# N802BN: 1967 Mcdonnell Douglas DC-8-62, registration cancelled 2006-06-19

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 19, 2006
- Exported to: Republic of the Congo
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas DC-8-62](https://openairdocs.org/model/mcdonnell-douglas-dc-8-62) (registry code 302197B)
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25) (OpenAirDocs)
- Serial number: 45909
- Year built: 1967
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: March 30, 1989
- Certificate issued: July 11, 2005
- Last registry action: August 5, 2005
- Mode S code: AAE971
- Owner when cancelled: [Aviation Parts Depot Inc](https://openairdocs.org/faa-owner/AVIATION%20PARTS%20DEPOT%20INC)
- Location: [Pittsboro, NC](https://openairdocs.org/faa-place/NC/Pittsboro)
- Owner type: Corporation
- Owner's area on the map: 35.7544° N, 79.1988° W: Placed by OpenAirDocs at the center of ZIP code 27312, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N802BN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=802BN
- Page: https://openairdocs.org/deregistered/N802BN-2006-06-19

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-8-62: https://openairdocs.org/model/mcdonnell-douglas-dc-8-62.md

## Service difficulty reports (88, newest 50)

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

- [SDR ARWA20030708](https://openairdocs.org/sdr/ARWA20030708), Jul 22, 2003: FLOORBEAM. CORRODED. DURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT STATION 1520, RBL 32 FLOORBEAM UPPER FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOO
- [SDR ARWA20030605](https://openairdocs.org/sdr/ARWA20030605), Jun 5, 2003: DOOR FRAME. CRACKED. DURING MAINTENANCE INSPECTION THE FOLLOWING WAS FOUND, FORWARD ENTRY DOOR FRAME, BOTTOM AFT CORNER HFEC INSPECTION REVEALED .1250 INCH CRACK. ACCOMPLISHED REPAI
- [SDR ARWA20030402](https://openairdocs.org/sdr/ARWA20030402), Apr 11, 2003: ROTARY ACTUATOR. JAMMED. RIGHT SUIT CASE HANDLE JAMMED IN FORWARD POSITION AND COULD NOT BE MOVED EVEN WITH C/B PULLED. REMOVED AND REPLACED RIGHT LONGITUDINAL TRIM SERVO ACTUATOR IAW M
- [SDR ARWA20030301](https://openairdocs.org/sdr/ARWA20030301), Mar 9, 2003: HOSE. LEAKING. IN FLIGHT LOSS OF HYDRAULIC QUANTITY OF PRESSURE; PERFORMED APPROACH CHECKLIST. FOUND HYDRAULIC PRESSURE HOSE LEAKING AT NR 2 ENGINE. REMOVED AND REPLACED HYDRA
- [SDR ARWA20030102](https://openairdocs.org/sdr/ARWA20030102), Jan 19, 2003: VALVE. INOPERATIVE. DURING TAXI, BEFORE TAKEOFF, ANTI SKID INOPERATIVE LIGHT ON WITH SWITCH IN (ON) POSITION. REMOVED AND REPLACED RT MAIN LANDING GEAR OUTBOARD ANTI SKID DUAL SERV
- [SDR ARWA20021203](https://openairdocs.org/sdr/ARWA20021203), Dec 11, 2002: HOSE. DAMAGED. LOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULIC HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMO
- [SDR ARWA20021108](https://openairdocs.org/sdr/ARWA20021108), Nov 20, 2002: CYLINDER. INOPERATIVE. IN FLIGHT, AFTER NORMAL GEAR RETRACTION , RED GEAR LIGHT ON AFTER UP LATCH CHECK. FOLLOWED ABNORMAL CHECKLIST. REMOVED AND REPLACED LEFT GEAR UP LATCH CYLINDER 
- [SDR ARWA20021106](https://openairdocs.org/sdr/ARWA20021106), Nov 14, 2002: ENGINE. FAILED. AT 2130Z, NR 2 OIL QUANTITY RAPIDLY DROPPED TO 1 GALLON, SUBSEQUENTLY OIL PRESSURE DROPPED TO 5 PSI AND OIL PRESSURE LOW LIGHT ILLUMINATED. PERFORMED IN FLIGHT 
- [SDR ARWA20021105](https://openairdocs.org/sdr/ARWA20021105), Nov 13, 2002: RECEIVER. INOPERATIVE. NR 2 VHF FIRST OFFICER SIDE COURSE DEVIATION INDICATOR INOPERATIVE, RETURNED TO MIAMI. REMOVED & REPLACED NR 2 VOR INSTRUMENT LANDING SYSTEM RECEIVER. SYSTEM OP
- [SDR ARWA20021102](https://openairdocs.org/sdr/ARWA20021102), Nov 7, 2002: HEAT EXCHANGER. FAILED. NR 1 ENGINE OIL TEMPERATURE INDICATED 140 DEGREES FOR 15 MINUTES; THEN WENT TO 150 DEGREES THROTTLE IDLE, ALL OTHER PARAMETERS NORMAL, PERFORMED IN FLIGHT ENGIN
- [SDR ARWA20021004](https://openairdocs.org/sdr/ARWA20021004), Oct 12, 2002: ENGINE. MALFUNCTIONED. DURING CRUISE NR 3 ENGINE IDLE PRESS. LIGHT ILLUMINATED. OIL PRESS. 25 PSI, QTY, 1 GALLON. TEMP 135 DEGREES. ENGINE SHUT DOWN AT 1421Z. WINDMILLING OIL PRESSURE
- [SDR ARWA20020901](https://openairdocs.org/sdr/ARWA20020901), Sep 2, 2002: CYLINDER. LEAKING. AFTER LANDING IN SKCL LOSS OF HYDRAULICS PRESSURE AND QUANTITY. FOUND HYDRAULIC LEAK IN LEFT BOGIE TRIM CYLINDER. REMOVED AND REPLACED LEFT HYDRAULIC BOGIE TRIM
- [SDR ARWA20020203](https://openairdocs.org/sdr/ARWA20020203), Feb 4, 2002: FITTING. CRACKED. DURING C-CHECK, RIGHT WING NR 4 ALTERNATE FUEL TANK INTERIOR S-58 END FITTING WITH 1 INCH CRACK AT STA XRS 408.00.
- [SDR ARWA20020202](https://openairdocs.org/sdr/ARWA20020202), Feb 4, 2002: FITTING. CRACKED. DURING C-CHECK, LT WING NR 1 ALTERNATE FUEL TANK INTERIOR S-57 END FITTING WITH 1 INCH CRACK STA XRS 408.00. REMOVED AND REPLACED STRINGER END FITTINGS IAW DC-8
- [SDR ARWA20011212](https://openairdocs.org/sdr/ARWA20011212), Dec 23, 2001: BLEED VALVE. LACK OF LUBE. NR 3 ENGINE COMPRESSOR STALL AT BRAKE RELEASE MAX POWER 1.89 EPR RETURN TO RAMP FOR CKV & FOR NOTE 13 DEGREE CELSIUS ENGINE ANTI ICE OFF AND NO WIND. LUBED SURG
- [SDR ARWA0011014](https://openairdocs.org/sdr/ARWA0011014), Nov 9, 2001: PUMP. LEAKING. IN CRUISE, HYDRAULIC QUANTITY DROPPED SLIGHTLY ABOVE EMERGENCY LEVEL. PERFORMED LOSS OF HYDRAULIC PRESSURE ABNORMAL EMERGENCY CHECKLIST. FLIGHT RESTRICTED TO MA
- [SDR ARWA0010803](https://openairdocs.org/sdr/ARWA0010803), Aug 7, 2001: SEAL. LOG PAGE 53334. DISCREPANCY: ON FINAL APPROACH SHUT DOWN #3 ENGINE DUE TO RAPID DROP IN OIL QUANTITY AND PRESSURE. CORRECTIVE ACTION: REMOVED HOUSING AND SEAL F
- [SDR ARWA0010403](https://openairdocs.org/sdr/ARWA0010403), Apr 7, 2001: GENERATOR. MALFUNCTIONED. NR 2 GENERATOR FIELD RELAY TRIPS AND WILL NOT RESET.CORRECTIVE ACTION: REMOVED AND REPLACED NR 2 GENERATOR OPERATIONAL CHECK NORMAL DURING RUN UP IAW MM 24-20-1
