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 IXXA09SMN082SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 912.000 LONGERON 1. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-05, SMN-FORM-07 IPI200Aug 7, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN081SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 822.000 LEFT BUTTOCK LINE 24. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-05, SMN-FORMAug 7, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN080SFitting · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 742.250 LONGERON 19 LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-1-21, DC8 SRM 51-1-8BAug 7, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN079SSupport · crackedDURING ROUTINE C CHECK INSPECTION FOUND MAIN CARGO COMPARTMENT INTERCOSTAL SUPPORT CRACKED AT STATION 857.125 LONGERON 19 LT. REMOVED CRACKED INTERCOSTAL SUPPORT. INSTALLED NEW INTERCOSTAL SUPPORT IAW DC8 SRM 51-1-20D, SRM 51-1-21, DC8 SRM 51-1-20D, SRM 51-3-1Aug 7, 2009 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA09SMN078SSkin · damagedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND INBOARD AILERON EXTERNAL LOWER SKIN PART BROKEN AT STATION XRS 624.000.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NAug 6, 2009 · N41CX · Doug DC862F · AileronsSDR IXXA09SMN076SSkin · brokenDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND OUTBOARD FLAP EXTERNAL SKIN UPPER PART BROKEN AT STATION XF 409.000.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEAug 6, 2009 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA09SMN075SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND INBOARD FLAP PANEL UPPER SKIN HAS SEVERAL DENTS AT STATION XW 2.000 - STATION XW 84.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. CLEANED, Aug 6, 2009 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA09SMN069SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XW 406.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND Aug 5, 2009 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN074SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 14 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.Aug 5, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN073SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 11 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.Aug 5, 2009 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN072SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 207.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL AND EAug 5, 2009 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN071SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND OUTER WING OUTBOARD LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 730.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN INTAug 5, 2009 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN070SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING CENTER LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 423.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANEAug 5, 2009 · N41CX · Doug DC862F · Wing, Center BoxSDR IXXA09SMN068SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 253.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDAug 5, 2009 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA090038OAntenna · defectiveDURING CRUISE, WEATHER RADAR WILL NOT PAINT AND STABILIZATION INOP. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER AND RADAR ANTENNA. OPS CHECK GOOD IAW MM 34-41-1. ACFT WAS RETURNED TO SERVICE.Aug 5, 2009 · N71CX · Doug DC862F · Weather Radar SystemSDR IXXA09SMN067SFitting · corrodedDURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CORRODED AT STA 940.000 LONGERON 24 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FITTING. FABRICATED SPLICES, DOUBLER, AND FILLERS. CLEAug 4, 2009 · N41CX · Doug DC862F · Master Cylinder/Brake ValveSDR IXXA090037OConnector · miswiredDURING CRUISE FROM WSAP WEATHER RADAR WILL NOT PAINT KNOWN WEATHER. THE CREW RETURNED TO WSAP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PINS 6 AND 9 REVERSED ON INDICATOR AND SHIELDS BROKEN. MAINTENANCE REPAIRED BROKEN SHIELDS AND CORRECTED PINS 6 AND 9 ON IAug 1, 2009 · N71CX · Doug DC862F · Navigation System WiringSDR IXXA090036OUnknown · malfunctionedDURING CLIMB OUT FROM WSAP WEATHER RADAR STABILIZATION INOP AND WILL NOT PAINT. THE CREW RETURNED TO WSAP WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED FOG GYROS AND BLEW OUT WAVE GUIDES WITH NITROGEN, CLEANED ALL ELECTRICAL CONNECTIONS ON WAVE GUIDES