N602AL, cancelled May 29, 2014

Service difficulty reports · 377

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 = 'N602AL' AND deregistration_id = 'N602AL-2014-05-29'
  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 IXXA110082OConnector · looseDURING UPLATCH CHECK, DOOR NOT LATCH LIGHT CAME ON. THE CREW CYCLED MAIN GEARS TWICE AND DOOR NOT LATCH LIGHT REMAINED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOORS AND FOUND THE LT GEAR DOOR SWITCH CONNECTOR LOOSE AND DIRTY. MDec 21, 2011 · N602AL · Doug DC873F · Landing Gear System WiringSDR IXXA110081OConnector · dirtyDURING CLIMB OUT, AFTER GEAR RETRACTION, DOOR NOT LATCH LIGHT REMAINED ON. CREW CYCLED MAIN GEAR AND LIGHT REMAINED ON. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAIN GEAR DOOR UPLATCH SWITCHES AND FOUND THE RT MAIN GEAR DOOR SWITCH CONNECTOR DIRTY. CLEADec 20, 2011 · N602AL · Doug DC873F · Landing Gear System WiringSDR IXXA110037OControl Tube · dirtyAT FLIGHT LEVEL 370, THE NR 2 ENGINE POWER ROLLED BACK FROM 94 PERCENT TO 87 PERCENT WITH A CORRESPONDING DROP IN EGT AND N2. THE PMC FOR NR 2 ENGINE WAS SWITCH OFF AND NR 2 ENG ROLLED DOWN MORE TO 50 PERCENT N1 AND 400 DEGREE EGT. THE CREW SHUTDOWN NR 2 ENGINMay 5, 2011 · N602AL · Doug DC873F · Engine (Turbine/Turboprop)SDR IXXA110024OWheel · dirtyDURING TAKE OFF ROLL THE CREW HAD NO DIRECTIONAL CONTROL OF AIRCRAFT, THE CREW ABORTED TAKEOFF AND THE AIRCRAFT CAME TO A REST WITH THE NOSE GEAR OFF THE RUNWAY. THE AIRCRAFT WAS TOWED BACK TO BLOCKS. MAINTENANCE ACCOMPLISHED REJECTED TAKEOFF INSPECTION, REPLAFeb 22, 2011 · N602AL · Doug DC873F · Wheel/Ski/FloatSDR IXXA110007OControl Valve · defectiveDURING CRUISE, DOOR NOT LATCHED, RED LIGHT ON WITH GEAR UP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED LT MLG DOOR CONTROL VALVE. OPS CHECK GOOD IAW MM 32-32-7. ACFT WAS RETURNED TO SERVICE.Jan 22, 2011 · N602AL · Doug DC873F · Landing Gear Retraction/Extension SystemSDR IXXA110002OMechanism · out of adjustDURING CLIMB OUT, THE DOOR NOT LATCH LIGHT CAME ON WITH GEAR RETRACTED. THE CREW CYCLED AND ACCOMPLISHED UPLATCH CHECK AND DOOR NOT LATCH LIGHT REMAINED ON. THEY RETURNED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT MAIN LANDING GEAR FOLLOW UP MECHANIJan 13, 2011 · N602AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA110001OWarning Switch · arcedDURING CLIMB OUT, THE "DOOR NOT LATCH" LIGHT CAME ON WITH LANDING GEAR RETRACTED. THE CREW CYCLED GEAR AND ACCOMPLISHED UPLATCH CHECK, DOOR NOT LATCH LIGHT REMAINED ON THE REMAINDER OF FLIGHT. LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND FLUID COJan 12, 2011 · N602AL · Doug DC873F · Landing Gear Position and WarningSDR IXXA10SMN114SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E LOWER SKIN HAS IMPROPER REPAIR AT STA XW 730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATNov 13, 2010 · N602AL · Doug DC873F · Wing, Plate/SkinSDR IXXA10SMN113SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 902.000 LONG 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-1.Nov 11, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN112SWeb · crackedDURING ROUTINE C-CHECK INSP FOUND NR 3 MAIN TANK WEB CRACKED AT STATON XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FINov 11, 2010 · N602AL · Doug DC873F · Fuel StorageSDR IXXA10SMN111SSkin · damagedDURING ROUTINE C-CHECK INSP FOUND LT WING T/E UPPER SKIN DOUBLER WITH IMPROPER REPAIR AT STA XW 736.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANNov 11, 2010 · N602AL · Doug DC873F · Wing, Plate/SkinSDR IXXA10SMN110SSpar Cap · crackedDURING ROUTINE C-CHECK INSP, FOUND NR 3 MAIN TANK LOWER CTR SPAR CAP AND WEB CRACKED AT STA XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLERNov 11, 2010 · N602AL · Doug DC873F · Wing SparSDR IXXA110039SFloor Panel · corrodedDURING ROUTINE C-CK INSP FOUND MAIN CARGO COMPARTMENT FLOOR PANEL SKIN CORRODED BETWEEN STA 1060.000 LT BOTTOM LINE10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLERS AND FILNov 10, 2010 · N602AL · Doug DC873F · Fuselage Floor PanelSDR IXXA10SMN109SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT SECTION FLOOR LONGERON 36 CORRODED AT STA 1690.000 - 1725.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON AND STRAPS. CLEANED, TREATED, PRIMED ARENov 10, 2010 · N602AL · Doug DC873F · Fuselage Structure (General)SDR IXXA10SMN108SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 781.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRNov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN107SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 857.