# N799AL: 1968 Mcdonnell Douglas DC-8-62F, registration cancelled 2018-03-06

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 6, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Mcdonnell Douglas DC-8-62F](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62f) (registry code 302197D)
- Engine: [Pratt & Whitney JT3D series](https://openairdocs.org/engine/pratt-whitney-jt3d-series) (registry code 52035)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45922
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 18, 1989
- Certificate issued: December 30, 2009
- Last registry action: December 15, 2014
- Mode S code: AAD97F
- Owner when cancelled: [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC)
- Location: [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington)
- Owner type: Corporation
- Owner's area on the map: 39.4607° N, 83.8443° W: Placed by OpenAirDocs at the center of ZIP code 45177, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N799AL
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=799AL
- Page: https://openairdocs.org/deregistered/N799AL-2018-03-06

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-8-62F: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62f.md

## Service difficulty reports (311, newest 50)

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

- [SDR IXXA20121121031O](https://openairdocs.org/sdr/IXXA20121121031O), Nov 21, 2012: VALVE. STUCK. 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 I
- [SDR IXXA20120922027O](https://openairdocs.org/sdr/IXXA20120922027O), Sep 22, 2012: CONTROL VALVE. LEAKING. DURING FLIGHT, HYDRAULIC QUANTITY LEVEL STARTED SLOWLY DECREASING. ACFT RETURNED TO ORIGINATING STATION. FOUND SLOT CONTROL VALVE LEAKING. R & R PACKING AND O-R
- [SDR IXXA20120706017O](https://openairdocs.org/sdr/IXXA20120706017O), Jul 6, 2012: LOCK. LACK OF LUBE. 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
- [SDR IXXA110055O](https://openairdocs.org/sdr/IXXA110055O), Aug 18, 2011: OXYGEN MASK. TORN. 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), May 18, 2011: FAN. DEFECTIVE. 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
- [SDR IXXA0041O](https://openairdocs.org/sdr/IXXA0041O), May 18, 2011: FAN. ODOR. 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), Apr 20, 2011: FAN. DEFECTIVE. 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 RE
- [SDR IXXA110030O](https://openairdocs.org/sdr/IXXA110030O), Mar 22, 2011: CSD. DEFECTIVE. 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 RETURNE
- [SDR IXXA000O](https://openairdocs.org/sdr/IXXA000O), Mar 22, 2011: GENERATOR. MALFUNCTIONED. 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
- [SDR IXXA11SMN016S](https://openairdocs.org/sdr/IXXA11SMN016S), Jan 22, 2011: FITTING. CRACKED. 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 ARE
- [SDR IXXA11SMN015S](https://openairdocs.org/sdr/IXXA11SMN015S), Jan 20, 2011: SKIN. CRACKED. 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
- [SDR IXXA11SMN014S](https://openairdocs.org/sdr/IXXA11SMN014S), Jan 20, 2011: ANGLE. CORRODED. DUIRNG ROUTINE C CHECK INSPECTION FOUND RIGHT VERTICAL STABILIZER TO FUSELAGE JOINT ANGLE CORRODED AT STA 1590. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED 
- [SDR IXXA11SMN012S](https://openairdocs.org/sdr/IXXA11SMN012S), Jan 18, 2011: SKIN. CORRODED. DURING ROUTINE C CHECK INSPECTION FOUND FUSELAGE EXTERNAL SKIN CORRODED AT SEVERAL POINTS AT STATION 1530.000 LONGERON 23-28LEFT. REMOVED CORROSION. FOUND OUT O
- [SDR IXXA11SMN013S](https://openairdocs.org/sdr/IXXA11SMN013S), Jan 18, 2011: SKIN. CORRODED. DUIRNG ROUTINE C CHECK INSPECTION FOUND AFT FUSELAGE SKIN CRACKED AT STATION 1580.000 LONGERON 20RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED
- [SDR IXXA11SMN011S](https://openairdocs.org/sdr/IXXA11SMN011S), Jan 18, 2011: SKIN. CORRODED. 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 FASTENE
- [SDR IXXA11SMN008S](https://openairdocs.org/sdr/IXXA11SMN008S), Jan 17, 2011: SKIN. CORRODED. 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. REMOVE
- [SDR IXXA11SMN007S](https://openairdocs.org/sdr/IXXA11SMN007S), Jan 17, 2011: SKIN. CORRODED. 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. REMOVE
- [SDR IXXA11SMN006S](https://openairdocs.org/sdr/IXXA11SMN006S), Jan 17, 2011: SKIN. CORRODED. 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. REMOVE
- [SDR IXXA11SMN004S](https://openairdocs.org/sdr/IXXA11SMN004S), Jan 17, 2011: SKIN. CORRODED. 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. R
- [SDR IXXA11SMN002S](https://openairdocs.org/sdr/IXXA11SMN002S), Jan 17, 2011: SKIN. CORRODED. 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 FAST
- [SDR IXXA11SMN003S](https://openairdocs.org/sdr/IXXA11SMN003S), Jan 17, 2011: SKIN. CORRODED. 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 FAST
- [SDR IXXA11SMN010S](https://openairdocs.org/sdr/IXXA11SMN010S), Jan 17, 2011: SKIN. CORRODED. 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 
- [SDR IXXA11SMN009S](https://openairdocs.org/sdr/IXXA11SMN009S), Jan 17, 2011: DOUBLER. CORRODED. 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. REMO