- [SDR ARWA1000204](https://openairdocs.org/sdr/ARWA1000204), Feb 25, 2001: O-RING. TORN. HYDRAULIC SYSTEM LOSS DOWN TO STADPIPE, EMERGENCY CHECK, LIST C/W. RETURNED TO STATION. FOUND O-RING FROM RT AILERON ACTUATOR TUBING FITTING LEAKING. REPLACED O
- [SDR ARWA0010203](https://openairdocs.org/sdr/ARWA0010203), Feb 7, 2001: LINK. BROKEN. FLAP IND HAS SPLIT NEEDLES. FOUND LEFTI/B FLAP LINK BROKEN ON THE O/B HINGE. REMOVED AND REPLACED WITH NEW P/N 5751152-501. REFERENCE MM 27-51-4. OPS CHECK SATI
- [SDR ARWA991001](https://openairdocs.org/sdr/ARWA991001), Oct 16, 1999: FIRE LOOP. FAILED. MIA - FLT 447 - AT 14,000 FT ALT, NR 1 ENGINE FIRE WARNING SOUNDED. ENGINE SHUTDOWN. OIL QTY AND OIL PRESSURE NORMAL AND OIL TEMP HIGH AT 140 DEGREES. REMOVED A
- [SDR ARWA990704](https://openairdocs.org/sdr/ARWA990704), Jul 27, 1999: STRUCTURE. CRACKED. MIA - FLT 574 - DURING ROUTINE INSPECTION DURING MAIN CARGO DOOR MAINTENANCE, DETECTED APPROXIMATELY 10 INCH CRACK IN STC DOUBLER EMANATING LOWER FORWARD CORNER
- [SDR ARWA990602](https://openairdocs.org/sdr/ARWA990602), Jun 22, 1999: ENGINE. FAILED. SJU - FLT 601 - CLIMBING-OUT THROUGH 16000 FT AT 1302Z, NR 4 ENGINE LOUD BANG ALL PARAMETERS ERRATIC. COMPLETED APPROPRIATE CHECK LISTS. DUMPED FUEL TO MAX LAND
- [SDR ARWA990502](https://openairdocs.org/sdr/ARWA990502), May 23, 1999: BRACKET. BROKEN. BOG - FLT 709 - NR 1 ENGINE INBOARD BYPASS AIR CONSTANT DUCT STRAP BRACKET BROKEN. BLOWOUT DOOR LOST IN FLIGHT. REMOVED AND REPLACED STRAP. REPLACED NR 1 ENGINE
- [SDR ARWA990304](https://openairdocs.org/sdr/ARWA990304), Mar 6, 1999: WHEEL. FAILED. MIA - FLT 807 - BLOCK TURN BACK, AT THE BEGINNING OF TAKEOFF HEARD A LOUD NOISE FROM LEFT MLG WHEEL WELL. RETURNED TO RAMP. MAINTENANCE FOUND NR 6 MLG WHEEL INB
- [SDR ARWA990203](https://openairdocs.org/sdr/ARWA990203), Feb 12, 1999: LIGHT. MALFUNCTIONED. MIA - LANDING GEAR DOOR NOT LATCHED. REMAINED ON, WARNING LIGHT ILLUMINATED. AFTER ALL ABNORMAL PROCEDURES WERE PERFORMED. RETURNED TO MIAMI WITHOUT INCIDENT. T
- [SDR 99T64R063AR](https://openairdocs.org/sdr/99T64R063AR), Feb 5, 1999: FRAME. CORRODED. FUSELAGE LONGERON 25L FRAME 119L FINGER DOUBLER AT FLOORBEAM COCKPIT SUB FLOOR CORROSION EXFOLIATION. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, FABRICATED 
- [SDR 99T64R062AR](https://openairdocs.org/sdr/99T64R062AR), Feb 2, 1999: FRAME. CORRODED. FUSELAGE STATION 148 LEFT SIDE FUSELAGE SUB FLOOR FRAME ATTACH ANGLE CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, AND INSTALLED PER EO DRAWING NR 99-00
- [SDR ARWA990106](https://openairdocs.org/sdr/ARWA990106), Jan 12, 1999: ENGINE. LEAKING. MIA - FLT 1628 - FL310, OIL QTY NR 1 ENGINE DROPPED TO .5 GALLON, OK OIL AND SUBSEQUENT ENGINE DAMAGE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AS EPR ABNORMAL C