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRNov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN106SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 1160.000, LONGERON 20RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53Nov 10, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN105SFitting · crackedDURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 717.000 LT BOTTOM LINE 22. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN104SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 700.000, LT BOTTOM LINE 23. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN103SFitting · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 - 980.000 RT BOTTOM LINE 28. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51Nov 9, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN102SSkin · delaminatedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 77.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATEDNov 9, 2010 · N602AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA10SMN101SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 132.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATENov 9, 2010 · N602AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA10SMN115SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND LT WING L/E LOWER PART CORRODED ST STATION XFS 335.250 - 341.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. FABRICATED DOUBLER AND FILLERS. CLEANED, TREANov 6, 2010 · N602AL · Doug DC873F · Wing, Plate/SkinSDR IXXA10SMN100SSkin · brokenDURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPER SKIN BROKEN AT STA XW 107.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIRNov 6, 2010 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA10SMN099SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN CORRODED AT STA XF 407.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITHNov 6, 2010 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA10SMN098SFitting · corrodedDURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT STATION 879.375, LONGERON 24LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREANov 3, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN097SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CRACKED AT STATION 920.000, LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, FILLERS, AND DOUBLERS. CLEANED, TREATED, PRINov 3, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA10SMN096SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND CRACKED FITTING AT STA 857.000 & 879.000 LONGERON 24LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP DRILL END OF CRACKS. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED INTERNAL AND EXTERNAL DNov 2, 2010 · N602AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA100047OFire Loop · defectiveDURING CRUISE, NR 2 ENGINE FIRE WARNING CAME ON AT FL270 SAT -52. THE CREW SHUTDOWN THE NR 2 ENGINE, WHILE PASSING THROUGH 14,000 FT THE ACFT WAS EXPERIENCING SOME TURBULANCE AND NR 2 FIRE WARNING AND SHORT CIRCUIT LIGHTS ILLUMINATED. CREW DISCHARGED BOTH FIRSep 23, 2010 · N602AL · Doug DC873F · Fire DetectionSDR IXXA100043OSensor · defectiveDURING TAKEOFF, THE MAX AIRSPEED WARNING LIGHT AND CLACKER CAME ON. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED THE OVERSPEED LIMIT SENSOR. OPS CHECK GOOD IAW MM 34-11-0. ACFT WAS RETURNED TO SERVICE.Aug 26, 2010 · N602AL · Doug DC873F · Airspeed/Mach IndicatorSDR IXXA100039OIndicator · defectiveDURING CLIMB OUT, STANDBY ATTITUDE INDICATOR INOPERATIVE, THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ATTITUDE INDICATOR. OPS CHECK GOOD IAW MM34-28-0. ACFT WAS RETURNED TO SERVICE.Aug 12, 2010 · N602AL · Doug DC873F · Attitude and Direction Data SystemSDR IXX2008F00089Switch · inoperativeFLIGHT ATN 802, DURING CRUISE FROM KTOL, GEAR DOOR NOT LATCHED LIGHT CAME ON INTERMITTENT. THE CREW ACCOMPLISHED ABNORMAL CHECK 3-13-01. THE CREW LANDED IN KLAX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BAD MAIN LANDING DOOR SWITCH. MAINTENANCE REPLACED Jul 30, 2008 · N602AL · Doug DC873F · Landing Gear Position and WarningSDR IXX2008F00021Connector · damagedFLT NR: ATN 842/KTOL TO KPHL. DURING CLIMB FROM KTOL THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE ACFT LANDED AT KPHL WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 4 ENGINE FIRE DETECTIONJul 18, 2008 · N602AL · Doug DC873F · Fire Protection System WiringSDR IXX2008F00014Fire Warning · illuminatedDURING CLIMB, THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE AC LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (K)Jul 18, 2008 · N602AL · Doug DC873F · Fire DetectionSDR IXX2008F00016Fire Detector · malfunctionedDURING CRUISE, NR 3 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR 3 ENGINE. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT CORE SENSING ELEMENT, LT AND RT FAN FIRE SENSING ELEMENT, AND BOTH FIRE BOTTLES, OPS CHECK GOOJul 10, 2008 · N602AL · Doug DC873F · Fire DetectionSDR IXXA08SMN185SFloor Panel · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL WITH CORROSION AT STATION 1425.000 RIGHT BOTTOM LINE 50. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOMay 7, 2008 · N602AL · Doug DC873F · Fuselage Floor PanelSDR IXXA08SMN184SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 6 TRACK WITH LUG WORN AT STATION 1580.000. REMOVED EXISTING SPLICES (AFT SIDE). REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED NEW SPLICES. CLEANED, TREATED AND PRIMED AREA, AND EXISTING Apr 24, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN138SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING DOUBLER SHOWS CRACK AT STATION XS 515.720. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND Apr 17, 2008 · N602AL · Doug DC873F · Wing, Plate/SkinSDR IXXA08SMN137SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 680.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND SPLApr 17, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN136SCargo Track · brokenDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 2 TRACK WITH LUGS, BROKEN AT STATION 55.000. REMOVED SEGMENT OF DAMAGED TRACK AND EXITING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXITING SPLICES. INSTALLED NEW TRACK AND REINSTALLApr 17, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN124SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PART WITH IMPROPER REPAIR AT STATION XW -2.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. Apr 17, 2008 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA08SMN123SCargo Track · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 3 TRACK WITH CORROSION AT STATION 590.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED EXINTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED SPLICES. Apr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN122SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 685.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPApr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN121SCargo Track · wornDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 310.000 - 425.000. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INSTALLED SEGMENT OF NEApr 10, 2008 · N602AL · Doug DC873F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA08SMN119SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN LEFT SIDE WITH CORROSION AT STATION FS 850.000 LONGERON 24. REMOVED FASTENERS FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDMar 27, 2008 · N602AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA08SMN111SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 225.000 TO STA XF 335.000. REMOVED AND REPLACED RIGHT WING NUMBER 4 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA08SMN112SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 5 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 345.000 TO STA XF 404.000. REMOVED AND REPLACED RIGHT WING NUMBER 5 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA08SMN113SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 6 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 415.000 TO STA XF 434.000. REMOVED AND REPLACED RIGHT WING NUMBER 6 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-20Mar 27, 2008 · N602AL · Doug DC873F · Trailing Edge FlapsSDR IXXA08SMN114SSkin Panel · delaminatedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER PANEL DELAMINATED BETWEEN STATION XRS 247.000 TO XRS 351.000. ADJUSTED LEFT AND RIGHT WING GROUND FLIGHT SPOILER CABLES. PERFORMED OPS CHECK, GOOD TO SPOILER SYSTEM IAW DC8 MM 27-60-0 PAGE Mar 27, 2008 · N602AL · Doug DC873F · SpoilersSDR IXXA08SMN120SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR WHEEL WELL FORWARD UPPER PART FITTING CRACKED AT STATION 857.125 AND STATION XCW 23.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK FOUND. CLEANED, TREAMar 27, 2008 · N602AL · Doug DC873F · Wing, Landing Gear Attach Fittings
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