# N611NA: 1969 Mcdonnell Douglas DC-9-32, registration cancelled 2008-06-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 18, 2008 - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-32](https://openairdocs.org/model/mcdonnell-douglas-dc-9-32) (registry code 302206C) - Engine: [Pratt & Whitney JT8D-9 series](https://openairdocs.org/engine/pratt-whitney-jt8d-9-series) (registry code 52048) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE), [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 47435 - Year built: 1969 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 29, 1996 - Certificate issued: April 24, 1996 - Last registry action: April 18, 2006 - Mode S code: A7F3A2 - Owner when cancelled: [Northwest Airlines Inc](https://openairdocs.org/faa-owner/NORTHWEST%20AIRLINES%20INC) - Location: [St Paul, MN](https://openairdocs.org/faa-place/MN/St%20Paul) - Owner type: Corporation - Owner's area on the map: 44.8873° N, 93.1924° W: Placed by OpenAirDocs at the center of ZIP code 55111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N611NA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=611NA - Page: https://openairdocs.org/deregistered/N611NA-2008-06-18 From the FAA registry file of October 31, 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 (47) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NWAA70089611](https://openairdocs.org/sdr/NWAA70089611), Jan 12, 2007: OUTFLOW VALVE. MALFUNCTIONED. DURING CLIMB AT FL 200 WITH WING ANTI-ICE ON SELECTED CABIN BEGAN TO CLIMB AND DESCEND RAPIDLY. FLIGHT DESCENDED TO FL 100. NO MENTION OF OXYGEN MASKS BEING DEP - [SDR 0600079611](https://openairdocs.org/sdr/0600079611), Jan 6, 2006: CONTROLLER. MALFUNCTIONED. DURING CLIMB OUT AT ABOUT FL190 THE CABIN PRESSURE INDICATOR ABRUPTLY PEGGED OUT IN CABIN CLIMB DIRECTION. FLIGHT CREW QUICKLY RECOVERED PRESSURE CONTROL BUT TH - [SDR 0501849611](https://openairdocs.org/sdr/0501849611), Dec 27, 2005: CONTROLLER. FAILED. DURING CRUISE FLIGHT AT FL340 THE AIRCRAFT SUDDENLY STARTED TO LOSE CABIN PRESSURIZATION VERY QUICKLY. THE ORANGE -CABIN PRESS AUTO FAIL- LIGHT DID NOT ILLUMINA - [SDR 0500639611](https://openairdocs.org/sdr/0500639611), Apr 26, 2005: CONTROLLER. MALFUNCTIONED. AT FL290 ON DESCENT, THE AIRCRAFT LOST AUTO PRESSURE CONTROL. CREW ATTEMPTED MANUAL CONTROL BUT RIGHT PACK WENT INTO OVERHEAT CONDITION AND SHUT DOWN. CABIN CLI - [SDR 0500489611](https://openairdocs.org/sdr/0500489611), Apr 1, 2005: SPAR CAP. CRACKED. DURING M-CHECK FOUND CRACK IN RT WING REAR SPAR CAP AT XRS 267. REPAIRED PER EA 96-201450. - [SDR 0500479611](https://openairdocs.org/sdr/0500479611), Apr 1, 2005: DOOR FRAME. CORRODED. DURING M-CHECK FOUND CRACK IN LT SIDE AFT ENTRY DOOR JAMB FRAME. REPAIRED PER EA 96-203207. - [SDR 0201289611](https://openairdocs.org/sdr/0201289611), Apr 11, 2002: DOOR FRAME. CRACKED. DURING CHK IN ATL, THE FORWARD UPPER CORNER OF THE CARGO DOOR JAMB WAS FOUND CRACKED .0625. THE REPAIRS WERE MADE IAW EA 96-188479. - [SDR 0201279611](https://openairdocs.org/sdr/0201279611), Apr 11, 2002: STIFFENER. CRACKED. DURING AN HCK IN ATL, ONE .60 INCH LONG CRACK WAS FOUND IN THE STA 756 BULKHEAD. THE CRACK IS LOCATED IN THE UPPER END OF THE VERTICAL STIFFENER AT X=22. THIS E - [SDR 0201269611](https://openairdocs.org/sdr/0201269611), Apr 8, 2002: PRESSURE PANEL. CORRODED. During Hck at ATL, corrosion was found on the APB WEB at L26R. The corrosion was found within Blue Print tolerance. Repaired per EA 96-188478. - [SDR 0201259611](https://openairdocs.org/sdr/0201259611), Apr 8, 2002: SKIN. CORRODED. DURING HCK IN ATL, CORROSION WAS FOUND ON THE LEADING EDGE OF LT WING. DAMAGE WAS TRIMMED OUT AND REPAIR WAS ACCOMPLISHED PER EA 96-188468. - [SDR 0201249611](https://openairdocs.org/sdr/0201249611), Apr 5, 2002: PRESSURE PANEL. CRACKED. During an Hck in ATl, three cracks were found in the flight compartment pressure panel at station 105. The cracks are located at x=25 1.5" long x=35 2.3" long a - [SDR 0002379611](https://openairdocs.org/sdr/0002379611), Jul 5, 2000: CONTROLLER. FAILED. EN ROUTE MSP-MCI, CABIN PRESSURE AUTO FAIL LIGHT ILLUMINATED. PRESSURIZATION