- [SDR ARWA990105](https://openairdocs.org/sdr/ARWA990105), Jan 10, 1999: BOLT. WORN. MIA - FLT 9627 - ON PRE-FLIGHT, FOUND RT AILERON INBD TO OTBD SECTION 2 INCH SPLIT. TROUBLESHOT, FOUND EYE BOLT ATTACHING INBD/OTBD AILERON LOOSE AND WORN. REPL
- [SDR ARWA981211](https://openairdocs.org/sdr/ARWA981211), Dec 19, 1998: PITOT TUBE. INOP. F/O PITOT HEAT INOP. REMOVED AND REPLACED CURRENT DETECTOR IAW DC-8 M/M 30-30-0. NO HELP. REMOVED AND REPLACED F/O PITOT TUBE IAW DC-8 M/M 30-30-0. PERFORMED PI
- [SDR ARWA981104](https://openairdocs.org/sdr/ARWA981104), Nov 18, 1998: CONNECTOR. LOOSE. NR 1 EGT FLUCTUATING AT 300 DEGREES, ADVANCING THROTTLE ON T/O ROLL. ABORTED T/O AND RETURNED TO RAMP. TIGHTEN CANNON PLUG ON EGT INDICATOR, OPS CHECKED NORMAL 
- [SDR ARWA980911](https://openairdocs.org/sdr/ARWA980911), Sep 22, 1998: FITTING. LOOSE. TUS - SHUTDOWN NR 4 ENGINE S/N 671443 AT 1345Z DUE TO STEADY OIL PRESS LIGHT AND INDICATED PRESS LESS THAN 35 PSI. WINDMILLING PRESS AT 18 PSI. TIGHTENED LOOS S
- [SDR ARWA980910](https://openairdocs.org/sdr/ARWA980910), Sep 19, 1998: SPAR. CRACKED. RT WING FRONT SPAR LOWER CAP HAS TWO ADJACENT ATTACHMENT HOLES CRACKED BETWEEN STA XFS 515.000 AND XFS 526.760. CUT OUT DAMAGED AREA PER DRA J060232, FABRICATED
- [SDR ARWA980803](https://openairdocs.org/sdr/ARWA980803), Aug 5, 1998: NUT. LOOSE. KELP - FLT 045 - DURING CLIMB-OUT, HYDRAULIC FLUID LOSS, PRESSURE FLUCTUATING, EMERGENCY CHECK LIST COMPLETED, 6 GALLONS REMAINING. RETURNED TO KELP. TIGHTENED 
- [SDR ARWA9807131](https://openairdocs.org/sdr/ARWA9807131), Jul 30, 1998: CONNECTOR. LOOSE. DAY - FLT 046 - AFTER TAKEOFF, GEAR DOOR NOT LATCH LIGHT ILLUMINATED, ABNORMAL CHECK LIST COMPLETED. DOOR NOT LATCH LIGHT REMAINED ILLUMINATED. RETURNED TO DAY,
- [SDR ARWA9807127](https://openairdocs.org/sdr/ARWA9807127), Jul 17, 1998: COOLING VALVE. MISWIRED. AIRCRAFT CABIN ALT AT 9000 AND CLIMBING WITH 3 T/C'S OPERATING AT 31,000 FOUND RADIO RACK COOLING VALVE OPEN WHEN AIRBORNE. CORRECTED WIRING AT RELAY R2-64, OPS
- [SDR ARWA9807126](https://openairdocs.org/sdr/ARWA9807126), Jul 17, 1998: B-NUT. LOOSE. 30 KNOT SPLIT ON AIRSPEED AND 1000 SPLIT ON ALTIMETERS CLIMBING THROUGH FL 310, SPLITS ON BOTH WERE INCREASING, BOTH HIGH ON F/O SIDE. SECURED LOOSE B NUT IN CE
- [SDR ARWA9807125](https://openairdocs.org/sdr/ARWA9807125), Jul 17, 1998: SUPPORT. CORRODED. FLOOR SUPPORT CROSS BEAM AT STATION 1540 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR 18R5370
- [SDR ARWA9807124](https://openairdocs.org/sdr/ARWA9807124), Jul 17, 1998: BULKHEAD BRACKET. CRACKED. BOTH ATTACH BRACKETS HOLDING PRESS. SEALS TRUMPETS ARE CRACKED AT AFT PRESSURE BULKHEAD AREA. FABRICATED REPAIR AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO 
- [SDR ARWA980508](https://openairdocs.org/sdr/ARWA980508), Jun 3, 1998: SWIVEL. LEAKING. ON LANDING ROLL, NOTICED HYD QUANTITY DECREASING DOWN TO STAND PIPE. REMOVED AND REPLACED AILERON TAB LOCK OUT CYLINDER SWIVEL GLAND IAW MM 27-11-7, OPERATION L