- [SDR IXXA11SMN005S](https://openairdocs.org/sdr/IXXA11SMN005S), Jan 17, 2011: SKIN. CRACKED. 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 A
- [SDR IXXA11SMN001S](https://openairdocs.org/sdr/IXXA11SMN001S), Jan 13, 2011: FASTENER. IMPROPER PART. 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. FABRICA
- [SDR IXXA100056O](https://openairdocs.org/sdr/IXXA100056O), Nov 23, 2010: SWITCH. SHORTED. 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
- [SDR IXXA100055O](https://openairdocs.org/sdr/IXXA100055O), Nov 23, 2010: CONTROL VALVE. DEFECTIVE. 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 W
- [SDR IXXA100033O](https://openairdocs.org/sdr/IXXA100033O), May 19, 2010: FUEL FILTER. CLOGGED. 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.
- [SDR IXXA100030O](https://openairdocs.org/sdr/IXXA100030O), May 3, 2010: PULLEY. FROZEN. 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 GE
- [SDR IXXA100019O](https://openairdocs.org/sdr/IXXA100019O), Mar 3, 2010: STRIKER. OUT OF ADJUST. 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 INCIDEN
- [SDR IXXA100018O](https://openairdocs.org/sdr/IXXA100018O), Feb 28, 2010: ANTI-ICE VALVE. DEFECTIVE. 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 V
- [SDR IXXA100017O](https://openairdocs.org/sdr/IXXA100017O), Feb 19, 2010: STRIKER. OUT OF ADJUST. 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. M
- [SDR IXXA100012O](https://openairdocs.org/sdr/IXXA100012O), Jan 31, 2010: OIL SYSTEM. LOW 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 
- [SDR IXXA100011O](https://openairdocs.org/sdr/IXXA100011O), Jan 30, 2010: PRESSURE SWITCH. MALFUNCTIONED. 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 
- [SDR IXXA090076O](https://openairdocs.org/sdr/IXXA090076O), Dec 18, 2009: FAN. SMOKE. 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), Oct 26, 2009: WIRE. BURNED. 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
- [SDR IXXA090061O](https://openairdocs.org/sdr/IXXA090061O), Oct 19, 2009: POWER SUPPLY. DEFECTIVE. DURING CRUISE, ALL FOUR FUEL FLOW INDICATORS WENT TO ZERO AND NUMBER FOUR EPR FAILED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLA
- [SDR IXXA090058O](https://openairdocs.org/sdr/IXXA090058O), Oct 18, 2009: CLAMP. LOOSE. DURING APPROACH INTO KBWI NUMBER FOUR ENGINE FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NUMBER FOUR ENGINE AS A PRECAUTION, THEY LANDED WITHOUT FURT
- [SDR IXXA090048O](https://openairdocs.org/sdr/IXXA090048O), Sep 3, 2009: DOOR. LACK OF LUBE. 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
- [SDR IXXA090047O](https://openairdocs.org/sdr/IXXA090047O), Sep 3, 2009: AMPLIFIER. DEFECTIVE. 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 G
- [SDR IXXA090044O](https://openairdocs.org/sdr/IXXA090044O), Aug 30, 2009: INDICATOR. DEFECTIVE. 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 
- [SDR IXXA090043O](https://openairdocs.org/sdr/IXXA090043O), Aug 29, 2009: ANTI-SKID SYS. DEFECTIVE. DURING TAKEOFF, ANTI-SKID INOP LIGHT ILLUMINATED ON SKID CONTROL MONITOR. THE CREW RETURNED TO BLOCK WITHOUT FURTHER INCIDENT. MX REPLACED ANTI-SKID CONTROL VAL
- [SDR IXXA09SMN014S](https://openairdocs.org/sdr/IXXA09SMN014S), Feb 23, 2009: SKIN. CRACKED. 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 
- [SDR IXXA09SMN026S](https://openairdocs.org/sdr/IXXA09SMN026S), Jan 27, 2009: SPLICE. CRACKED. 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. 
- [SDR IXXA09SMN016S](https://openairdocs.org/sdr/IXXA09SMN016S), Jan 27, 2009: SKIN. CORRODED. 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. RE
- [SDR IXXA09SMN022S](https://openairdocs.org/sdr/IXXA09SMN022S), Jan 26, 2009: SEAT TRACK. CORRODED. 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. REM
- [SDR IXXA09SMN021S](https://openairdocs.org/sdr/IXXA09SMN021S), Jan 26, 2009: SEAT TRACK. CORRODED. 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
- [SDR IXXA09SMN020S](https://openairdocs.org/sdr/IXXA09SMN020S), Jan 26, 2009: CARGO TRACK. CORRODED. DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK CORRODED AT STATION 970.000 - 1020.000. REMOVED EXISTING SPLICES. REMOVED CORROSI
- [SDR IXXA09SMN019S](https://openairdocs.org/sdr/IXXA09SMN019S), Jan 26, 2009: FITTING. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT CRACKED FITTING AT STATION 822.500 LONGERON 21-22 LEFT. REMOVED CRACKED FITTING. CLEANED, TRE
- [SDR IXXA09SMN015S](https://openairdocs.org/sdr/IXXA09SMN015S), Jan 26, 2009: DOUBLER. CRACKED. DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SURFACE INTERNAL DOUBLER CRACKED AT STATION XFS 422.750. REMOVED CRACKED INTERNAL D

All 311: https://openairdocs.org/deregistered/N799AL-2018-03-06/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19970510015709I](https://openairdocs.org/incident/19970510015709I), May 10, 1997: Doug DC862 (N799AL), Boston, MA. Narrative: zantop 300 (cargo) DC-8 on pushback from south cargo area Boston Logan airport, jet blast pushed two hudson baggage carts, which were not properly…

## Other aircraft with N799AL

- [Registered now](https://openairdocs.org/aircraft/N799AL): Beech 300, S/N FA-157, built 1988

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