N799AL, cancelled Mar 6, 2018

Service difficulty reports · 311

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 = 'N799AL' AND deregistration_id = 'N799AL-2018-03-06'
  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 IXXA20121121031OValve · stuckACFT RETURNED TO DEPARTURE, DUE TO NO HEAT IN THE PASSENGER COMPARTMENT. TROUBLESHOT AND FOUND NASI MIX VALVE STUCK IN THE FULL COLD POSITION. R & R MIX VALVE IAW MM 21.04.25. OPS CHECKED GOOD.Nov 21, 2012 · N799AL · Doug DC862F · Cabin Temperature Control SystemSDR IXXA20120922027OControl Valve · leakingDURING FLIGHT, HYDRAULIC QUANTITY LEVEL STARTED SLOWLY DECREASING. ACFT RETURNED TO ORIGINATING STATION. FOUND SLOT CONTROL VALVE LEAKING. R & R PACKING AND O-RINGS IAW MM 20-60-0 AND 27-80-4. SYS OPS AND LEAK CHECKS GOOD IAW MM 27-80-0. SERVICED HYD SYS Sep 22, 2012 · N799AL · Doug DC862F · Hydraulic System, MainSDR IXXA20120706017OLock · lack of lubeHAD A DOOR NOT LATCH LAMP ON DURING UPLATCH CHECK. UNSATISFACTORY UP LATCH, BOTH ALTERNATE DOOR LIGHTS DID NOT COME ON AFTER RECYCLE OF THE LANDING GEAR. JACKED ACFT IAW MM 7-11-0. PERFORMED OPS CHECK OF MLG IAW MM 32-30-0 FOUND RT MAIN GEAR DOOR LOCK MECHAJul 6, 2012 · N799AL · Doug DC862 · Landing Gear Position and WarningSDR IXXA110055OOxygen Mask · tornDURING POST FLIGHT INSP, FOUND F/A DEMO KIT O2 MASK TORN. MX REPLACED O2 MASK IN F/A DEMO KIT IAW MM 16.02.Aug 18, 2011 · N799AL · Doug DC862F · Emergency EquipmentSDR IXXA110041OFan · defectiveDURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR. THE CREW SHUT OFF THE LT RECIRCULATION FAN AND BURNED ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNEDMay 18, 2011 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA0041OFan · odorDURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR IN COCKPIT. THE CREW SHUTOFF LT RECIRCULATION FAN AND ODOR WENT AWAY. OPENMay 18, 2011 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA110034OFan · defectiveDURING CRUISE, THE RT RECIRCULATION FAN EMMITTING A BURNING ODOR, TURNED OFF THE RT RECIRCULATION FAN AND ODOR WENT AWAY, LANDED WITHOUT FURTHER INCIDENT. MX REPLACED RT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.Apr 20, 2011 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA110030OCsd · defectiveDURING CLIMB OUT, NR 4 GENERATOR BREAKER CYCLED OPEN AND CLOSED SEVERAL TIMES, GENERATOR WOULD NOT CARRY ITS OWN BUSS, VOLTS AND FREQUENCYS OK. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. NR 4 GENERATOR WAS DEFERRED IAW MEL 24-10-01. MX REPLACEDMar 22, 2011 · N799AL · Doug DC862F · AC Generator-AlternatorSDR IXXA000OGenerator · malfunctionedDURING CLIMB OUT, NR 4 GENERATOR BREAKER CYCLES OPEN AND CLOSED SEVERAL TIMES, GENERATOR WOULD NOT CARRY ITS OWN BUSS, VOLTS AND FREQUENCY OK. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. IN WORK.Mar 22, 2011 · N799AL · Doug DC862F · AC Generator-AlternatorSDR IXXA11SMN016SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 1 STUB WING FITTING INTERNAL PART CRACKED AT STA XW 454.000. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3Jan 22, 2011 · N799AL · Doug DC862F · Wing, Attach FittingsSDR IXXA11SMN015SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 28.843. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. Jan 20, 2011 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA11SMN014SAngle · corrodedDUIRNG ROUTINE C CHECK INSPECTION FOUND RIGHT VERTICAL STABILIZER TO FUSELAGE JOINT ANGLE CORRODED AT STA 1590. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED ANGLE, SPLICE, FILLER AND SJan 20, 2011 · N799AL · Doug DC862F · Vertical Stabilizer, Attach FittingsSDR IXXA11SMN012SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND FUSELAGE EXTERNAL SKIN CORRODED AT SEVERAL POINTS AT STATION 1530.000 LONGERON 23-28LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKINJan 18, 2011 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA11SMN013SSkin · corrodedDUIRNG ROUTINE C CHECK INSPECTION FOUND AFT FUSELAGE SKIN CRACKED AT STATION 1580.000 LONGERON 20RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, INTERNAL DOUBLER AND FILLER. CLEANED, TRJan 18, 2011 · N799AL · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA11SMN011SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 360.000 STRINGER 6. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUNJan 18, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN008SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 385.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN007SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 347.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN006SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 341.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN004SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 811.000 STRINGER 3 TO STRINGER 4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN002SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 763.000 STRINGER 2-4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN003SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 795.000 STRINGER 3-5. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN010SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER PANEL CORRODED AT STA XW 408.000. REMOVED CORRION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND RJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN009SDoubler · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER SURFACE DOUBLER CORRODED AT STA XFS 423.000 - XFS 400.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED DOUBLER. FABRICATED DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN005SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING UPPER SKIN CRACKED AND CORRODED AT STA XRS -17.000 STR-9. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FJan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/SkinSDR IXXA11SMN001SFastener · improper partDURING ROUTINE C-CHECK INSP, FOUND CHERRY MAX RIVETS USED IN REPAIR AT STATION ES 1360-1380. REMOVED FASTENERS FROM REPAIRED AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FINGER DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEJan 13, 2011 · N799AL · Doug DC862F · Fuselage Structure (General)SDR IXXA100056OSwitch · shortedFIFTEEN MINUTES INTO FLIGHT, BOTH AIR CYCLE MACHINES ON THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE BATTERY DIRECT PACS OVERTEMP TRIPPED. NO CONTROL OF THE LOAD CONTROL VALVE WAS AVAILABLE. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT.Nov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling SystemSDR IXXA100055OControl Valve · defectiveAFTER TAKEOFF, WHEN THE RT AIR CONDITIONING PACK WAS TURNED ON, THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE RT ACM CONTROL CIRCUIT BREAKER OPENED AND WOULD NOT RESET. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT THE SYSNov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling SystemSDR IXXA100033OFuel Filter · cloggedAFTER LEVEL OFF, WITH ANTI-ICE OFF NR 3 ENG N1 ROLLED BACK TO 80 PERCENT, N2 89 PERCENT, OIL PRESSURE 50PSI, FUEL FLOW FLUCTATING 2000-2800 AND PPH EPR 1.4-1.6. TURNED ON ANTI-ICE, NO HELP OIL TEMP BEGAN TO RISE FROM 90 TO 120. THE CREW SHUTDOWN NR 3 ENG. THEMay 19, 2010 · N799AL · Doug DC862F · Aircraft Fuel Filter/StrainerSDR IXXA100030OPulley · frozenDURING CLIMB OUT, AFTER GEAR RETRACTION GEAR DOOR LIGHT ILLUMINATED. THE CREW CYCLED GEAR AND LIGHT REMAINED ON. THE ALTERNATE LIGHT TESTED GOOD WHEN FWD RED GEAR DOOR LIGHT WAS ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND EXCESSIVE AMOUMay 3, 2010 · N799AL · Doug DC862F · Landing Gear Retraction/Extension SystemSDR IXXA100019OStriker · out of adjustDURING CLIMBOUT, AFTER GEAR RETRACTION THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEAR AND LIGHT REMAINED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE LT GEAR DOOR STRIKER OUT OF ADJUSTMENT. THEY ADJUSTED THE DOOR STRIKER. OPS CHECK GOMar 3, 2010 · N799AL · Doug DC862F · Landing Gear Position and WarningSDR IXXA100018OAnti-Ice Valve · defectiveDURING CLIMB OUT WITH ANTI-ICE ON NR 4 ENG COMPRESSOR STALLED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED NR 4 INBD ANTI-ICE CONTROL VALVE REGULATOR. OPS CHECK GOOD IAW MM 75-10-1. ACFT WAS RETURNED TO SERVICE.Feb 28, 2010 · N799AL · Doug DC862F · Engine Anti-Icing SystemSDR IXXA100017OStriker · out of adjustDURING CLIMBOUT, THE DOOR NOT LATCH LIGHT REMAINED ON AFTER GEAR RETRACTION, CREW CYCLED THE GEAR AND LIGHT REMAINED ON. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MLG AND FOUND THE LT MLG DOOR STRIKER OUT OF ADJUSTMENT. THEY ADJUSTED THE DOOR STRIKEFeb 19, 2010 · N799AL · Doug DC862F · Landing Gear Position and WarningSDR IXXA100012OOil System · low pressureDURING CRUISE FROM NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON. THE CREW SHUTDOWN NR 2 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED MAIN OIL FILTER, LOW OIL PRESSURE SWITCH AND OIL PRESSURE DIFFERENTIAL SWITCH. OPS CHECK GOOD IAW MM 79-20-7, ERH 01.03.1Jan 31, 2010 · N799AL · Doug DC862F · Engine Oil PressureSDR IXXA100011OPressure Switch · malfunctionedDURING CRUISE, NR 2 ENG LOW PRESSURE LIGHT CAME ON. THE CREW SHUTDOWN NR 2 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED LOW OIL PRESSURE SWITCH AND OIL DIFFERENTIAL SWITCH. OPS CHECK GOOD IAW MM 79-33-1 AND 79-32-2. ACFT WAS RETURNED TO SERVICE.Jan 30, 2010 · N799AL · Doug DC862F · Engine Oil PressureSDR IXXA090076OFan · smokeDURING CRUISE, THE LT RECIRCULATION FAN EMITTING BURNED ODOR. THE CREW TURNED OFF LT RECIRCULATION FAN AND LANDED WITHOUT FURTHER INCIDENT. IN WORK.Dec 18, 2009 · N799AL · Doug DC862F · Air Distribution FanSDR IXXA090064OWire · burnedDURING CLIMB OUT FROM TAPA NR 4 ENG EPR INOP, NR 4 GENERATOR CAUSED A MOMENTARY LOSS OF ALL POWER THEN LOCKED OUT-SHORTLY AFTER ZOLTS AND FREQUENCY WENT TO ZERO, AND NR 4 ENG BEGAN TO SPARK EVERY 25 SECONDS THE CREW SHUTDOWN NR 4 ENG. THEY RETURNED TO TAPA WIOct 26, 2009 · N799AL · Doug DC862F · Engine Indicating System WiringSDR IXXA090061OPower Supply · defectiveDURING CRUISE, ALL FOUR FUEL FLOW INDICATORS WENT TO ZERO AND NUMBER FOUR EPR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOTH FUEL FLOW POWER SUPPLY. OPERATIONAL CHECK GOOD IAW ATI ERH 71.01 AND ERH 70.01. AIRCRAFT WAOct 19, 2009 · N799AL · Doug DC862F · Fuel Indicating SystemSDR IXXA090058OClamp · looseDURING APPROACH INTO KBWI NUMBER FOUR ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NUMBER FOUR ENGINE AS A PRECAUTION, THEY LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED LOOSE CLAMP ON HIGH STAGE BLEED VALVE. OPERATIONALOct 18, 2009 · N799AL · Doug DC862F · Engine Bleed Air SystemSDR IXXA090048ODoor · lack of lubeDURING CLIMB OUT, CREW HEARD A VIBRATION SOUND COMING FROM THE NLG AREA. THEY CYCLED THE NLG AND THE NOISE CONTINUED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND RT NOSE GEAR DOOR WAS DOWN. MX LUBED DOOR LOCK MECHANISM. OPSSep 3, 2009 · N799AL · Doug DC862F · Landing Gear Door Retract SectionSDR IXXA090047OAmplifier · defectiveDURING CLIMB OUT, NR 2 COMPASS SYS PRECESSED EXCESSIVELY. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED NR 2 INSTRUMENT AMP RACK. OPS CHECK GOOD IAW MM 34-20-2. ACFT WAS RETURNED TO SERVICE.Sep 3, 2009 · N799AL · Doug DC862F · Magnetic CompassSDR IXXA090044OIndicator · defectiveDURING TAKEOFF FROM NR 1 EPR GUAGE WOULD NOT ACCELERATE. THE CREW RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 EPR TRANSMITTER. OPS CHECK GOOD IAW MM 77-11-1, AND ERH 70.01.1. ACFT WAS RETURNED TO SERVICE.Aug 30, 2009 · N799AL · Doug DC862F · Engine Pressure Ratio (EPR)SDR IXXA090043OAnti-Skid Sys · defectiveDURING TAKEOFF, ANTI-SKID INOP LIGHT ILLUMINATED ON SKID CONTROL MONITOR. THE CREW RETURNED TO BLOCK WITHOUT FURTHER INCIDENT. MX REPLACED ANTI-SKID CONTROL VALVE AND ANTI-SKID TRANSDUCER. OPS CHECK GOOD IAW MM 32-43-0, 32-43-3. ACFT WAS RETURNED TO SERVICEAug 29, 2009 · N799AL · Doug DC862F · Brake Anti-Skid SectionSDR 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/Skin
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