# N756NW: 1968 Douglas DC-9-41, registration cancelled 2013-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Douglas DC-9-41](https://openairdocs.org/model/douglas-dc-9-41) (registry code 302207N) - 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: 47180 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: April 2, 1992 - Last registry action: February 7, 2012 - Mode S code: AA3194 - Location: [Mcminnville, OR](https://openairdocs.org/faa-place/OR/Mcminnville) - Owner type: Individual - Owner's area on the map: 45.2117° N, 123.2817° W: Placed by OpenAirDocs at the center of ZIP code 97128, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N756NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=756NW - Page: https://openairdocs.org/deregistered/N756NW-2013-08-23 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 Douglas DC-9-41: https://openairdocs.org/model/douglas-dc-9-41.md ## Service difficulty reports (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NWAA080689756](https://openairdocs.org/sdr/NWAA080689756), Feb 27, 2008: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. THE BATTERY PACK AT THE FORWARD CAB - [SDR 0601989756](https://openairdocs.org/sdr/0601989756), Sep 5, 2006: DOOR FRAME. CRACKED. DURING H-CHECK FOUND CRACKS IN THE LOWER AFT CORNER OF FWD SERVICE DOOR JAMB. REPAIRED PER EA 97-206872. - [SDR 0401039756](https://openairdocs.org/sdr/0401039756), Jun 22, 2004: DUCT. DAMAGED. DURING SLAT RETRACTION AFTER TAKEOFF, THE AIRCRAFT ROLLED TO THE LEFT ACCOMPANIED BY THE SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES WHICH REQUIRED TH - [SDR 0203209756](https://openairdocs.org/sdr/0203209756), Sep 13, 2002: SKIN. CRACKED. While in DHN for Hck, a .44 inch crack was found in the skin at a fastener hole 5" above Longeron 18 right. Repaired per EA 97-191331. - [SDR 9900629756](https://openairdocs.org/sdr/9900629756), Feb 18, 1999: BULKHEAD DOUBLER. CRACKED. DURING PERIODIC CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL LOWER RIGHT CORNER DOUBLER CRACKED AT LONGERONS 10R THRU 14R. REPAIRED PER EM 5310-01012. - [SDR 9806959756](https://openairdocs.org/sdr/9806959756), Apr 20, 1998: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS CABIN AREA DIM WHEN OPERATED. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL - [SDR 9806699756](https://openairdocs.org/sdr/9806699756), Apr 15, 1998: BATTERY. INOPERATIVE. FLIGHT ATTENDANT REPORTED THE EMERGENCY FLASHLIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATIONAL CHECK NORMAL. - [SDR 9800699756](https://openairdocs.org/sdr/9800699756), Jan 11, 1998: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT FORWARD GALLEY DOOR, FORWARD CABIN OVERHEAD, FLOOR PROXIMITY, AND AFT STAIRS INOPERATIVE. REPLACED - [SDR 9724599756](https://openairdocs.org/sdr/9724599756), Dec 31, 1997: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND A SECTION OF EMERGENCY LIGHTS INOPERATIVE IN CEILING. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL CHECK OK. - [SDR 9706439756](https://openairdocs.org/sdr/9706439756), Mar 21, 1997: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. - [SDR 9701939756](https://openairdocs.org/sdr/9701939756), Jan 27, 1997: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND CENTER CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK OK. - [SDR 9619109756](https://openairdocs.org/sdr/9619109756), Aug 27, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER FRONT SPAR GUSSET FITTING LEFT SIDE AT FS 155. REPLACED FITTING PER SRM 51-30-2, 51-30-5. - [SDR 9619089756](https://openairdocs.org/sdr/9619089756), Aug 26, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING NR 4 FLAP HINGE FITTING INBOARD INTERIOR FLAP WELL. REPLACED FITTING PER SRM 51-30-2. - [SDR 9619079756](https://openairdocs.org/sdr/9619079756), Aug 26, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A 4 INCH CRACK IN THE LEFT WING FALSE SPAR TO MAIN LANDING GEAR ATTACH FITTING. REPLACED FITTING (P/N 3912765-503) PER SRM 51-30-5. - [SDR 9619069756](https://openairdocs.org/sdr/9619069756), Aug 26, 1996: DOUBLER. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE RIGHT MAIN LANDING GEAR SUPPORT UPPER DIAMOND DOUBLER. REPLACED DOUBLER (P/N 5912438-2) PER DWG 9910010, 5910464. - [SDR 9621539756](https://openairdocs.org/sdr/9621539756), Aug 24, 1996: SPAR. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE RIGHT WING REAR SPAR LOWER CAP AT XRS 164. REPAIRED CAP (P/N 5911301) PER EA 97-110758. - [SDR 9619059756](https://openairdocs.org/sdr/9619059756), Aug 24, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 794. REPLACED FITTING (P/N 5924878-501) PER EA 97-110748. - [SDR 9618119756](https://openairdocs.org/sdr/9618119756), Aug 18, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LONGERON 26R END FITTING AT FS 1019. REPLACED FITTING (P/N 4912798-507) PER SRM 51-30-5. - [SDR 9614679756](https://openairdocs.org/sdr/9614679756), Jul 4, 1996: FIRE LOOP. MALFUNCTIONED. DURING CLIMBOUT, THE LEFT ENGINE FIRE WARNING SOUNDED. FOLLOWED ENGINE FIRE PROCEDURE AND FIRE INDICATION CONTINUED. DISCHARGED BOTH FIRE BOTTLES, RETURNED TO M - [SDR 9600859756](https://openairdocs.org/sdr/9600859756), Jan 13, 1996: PRESS SWITCH. MALFUNCTIONED. EN ROUTE DTW-YHZ, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT REMAINED ON DURING WING ANTI-ICE OPERATION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. - [SDR 9502499756](https://openairdocs.org/sdr/9502499756), Feb 10, 1995: TRACK. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON RIGHT CARGO TRACK UPPER SURFACE IN THE AFT CARGO COMPARTMENT. REPLACED TRACK PER EA 97-096677. - [SDR 9502489756](https://openairdocs.org/sdr/9502489756), Feb 10, 1995: JAMB. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION IN FORWARD CARGO DOOR JAMB PAN AFT SIDE. REPAIRED PER EA 97-096686. - [SDR 9502479756](https://openairdocs.org/sdr/9502479756), Feb 10, 1995: SKIN. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION AT THE SKIN BUTT JOINT FS 401 - 406 AT THE FORWARD CARGO DOOR LOWER FLANGE. REPAIRED PER EA 97-096671. - [SDR 9502469756](https://openairdocs.org/sdr/9502469756), Feb 10, 1995: STRINGER. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN LONGERON 16R, PARTIAL CRACK AT FS 370 AND CRACKED COMPLETELY THROUGH AT FS 389 AND FS 408. REPAIRED PER EA 97-093818. - [SDR 9502059756](https://openairdocs.org/sdr/9502059756), Feb 9, 1995: LATCHES. OUT OF ADJUST. DURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ADJUSTED THE LATCHES. CHECKED OK. - [SDR 9502259756](https://openairdocs.org/sdr/9502259756), Feb 8, 1995: FITTING. CRACKED. DURING PERIODIC CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD VAULT DOOR UPPER RIGHT STOP FITTING AND SILL. ALSO, FOUND A CRACK IN THE SILL AT THE UPPER LEFT - [SDR 9502239756](https://openairdocs.org/sdr/9502239756), Feb 7, 1995: FRAME. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON WINDOW CUTOUT 25L. REPAIRED PER EA 97-72509. - [SDR 9502209756](https://openairdocs.org/sdr/9502209756), Feb 6, 1995: FITTING. RUSTED. DURING PERIODIC CHECK, FOUND RUST ON THE LOWER SURFACE OF THE LOWER 'BEAVER TAIL' FITTING AND UPPER AND LOWER SURFACES OF THE UPPER 'BEAVER TAIL' FITTING. REPLA - [SDR 9502149756](https://openairdocs.org/sdr/9502149756), Feb 3, 1995: FITTING. RUSTED. DURING PERIODIC CHECK, FOUND RUST ON THE UPPER SURFACE OF THE UPPER 'BEAVER TAIL' FITTING AND THE LOWER SURFACE OF THE LOWER 'BEAVER TAIL' FITTING RIGHT PYLON F - [SDR 9502139756](https://openairdocs.org/sdr/9502139756), Feb 2, 1995: FRAME. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN THE LEFT FORWARD EMERGENCY EXIT DOOR PAN AT THE NR 14 STOP FITTING. REPAIRED PAN PER EA 97-093728. - [SDR 9502129756](https://openairdocs.org/sdr/9502129756), Feb 2, 1995: FRAME. CRACKED. DURING PERIODIC CHECK, FOUND CRACK IN MAIN CABIN DOOR NR 7 BEAM AFT END IN THE RADIUS. REPLACED END FITTING AND REPAIRED THE BEAM PER SRM 52-05, FIG.31. ## Other aircraft with N756NW - [Cancelled 1981-01-31](https://openairdocs.org/deregistered/N756NW-1981-01-31): Cessna U206G, S/N U20604233. Exported to Canada. Owner: [Island Air Service Inc](https://openairdocs.org/faa-owner/ISLAND%20AIR%20SERVICE%20INC), [Kodiak, AK](https://openairdocs.org/faa-place/AK/Kodiak) --- 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.