N605AL, cancelled May 1, 2014

Service difficulty reports · 522

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N605AL' AND deregistration_id = 'N605AL-2014-05-01'
  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 IXXA110060OEngine · slowREJECTED TAKEOFF DUE TO ASSYMETRICAL THRUST ON TAKEOFF ROLL. THE NR 4 ENGINE SLOW TO ACCELERATE, DID NOT REACH MAX POWER. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX PREFORMED ACCELERATION CHECK, OPS CHECKED GOOD IAW ERH 72.01.1. PREFORMED REJESep 11, 2011 · N605AL · Doug DC873F · Engine (Turbine/Turboprop)SDR IXXA110049ODamper · defectiveDURING CLIMB OUT, THE CREW NOTICED AT 250 KNOTS A PULSING IN BOTH CONTROL COLUMNS. THE PULSE INCREASED THROUGH ANY PITCH CHANGE WHETHER USING THE AUTOPILOT OR MANUALLY FLYING THE ACFT (MORE NOTICEABLE PULSE). THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENJun 27, 2011 · N605AL · Doug DC873F · Elevator Control SystemSDR IXXA110043OLock Sensor · defectiveAFTER TAKEOFF, NR 2 THRUST REVERSER LIGHT WAS BLINKING. THE CREW ACTUATED THE EMERGENCY STOW PUMP BUT NO HELP. THEY RETURNED TO DEPARTURE AND UPON LANDING THE LIGHT WENT OUT. MX TROUBLESHOT THE THRUST REVERSER SYS AND FOUND RT UPPER AND LOWER THRUST REVERSEMay 30, 2011 · N605AL · Doug DC873F · Engine Thrust ReverserSDR IXXA110020OProximity Switch · defectiveAFTER TAKEOFF, WHEN MLG RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED MLG AND LIGHT REMAINED ON. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT MLG PROXIMITY SWITCH. OPERATIONAL CHECK GOOD IAW MM 32-60-0. AIFeb 11, 2011 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA110018OTarget · looseDURING CLIMBOUT, AFTER GEARS WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEARS, DOOR NOT LATCH LIGHT STILL REMAINED ON, AFTER ACCOMPLISHING UPLATCH CHECK LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH LT AFeb 9, 2011 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA110012OSwitch · contaminatedAFTER TAKEOFF, WHEN GEAR WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEAR THE DOOR NOT LATCH LIGHT STILL REMAINED ON THE ALT GEAR DOOR LIGHT REMAINED OUT. ON DECENT THE LT ALT GEAR DOOR LIGHT MOMENTARILY FLASHED ON THEN OFF. THEY Feb 3, 2011 · N605AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA100057SSkin · puncturedPUNCTURE IN LT FWD SIDE OF FUSELAGE AFT AND ABOVE OF LT ACM HEAT EXCHANGE LOUVER DOORS. REPAIRED IAW 53-10653-1. ACFT RETURNED TO SERVICE.Dec 7, 2010 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA100045OTransceiver · defectiveAFTER TAKEOFF, "TOO LOW" AUDIBLE WARNING WENT OFF WITH BOTH RADIO ALTIMETER FLAGS IN VIEW AND GPWS LIGHT ON. DUE TO FUEL AND RVSM ISSUES THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED RADIO ALTIMETER TRANSCEIVER. OPS CHECK GOOD IAW MM 3Sep 15, 2010 · N605AL · Doug DC873F · Ground Proximity SystemSDR IXXA100031OConnector · dirtyDURING CLIMB OUT NR 4 BLEED AIR SHUTOFF VALVE CLOSED CONFIRMING NO BLEED FROM ENGINE. THE CREW CYCLED SWITCH SEVERAL TIMES AND MOVED THROTTLE WITH NO HELP. ON DESCENT NR 4 BLEED AIR SHUTOFF VALVE OPENED. THEY LANDED AT DEPARTURE WITHOUT FURTHER INCIDENT. MX INMay 4, 2010 · N605AL · Doug DC873F · Pneumatic System WiringSDR IXXA100020OGuide · misinstalledDURING TAKEOFF THE CREW USED EXCESSIVE DOWNWARD FORCE ON ELEVATOR. THEY REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED ELEVATORS AND FOUND CABLE GUIDE UNDER F/O`S FLOOR (FWD) NOT PROPERLY INSTALLED, BOLT ON CABLE SECTOR DRIVE RUMar 3, 2010 · N605AL · Doug DC873F · Elevator Control SystemSDR IXXA090056OSteering Sys · lack of lubeDURING TAKEOFF FROM KLRD THE NOSE WHEEL CONTROL DID NOT RESPOND TO CONTROL WHEEL OR RUDDER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MAINTENANCE LUBRICATED NOSE GEAR SREERING SYSTEM. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENAOct 7, 2009 · N605AL · Doug DC873F · Landing Gear Steering SystemSDR IXXA090033OSeal · leakingDURING CLIMB-OUT FROM KBFI NUMBER THREE ENGINE FLAMED OUT. THE CREW ACCOMPLISHED QRH CHECKLIST, AND RESTART ATTEMPT, ENGINE WOULD NOT START. THE CREW LANDED IN KPDX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NUMBER THREE ENGINE AND FOUND FUEL LEAK ON FJun 18, 2009 · N605AL · Doug DC873F · Engine Fuel and ControlSDR IXXA09SMN066SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 220.000-240.000 LONGERON 28-31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED Apr 11, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN065SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION 480.000 LONGERON 23-24 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AREA, AApr 11, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN059SLongeron Splice · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1770.000 LONGERON 17 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW SPLICE FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.Apr 9, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN64SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SEMAN FORM-07Apr 7, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN058SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 55.000 RIGHT BUTTOCKS LINE 45. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-0Apr 7, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN055SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-4, AND DC8 SRM 51-1-8B.Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN054SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1280.000 LONGERON 35 RT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-4, AND SRM 51-1-8B.Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN057SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 65.000 LONGERON 21 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5, AND SMN-FORM-07 IPI Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN056SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 70.000 LONGERON 21 RIGHT- RIGHT BOTTOM LONE 50. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION 2003-5Apr 2, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN062SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER CAP CRACKED STATION XE 29.812. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FORM-07 IPI NUMBER 2009420.Apr 1, 2009 · N605AL · Doug DC873F · Horizontal Stabilizer StructureSDR IXXA09SMN53SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 717.000 LEFT BOTTOM LINE 1. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1.Apr 1, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN052SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT RUDDER SKIN CRACKED AT STATION ZR 71.437. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED RUDDER WEIGHT AND BAApr 1, 2009 · N605AL · Doug DC873F · Rudder, Plate/SkinSDR IXXA09SMN063SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK LUGS WORN AT STATION 1670.000-1752.000. REMOVED WORN TRACK SEGMENT AND EXISTING SPLICES. FABRICATED TRACK SEGMENT. CLEANED, TREATED, PRIMED AREA AND SEGMENT TRACK AND EXISTING SPMar 31, 2009 · N605AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA09SMN050SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35 RIGHT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN049SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED STATION 1260.000 - 1280.000 LONGERON 35LEFT. REMOVED CRACKED LONGERON. FABRICATED LONGERON, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLEDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN051SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CRACKED AT STATION 1260.000 - 1280.000 LONGERON 36. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT EXTRUSION, SPLICE, AND DOUBLER. CLEANED, TREATED, PRIMED AREA ANDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN048SLongeron · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT BILGE LONGERON CORRODED AT STATION 1490.000 - 1500.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON. FABRICATED LONGERON SEGMENT, AND SPLICES. PERFORMEDMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN047SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT LONGERON BATHTUB FITTING CRACKED AT STATION 902.125 LONGERON 5 LEFT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA90SMN046SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STATION 1230.000 LONGERON 32-33 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, AND SRM 51-3-1.Mar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN045SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 LEFT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW SRM 53-5-3 FIGURE 5 SHEET 1 IMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN044SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE LONGERON CRACKED AT STATION 1786.000 LONGERON 17 RIGHT. REMOVED CRACKED LONGERON. CLEANED, TREATED, AND PRIMED AREA. FABRICATED EXTRUSION LONGERON. INSTALLED REPAIR PART IAW DC8 SRM 53-5-3 FIGURE 5 SHEEMar 31, 2009 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA09SMN042SStiffener · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 3 ENGINE THRUST REVERSER RIGHT COWLING RAIL FITTING CRACKED AT 6 O'CLOCK POSITION. REMOVED RAIL FITTING FASTENERS. FABRICATED NEW STIFFENER. PROTECTED STIFFENER WITH CHROMIC ANODIZED. INSTALLED NEW FASTENERS,Mar 30, 2009 · N605AL · Doug DC873F · Engine Thrust ReverserSDR IXXA09SMN041SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.000 STRINGER 12. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORRMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN061SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 RIGHT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND SMN-FOMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN060SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FORWARD ACCESSORY COMPARTMENT LEFT CAP CRACKED STATION 55.000 - 70.000 LEFT BOTTOM LINE 45. REMOVED CRACKED CAP. INSTALLED NEW CAP IAW DC8 SRM 51-1-20D, SRM 51-3-1, REPAIR SPECIFICATION NR 2003-05, AND SMN-FORM-07 IPMar 30, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN039SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR FITTING CRACKED AT STATION XF 337.000. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, ATI REPAIR SMar 30, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA09SMN043SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FRONT SPAR LOWER FITTING CRACKED AT STATION XFS 60.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.Mar 30, 2009 · N605AL · Doug DC873F · Horizontal Stabilizer, Attach FittingsSDR IXXA09SMN040SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP INTERIOR HAS FITTING CRACKED AT STATION XF 411.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1, SRM 51-1-21.Mar 30, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA09SMN036SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER SKIN CRACKED AT STATION 104.000 - 122.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED REPAIR PART IAW SRM 57-7-1 FIGURE 1 ITEM "D",Mar 28, 2009 · N605AL · Doug DC873F · Trailing Edge FlapsSDR IXXA09SMN034SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN033SStructure · crackedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION EXTERIOR PRIMARY HEAT EXCHANGER AFT LOWER CORNER CRACKED AT STATION 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, StructureSDR IXXA09SMN038SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT PASSENGER DOOR FITTING CRACKED AT STATION 1621.000. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1.Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN037SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 781.500 LONGERON 13 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D DC8 SRM 51-1-8B, AND SRM 51-3-1.Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN035SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 11 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-23, SRM 51-1-20D, DC8 SRM 51-1-8B, AND SRM 51-3-Mar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA09SMN032SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERIOR LOWER SKIN CORRODED AT STATION 660.000 LONGERON 31 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AMar 27, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA09SMN030SStructure · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON MAIN CARGO DOOR FORWARD LOWER JAMB CORNER AT STATION 120.000 - 210.000 LONGERON 19-23 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. Mar 26, 2009 · N605AL · Doug DC873F · Cargo/Baggage DoorsSDR IXXA09SMN027SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD HAS IMPROPER REPAIR AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNAMar 21, 2009 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA080033OGyro · failedDURING CRUISE FROM KTOL TO KBFI, THE CAPTAINS ADI AND HSI FAILED. THE CREW DIVERTED TO KRFD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FIBER OPTIC VG/DG GYRO. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.Nov 20, 2008 · N605AL · Doug DC873F · Directional Gyro and Indicating System
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