# N758NW: 1968 Mcdonnell 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: [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: 47286 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 5, 1992 - Last registry action: February 7, 2012 - Mode S code: AA3902 - 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/N758NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=758NW - Page: https://openairdocs.org/deregistered/N758NW-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 Mcdonnell Douglas DC-9-41: https://openairdocs.org/model/mcdonnell-douglas-dc-9-41.md ## Service difficulty reports (37) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NWAA083959758](https://openairdocs.org/sdr/NWAA083959758), Aug 19, 2008: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE LT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHT RETURNED TO - [SDR NWAA083119758](https://openairdocs.org/sdr/NWAA083119758), Jul 13, 2008: OUTFLOW VALVE. MALFUNCTIONED. WHILE EN ROUTE TO DTW THE ACFT EXPERIENCED A LOSS OF CABIN PRESSURIZATION CONTROL WHICH REQUIRED AN EMERGENCY DESCENT TO FL140. OXYGEN MASK DID NOT DEPLOY AND T - [SDR NWAA080389758](https://openairdocs.org/sdr/NWAA080389758), Feb 4, 2008: O-RING. FAILED. IN CRUISE FLT AT FL310, THE RT HYD SYS FAILED. QTY AND PRESSURE WERE BOTH LOST REQUIRING CREW TO SECURE SYSTEM. FLT CONTINUED AS SCHEDULED AND THE EMERGENCY GEA - [SDR NWAA071089758](https://openairdocs.org/sdr/NWAA071089758), Mar 2, 2007: DOOR FRAME. DAMAGED. DURING "H" CHECK, FOUND FORWARD CARGO DOOR JAMB DOUBLER WITH MULTIPLE OVERSIZED HOLES. REPAIRED PER EA 97-208465 SECTION I. SECTION II REQUIRES INSPECTIONS AT " - [SDR 0501009758](https://openairdocs.org/sdr/0501009758), Jul 12, 2005: APU. LEAKING. DURING CLIMB, AFT RT LAV SMOKE DETECTOR SOUNDED AND FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN AREA. NO FIRE DETECTED. FLIGHT CREW RETURNED A/C TO DEPARTURE AIR - [SDR 0400949758](https://openairdocs.org/sdr/0400949758), May 6, 2004: SKIN. CRACKED. DURING L-CHECK FOUND CRACKS IN FUSELAGE LT & RT NOSE SKIN AT BS 69.5. REPAIRED PER EA 97-198147. - [SDR 0103939758](https://openairdocs.org/sdr/0103939758), Oct 17, 2001: PAD. CRACKED. DURING A RON IN DTW, A CHAFE PAD LOCATED ON THE AFT DOOR JAMB ON THE RHS AFT EMERGENCY EXIT WAS FOUND CRACKED. IN SPITE OF THE DAMAGE, THE CHAFE WAS REPORTED SE - [SDR 0103639758](https://openairdocs.org/sdr/0103639758), Oct 17, 2001: SHIM. CRACKED. During a RON in DTW, A shim angle P/N 5919159-15 located on the aft door jamb on the RHS aft emergency exit was found cracked. Repaired per EA 97-185229. - [SDR 9905269758](https://openairdocs.org/sdr/9905269758), Dec 4, 1999: PUMP. FAILED. DURING CRUISE FLIGHT, THE RIGHT ENGINE FLAMED OUT AT FL350; SMOOTH AIR, NO VIBRATION, AND NO RELIGHT. THE RIGHT ENGINE WAS WINDMILLED AT 17-22 PERCENT AND POSIT - [SDR 9904469758](https://openairdocs.org/sdr/9904469758), Sep 2, 1999: CARGO TRACK. CORRODED. DURING SCHEDULED INSPECTION, FOUND CORROSION ON THE OUTBOARD FLANGE OF THE CARGO TIE DOWN TRACK (S2922357), FS 408 - 427. BLEND OUT WAS BELOW SRM LIMITS. REPAIR - [SDR 9903699758](https://openairdocs.org/sdr/9903699758), Aug 24, 1999: DOUBLER. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION BETWEEN SKIN AND DOOR DOUBLER. TRIMMED FORWARD CARGO DOOR DOUBLER BETWEEN LOWER FORWARD AND AFT CORNERS PER EA 169077. - [SDR 9904649758](https://openairdocs.org/sdr/9904649758), Aug 19, 1999: CHANNEL. CRACKED. DURING APB INSPECTIONS, A 1.25 CRACK WAS FOUND IN THE UPPER INBOARD BEND RADIUS OF THE LEFT CHANNEL 5910130-9. REPAIRED PER EA 97-169048. - [SDR 9903679758](https://openairdocs.org/sdr/9903679758), Aug 12, 1999: BULKHEAD. CORRODED. DURING PERIODIC CHECK, CORROSION WAS FOUND IN RIGHT SLANT PRESSURE PANEL FS 737. REPAIRED PER EA 97-168991. - [SDR 9808009758](https://openairdocs.org/sdr/9808009758), May 2, 1998: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9807999758](https://openairdocs.org/sdr/9807999758), May 2, 1998: BULBS. NOT SECURE. DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 20 THRU 23 INOPERATIVE. SECURED BULBS IN SOCKETS, OPERATIONAL CHECK NORMAL. - [SDR 9805779758](https://openairdocs.org/sdr/9805779758), Apr 2, 1998: WIRE. FAILED. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT AND IN VENTRAL STAIR AREA INOPERATIVE. REPAIRED WIRING AT S3-156. OPERATIONAL - [SDR 9802619758](https://openairdocs.org/sdr/9802619758), Feb 11, 1998: CONNECTOR. LOOSE. DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT RIGHT FORWARD EMERGENCY EXIT AND BETWEEN ROWS 5 THROUGH 8 INOPERATIVE. MAINTNANCE FOUND LOOSE CONN - [SDR 9802609758](https://openairdocs.org/sdr/9802609758), Feb 10, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9800709758](https://openairdocs.org/sdr/9800709758), Jan 11, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT AND FIRST FOUR RIGHT MAIN CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY P - [SDR 9700809758](https://openairdocs.org/sdr/9700809758), Jan 13, 1997: PACKS. FAILED. DURING CLIMBOUT, BOTH PACKS SHUT DOWN AND AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE ASSIGNED MEL 21-5A. - [SDR 9617569758](https://openairdocs.org/sdr/9617569758), Aug 3, 1996: FLOOR BEAM. CORRODED. DURING H-CHECK, FOUND CORROSION IN THE CENTER LINE FLOOR CAP BL 0 FROM FS 218 TO 237. REPAIRED CAP (P/N 5910137-9) PER EA 97-110704. - [SDR 9617549758](https://openairdocs.org/sdr/9617549758), Aug 1, 1996: PRESS WEB. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE WEB FS 105 AT BL 25 AND 37 LEFT AND RIGHT. REPAIRED WEB (P/N 9910073-313) P - [SDR 9616799758](https://openairdocs.org/sdr/9616799758), Aug 1, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE AFT ENTRY DOOR AT THE UPPER LEFT DOOR STOP. REPLACED FITTING. - [SDR 9616779758](https://openairdocs.org/sdr/9616779758), Jul 30, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE KEEL LONGERON 30 RIGHT SIDE END FITTING AT FS 699. REPLACED FITTING (P/N 3924029-502N) PER SRM 51-30-5. - [SDR 9616759758](https://openairdocs.org/sdr/9616759758), Jul 29, 1996: LONGERON. CORRODED. DURING H-CHECK, FOUND CORROSION ON LONGERON 29L AND IN ITS END FITTING AT FS 170. REPAIRED LONGERON AND REPLACED FITTING PER SRM 53-02 FIG 2 AND 51-30-2 PG 2 FI - [SDR 9617429758](https://openairdocs.org/sdr/9617429758), Jul 25, 1996: SUPPORT. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE VENTRAL STAIRWAY PRESSURE DOME DOOR SUPPORT. REPAIRED SUPPORT (P/N 9915565-29) PER EA 97-110982. - [SDR 9616539758](https://openairdocs.org/sdr/9616539758), Jul 22, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE AFT CARGO DOOR FORWARD END FITTINGS ON BEAMS NR 2, 3 AND 5. REPLACED FITTINGS PER SRM 51-30-5. - [SDR 9608709758](https://openairdocs.org/sdr/9608709758), Apr 18, 1996: HYD PUMP. FAIL. DURING CLIMB, THE LEFT HYDRAULIC SYSTEM LOST HYDRAULIC PRESSURE. LEFT HYDRAULIC SYSTEM PRESSURE WAS RESTORED WITH ALTERNATE HYDRAULIC PUMP AND RIGHT HYDRAULIC S - [SDR 9604079758](https://openairdocs.org/sdr/9604079758), Feb 17, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND OVERWING AFT LIGHT VERY DIM. REPLACED BATTERIES AND POWER SUPPLY, OPERATIONAL CHECK GOOD. - [SDR 9604689758](https://openairdocs.org/sdr/9604689758), Feb 15, 1996: FITTING. CRACKED. DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE SPOILER SUPPORT FITTING BETWEEN THE INBOARD AND OUTBOARD SPOILERS. REPLACED FITTING PER SRM 51-30-2. - [SDR 9607069758](https://openairdocs.org/sdr/9607069758), Feb 14, 1996: CLIP. CRACKED. DURING SPECIAL MAINTENANCE VISIT, FOUND A CRACK IN THE CENTER WING STRINGER 11R CLIP AT RBL 42 AT THE REAR SPAR. REPLACED CLIP (P/N 4912014) PER EA 97-106790. - [SDR 9516739758](https://openairdocs.org/sdr/9516739758), Oct 25, 1995: BOLT. BROKEN. ON APPROACH DURING SLAT EXTENSION, A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN BOLT A - [SDR 9515359758](https://openairdocs.org/sdr/9515359758), Oct 11, 1995: T-DUCTS. LACK OF LUBE. MEM - DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED ON SLAT EXTENSION. A SLIGHT ROLL WAS EXPERIENCED BEFORE BOTH SLATS WERE FULLY EXTENDED. AN UNEVENTFUL - [SDR 9515169758](https://openairdocs.org/sdr/9515169758), Sep 27, 1995: FRAME. CRACKED. DURING LINE CHECK, FOUND A 2.5 INCH VERTICAL CRACK IN THE FS 756, MAIN FRAME INBOARD AFT FLANGE. REPAIRED FRAME (P/N 9923436-1), PER EA 97-103285. - [SDR 9509699758](https://openairdocs.org/sdr/9509699758), Jun 17, 1995: EPR TRANSMITTER. MALFUNCTIONED. NR 2 ENGINE EPR INDICATION BEGAN DECREASING SHORTLY AFTER DEPARTURE. THE FLIGHT RETURNED TO MSP LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE EPR TRANSMITT - [SDR 9503269758](https://openairdocs.org/sdr/9503269758), Feb 28, 1995: BULKHEAD. CORRODED. DURING LINE CHECK, FOUND CORROSION ON THE CANTED BULKHEAD FS 729 AT LBL 40 BETWEEN THE LOWER CHORD AND WEB. REPAIRED PER EA 97-096744. - [SDR 9500299758](https://openairdocs.org/sdr/9500299758), Jan 6, 1995: AC GEN SYST. MALFUNCTIONED. LOSS OF LEFT DC BUS AND TWO AC PHASE OCCURRED ENROUTE MDT-DTW. FLIGHT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT AC POWER RELAY, VOLTAGE REG ## 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 19991204034519I](https://openairdocs.org/incident/19991204034519I), Dec 4, 1999: Doug DC941 (N758NW), Buffalo, NY. (-23) On Saturday, December 4, 1999, during a flight from pvd to dtw at FL350 in smooth air with no vibration, the right hand engine flamed out of a DC-9-41,… ## Other aircraft with N758NW - [Cancelled 1980-12-01](https://openairdocs.org/deregistered/N758NW-1980-12-01): Cessna R172K, S/N R1723238. Exported to Canada. Owner: [Aviconorth Ltd](https://openairdocs.org/faa-owner/AVICONORTH%20LTD), [Madison, WI](https://openairdocs.org/faa-place/WI/Madison) --- 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.