Douglas DC-8-62F

Service difficulty reports · 1,163

Newest first. General aviation reporting is voluntary.

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 ARWA20030315Stiffener · crackedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR W/W STA 857 AND XCW51 PRESSURE BULKHEAD STIFFENER UPPER SECTION ANGLE WITH CRACK. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED REINFORCEMENT IAW DC8 SRM 53-2-0, PRIMMar 15, 2003 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA20030314Angle · crackedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND, AFT LOWER CARGO COMPARTMENT STA 1280, FLOOR PANEL ANGLES (02 EACH) CRACKED. REMOVED ANGLES IAW DC8 SRM 51-1-21, FABRICATED NEW ANGLES IAW DC8 SRM 51-1-4, PRIMED NEW ANGLES IAW DC8 SRM 51-1-8 AND INSTALLED NEWMar 15, 2003 · N791AL · Doug DC862F · Fuselage Miscellaneous StructureSDR ARWA20030313Bulkhead · crackedDURING C-CHECK, THE FOLLOWING WAS FOUND, RADOME BULKHEAD WEB LOWER SECTION WITH CRACKS, STA 44. CUT OUT DAMAGED AREA, FABRICATED STRAP AND FILLER IAW DC8 SRM 53-2-0, PRIMED PARTS IAW DC8 SRM 51-1-8 AND INSTALLED PARTS IAW DC8 SRM 53-2-0.Mar 15, 2003 · N791AL · Doug DC862F · Fuselage Main, BulkheadSDR ARWA20030312Cargo Track · brokenDURING C-CHECK, THE FOLLOWING WAS FOUND; MAIN CARGO DOOR COMPARTMENT STA 420, LBL 50 TRACK WITH BREAKAGE. CUT AWAY DAMAGED SECTION OF TRACK IAW DC8 SRM 53-2-3, PREPARED A NEW SECTION OF TRACK AND FABRICATED SPLICES IAW DC8 SRM 53-2-3, PRIMED PARTS IAW DC8 SRMMar 15, 2003 · N791AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0300001OIndicator · malfunctionedAFTER DEPARTURE FROM BWI CREW NOTICED FIRST OFFICERS HORIZONTAL SITUATION INDICATOR WOULD NOT ROTATE. CREW DIVERTED TO WRI FOR AN UNEVENTFUL LANDING. MAINTENANCE REPLACED INSTRUMENT AMPLIFIER AND FIRST OFFICERS HORIZONTAL SITUATION INDICATOR IAW WITH THE AIRJan 3, 2003 · N31CX · Doug DC862F · Integrated Flight SystemSDR IXXA0200107SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT STATION 922 AND LONGERON 20L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUALAug 19, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA0200106SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE STATION 902 STRINGER 11. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND DRAWING Q95-RAug 19, 2002 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA0200105SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FUSELAGE STATION 742.250 LONGERON 21R BELOW FORWARD EMERGENCY DOOR. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FINGER DOUBLER AND DOUBLER IN ACCORDANCE WITHAug 13, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA0200104SWindow Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FOURTH LEFT CABIN WINDOW FRAME FUSELAGE STATION 490 LONGERON 16L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUJul 31, 2002 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA0200103SWindow Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FIRST LEFT CABIN WINDOW FRAME FUSELAGE STATION 300 LONGERON 16L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW DOUGLAS SRM.Jul 31, 2002 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA0200102SStructure · damagedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND DENTS WERE DISCOVERED ON THE C-3 DOOR SCUFF PLATE. REPAIR ACCOMPLISHED, REMOVAL OF SCUFF PLATE AND DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPLER AND NEW SCUFF PLATE IN ACCORDANCE WITHJul 23, 2002 · N41CX · Doug DC862F · Cargo/Baggage DoorsSDR IXXA0200101SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FORWARD COMPARTMENT DOOR CUT OUT LOWER CORNER AFT SECTION. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF BELLY SKIN FROM STATION 270 TO 390 IN ACCORDANCE WITH THE DOUGLASJul 20, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA0200100SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SKIN STATION 1000 LONGEORN 19L. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLAION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEEJul 20, 2002 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA0200111SDrain Mast · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE BASE OF THE DRAIN MAST AT STATION 1574 LONGERON 28R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAJul 18, 2002 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA0200099SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE AT FUSELAGE STATION 1030 LONGERON 21R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND ENGINEERING DRAWING 53-02491-3.Jul 18, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA0200110SFrame · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE AFT TAIL COMPARTMENT RT CIRCUMFERENTIAL FRAME, AFT AND ABOVE ACCESS PANEL 62 ZONE 37. REPAIR ACCOMPLISHED, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL Jul 16, 2002 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA0200108SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON A SCREW HOLE ON THE LEFT WING OUTBOARD LEADING EDGE STA XFS 710. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTJul 16, 2002 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA0200098SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE AT XW 485. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND EXTERNAL DOUBLER IAW THE DOUGLAS SRM.Jul 16, 2002 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA0200097SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED UNDER AN EXISTING REPAIR ON THE FUSELAGE AT STATION 1530 LONGERON 21L TO LONGERON 21R. REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA AND EXISTING DOUBLER, FABRICATION AND INSTALLATION OF NEW REJul 16, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA0200096SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE OUTBOARD XW488. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW THE DOUGLAS SRM AND EA 28298-5269-02-129Jul 16, 2002 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA0200095SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE FUSELAGE STATION 1210 LONGERON 19L FORWARD OF THE AFT EMERGENCY EXIT DOOR. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND DRJul 16, 2002 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR ARWA20020705O-Ring · defectiveAPPROXIMATELY ONE AND HALF (1.5) HOURS AFTER TAKE OFF, HYDRAULIC QUANTITY DROPPED TO THE STAND PIPE. FOUND DEFECTIVE O-RING ON ENGINE DRIVEN PUMP PRESSURE LINE FITTING RT ENGINE DRIVEN PUMP. REMOVED AND REPLACED O-RING IAW MM 29-10-12; OPS CHECKED NORMAL ON Jul 16, 2002 · N810BN · Doug DC862F · Hydraulic System, MainSDR IXXA0200093SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RUDDER TRAILING EDGE ABOVE THE TAB. REPAIR ACCOMPLISHED, REMOVED SURFACE CORROSION IAW THE DOUGLAS SRM.Jul 14, 2002 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA0200094SSkin Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE PANEL BY THE NUMBER FOUR PYLON. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND DRAWING 57-0249Jul 13, 2002 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA0200042OLinkage · bindingEN ROUTE FROM QPG THE FLIGHT CREW NOTICED THE CABIN PRESSURIZATION COULD NOT BE MAINTAINED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES WITH NO EVAL AND RETURNED TO QPG FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE OUTFLOW Jul 1, 2002 · N799AL · Doug DC862F · Cabin Pressure Control SystemSDR RRXA11159Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO EXTERIOR SKIN AT STA.1220 AND L25R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-1 FIMay 18, 2001 · N996CF · Doug DC862F · Fuselage Main, Plate/SkinSDR RRXA11157Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.560 AND L34L-L35L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53May 13, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11156Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.520-560 AND L35L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-May 13, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11155Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO PIT L28L AT STA.510-560, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-2 FIMay 10, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11154Skin · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO R/H O/B SLOT VANE O/B END HAS SCREWS PULLING THRU SKIN, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW May 9, 2001 · N996CF · Doug DC862F · Wing, Plate/SkinSDR RRXA11153Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO F/E AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG#5888367.May 9, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11152Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA.540 AND L34L-L35L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2D, 51-1-20D.May 9, 2001 · N996CF · Doug DC862F · Fuselage Main, Attach FittingsSDR RRXA11151Rub Strip · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO RT WING L/E O/B SLOT VANE ATTACH FITTING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 5769857-1.May 9, 2001 · N996CF · Doug DC862F · Wing Miscellaneous StructureSDR RRXA11150Support · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H UPPER SUPPORT INSIDE THE R/H REFRIGERANT CONDENSOR DOOR AREA AT STA208 AND LBL44, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIMay 9, 2001 · N996CF · Doug DC862F · Fuselage Structure (General)SDR RRXA11149Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA500 AND L29L-L30L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-May 5, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11148Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING LOWER SKIN FAST HOLES IN THE AREA SURROUNDING THE 3 O/B FASTNERS OF STRINGER 64L END FITTING AT STA. XRS543.2 AND STR 64, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SMay 5, 2001 · N996CF · Doug DC862F · Wing, Plate/SkinSDR RRXA11143Seat Track · brokenDURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO SEAT TRACK AT STA.1420-1470 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-7-2 FMay 5, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11142Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.1330 AND LBL26-LBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-7-2 FIMay 5, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11139Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD SERVICE DOOR AFT FRAME LWR FITTING AT STA.390 AND L21R, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLMay 4, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11138Fitting · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO L/H WING EXHAUST GATE OUTBOARD FITTING, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, May 4, 2001 · N996CF · Doug DC862F · Wing, Control SurfacesSDR RRXA11137Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO D-PIT DOOR LOWER FRAME, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG#5649820.May 4, 2001 · N996CF · Doug DC862F · Cargo/Baggage DoorsSDR RRXA11136Door Frame · tool damageDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO MCD JAMB DOOR FRAME AT STA330 AND L17L-L21L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-743.May 4, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11135Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO O/B FLANGE AT STA.500-560 AND L29L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-2May 3, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11134Seat Track · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SEAT TRACK AT STA.870-915 AND LBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG1May 3, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11133Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA.910-1050 AND LBL50, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3May 3, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11158Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA.460-560 AND L36, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-2 FIG4May 1, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11144Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO EXTERIOR SKIN AT STA.203 AND L16L, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 996-493.May 1, 2001 · N996CF · Doug DC862F · Fuselage Main, Plate/SkinSDR RRXA11127Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.345-350 AND LBL25, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG14Apr 30, 2001 · N996CF · Doug DC862F · Fuselage Main, StructureSDR RRXA11126Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FWD CARGO PIT CROSS SLIDE DOOR JAMB BACK UP FITTING NR 1 LWR TEE BOLT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 5Apr 30, 2001 · N996CF · Doug DC862F · Fuselage Main, Attach FittingsSDR RRXA11125Seat Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA.825-990 AND RBL46, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0,Apr 30, 2001 · N996CF · Doug DC862F · Fuselage Main, Structure
Back to Douglas DC-8-62F