- [SDR ARWA980409](https://openairdocs.org/sdr/ARWA980409), Apr 27, 1998: COWLING. DAMAGED. DURING GROUND HANDLING, NR 2 ENGINE COWLING DAMAGED BY BELT LOADER, LT AND RT FWD COWLINGS. LT AND RT AFT COWLINGS AND T/R LOWER STRINGER, REMOVED AND REPLACED 
- [SDR ARWA980311](https://openairdocs.org/sdr/ARWA980311), Mar 31, 1998: DUCT. FAILED. AT 39,000 LOSS PRESSURIZATION, PROCED FOR EMERGENCY DESCENT. RETURNED TO MIAMI. AT ARRIVAL AIRCRAFT WILL NOT ACCEPT EXTERNAL POWER. FOUND CLAMP TO NR 3 T/C DUCT
- [SDR ARWA980308](https://openairdocs.org/sdr/ARWA980308), Mar 24, 1998: WINGTIP. DAMAGED. ON RAMP, WHILE BEING MANSHALLED INTO THE RAMP, THE LEFT WING TIP MADE CONTACT WITH ANOTHER AIRCRAFT. TEMPORARY REPAIR ACCOMPLISHED IAW MM 6 PAR 5-1 TO FLY A/C B
- [SDR ARWA980203](https://openairdocs.org/sdr/ARWA980203), Feb 2, 1998: CONTROL BOX. FAILED. AFTER T/O, ANTI-SKID LIGHT CAME ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECKED GOOD IAW MM 32-43-3. REMOVED AND REPLACED DUAL ANTI-SKID VALVE, OPS 
- [SDR ARWA980101](https://openairdocs.org/sdr/ARWA980101), Jan 7, 1998: CONTROL CABLE. BROKEN. AIRCRAFT RETURNED TO BLOCKS RUDDER MOVEMENT LIMITED, HAS NOT FULL DEFLECTION WITH FLAPS DOWN. T/S FOUND RUDDER THROW LIMITER CABLE BROKEN. REMOVED AND REPLACED 
- [SDR ARWA970901](https://openairdocs.org/sdr/ARWA970901), Sep 7, 1997: DUCT. LOOSE. UNABLE TO PRESSURISE ABOVE 1 PSI, 3 TC'S BLEEDS HIGH OUTFLOW HANDLE FULL UP AND LOCKED. DUMPED APPROXIMATELY 6.000 FUEL. FOUND EXHAUST DUCT OFF NR 3 T/C, REINST
- [SDR ARWA9702002](https://openairdocs.org/sdr/ARWA9702002), Feb 6, 1997: RADAR SCOPE. FAILED. AFTER DEPARTURE, WEATHER RADAR DID NOT PAINT TARGET. RETURNED TO MIAMI, TROUBLESHOT SYSTEM FOUND RADAR SCOPE FAILING. REMOVED AND REPLACED SCOPE, OPS CHECKED NO
- [SDR ARWA9611004](https://openairdocs.org/sdr/ARWA9611004), Nov 15, 1996: COMPRESSOR. MALFUNCTIONED. AIR TURNBACK, NR 4 TURBO COMPRESSOR OVERHEAT LIGHT ON. UNABLE TO HOLD CABIN ALTITUDE. RETURNED TO MIAMI WITHOUT INCIDENT. REMOVED AND REPLACED NR 4 T/C, SYS OPS
- [SDR ARWA9609030](https://openairdocs.org/sdr/ARWA9609030), Sep 20, 1996: RELAY. MALFUNCTIONED. WHILE ON CLIMBOUT, LOST NR 1 DC BUS, CAPTAIN'S INSTRUMENTS LIGHTS OUT, 1 AND 2 ENGINE OIL TEMP, OIL QTY, CSD NR 1 FUEL FEED PUMP NR 1 ALT FUEL PUMP, HYD QTY. RE

All 88: https://openairdocs.org/deregistered/N802BN-2006-06-19/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 19980205005809I](https://openairdocs.org/incident/19980205005809I), Feb 5, 1998: Doug DC862 (N802BN), Dayton, OH. Narrative: on the above date and time inspectors, mark m. mcconaughy and James l. jackson responded to the Dayton international airport on the complaint of a…

## Other aircraft with N802BN

- [Cancelled 2024-05-11](https://openairdocs.org/deregistered/N802BN-2024-05-11): Cessna U206G, S/N U20606346. Sale reported, canceled. Owner: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

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