# N751NW: 1968 Mcdonnell Douglas DC-9-41, registration cancelled 2011-02-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 9, 2011 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-41](https://openairdocs.org/model/mcdonnell-douglas-dc-9-41) (registry code 302207P) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47115 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 22, 1992 - Certificate issued: December 31, 2009 - Last registry action: December 31, 2009 - Mode S code: AA1F01 - Owner when cancelled: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC) - Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta) - Owner type: Corporation - Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N751NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=751NW - Page: https://openairdocs.org/deregistered/N751NW-2011-02-09 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-9-41: https://openairdocs.org/model/mcdonnell-douglas-dc-9-41.md ## Service difficulty reports (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DALA1029699751](https://openairdocs.org/sdr/DALA1029699751), Oct 27, 2010: BATTERY. NOT SEATED. DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN ROWS 9-10 OF THE CABIN WERE INOPERATIVE. MAINTENANCE RE-SEATED THE BATTERIE - [SDR DALA1023499751](https://openairdocs.org/sdr/DALA1023499751), Sep 20, 2010: BATTERY PACK. INOPERATIVE. DURING MX CHECK FOUND LT AFT EMERGENCY EXIT LIGHT INOP, REPLACED BATTERIES AND TESTS, OK. - [SDR DALA102489751](https://openairdocs.org/sdr/DALA102489751), Feb 1, 2010: STRINGER. DAMAGED. DURING GROUND OPERATIONS STR 19 LT WAS DAMAGED AT BS 235. REPAIRED IAW ERA 479576-14. - [SDR DALA102479751](https://openairdocs.org/sdr/DALA102479751), Feb 1, 2010: SKIN. DAMAGED. DURING GROUND OPERATIONS FUSELAGE SKIN WAS DAMAGED AT BS 235 S19L. REPAIRED IAW ERA 479576-14. - [SDR DALA100549751](https://openairdocs.org/sdr/DALA100549751), Jan 18, 2010: FLOOR PANEL. CRACKED. DURING "L" CHECK FOUND CRACKED FASTENER HOLE ON FLOOR PANEL NR 63. REPAIRED IAW SRM 51-30-1. - [SDR DALA100529751](https://openairdocs.org/sdr/DALA100529751), Jan 18, 2010: SKIN. GOUGED. DURING "L" CHECK FOUND 4 GOUGES IN FUSELAGE SKIN AT BS 1154 BETWEEN L22R AND L23R. REPAIRED IAW SRM 53-01 AND DWG 09A51-37583. - [SDR DALA100539751](https://openairdocs.org/sdr/DALA100539751), Jan 16, 2010: PAN. CRACKED. DURING "L CHECK AND INSPECTION IAW EA 98-89790 FOUND CRACK IN LT FWD EMERGENCY DOOR PAN BEYOND PREVIOUS STOP DRILL. REPLACED LT FORWARD EMERGENCY EXIT DOOR IAW - [SDR DALA100519751](https://openairdocs.org/sdr/DALA100519751), Jan 16, 2010: FORMER. LOOSE. DURING "L" CHECK FOUND 3 EA BLIND FASTENERS LOOSE IN VERTICAL STABILIZER FORMER. REPAIRED IAW SRM 55-30-0, SRM 55-31-0 & SRM 51-30-8. - [SDR NWAA093219751](https://openairdocs.org/sdr/NWAA093219751), Sep 15, 2009: DUCT. RUPTURED. DURING CLIMB ENGINE FIRE INDICATION FOR THE NR 1 ENGINE ENUNCIATED. FLIGHT CREW COMPLIED WITH COM, FIRE EXTINGUISHER WAS ACTIVATED AND THE NR 1 ENGINE WAS SHUT - [SDR NWAA091849751](https://openairdocs.org/sdr/NWAA091849751), May 21, 2009: BULKHEAD. CRACKED. DURING OVERNIGHT CHECK VISIT FOR REPEAT INSPECTIONS PER SB 53-264, FOUND CRACK INDICATION ON LT AFT PRESSURE BULKHEAD WEB STATION Z=63.5 AT OUTBOARD EDGE OF DOO - [SDR NWAA082709751](https://openairdocs.org/sdr/NWAA082709751), Jun 12, 2008: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 13-15 OF THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND IMPROPER INSTALLATION OF - [SDR NWAA080799751](https://openairdocs.org/sdr/NWAA080799751), Mar 2, 2008: WIRE. DISCONNECTED. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR ROWS 5, 6, 7, 8, 14, AND 17 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND A DISCO - [SDR NWAA080709751](https://openairdocs.org/sdr/NWAA080709751), Feb 21, 2008: OIL SYSTEM. OVERSERVICED. THE FLIGHT ATTENDANT AND PASSENGER BOTH REPORTED A BURNING ODOR IN THE CABIN. FLIGHT CONTINUED AS SCHEDULED AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE INSP - [SDR NWAA080039751](https://openairdocs.org/sdr/NWAA080039751), Jan 5, 2008: ACM. ODOR. ON FINAL APPROACH INTO MSP, ODOR OF SMOKE FILLED THE AFT CABIN SECTION. THE AFT LAVATORY SMOKE DETECTOR WENT INTO ALARM AND ILLUMINATED THE WARNING INDICATOR IN - [SDR NWAA072169751](https://openairdocs.org/sdr/NWAA072169751), Jun 13, 2007: YAW DAMPER. MALFUNCTIONED. IN LEVEL FLIGHT AT 12,000 FT AND 250 KNOTS WITH AUTOPILOT OFF, THE PILOT IN COMMAND EXPERIENCED UNRESPONSIVE RUDDER CONTROL. THE CAPTAIN REQUESTED THE FIRST OFF - [SDR NWAA071519751](https://openairdocs.org/sdr/NWAA071519751), Apr 21, 2007: WEB. CRACKED. DURING SCHEDULED ENGINE CHANGE, FOUND CRACK IN LOWER EDGE OF RT PYLON CLOSURE WEB LIGHTENING HOLE AT STA YN 164. REPAIRED PER EA 97-208937. - [SDR NWAA070749751](https://openairdocs.org/sdr/NWAA070749751), Mar 3, 2007: FCU. MALFUNCTIONED. DURING DESCENT, AT 14,000 FT, NR 1 ENGINE FLAMED OUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FUEL PUMP - [SDR 0104309751](https://openairdocs.org/sdr/0104309751), Jun 21, 2001: FORMER. CRACKED. During Inspection in CMH a crack was found in the -45 former. The crack extended from the O/B most fastener hole. Repaired per EA 97-181291. - [SDR 0003939751](https://openairdocs.org/sdr/0003939751), Oct 14, 2000: WIRE. SHORTED. DURING PREFLIGHT CHECK, FOUND EMERGENCY LIGHTS CHARGER CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND IT TRIPPED AGAIN. REPLACED A WIRE SHORTING TO GROUND. - [SDR 9901579751](https://openairdocs.org/sdr/9901579751), Apr 22, 1999: TRACK. BROKEN. SLAT DISAGREEMENT OCCURRED ON LANDING INTO MSP, CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AND AIRCRAFT LANDED WITHOUT INCIDENT USING FLAPS ONLY. MAINTENANCE - [SDR 9810559751](https://openairdocs.org/sdr/9810559751), Dec 1, 1998: ACM. INOPERATIVE. DURING CLIMB-OUT, THE FLIGHT CREW REPORTED AN AERIAL TYPE SMELL COMING FROM THE GALLEY AREA. FLIGHT CREW PERFORMED ON AIR CONDITIONING SMOKE PROCEDURE, DECLARED - [SDR 9805749751](https://openairdocs.org/sdr/9805749751), Apr 2, 1998: PRESS SWITCH. ERRATIC. DURING CLIMB-OUT FROM DTW, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED UPON SELECTION OF WING ANTI-ICE. FLIGHT WAS DIVERTED TO IND AND LANDED WIT - [SDR 9805099751](https://openairdocs.org/sdr/9805099751), Mar 26, 1998: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND WING/NACELLE EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED RELAY R2-213, BATTERY PACKS AND RELAMPED LIGHTS, OPERATIONAL CHECK NO - [SDR 9803529751](https://openairdocs.org/sdr/9803529751), Feb 27, 1998: WIRE. LOOSE. DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. TIGHTENED LOOSE WIRE AT BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9803279751](https://openairdocs.org/sdr/9803279751), Feb 23, 1998: CONTROL CABLE. OUT OF ADJ. DURING CLIMB-OUT, THE AUTO SPOILER DO NOT USE INDICATION ILLUMINATED AND THE AUTOMATIC PRESSURIZATION CONTROL BECAME INOPERATIVE AFTER LANDING GEAR RETRACTION. - [SDR 9705049751](https://openairdocs.org/sdr/9705049751), Mar 7, 1997: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND LEFT OVERWING DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES B5-32. OPERATIONAL CHECK OK. - [SDR 9703649751](https://openairdocs.org/sdr/9703649751), Feb 18, 1997: STRUT. REQD SERVICE. AFTER TAKEOFF FROM FAR, UNABLE TO RETRACT GEAR. NOSE GEAR STEERABLE. FLIGHT RETURNED TO FAR AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR STRUT FLAT. REPACKED NO - [SDR 9703129751](https://openairdocs.org/sdr/9703129751), Feb 11, 1997: TERMINAL. BROKEN. PITOT HEAT OFF LIGHT REMAINED ILLUMINATED CONTINUOUSLY FOR FIFTEEN MINUTES THEN STARTED TO FLICKER. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR 9610799751](https://openairdocs.org/sdr/9610799751), May 15, 1996: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE ON FIRST CLASS FLOOR TRACK. REPLACED BATTERIES IN BATTERY PACKS. OPERATIONAL CHECK OK. - [SDR 9608839751](https://openairdocs.org/sdr/9608839751), Apr 17, 1996: ANGLE. CRACKED. DURING H-CHECK, FOUND A TWO INCH CRACK IN THE RIGHT SIDE DORSAL FIN ATTACH ANGLE FS 1171. REPAIRED ANGLE (P/N 5912141-60) PER EA 97-109496. - [SDR 9611529751](https://openairdocs.org/sdr/9611529751), Apr 12, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 794. REPLACED FITTING (P/N 5924878-505) PER EA 97-109495. - [SDR 9608509751](https://openairdocs.org/sdr/9608509751), Apr 11, 1996: ACT FITTING. CRACKED. DURING H-CHECK, FOUND A TWO INCH CRACK IN THE RIGHT MAIN LANDING GEAR INBOARD DOOR RETURN CYLINDER SUPPORT FITTING AT THE KEEL. REPLACED FITTING PER SRM 51-30-5 - [SDR 9608759751](https://openairdocs.org/sdr/9608759751), Apr 10, 1996: FLOOR BEAM. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 1041 FLOOR BEAM AT APPROXIMATELY LBL 18. REPAIRED BEAM (P/N 9958212-3) PER EA 97-109477. - [SDR 9608749751](https://openairdocs.org/sdr/9608749751), Apr 10, 1996: FLOOR BEAM. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 1056 FLOOR BEAM AT APPROXIMATELY LBL 26 AND RBL 34. REPAIRED BEAM (P/N 9958187-1) PER EA 97-109476. - [SDR 9608499751](https://openairdocs.org/sdr/9608499751), Apr 10, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE AFT ENTRY DOOR BEAM RIGHT SIDE END FITITNGS; NR 1 UPPER, NR 3 UPPER AND LOWER AND NR 4 UPPER. REPLACED ALL FITTINGS PER SRM - [SDR 9608469751](https://openairdocs.org/sdr/9608469751), Apr 10, 1996: LATCH FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR UPPER LATCH FITTING. REPLACED FITTING PER SRM 51-30-2. - [SDR 9608059751](https://openairdocs.org/sdr/9608059751), Apr 6, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LONGERON 28L END FITTING AT FS 1072. REPLACED FITTING PER SRM 51-30-2 AND 51-30-5. - [SDR 9608049751](https://openairdocs.org/sdr/9608049751), Apr 4, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 984 FRAME FITTING AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30-5 AND 51-30-1. - [SDR 9606869751](https://openairdocs.org/sdr/9606869751), Mar 23, 1996: WIRE. BROKEN. DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 6 TO 13. REPAIRED BROKEN WIRE AND OPERATIONAL CHECK GOOD. - [SDR 9521959751](https://openairdocs.org/sdr/9521959751), Dec 30, 1995: ACTUATOR. LEAKING. LOSS OF RIGHT HYDRAULIC SYSTEM OCCURRED DURING APPROACH INTO MSP. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FO - [SDR 9521979751](https://openairdocs.org/sdr/9521979751), Dec 29, 1995: STRUT. DEFLATED. NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPACKED NOSE GEAR STRUT AND - [SDR 9517329751](https://openairdocs.org/sdr/9517329751), Nov 2, 1995: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT SEVERAL ROWS INOPERATIVE. REPLACED THREE SETS OF BATTERY PACKS, OPERATIONAL CHECK GOOD. - [SDR 9517589751](https://openairdocs.org/sdr/9517589751), Oct 2, 1995: SKIN. CRACKED. DURING B-CHECK, FOUND TWO, 2 INCH CRACKS IN THE RIGHT ELEVATOR LOWER SKIN AT STA 658. REPAIRED PER EA 97-102591. - [SDR 9507369751](https://openairdocs.org/sdr/9507369751), May 1, 1995: INDICATION. MALFUNCTIONED. DURING CLIMBOUT FROM DTW, ALL THREE LANDING GEAR RED UNSAFE LIGHTS AND DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR HANDLE AND ALL INDICA - [SDR 9504329751](https://openairdocs.org/sdr/9504329751), Mar 15, 1995: SWITCHES. MALFUNCTIONED. STALL INDICATION FAILURE LIGHT AND STICK SHAKER ACTIVATED DURING SLAT RETRACTION AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED SLA - [SDR 9503489751](https://openairdocs.org/sdr/9503489751), Mar 6, 1995: UPLIMIT SWITCH. MALFUNCTIONED. NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DURING CLIMB-OUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE GEAR UP ## 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 19920813038259I](https://openairdocs.org/incident/19920813038259I), Aug 13, 1992: Doug DC941 (N751NW), Buffalo, NY. NR1 engine oil filter by-pass light on. Shut engine down. Diverted to Buffalo. Replaced oil screen. --- 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.