COULD NOT BE MAINTAINED ABOVE 22,000 FEET. FLIGHT CONTINUED TO DESTINATION AND CREW - [SDR 0001449611](https://openairdocs.org/sdr/0001449611), Apr 22, 2000: TIRE. FAILED. ABORTED TAKEOFF AT 120 KNOTS FOR HEAVY VIBRATION. CREW SUSPECTED A BLOWN TIRE AND ALSO FOLLOWED COM PROCEDURES FOR HOT BRAKES AFTER CLEARING RUNWAY. MAINTENANCE - [SDR 0000769611](https://openairdocs.org/sdr/0000769611), Mar 30, 2000: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD ENTRY, SERVICE DOOR, AND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK B5-23, OPERATION - [SDR 9904999611](https://openairdocs.org/sdr/9904999611), Nov 24, 1999: ENGINE. FAILED. DURING CLIMBOUT PASSING 10,000 FEET, THE RIGHT ENGINE EXPERIENCED A FLAME-OUT. THE FLIGHT CREW INITIATED EMERGENCY CHECK LIST PROCEDURES, RETURNED TO MKE, AND L - [SDR 9810889611](https://openairdocs.org/sdr/9810889611), Dec 13, 1998: ACTUATOR. FAILED. LEFT MAIN LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND RED NOSE GEAR UNSAFE LIGHT REMAINED ON. FLIGHT WAS RETURNED TO DTW - [SDR 9810549611](https://openairdocs.org/sdr/9810549611), Nov 26, 1998: LIGHT. INOPERATIVE. DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR DOWN AND LOCKED GREEN INDICATION LIGHT ILLUMINATED WITH THE LANDING GEAR IN THE RETRACTED POSITION. THE FLIGHT CREW - [SDR 9809099611](https://openairdocs.org/sdr/9809099611), May 12, 1998: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND CATWALK EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED TAIL COMPARTMENT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHE - [SDR 9808059611](https://openairdocs.org/sdr/9808059611), May 1, 1998: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9808039611](https://openairdocs.org/sdr/9808039611), May 1, 1998: POWER SUPPLY. INOPERATIVE. DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9806849611](https://openairdocs.org/sdr/9806849611), Apr 19, 1998: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9806789611](https://openairdocs.org/sdr/9806789611), Apr 19, 1998: SEAL. LEAKING. DURING CRUISE FLIGHT, APU OIL PRESSURE LOW LIGHT CAME ON AND APU SHUT DOWN. CROSSTIE RELAY WAS ON MEL. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE FO - [SDR 9804289611](https://openairdocs.org/sdr/9804289611), Mar 12, 1998: RETRACT MECH. LACK OF LUBE. DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR AND NOSE GEAR UNSAFE LIGTHS REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT WAS CON - [SDR 9804019611](https://openairdocs.org/sdr/9804019611), Mar 8, 1998: TERMINAL. LOOSE. DURING CRUISE FLIGHT AT 35,000 FT EN ROUTE, NUMEROUS SYSTEMS FAILED WITH MULTIPLE FLAGS AND ANNUNCIATOR LIGHTS. THESE SYSTEMS INCLUDED ACARS, TCAS, RADIO RACK F - [SDR 9800839611](https://openairdocs.org/sdr/9800839611), Jan 13, 1998: BATTERIES. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9800689611](https://openairdocs.org/sdr/9800689611), Jan 9, 1998: POWER SUPPLY. DISCHARGED. FLOOR PROXIMITY EMERGENCY LIGHTS AT OVERWING EXITS ILLUMINATED DURING FLIGHT. REPLACED POWER SUPPLY AT FS 657 AND BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9723779611](https://openairdocs.org/sdr/9723779611), Dec 14, 1997: JAMB. CRACKED. DURING LINE CHECK, FOUND CRACK IN THE UPPER LEFT CORNER OF THE DOOR JAMB FOR THE REAR CABIN DOOR. REPAIRED PER EA 96-154223. - [SDR 9720459611](https://openairdocs.org/sdr/9720459611), Oct 28, 1997: LONGERON. CRACKED. DURING L-CHECK, FOUND CRACK IN LONGERON 2R, FS 1076 AT INBOARD FASTENER IN FRAME. REPAIRED PER EA 96-151793. - [SDR 9720449611](https://openairdocs.org/sdr/9720449611), Oct 28, 1997: LONGERON. CRACKED. DURING L-CHECK, FOUND CRACK IN LONGERON 2L, FS 1076 AT OUTBOARD FASTENER. REPAIRED PER EA 96-151793. - [SDR 9720069611](https://openairdocs.org/sdr/9720069611), Oct 26, 1997: SLIDE. LOW BATTERY. DURING PERIODIC CHECK, FOUND FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE BATTERY LOW. REPLACED SLIDE. - [SDR 9719969611](https://openairdocs.org/sdr/9719969611), Oct 23, 1997: BATTERY PACK. DISCHARGED. DURING PERIODIC CHECK, FOUND RIGHT TAILCONE EMERGENCY SPOTLIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9719859611](https://openairdocs.org/sdr/9719859611), Oct 