# N606NW: 1968 Mcdonnell Douglas DC-9-32, registration cancelled 2008-08-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 25, 2008 - 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 series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47225 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: March 17, 1996 - Last registry action: July 21, 2008 - Mode S code: A7DECA - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Individual - Owner's area on the map: 26.1860° N, 80.1727° W: Placed by OpenAirDocs at the center of ZIP code 33309, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N606NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=606NW - Page: https://openairdocs.org/deregistered/N606NW-2008-08-25 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 (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR NWAA081119606](https://openairdocs.org/sdr/NWAA081119606), Mar 21, 2008: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE TAIL - [SDR NWAA080969606](https://openairdocs.org/sdr/NWAA080969606), Mar 14, 2008: BATTERY PACK. INOPERATIVE. DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATT - [SDR NWAA072999606](https://openairdocs.org/sdr/NWAA072999606), Sep 4, 2007: BATTERY PACK. INOPERATIVE. TAIL COMPARTMENT PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATION CHECKS GOOD. - [SDR NWAA071609606](https://openairdocs.org/sdr/NWAA071609606), Apr 25, 2007: LINE. DISCONNECTED. DURING CLIMB, THE FLIGHT ATTENDANT REPORTED BOTH AFT LAVATORY SMOKE DETECTORS WERE SOUNDING. A MINUTE LATER THE FLIGHT CREW SMELLED FUMES IN THE COCKPIT. NO MEN - [SDR 0500829606](https://openairdocs.org/sdr/0500829606), Mar 29, 2005: VERTICAL SUPPORT. CRACKED. DURING H-CHECK, FOUND CRACK IN BULKHEAD VERTICAL SUPPORT AT BS 756 L26L AND L26R. REPAIRED PER EA 96-202532. - [SDR 0300729606](https://openairdocs.org/sdr/0300729606), Mar 17, 2003: CLAMP. BROKEN. CLIMBING THROUGH FL 210 CREW FELT A THUMP IN THE FORWARD CABIN AND SUBSEQUENTLY LOST CONTROL OF CABIN PRESSURE. OUTFLOW VALVE INDICATED FULL CLOSED BUT THE CABI - [SDR 0101489606](https://openairdocs.org/sdr/0101489606), Apr 19, 2001: ROLLER. LOOSE. DURING APPROACH INTO MSP, THE LANDING GEAR INDICATED DOWN AND LOCKED. THEN THE RIGHT MAIN GEAR INTERMITTENTLY INDICATED BOTH DOWN TO UNSAFE WITH ACCOMPANYING WA - [SDR 0002799606](https://openairdocs.org/sdr/0002799606), Jul 26, 2000: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. - [SDR 9811029606](https://openairdocs.org/sdr/9811029606), Dec 24, 1998: POWER SUPPLY. INOP. DURING B-CHECK, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. - [SDR 9810149606](https://openairdocs.org/sdr/9810149606), Sep 25, 1998: ROLLER. OUT OF ADJUST. AFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RECYCLED THE LANDING GEAR SYSTEM, - [SDR 9804689606](https://openairdocs.org/sdr/9804689606), Mar 19, 1998: ENGINE. FAILED. AS TAKEOFF POWER WAS APPLIED, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS FROM THE RIGHT ENGINE. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACE - [SDR 9725009606](https://openairdocs.org/sdr/9725009606), Dec 8, 1997: BULKHEAD. CRACKED. DURING LINE CHECK, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER LEFT AND RIGHT DOOR STOPS. REPAIRED PER EA 96-153409. - [SDR 9720649606](https://openairdocs.org/sdr/9720649606), Nov 1, 1997: BATTERY. DISCHARGED. DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. - [SDR 9720729606](https://openairdocs.org/sdr/9720729606), Oct 31, 1997: BATTERY PACKS. DISCHARGED. DURING PERIODIC CHECK, RIGHT AND LEFT NACELLE EMERGENCY LIGHT BATTERY PACKS FAILED TEN MINUTE TEST. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. - [SDR 9717799606](https://openairdocs.org/sdr/9717799606), Sep 18, 1997: BATTERY. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD EMERGENCY FLASHLIGHT INDICATOR NOT FLASHING. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. - [SDR 9715719606](https://openairdocs.org/sdr/9715719606), Aug 15, 1997: TEMP SENSOR. MALFUNCTIONED. LEFT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AT 70 KNOTS AND RETURNED TO GATE. MAINTENANCE REPLACED - [SDR 9712479606](https://openairdocs.org/sdr/9712479606), Jun 20, 1997: BATTERY PACK. DISCHARGED. DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD ENTRY DOOR EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. - [SDR 9700479606](https://openairdocs.org/sdr/9700479606), Jan 4, 1997: LATCHES. OUT OF ADJUST. UPON ARRIVAL AT AIRCRAFT, TAILCONE ANNUNCIATOR LIGHT WAS ILLUMINATED. HANDLE HAD BEEN INADVERTANTLY PULLED. TAILCONE DID NOT DEPLOY BUT ALL LATCHES WERE RELEASE - [SDR 9623689606](https://openairdocs.org/sdr/9623689606), Nov 7, 1996: WIRE. BROKEN. DURING PERIODIC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK NORMAL. - [SDR 9622909606](https://openairdocs.org/sdr/9622909606), Oct 27, 1996: FUEL CONTROL. OUT OF ADJUST. WHEN APPLYING POWER FOR TAKEOFF, THE RIGHT ENGINE WOULD NOT REACH TAKEOFF POWER. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRIMMED THE RIGHT ENGINE - [SDR 9618439606](https://openairdocs.org/sdr/9618439606), Aug 9, 1996: DOOR. NOT SECURED. DURING CLIMB, NOTED A LOUD RUMBLE FROM THE NOSE LANDING GEAR VICINITY AND INABILITY TO PRESSURIZE. RETURNED TO MSP WITHOUT FURTHER INCIDENT. FOUND THE FORWARD E - [SDR 9606959606](https://openairdocs.org/sdr/9606959606), Mar 22, 1996: EPR INDICATOR. MALFUNCTIONED. NR 2 ENGINE EPR INDICATION TOO LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A - [SDR 9606949606](https://openairdocs.org/sdr/9606949606), Mar 22, 1996: EPR TRANSMITTER. MALFUNCTIONED. NR 2 ENGINE EPR INDICATION TOO LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER WITH A SE - [SDR 9607229606](https://openairdocs.org/sdr/9607229606), Mar 15, 1996: STRINGER. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT AND RIGHT WING LOWER STRINGERS 17 TO 22 FROM XRS 58 TO 91. REPAIRED STRINGERS PER EA 9 - [SDR 9607219606](https://openairdocs.org/sdr/9607219606), Feb 28, 1996: SKIN. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE SKIN CUTOUT FOR THE LEFT PYLON AFT UPPER SPAR CAP STRAP FS 1038. REPAIRED SKIN (P/N 5952562-7 - [SDR 9607209606](https://openairdocs.org/sdr/9607209606), Feb 23, 1996: DOUBLER. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB DOUBLER BETWEEN FS 389 TO 408. REPAIRED DOUBLER (P/N 9912455) PER E - [SDR 9607199606](https://openairdocs.org/sdr/9607199606), Feb 19, 1996: DOUBLER. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT CARGO DOOR CUTOUT DOUBLER LOWER EDGE. REPAIRED DOUBLER (P/N 5910158-25) PER EA 99-10883 - [SDR 9607439606](https://openairdocs.org/sdr/9607439606), Feb 18, 1996: FRAME. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A ONE INCH CRACK IN THE FS 718 RIB AT LONGERON 20R. REPAIRED RIB PER EA 99-103161. - [SDR 9607189606](https://openairdocs.org/sdr/9607189606), Feb 14, 1996: FRAME. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 148 FRAME BETWEEN LONGERONS 6R TO 7R. REPAIRED FRAME (P/N 9911514) PER EA 99-108988. - [SDR 9603929606](https://openairdocs.org/sdr/9603929606), Feb 13, 1996: FITTING. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 29L END FITTING AT FS 579 TO 604. REPLACED FITTING PER SRM 51-01, 51-30-2 AND 51-3 - [SDR 9607179606](https://openairdocs.org/sdr/9607179606), Feb 12, 1996: SPAR CAP. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING REAR SPAR UPPER CAP BETWEEN XRS 531-570. REPAIRED CAP (P/N 5911300-501) PER EA 99 - [SDR 9603919606](https://openairdocs.org/sdr/9603919606), Feb 12, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 28R END FITTING AT FS 996. REPLACED FITTING PER SRM 51-01. - [SDR 9603299606](https://openairdocs.org/sdr/9603299606), Feb 7, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 794 TO LONGERON 30 SPLICE FITTING. REPLACED FITTING PER SRM 51-01. - [SDR 9603269606](https://openairdocs.org/sdr/9603269606), Feb 1, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 996 FLOORBEAM FITTING AT RBL 58. REPLACED FITTING PER SRM 51-01. - [SDR 9603259606](https://openairdocs.org/sdr/9603259606), Feb 1, 1996: FITTINGS. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 756 ATTACH FITTINGS AT LONGERONS 29L AND 29R. REPLACED BOTH FITTINGS PER SRM 51-30-5. - [SDR 9602499606](https://openairdocs.org/sdr/9602499606), Jan 31, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE FS 1095 FRAME TO LONGERON 25L ATTACH FITTING. REPLACED FITTING PER SRM 51-01 AND 51-30-5. - [SDR 9602479606](https://openairdocs.org/sdr/9602479606), Jan 30, 1996: FITTING. CORRODED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT MAIN LANDING GEAR WHEEL WELL FITTINGS AT FS 756, LONGERON 30. REPLACED - [SDR 9602389606](https://openairdocs.org/sdr/9602389606), Jan 26, 1996: FITTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LONGERON 5L TO FS 1095 FRAME ATTACH FITTING. REPLACED FITTING PER SRM 51-01. - [SDR 9601679606](https://openairdocs.org/sdr/9601679606), Jan 18, 1996: CASTING. CRACKED. DURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT DIAGONAL WEB ATTACH CASTING IN THE NOSE LANDING GEAR WHEEL WELL FS 70. REPLACED CASTING ## 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 20001212026589I](https://openairdocs.org/incident/20001212026589I), Dec 12, 2000: Doug DC932 (N606NW), Omaha, NE. (-23) N606NW, on repositioning flight 868 from sioux city, IA to Kansas city, MO when diverted into Omaha, NE, due to smoke in the cabin. The a/c had been… --- 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.