# Service difficulty reports: N799AL, cancelled Mar 6, 2018 A list on [N799AL, cancelled Mar 6, 2018](https://openairdocs.org/deregistered/N799AL-2018-03-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 7 · 311 reports - [SDR IXXA20121121031O](https://openairdocs.org/sdr/IXXA20121121031O.md): Valve · stuck · Nov 21, 2012 · N799AL · Doug DC862F · Cabin Temperature Control System > ACFT 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. - [SDR IXXA20120922027O](https://openairdocs.org/sdr/IXXA20120922027O.md): Control Valve · leaking · Sep 22, 2012 · N799AL · Doug DC862F · Hydraulic System, Main > DURING 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 - [SDR IXXA20120706017O](https://openairdocs.org/sdr/IXXA20120706017O.md): Lock · lack of lube · Jul 6, 2012 · N799AL · Doug DC862 · Landing Gear Position and Warning > HAD 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 MECHA - [SDR IXXA110055O](https://openairdocs.org/sdr/IXXA110055O.md): Oxygen Mask · torn · Aug 18, 2011 · N799AL · Doug DC862F · Emergency Equipment > DURING POST FLIGHT INSP, FOUND F/A DEMO KIT O2 MASK TORN. MX REPLACED O2 MASK IN F/A DEMO KIT IAW MM 16.02. - [SDR IXXA110041O](https://openairdocs.org/sdr/IXXA110041O.md): Fan · defective · May 18, 2011 · N799AL · Doug DC862F · Air Distribution Fan > DURING 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 RETURNED - [SDR IXXA0041O](https://openairdocs.org/sdr/IXXA0041O.md): Fan · odor · May 18, 2011 · N799AL · Doug DC862F · Air Distribution Fan > DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ODOR IN COCKPIT. THE CREW SHUTOFF LT RECIRCULATION FAN AND ODOR WENT AWAY. OPEN - [SDR IXXA110034O](https://openairdocs.org/sdr/IXXA110034O.md): Fan · defective · Apr 20, 2011 · N799AL · Doug DC862F · Air Distribution Fan > DURING 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. - [SDR IXXA110030O](https://openairdocs.org/sdr/IXXA110030O.md): Csd · defective · Mar 22, 2011 · N799AL · Doug DC862F · AC Generator-Alternator > DURING 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 REPLACED - [SDR IXXA000O](https://openairdocs.org/sdr/IXXA000O.md): Generator · malfunctioned · Mar 22, 2011 · N799AL · Doug DC862F · AC Generator-Alternator > DURING 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. - [SDR IXXA11SMN016S](https://openairdocs.org/sdr/IXXA11SMN016S.md): Fitting · cracked · Jan 22, 2011 · N799AL · Doug DC862F · Wing, Attach Fittings > DURING 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 51-3 - [SDR IXXA11SMN015S](https://openairdocs.org/sdr/IXXA11SMN015S.md): Skin · cracked · Jan 20, 2011 · N799AL · Doug DC862F · Horizontal Stabilizer, Plate/Skin > DURING 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. - [SDR IXXA11SMN014S](https://openairdocs.org/sdr/IXXA11SMN014S.md): Angle · corroded · Jan 20, 2011 · N799AL · Doug DC862F · Vertical Stabilizer, Attach Fittings > DUIRNG 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 S - [SDR IXXA11SMN012S](https://openairdocs.org/sdr/IXXA11SMN012S.md): Skin · corroded · Jan 18, 2011 · N799AL · Doug DC862F · Fuselage Main, Plate/Skin > DURING 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 SKIN - [SDR IXXA11SMN013S](https://openairdocs.org/sdr/IXXA11SMN013S.md): Skin · corroded · Jan 18, 2011 · N799AL · Doug DC862F · Fuselage Main, Plate/Skin > DUIRNG 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, TR - [SDR IXXA11SMN011S](https://openairdocs.org/sdr/IXXA11SMN011S.md): Skin · corroded · Jan 18, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 FOUN - [SDR IXXA11SMN008S](https://openairdocs.org/sdr/IXXA11SMN008S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 DISCREP - [SDR IXXA11SMN007S](https://openairdocs.org/sdr/IXXA11SMN007S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 DISCREP - [SDR IXXA11SMN006S](https://openairdocs.org/sdr/IXXA11SMN006S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 DISCREP - [SDR IXXA11SMN004S](https://openairdocs.org/sdr/IXXA11SMN004S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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. FABR - [SDR IXXA11SMN002S](https://openairdocs.org/sdr/IXXA11SMN002S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 - [SDR IXXA11SMN003S](https://openairdocs.org/sdr/IXXA11SMN003S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 - [SDR IXXA11SMN010S](https://openairdocs.org/sdr/IXXA11SMN010S.md): Skin · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 R - [SDR IXXA11SMN009S](https://openairdocs.org/sdr/IXXA11SMN009S.md): Doubler · corroded · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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. INSTAL - [SDR IXXA11SMN005S](https://openairdocs.org/sdr/IXXA11SMN005S.md): Skin · cracked · Jan 17, 2011 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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. F - [SDR IXXA11SMN001S](https://openairdocs.org/sdr/IXXA11SMN001S.md): Fastener · improper part · Jan 13, 2011 · N799AL · Doug DC862F · Fuselage Structure (General) > DURING 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 NE - [SDR IXXA100056O](https://openairdocs.org/sdr/IXXA100056O.md): Switch · shorted · Nov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling System > FIFTEEN 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. - [SDR IXXA100055O](https://openairdocs.org/sdr/IXXA100055O.md): Control Valve · defective · Nov 23, 2010 · N799AL · Doug DC862F · Cabin Cooling System > AFTER 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 SYS - [SDR IXXA100033O](https://openairdocs.org/sdr/IXXA100033O.md): Fuel Filter · clogged · May 19, 2010 · N799AL · Doug DC862F · Aircraft Fuel Filter/Strainer > AFTER 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. THE - [SDR IXXA100030O](https://openairdocs.org/sdr/IXXA100030O.md): Pulley · frozen · May 3, 2010 · N799AL · Doug DC862F · Landing Gear Retraction/Extension System > DURING 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 AMOU - [SDR IXXA100019O](https://openairdocs.org/sdr/IXXA100019O.md): Striker · out of adjust · Mar 3, 2010 · N799AL · Doug DC862F · Landing Gear Position and Warning > DURING 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 GO - [SDR IXXA100018O](https://openairdocs.org/sdr/IXXA100018O.md): Anti-Ice Valve · defective · Feb 28, 2010 · N799AL · Doug DC862F · Engine Anti-Icing System > DURING 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. - [SDR IXXA100017O](https://openairdocs.org/sdr/IXXA100017O.md): Striker · out of adjust · Feb 19, 2010 · N799AL · Doug DC862F · Landing Gear Position and Warning > DURING 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 STRIKE - [SDR IXXA100012O](https://openairdocs.org/sdr/IXXA100012O.md): Oil System · low pressure · Jan 31, 2010 · N799AL · Doug DC862F · Engine Oil Pressure > DURING 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 01.03.1 - [SDR IXXA100011O](https://openairdocs.org/sdr/IXXA100011O.md): Pressure Switch · malfunctioned · Jan 30, 2010 · N799AL · Doug DC862F · Engine Oil Pressure > DURING 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. - [SDR IXXA090076O](https://openairdocs.org/sdr/IXXA090076O.md): Fan · smoke · Dec 18, 2009 · N799AL · Doug DC862F · Air Distribution Fan > DURING CRUISE, THE LT RECIRCULATION FAN EMITTING BURNED ODOR. THE CREW TURNED OFF LT RECIRCULATION FAN AND LANDED WITHOUT FURTHER INCIDENT. IN WORK. - [SDR IXXA090064O](https://openairdocs.org/sdr/IXXA090064O.md): Wire · burned · Oct 26, 2009 · N799AL · Doug DC862F · Engine Indicating System Wiring > DURING 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 WI - [SDR IXXA090061O](https://openairdocs.org/sdr/IXXA090061O.md): Power Supply · defective · Oct 19, 2009 · N799AL · Doug DC862F · Fuel Indicating System > DURING 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 WA - [SDR IXXA090058O](https://openairdocs.org/sdr/IXXA090058O.md): Clamp · loose · Oct 18, 2009 · N799AL · Doug DC862F · Engine Bleed Air System > DURING 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. OPERATIONAL - [SDR IXXA090048O](https://openairdocs.org/sdr/IXXA090048O.md): Door · lack of lube · Sep 3, 2009 · N799AL · Doug DC862F · Landing Gear Door Retract Section > DURING 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. OPS - [SDR IXXA090047O](https://openairdocs.org/sdr/IXXA090047O.md): Amplifier · defective · Sep 3, 2009 · N799AL · Doug DC862F · Magnetic Compass > DURING 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. - [SDR IXXA090044O](https://openairdocs.org/sdr/IXXA090044O.md): Indicator · defective · Aug 30, 2009 · N799AL · Doug DC862F · Engine Pressure Ratio (EPR) > DURING 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. - [SDR IXXA090043O](https://openairdocs.org/sdr/IXXA090043O.md): Anti-Skid Sys · defective · Aug 29, 2009 · N799AL · Doug DC862F · Brake Anti-Skid Section > DURING 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 SERVICE - [SDR IXXA09SMN014S](https://openairdocs.org/sdr/IXXA09SMN014S.md): Skin · cracked · Feb 23, 2009 · N799AL · Doug DC862F · Elevator, Plate/Skin > DURING 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 - [SDR IXXA09SMN026S](https://openairdocs.org/sdr/IXXA09SMN026S.md): Splice · cracked · Jan 27, 2009 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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. CLEANED - [SDR IXXA09SMN016S](https://openairdocs.org/sdr/IXXA09SMN016S.md): Skin · corroded · Jan 27, 2009 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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. PERFORMED - [SDR IXXA09SMN022S](https://openairdocs.org/sdr/IXXA09SMN022S.md): Seat Track · corroded · Jan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 P - [SDR IXXA09SMN021S](https://openairdocs.org/sdr/IXXA09SMN021S.md): Seat Track · corroded · Jan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings > DURING 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 - [SDR IXXA09SMN020S](https://openairdocs.org/sdr/IXXA09SMN020S.md): Cargo Track · corroded · Jan 26, 2009 · N799AL · Doug DC862F · Fuselage, Seat/Cargo Attach Fittings > DURING 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, - [SDR IXXA09SMN019S](https://openairdocs.org/sdr/IXXA09SMN019S.md): Fitting · cracked · Jan 26, 2009 · N799AL · Doug DC862F · Fuselage Main, Attach Fittings > DURING 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 SP - [SDR IXXA09SMN015S](https://openairdocs.org/sdr/IXXA09SMN015S.md): Doubler · cracked · Jan 26, 2009 · N799AL · Doug DC862F · Wing, Plate/Skin > DURING 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 IN Next page: https://openairdocs.org/deregistered/N799AL-2018-03-06/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N799AL-2018-03-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.