Douglas DC-8-62F

Service difficulty reports · 1,163

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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 = 'DC862F'
  ORDER BY difficulty_date DESC"

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SDR IXXA08SMN029SSplice · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL SPLICE CRACKED AT STATION 879.375. REMOVED FASTENERS AS TO PERFORM REPAIR. REMOVED CRACKED SPLICE. FABRICATED NEW SPLICE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALJan 22, 2008 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN028SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 420.000 STRINGER 5. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR APPLIED SEALANT ON BLEND Jan 22, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN021SSkin · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CABIN COMPARTMENT SKIN WORN AT STATION FS 340 L21L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTENT REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION DETECTED AFTER Jan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN019SSkin · wornDURING ROUTINE C CHECK INSPECTION, FOUND OUTER FUSELAGE WORN AT STATION FS 443.000 L21L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTENT REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION DETECTED AFTER INSPECTIONJan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN023SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTER FLAP LOWER PANEL SKIN DENTED AT STATION 164.000 TO STATION XF 186.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITJan 19, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA080009SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT STATION 485.000 LONGERON 26 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGE AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATED REPAIR DOUBLER, ANJan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN027SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT STATION 485.000 LONGERON 25 RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGE AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATED REPAIR DOUBLER, ANJan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN026SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 702.000 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0 AND SRM 51-3-1.Jan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA08SMN025SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 822.500 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACKED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-3-1,Jan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA08SMN024SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 759.000 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACK FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0 AND SRM 51-3-1.Jan 19, 2008 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA08SMN022SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING DENTED AT UPPER LEADING EDGE AT STA XFS 7.5000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK, NO CORROSION FOUND. PERFORMED MEASUREMENT DIAMETER FOUND WITHIN ALLOWABLE LIMITS APPLIED PRO-SEAL 735 IAW DC8Jan 19, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN018SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION CRACKED AT PNEUMATIC AIR INLET DOOR FRAME INNER REVERSE. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED FILLER AND DOUBLER. CLEANED, TREATED AND PRIMED AREA, ANDJan 15, 2008 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA08SMN017SFlange · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT COWLING AFT FLANGE CRACK STATION YN 181.000. REMOVED SPLICE CRACKED. FABRICATED SPLICE. CLEANED, TREATED AND PRIMED REPAIR PART INSTALLED REPAIR PART IAW DC8 SRM 51-1-21, DC8 SRM 54-3-2 FIGURE 33, BOEING MESSAGJan 15, 2008 · N41CX · Doug DC862F · Nacelle/Pylon Miscellaneous StructureSDR IXXA08SMN016SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 278.000 STRINGER10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. FILLED WITH SEALANT REWORKED AREA. PERFORMED NDJan 15, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN015SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 358.000 -371.000, STRINGER 5 TO STRINGER 8. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. FAJan 15, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA080008SSupport · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO PANELS SUPPORT CRACK AT STATION 460 LONGERON 29LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED ANGLE DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS Jan 15, 2008 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA08SMN014SSkin Panel · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO PANELS SUPPORT CRACK AT STATION 460 LONGERON 30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED ANGLE DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERSJan 15, 2008 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA08SMN005SPanel · crackedDURING ROUTINE C CHECK INSPECTION, FOUND WING FUSELAGE PANEL NUMBER 716 FILLET PANEL RIGHT SIDE CRACKED AT STATION 690.