23, 1997: BATTERY PACK. DISCHARGED. DURING PERIODIC CHECK, EXTERNAL EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9713589611](https://openairdocs.org/sdr/9713589611), Jul 9, 1997: BULB. WRONG PARTY. DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND NORMAL INDICAITONS WERE ACHIEVED. AIRCRAFT LANDED - [SDR 9712319611](https://openairdocs.org/sdr/9712319611), Jun 21, 1997: DOWNLOCK IND. FAILED. DURING APPROACH, NOSE GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND VERIFIED VISUALLY THROUGH PERISCOPE THAT - [SDR 9712059611](https://openairdocs.org/sdr/9712059611), Jun 19, 1997: RELAY. FAILED. DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND RESET CIRCUIT BREAKER P-27, NORMAL INDICATIONS WE - [SDR 9706729611](https://openairdocs.org/sdr/9706729611), Mar 31, 1997: FUSE. BLOWN. DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN EMERGENCY LIGHTS AND AFT WALL MOUNTED EXIT SIGN LIGHT, INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL. - [SDR 9626599611](https://openairdocs.org/sdr/9626599611), Dec 13, 1996: TRANSMITTER. INOPERATIVE. WHEN APPLYING TAKEOFF POWER, THE RIGHT ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGI - [SDR 9615849611](https://openairdocs.org/sdr/9615849611), Jul 22, 1996: AUGMENTATION VLV. FAILED. TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT AUGMENTATION V - [SDR 9609259611](https://openairdocs.org/sdr/9609259611), Apr 23, 1996: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. - [SDR 9608019611](https://openairdocs.org/sdr/9608019611), Mar 27, 1996: SKIN. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FUSELAGE SKIN AT LONGERON 27R FROM FS 370 TO 427. REPAIRED SKIN PER EA 12-5330-9-C0829. - [SDR 9606639611](https://openairdocs.org/sdr/9606639611), Mar 16, 1996: ENGINE MOUNT. RUSTED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND RUST ON THE NR 1 ENGINE AFT MOUNT CONE FITTING ASSEMBLY. REPLACED AFT MOUNT PER MM 71-20-2. - [SDR 9607999611](https://openairdocs.org/sdr/9607999611), Mar 5, 1996: CHORD. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT HORIZONTAL STABILIZER REAR SPAR AT THE OUTBOARD ELEVATOR HINGE BRACKET MOUNTING HOLES. - [SDR 9605669611](https://openairdocs.org/sdr/9605669611), Mar 5, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE INTERCOSTAL ATTACH FITTING AT FS 996, LONGERON 28R. REPLACED FITTING PER SRM 51-30-02. - [SDR 9605659611](https://openairdocs.org/sdr/9605659611), Mar 5, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN A LEFT ELEVATOR GEARED TAB HINGE FITTING. REPLACED FITTING (P/N 3918075-509) PER SRM 51-30-2. - [SDR 9607989611](https://openairdocs.org/sdr/9607989611), Feb 29, 1996: ANGLE. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR UPPER CUSP ANGLE FS 200 AT LONGERON 18L. REPAIRED ANGLE PER EA 12-5310-9-C0 - [SDR 9605259611](https://openairdocs.org/sdr/9605259611), Feb 29, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION IN THE FLOOR SUPPORT CORNER FITTING AT FS 996, LONGERON 18L LBL 50. REPLACED FITTING ( - [SDR 9607979611](https://openairdocs.org/sdr/9607979611), Feb 27, 1996: LONGERON. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE CENTER WING STR 20 FROM WS 58R TO 91R. REPAIRED THE STRINGER PER EA 12-5710-9-C0783. ## FAA accident and incident reports (2) 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 19991123038909I](https://openairdocs.org/incident/19991123038909I), Nov 23, 1999: Doug DC932 (N611NA), Milwaukee, WI. During climbout passing 10,000 ft. the right engine flamed out. Red bordered check list procedure was accomplished. The engine did not relight so the… - [Incident 19970424011399I](https://openairdocs.org/incident/19970424011399I), Apr 24, 1997: Doug DC931 (N611NA), Syracuse, NY. Narrative: on April 24, 1997, at 2007 EST, a Douglas DC-9, N611NA, flight number 891, operated by northwest airlines, while fifty miles south of Syracuse, new… ## Other aircraft with N611NA - [Registered now](https://openairdocs.org/aircraft/N611NA): Zipline International P2 ZIP, S/N 18735P2969 --- 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.