASTENERS INSTALLED ON THE LEFT OUTBOARD AILERON EXTERNAL LOWER SKIN FROM STATION XA542.000 TO STATION XA566.000. REMOVED IMPROPER FASTENERS AND FOUND SKIN DAMAGED. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN ANNov 4, 2006 · N799AL · Doug DC862 · AileronsSDR IXXA06SMN347SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND FITTING CRACKED AT STATION 742.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. HEAT TREATED NEW FITTING FROM 7075-T651 TO 7075-T6. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. CLEANED,Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Miscellaneous StructureSDR IXXA06SMN346SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FITTING CRACKED AT STATION 857.000, LONGERON 19 RIGHT. REMOVED CRACK FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1 AND DC8 SRM 51-1-8B.Nov 4, 2006 · N799AL · Doug DC862 · Fuselage Miscellaneous StructureSDR IXXA06SMN339SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING SKIN CORROSION AT STATION XF803.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. AFTER DAMAGE REMOVAL. FABRICATED REPAIR PARTS, Nov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA06SMN352SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS341.500. REMOVED FASTENERS AS NEEDED TO REMOVE CORROSION. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION, NO Nov 4, 2006 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA06SMN351SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN DENTED AT STATION XA558.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED BOTH PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND NEW SKIN INTERNAL SURFACNov 4, 2006 · N799AL · Doug DC862 · Ailerons
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