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOLJan 14, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN007SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING JOINT FLAP DELAMINATED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. REMOVED CORE AND CLEANED AREA. INSTALLED CORE AND NEW FASTENERS AND REPAIRED PARTS IAW DC8Jan 14, 2008 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA08SMN006SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING JOINT FLAP DELAMINATED SKIN. REMOVED DAMAGED JOINT FLAP. INSTALLED NEW JOINT FLAP IAW DC8 SRM 51-3-0, 51-3-1.Jan 14, 2008 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA08SMN003STab · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CONTROL TAB AILERON DELAMINATED. REMOVED REPLACE AILERON CONTROL TAB IAW DC8 MM 27-11-4 PAGES 201-205, PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS GOOD IAW DC8 MM 27-11-0 PAGES 10-14, DC8 MM 27-21-0 PAGES 5-9,Jan 14, 2008 · N41CX · Doug DC862F · Aileron TabsSDR IXXA08SMN002SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING CENTER LEADING EDGE OUTER LOWER SKIN AT STATION XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREJan 11, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA08SMN001SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER SKIN CENTRAL LEADING EDGE CRACKED AT STATION XF 428.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION DETECTED AFTER TEST. FABRJan 11, 2008 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA070048OPitot Tube · damagedDURING CLIMB-OUT FROM PHIK, THE CREW NOTICED THE PITOT HEATER INOP LIGHT ILLUMINATED, ZERO AMPS INDICATED ON THE FIRST OFFICER'S PITOT TUBE POSITION. THE CREW RETURNED TO PHIK, MADE 50 DEGREES FLAP EMERGENCY OVERWEIGHT LANDING AND LANDED WITH OUT INCIDENT. MSep 11, 2007 · N71CX · Doug DC862F · Pitot/Static SystemSDR IXXA070044OUplock · stiffDURING CRUISE FROM PHIK BOTH MAIN GEAR DOORS OPENED DURING UPLATCH CHECK, THE CREW CYCLED THE GEARS THREE TIMES REQUIRED TO GETTING A VALID UPLATCH CHECK. THE CREW LANDED AT KSUU WITHOUT INCIDENT. MAINTENANCE INSPECTED MAIN GEAR DOORS AND FOUND BOTH UPLATCH OVAug 24, 2007 · N799AL · Doug DC862F · Landing Gear Retraction/Extension SystemSDR IXXA070042OFire Loop · malfunctionedDURING TAKEOFF FROM TAPA, THE NUMBER TWO FIRE WARNING INDICATION LIGHT AND BELL CAME ON, THE LIGHT AND BELL WENT OUT WHEN THE CREW RETARDED POWER LEVERS TO IDLE. THE CREW RETURNED TO BLOCKS AT TAPA WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER TWO LOWER Aug 22, 2007 · N41CX · Doug DC862F · Fire DetectionSDR IXXA070041OFan · failedDURING CRUISE FROM PKWA, THE CREW DETECTED A BURNING ODOR IN COCKPIT. LEFT RECIRC FAN BECAME NOISY, THE CREW TURNED OFF THE RECIRC FAN AND ODOR WENT AWAY. THE CREW LANDED IN PHIK WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT RECIRC FAN IAW DC MAINTENANCE MANUAug 21, 2007 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA070034ODoor · unlockedDURING TAKEOFF FROM WSAP AT SIXTY KNOTS, THE DOOR WARNING LIGHT (MASTER WARNING) ILLUMINATED. THE CREW ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO BLOCKS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND R-2 DOOR UNLOCKED. MAINTENANCE RESECURED THE DOOR ANJul 17, 2007 · N71CX · Doug DC862F · Passenger/Crew DoorsSDR IXXA070033OLanding Gear · malfunctionedDURING CLIMB OUT FROM OBBI, THE CREW FELT VIBRATION FROM NOSE GEAR AREA AFTER GEAR RETRACTION. THE CREW CYCLED THE GEAR AND STILL FELT VIBRATION. THE CREW RETURNED TO OBBI WITH OUT INCIDENT. MAINTENANCE INSPECTED NOSE GEAR AREA AND FOUND LEFT NOSE GEAR DOORJul 3, 2007 · N799AL · Doug DC862F · Nose/Tail Landing GearSDR IXXA070031OClamp · brokenDURING CLIMB FROM KTOL NR 1 ENGINE ANTI-ICE LIGHT ILLUMINATED, OIL PRESSURE LIGHT FLICKERED, EGT DROPED TO 270°C, LOW PRESSURE PNEUMATIC CONTROL CIRCUIT BREAKER POPPED, ENGINE GENERATOR FAIL LIGHT ILLUMINATED WHILE VOLTS AND FREQUENIES WERE NORMAL. CLIMB POWERJun 4, 2007 · N799AL · Doug DC862F · Ice/Rain Protection SystemSDR IXXA070026OLine · leakingDURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANITY STARTED DROPPING RAPIDLY TOWARD EMPTY. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND PRESSURE FLEX LINE LEAKING AT NUMBER TWO ENGINE DRIVEN HMay 15, 2007 · N71CX · Doug DC862F · Hydraulic System, MainSDR IXXA070025OPump · leakingDURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANTITY DECREASING. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE RUDDER HYDRAULIC PUMP WAS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THMay 15, 2007 · N71CX · Doug DC862F · Hydraulic Pump (Electric/Engine), MainSDR IXXA070028OAudio Panel · defectiveDURING FLIGHT FROM RJTY THE CREW SMELLED SMOKE, THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPENED THE SMELL OF SMOKE STOPPED. THE CREW LANDED IN WSAP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S AUDIO SELECT PANEL IAW DACO DC8 MAINTENANCApr 24, 2007 · N71CX · Doug DC862F · Communications SystemSDR IXXA070027OSpeaker · defectiveDURING TAXI OUT AT WSAP, THE CREW SMELLED SMOKE, THEN THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPEN, THE FIRST OFFICER'S OVER HEAD SPEAKER WAS HOT TO TOUCH, THE CREW RETURNED TO BLOCK WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S OVERHEAApr 20, 2007 · N71CX · Doug DC862F · Interphone/Passenger Announcement (PA) SystemSDR IXXA070020OTransceiver · defectiveDURING FLIGHT FROM KSUU, THE CREW NOTICE THAT BOTH NR 1 AND NR 2 HF TRANSCEIVER WAS NOT TRANSMITTING OR RECEIVEING. THE CREW RETURNED TO KSUU WITHOUT INCIDENT. MAINTENANCE FOUND BOTH NR 1 AND NR 2 HF TRANSCEIVER WERE INOP. MAINTENANCE REPLACED BOTH HF TRANSApr 8, 2007 · N71CX · Doug DC862F · HF Communications SystemSDR IXXA070019OHf Comm · defectiveDURING FLIGHT FROM KBWI THE NR 1 AND NR 2 HF SYSTEM FAILED. THE CREW DID ALL NECESSARY PROCEDURES AND RETURNED TO KBWI LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 AND NR 2 HF SYSTEM, RESEATED THE NR 1 HF SYSTEM OPERATIONAL CHECK GOOD. REPLACED NMar 24, 2007 · N41CX · Doug DC862F · HF Communications SystemSDR IXXA07SMN131SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND HORIZONTAL STABILIZER ELEVATOR UPPER SKIN CORRODED FROM STATION XE 149.000 TO XE 222.875.REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER BONDED REPAIR Feb 23, 2007 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA07SMN130SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND LT HORIZONTAL STABILIZER ELEVATOR LOWER SKIN CORRODED & UNBONDED, BETWEEN STATION XE 77.000 & XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDEDFeb 23, 2007 · N71CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA07SMN129SPanel · corrodedDURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER, T/E LWR PANEL, CORRODED STA XE 149.906 - STA XE 220.343. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DFeb 23, 2007 · N71CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA07SMN128SSkin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING OUTBOARD SECTION LEADING EDGE HAS A NONE STANDARD REPAIR DOUBLER AT STATION XFS 710. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND AFTER NDT Feb 23, 2007 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA07SMN127SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 STUB WING SKIN LOWER PART HAS A NON STANDARD REPAIR AT STATION XFS 562.5. REMOVED EXISTING NON STANDARD REPAIR. PERFORMED STOP HOLE ON CRACK END. FABRICATED EXTERNAL DOUBLER AND INTERNAL DOUBLER. PERFORMEFeb 23, 2007 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA07SMN126SBeam · crackedDURING ROUTINE C CHECK INSPECTION, MAIN CARGO UPPER FLANGE BEAM WITH CRANK 1" AT STA 1540.000 RBL 39". PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 8,12 TR NR 51-130 DATE 01/26/04. REMOVED FASTENERS IAW SRM 51-1-21, CUT DAMAGED AREA AND FABRICATED NEW FFeb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, StructureSDR IXXA07SMN125SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, MAIN CARGO BATHTUB FITTING SHOWS CRACK 2" AT STA 1530, L26R. REMOVED AND REPLACED MAIN CARGO BATHTUB FITTING AT STA. 1530.000 L-26R (P/N 4641324U501) IAW DC8 SRM 51-1-21.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN124SFitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND MAIN CARGO BATHTUB FITTING CRACKED AT STATION 1530 L34L. REMOVED AND REPLACED BATHTUB FITTING. IAW DC8 SRM 51-1-21.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN123SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT WING OTBD L/E OUTER SECTION SHOWS 1" CRACKED AT STA XFS 885.000 (NEAR EXISTING REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 07110 DATE 03/14/07, SEMAN DRAWING NR ED-4463. DATE 02-15-07 AND EO SEMAN NR 2007221 DFeb 23, 2007 · N71CX · Doug DC862F · Wing, Plate/SkinSDR IXXA07SMN122SSplice · corrodedDURING ROUTINE C CHECK INSPECTION, NR 4 ALT TANK SPLICES FITTING SHOW CORROSION OUT OF LIMITS AT STA XRS 435 NEAR S60. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. REMOVED CORRODED SPLICE FITTING IAW DC8 Feb 23, 2007 · N71CX · Doug DC862F · Wing Main, Frame StructureSDR IXXA07SMN121SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-35 RIGHT CRACKED AT STATION 1100.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERNAL DOUBLER. INSTALLFeb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA07SMN119SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED ON FITTING AT STATION 781.000 LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN117SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 781.000 RIGHT BOTTOM LINE 24". REPLACED FITTING IAW SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1, EO NUMBER 53-DC8-2235.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA07SMN118SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 759.000, LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, AND EO NUMBER 53-DC8-2235.Feb 23, 2007 · N71CX · Doug DC862F · Fuselage Main, Attach Fittings
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