AND ANTEJul 30, 2009 · N71CX · Doug DC862F · Weather Radar SystemSDR IXXA090032OWire · chafedDURING CRUISE FROM FJDG, THE CIRCUIT BREAKER PANEL ABOVE R2 DOOR AT RIGHT GALLEY BEGAN TO ARC AND HAD MOMENTARY FIRE. FOUND 20 AMP CURRENT LIMITER TRIPPED AND BURNT BUT NO CIRCUIT BREAKER TRIPPED. THE CREW REMOVED POWER FROM GALLEY AND LANDED IN WSAP WITHOUTJun 11, 2009 · N71CX · Doug DC862F · Equipment/Furnishings WiringSDR IXXA090030OEngine · power lossDURING CRUISE FROM BGTL NR 2 ENGINE LOST POWER, THE ENGINE DID NOT RESPOND TO THROTTLE MOVEMENT AND THERE WAS AN AUDIBLE ENGINE STALL. THE GENERATOR DID NOT GO OFF LINE AND OIL PRESSURE LIGHT DID NOT ILLUMINATE THE IGNITION OFF. THE CREW SHUTDOWN NUMBER TWO EMay 15, 2009 · N41CX · Doug DC862F · Engine (Turbine/Turboprop)SDR IXXA090017OIndicator · defectiveDURING TAKEOFF ROLL FROM KWRI NUMBER THREE ENGINE N2 ROLLED BACK, EPR FLUCTUATED. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED N2 INDICATOR. OPERATIONAL CHECK GOOD IAW DACO MAINTENANCE MANUAL 77-12-0. AIRCApr 13, 2009 · N41CX · Doug DC862F · Engine RPM Indicating SystemSDR IXXA090011OFan · odorDURING CRUISE FROM PKWA, THE LEFT RECIRCULATION FAN EMITTED A SMOKE ODOR. THE CREW TURNED OFF LEFT RECIRCULATION FAN. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAMar 31, 2009 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA090013OControl Valve · defectiveDURING CRUISE FROM KBWI TO LPLA THE CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE ON ONE PACK. THE CREW HAD TO DESCEND TO 10,000 FEET. THE CREW LANDED IN KWRI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT FLOW CONTROL VALVE. OPERATIONAL CHECK GOOD IAW DACO Mar 28, 2009 · N41CX · Doug DC862F · Cabin Pressure Control SystemSDR IXXA090012OController · malfunctionedAT START OF DESCENT INTO PKWA PRESSURIZATION CONTROL LEVER AND OUTFLOW VALVE FROZE UP. THE CREW HAD TO DO AN EMERGENCY DESCENT, THE O2 MASK IN CABIN DROPPED WHEN ALT INCREASED TO 15000 FT. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN PKWA DEFERRMar 25, 2009 · N71CX · Doug DC862F · Cabin Pressure ControllerSDR IXXA090007OFan · smokeDURING CRUISE FROM PKWA LEFT RECIRC FAN SMOKE'S WHEN RUNNING. THE CREW TURNED OFF LEFT RECIRC FAN AND LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT RECIRC FAN. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 21-21-01. AIRCRAFT WMar 3, 2009 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA09SMN014SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN CRACKED AT STATION XE 166.312. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED Feb 23, 2009 · N799AL · Doug DC862F · Elevator, Plate/SkinSDR IXXA09SMN026SSplice · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING CENTER LEADING EDGE UPPER SPLICE CRACKED AT STATION XS 427.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED SPLICE. PERFORMED DYE PENETRANT INSPECTION. NO CRACK AND NO CORROSION FOUND. CLEANEDJan 27, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN016SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION 428.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMEDJan 27, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN022SSeat Track · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND IN PASSENGER CABIN NUMBER FOUR TRACK CORRODED AT STATION 1420.000-1564.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PJan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN021SSeat Track · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND IN PASSENGER CABIN AUX TRACK CORRODED AT STATION 1500.000-1564.000 LEFT BOTTOM LINE-11. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED, AND PRIMED AREA Jan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN020SCargo Track · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK CORRODED AT STATION 970.000 - 1020.000. REMOVED EXISTING SPLICES. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED,Jan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN019SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT CRACKED FITTING AT STATION 822.500 LONGERON 21-22 LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-3-1, ATI REPAIR SPJan 26, 2009 · N799AL · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN015SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SURFACE INTERNAL DOUBLER CRACKED AT STATION XFS 422.750. REMOVED CRACKED INTERNAL DOUBLER. FABRICATED INTERNAL DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED INJan 26, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA090003OReceptacle · shortedDURING CRUISE, FLT ENGINEER TRIED TO SEND DEPARTURE MESSAGE, BUT BOTH VHF 1 AND 2 WOULD NOT TRANSMIT. THE CREW UNPLUGGED CAPTAIN, FO, AND FLT ENGINEER MIC’S. NR 1 VHF WOULD WORK IF FO MIC WAS NOT PLUGGED IN. FO RECEIVED A SHOCK WHEN MIC WAS UNPLUGGED. THE CREWJan 26, 2009 · N41CX · Doug DC862F · VHF Communications SystemSDR IXXA09SMN025SFrame · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION RIGHT TUNNEL FRAME CORRODED AT STATION 181.000 LONGERON29-30 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED DAMAGED AREA. FABRICJan 23, 2009 · N799AL · Doug DC862F · Fuselage Main, FrameSDR IXXA09SMN018SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 980.000 - 1000.000 L23R. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. FABRICATION NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, ATIJan 23, 2009 · N799AL · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN017SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT CRACKED FITTING AT STATION 1440.000 LONGERON 21-22 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-3-1, ATI REPAIR Jan 23, 2009 · N799AL · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA09SMN013SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN CRACKED AT STATION XF 210.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED Jan 22, 2009 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA09SMN011SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SURFACE SCRATCHED AT STATION XW 120.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. Jan 22, 2009 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA09SMN010SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 105.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTJan 22, 2009 · N799AL · Doug DC862F · Trailing Edge FlapsSDR IXXA09SMN009SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LEFT SKIN CORRODED AT STATION 1540.000 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. CLEANED, TREATED, PRIMED AREA ANJan 22, 2009 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA090002OFan · defectiveDURING CRUISE FROM PKWA RIGHT RECIRCULATION FAN OVERHEATED CAUSING BURNING ODOR. THE CREW TURNED OFF RIGHT RECIRCULATION FAN, THE ODOR DISSIPATED. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT RECIRCULATION FAN. OJan 22, 2009 · N71CX · Doug DC862F · Air Distribution FanSDR IXXA09SMN024SCargo Track · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 3 TRACK LUG CORRODED AT STATION 494.000 - 570.000. REMOVED EXISTING SPLICES. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATJan 21, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN023SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 83.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND STIFFENERS. CLEANED, TREATED, PRIMED AREJan 21, 2009 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA09SMN012SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND HORIZONTAL STABILIZER LOWER FORWARD PANEL WITH STIFFENER CRACKED AT RIGHT BOTTOM LINE-10. REMOVED CRACKED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW S/B 55-15 REV 3 CONDITIONS 4, SRM 55-1-0 PAGE Jan 21, 2009 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA09SMN008SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LEFT SKIN CORRODED AT STATION 1606.000 LONGERON 28 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. CLEANED, TREATED, PRIMED AREA AND Jan 21, 2009 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA09SMN007SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE RIGHT SIDE EXTERNAL SKIN CRACKED AT STATION 1586.000 LONGERON 15-16 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLERS, INTERNALJan 21, 2009 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA09SMN005SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT CENTER LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 280.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED Jan 20, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN004SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT CENTER LEADING EDGE UPPER SKIN CORRODED AT STATION XW 253.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NJan 20, 2009 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA09SMN003SDoubler · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION BROKEN INTERNAL DOUBLER AT PNEU AIR INLET AT STATION 35.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED INTERNAL DOUBLER. FABRICATED INTERNAL DOUBLER. PERFORMED HEAT TREATMEJan 20, 2009 · N799AL · Doug DC862F · Fuselage Main, Plate/Skin
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