# N941N: 1969 Mcdonnell Douglas DC-9-32, registration cancelled 2009-07-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 29, 2009 - Status when cancelled: Sale reported - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D-5](https://openairdocs.org/engine/pratt-whitney-jt8d-5) (registry code 52046) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47450 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 31, 1973 - Last registry action: July 29, 2009 - Mode S code: AD120B - 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/N941N - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=941N - Page: https://openairdocs.org/deregistered/N941N-2009-07-29 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-9-32: https://openairdocs.org/model/mcdonnell-douglas-dc-9-32.md ## Service difficulty reports (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0401319919](https://openairdocs.org/sdr/0401319919), Aug 10, 2004: LINE. RUPTURED. FLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE - [SDR 0202999919](https://openairdocs.org/sdr/0202999919), Sep 22, 2002: CYLINDER. FAILED. THE RIGHT MAIN LANDING GEAR COLLAPSED DURING TAXI TO RUNWAY. PRELIMINARY INVESTIGATION REVEALED A FAILED MAIN LANDING GEAR STRUT CYLINDER BARREL. - [SDR 0203319919](https://openairdocs.org/sdr/0203319919), Sep 4, 2002: LONGERON. CRACKED. During an Hck in ATL, an existing repair was found cracked. The crack at station 320 was repaired per EA. 99-190665. - [SDR 0203099919](https://openairdocs.org/sdr/0203099919), Sep 4, 2002: LONGERON. CRACKED. During HCK in ATL, an existing repair had been found cracked. The repair at station 320 was repaired per EA 99-190665. - [SDR 0202319919](https://openairdocs.org/sdr/0202319919), Jul 17, 2002: ACM. FLIGHT ATTENDANT REPORTED SLIGHT HAZE, FUMES, AND THE AFT LAV SMOKE DETECTOR SOUNDED DURING TAKEOFF. SYMPTOMS LASTED A COUPLE OF MINUTES THEN CLEARED AND THE AL - [SDR 0202059919](https://openairdocs.org/sdr/0202059919), Jun 30, 2002: SMOKE. DETECTED. THE FORWARD LAV SMOKE DETECTOR ACTIVATED IMMEDIATELY AFTER TAKEOFF AND THE LEAD FLIGHT ATTENDANT OBSERVED SMOKE IN THE CABIN. FLIGHT RETURNED TO MSP AND LANDED - [SDR 0201089919](https://openairdocs.org/sdr/0201089919), Mar 30, 2002: LINE. LOOSE. WHILE CRUISING AT FL260 WITH ENGINE AND AIRFOIL ANTI-ICE ON, THE CABIN BEGAN A 500 FPM CLIMB. PACK SUPPLY PRESSURE INDICATED 25 PSI ON BOTH PACKS. TURNING OFF T - [SDR 9900899919](https://openairdocs.org/sdr/9900899919), Mar 9, 1999: WIRE. FAILED. EN ROUTE MSP-IAD, C PHASE OF LEFT GENERATOR BUS CIRCUIT BREAKERS POPPED FOLLOWED BY ALL ROW H FUEL PUMP CIRCUIT BREAKERS. CREW DECLARED AN EMERGENCY AND FLIGHT - [SDR 9806639919](https://openairdocs.org/sdr/9806639919), Apr 14, 1998: FUSE. BLOWN. DURING LINE CHECK, FOUND ESCAPE PATH LIGHTING AT SEAT ROWS 8 THRU 10 INOPERATIVE. MAINTENANCE REPLACED FUSE, OPERATIONAL CHECK NORMAL. - [SDR 9802699919](https://openairdocs.org/sdr/9802699919), Feb 15, 1998: FUSE. BLOWN. DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 11 AND 13 INOPERATIVE. REPLACED BLOWN FUSE. OPERATIONAL CHECK NORMAL. - [SDR 9713409919](https://openairdocs.org/sdr/9713409919), Jul 7, 1997: RADAR TR UNIT. FAILED. WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER AND ANTENNA, OPERATION - [SDR 9712499919](https://openairdocs.org/sdr/9712499919), Jun 24, 1997: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. - [SDR 9711159919](https://openairdocs.org/sdr/9711159919), Jun 7, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9710529919](https://openairdocs.org/sdr/9710529919), Jun 1, 1997: EPR INDICATOR. FAILED. AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICAITON WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE - [SDR 9708899919](https://openairdocs.org/sdr/9708899919), May 2, 1997: STRUT. REQD SERVICE. AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR, NOSE WHEEL WAS STEERABLE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO YHZ. FLIGHT LANDED WITHOUT I - [SDR 9708889919](https://openairdocs.org/sdr/9708889919), May 2, 1997: STRUT. FAILED. AFTER TAKEOFF FROM YHZ, UNABLE TO RAISE GEAR. NOSE GEAR REMAINED STEERABLE WITH AIRCRAFT IN GROUND MODE. FLIGHT RETURNED TO YHZ AND LANDED WITHOUT INCIDENT. FOU - [SDR 9705789612](https://openairdocs.org/sdr/9705789612), Mar 19, 1997: FUEL CONTROL. MALFUNCTIONED. DURING TAKEOFF ROLL AT 80 KNOTS, THE RIGHT ENGINE N1 AND EPR INDICATIONS ROSE ABOVE PRESET LIMITS. TAKEOFF WAS ABORTED AND DURING TAXI, THE RIGHT ENGINE WOULD N - [SDR 9705569919](https://openairdocs.org/sdr/9705569919), Mar 17, 1997: PRESS SWITCH. MALFUNCTIONED. EN ROUTE MSP-HPN, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH TAIL DEICE SELECTED. RESET CIRCUIT BREAKER WITH NO HELP. FLIGHT DIVERTED TO DT - [SDR 9701319919](https://openairdocs.org/sdr/9701319919), Jan 22, 1997: LONGERON. CRACKED. DURING H-CHECK, FOUND LONGERON 29L CRACKED IN THE FORWARD CARGO COMPARTMENT. REPAIRED PER EA 99-122034. - [SDR 9623349919](https://openairdocs.org/sdr/9623349919), Nov 2, 1996: INDICATION BULBS. FAILED. DURING APPROACH, NOSE GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. CREW EXECUTED GO-AROUND PROCEDURES AND TOWER REPORTED THAT GEAR APPE - [SDR 9620929919](https://openairdocs.org/sdr/9620929919), Sep 27, 1996: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND BOTH AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9614609919](https://openairdocs.org/sdr/9614609919), Jul 1, 1996: SWITCH. MALFUNCTIONED. DURING APPROACH, LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT I - [SDR 9613929919](https://openairdocs.org/sdr/9613929919), Jun 24, 1996: STALL WARN COMP. MALFUNCTIONED. STALL WARNING SYSTEM ACTIVATED ON ROTATION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT STALL WARNING COMPUTER AND RIGHT AOA T - [SDR 9609469919](https://openairdocs.org/sdr/9609469919), Apr 29, 1996: PT7 LINE. BROKEN. ON POWER REDUCTION AFTER TAKEOFF, THE NR 1 EPR INDICATION BECAME ERRATIC. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A BROKE - [SDR 9605699919](https://openairdocs.org/sdr/9605699919), Mar 7, 1996: SWITCH. DIRTY. DURING APPROACH INTO SLC, AMBER GEAR DOOR LIGHT CAME ON AFTER GEAR WAS EXTENDED. CREW DID GO-AROUND DURING WHICH GEAR DOOR LIGHT EXTINGUISHED. EMERGENCY EQUIPME - [SDR 9604969919](https://openairdocs.org/sdr/9604969919), Feb 22, 1996: GUIDE PINS. WORN. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE TAIL CONE HANDLE AND THAT THE TAIL CONE DID NOT DROP. ALSO, FOUND 16 WORN GUIDE PINS AND - [SDR 9521939919](https://openairdocs.org/sdr/9521939919), Dec 29, 1995: SHOCK STRUT. FAILED. DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. UTILIZED LANDING GEAR RELEASE BUTTON AND LANDING GEAR RETRACTED. AIRCRAFT DID NOT SHIFT INTO FLIGHT MODE UNITL - [SDR 9520059919](https://openairdocs.org/sdr/9520059919), Dec 9, 1995: RETRACT MECH. OUT OF ADJUST. DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRACTION BY USING LANDING GEAR HANDLE RELEASE BUTTON. RECYCLED LANDING GEAR AND LANDING GE - [SDR 9520069919](https://openairdocs.org/sdr/9520069919), Dec 7, 1995: RETRACT MECH. LACK OF LUBE. DURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BIL AND LANDED WITHOUT INCIDENT. REMOVED AND LUBRICATED APEX BOLT ON NOSE LANDING GEAR TR - [SDR 9510899919](https://openairdocs.org/sdr/9510899919), Jun 1, 1995: SKIN. CRACKED. DURING PERIODIC CHECK, FOUND .50 INCH CRACK IN THE FUSELAGE SKIN EXTENDING FROM THE MAIN CABIN DOOR UPPER AFT DOOR STOP HOLE. REPAIRED PER EA 99-98394. - [SDR 9509219919](https://openairdocs.org/sdr/9509219919), May 30, 1995: BEAM. CRACKED. DURING PERIODIC CHECK, FOUND A .375 INCH CRACK IN THE FORWARD CARGO DOOR LOWER BEAM FORWARD END. REPAIRED BEAM (P/N 5910141-63) PER EA 99-98388. - [SDR 9501099919](https://openairdocs.org/sdr/9501099919), Jan 16, 1995: MLG DOOR. OPEN. LEFT MAIN GEAR DOOR WAS OPEN ON LANDING INTO TUS. REPLACED THE LEFT MAIN GEAR DOOR SEQUENCE VALVE AND ACTUATOR DUE TO DAMAGE INCURRED. LEAK AND OPERATIONAL CHEC ## NTSB investigations (2) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CHI02FA289](https://openairdocs.org/ntsb/CHI02FA289), Sep 22, 2002: McDonnell Douglas DC-9-32 (N941N), Minneapolis, MN, substantial damage. Probable cause: The fatigue failure of the main landing gear strut due to inclusions in the material, residual stresses, and dissolved hydrogen content. - [NTSB CHI79FA047](https://openairdocs.org/ntsb/CHI79FA047), Apr 21, 1979: Douglas DC-9 (N941N), Mosinee, WI, substantial damage ## FAA accident and incident reports (4) 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. - [Accident 20020922037939A](https://openairdocs.org/incident/20020922037939A), Sep 22, 2002: Doug DC932 (N941N), Minneapolis, MN, Substantial damage. (-23) On taxi for departure, the right main landing gear collapsed. The upper strut housing cracked which allowed the inner strut to become free. The… - [Incident 20020715028039I](https://openairdocs.org/incident/20020715028039I), Jul 15, 2002: Doug DC932 (N941N), Omaha, NE. (-23) N941N, DC9-32, being operated by northwest airlines as flight 1526 departed Omaha, NE, enroute to minneapolis, MN. During climb the crew reported smoke… - [Incident 19920322011279I](https://openairdocs.org/incident/19920322011279I), Mar 22, 1992: Doug DC932 (N941N), Detroit, MI, Minor damage. 2 Compressor stalls on takeoff. Aborted. Returned to gate. Engine checked normal. Suspect water and slush ingestion - [Incident 19910702039659I](https://openairdocs.org/incident/19910702039659I), Jul 2, 1991: Doug DC932 (N941N), Great Falls, MT. Gear warning light. Gear appeared down. Landed safely. Connecting rod from gear to gear door broke. --- 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.