# N94S: Douglas DC9-15, registration cancelled 1999-09-21 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 21, 1999 - Status when cancelled: Sale reported - Airframe: [Douglas DC9-15](https://openairdocs.org/model/douglas-dc9-15) (registry code 3022036) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 47204 - Type of aircraft: Fixed wing multi engine - Last registry action: September 21, 1999 - Mode S code: AD0C5F - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Individual - Owner's area on the map: 25.8050° N, 80.3151° W: Placed by OpenAirDocs at the center of ZIP code 33122, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N94S - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=94S - Page: https://openairdocs.org/deregistered/N94S-1999-09-21 From the FAA registry file of November 5, 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 DC9-15: https://openairdocs.org/model/douglas-dc9-15.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 9810599104](https://openairdocs.org/sdr/9810599104), Sep 16, 1998: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL - [SDR 9809829104](https://openairdocs.org/sdr/9809829104), Jul 18, 1998: RETRACT MECH. OUT OF ADJUST. AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RETRACTED THE LANDING GEAR BY PUSHING THE LANDING HANDLE RELEASE BUT - [SDR 9807279104](https://openairdocs.org/sdr/9807279104), Apr 24, 1998: SOCKET. INOPERATIVE. DURING LINE CHECK, FOUND 2 RED EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED 2 SOCKET ASSEMBLIES, OPERATIONAL CHECK NORMAL. - [SDR 9721949104](https://openairdocs.org/sdr/9721949104), Nov 20, 1997: FLAP ASSY. FAILED. DURING DESCENT, AIRCRAFT INCURRED A NON-SYMMETRICAL FLAP CONDITION WITH THE LEFT FLAP SETTING AT 50 DEGREES AND THE RIGHT FLAP SETTING AT 30 DEGREES. CAPTAIN DE - [SDR 9715779104](https://openairdocs.org/sdr/9715779104), Jul 14, 1997: SKIN. CORRODED. DURING LINE CHECK, FOUND CORROSION ON SKIN JUST AFT OF RIGHT BATTERY VENT DISCHARGE PORT. REPAIRED PER EA 91-151146. - [SDR 9715769104](https://openairdocs.org/sdr/9715769104), Jul 14, 1997: DOUBLER. CORRODED. DURING LINE CHECK, FOUND CORROSION ON INNER DOUBLER FORWARD OF E/E COMPARTMENT. REPAIRED PER EA 91-151146. - [SDR 9709899104](https://openairdocs.org/sdr/9709899104), May 19, 1997: VERT GYRO. INOPERATIVE. NR 1 VERTICAL GYRO BECAME INOPERATIVE EN ROUTE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 VERTICAL GYRO, OPERATIONAL CHECK OK. - [SDR 9705509104](https://openairdocs.org/sdr/9705509104), Mar 14, 1997: WIRE. BROKEN. DURING LINE CHECK, FOUND EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. FOUND BROKEN WIRE IN FRONT OF ROW 1. REPAIRED WIRE. OPERATIONAL CHECK OK. - [SDR 9703389104](https://openairdocs.org/sdr/9703389104), Feb 14, 1997: WATER LINE. DAMAGED. AS DESCENT WAS INITIATED, THE RIGHT ENGINE THRUST LEVER WOULD NOT MOVE FROM ITS CURRENT POSITION. CREW SHUT DOWN THE RIGHT ENGINE. CONTINUED TO DESTINATION AND - [SDR 9625069104](https://openairdocs.org/sdr/9625069104), Nov 19, 1996: CSD. FAILED. DURING CLIMBOUT AT ABOUT 3,000 FT EXPERIENCED WHAT APPEARED TO BE INTERMITTANT POWER INTERRUPTIONS. FLASHING ANNUNCIATOR LIGHTS AND CLICKING SOUNDS COMING FROM - [SDR 9619179104](https://openairdocs.org/sdr/9619179104), Sep 5, 1996: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK OK. - [SDR 9618219104](https://openairdocs.org/sdr/9618219104), Aug 20, 1996: STALL WARNING. ACTIVATED. AFTER TAKEOFF, FIRST OFFICER'S STALL WARNING AND STICK SHAKER ACTIVATED. UNABLE TO ISOLATE WHICH SYSTEM FAILED. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REP - [SDR 9617089104](https://openairdocs.org/sdr/9617089104), Aug 8, 1996: OIL FILTER. CLOGGED. DURING TAKEOFF ROLL, RIGHT ENGINE OIL STRAINER CLOGGING LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REPLACED RIGH - [SDR 9616909104](https://openairdocs.org/sdr/9616909104), Aug 5, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND FORWARD AND AFT EMERGENCY CEILING LIGHTS INOPERATIVE. REPLACED BATTERY PACKS BETWEEN GALLEYS AND RIGHT AFT LAV, OPERATIONAL CHECK OK. - [SDR 9617599104](https://openairdocs.org/sdr/9617599104), Aug 4, 1996: BULKHEAD DOUBLER. CRACKED. DURING LINE CHECK, FOUND A .25 INCH CRACK IN THE AFT PRESSURE BULKHEAD UPPER CORNER DOUBLER AND WEB SKIN. REPAIRED SAME (P/N 5910130-13, -111, -113) PER EA DC9- - [SDR 9616679104](https://openairdocs.org/sdr/9616679104), Jul 10, 1996: BULKHEAD. CRACKED. DURING LINE CHECK, FOUND A 4.5 INCH CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER RADIUS, UPPER RIGHT CORNER. REPAIRED BULKHEAD DOUBLER (P/N 5910130-1) PER EA - [SDR 9608559104](https://openairdocs.org/sdr/9608559104), Apr 10, 1996: CLIPS. OUT OF ADJUST. DURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAIL CONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. - [SDR 9522199104](https://openairdocs.org/sdr/9522199104), Dec 28, 1995: SKIN. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AFT OF THE MAIN CABIN DOOR FS 200, AT THE 6TH STOP FROM THE TOP. REPAIRED SKIN (P/N 5911406-59) PER EA 91-102 - [SDR 9521839104](https://openairdocs.org/sdr/9521839104), Dec 28, 1995: SKIN. CRACKED. DURING H-CHECK, FOUND A .25 INCH CRACK IN THE MAIN CABIN DOOR SKIN AT THE AFT SIDE FS 200, NR 4 STOP. REPAIRED SKIN (P/N 5911406-59) PER EA 91-102632. - [SDR 9522189104](https://openairdocs.org/sdr/9522189104), Dec 27, 1995: DOOR PANS. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE LEFT AND RIGHT OVERWING EMERGENCY EXIT DOOR PANS AT THE UPPER STOPS. REPAIRED PANS (P/N 5913195-1) PER EA 91-103350 AND EA 9 - [SDR 9514459104](https://openairdocs.org/sdr/9514459104), Sep 24, 1995: FUEL SYS. VENTING. AFTER TAKEOFF, FUEL BEGAN VENTING FROM LEFT WING. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PERFORMED BOOST PUMP CHECK VALVE BACKFLUSH PROCEDURE PER M - [SDR 9514849104](https://openairdocs.org/sdr/9514849104), Sep 12, 1995: ANGLE. CRACKED. DURING B-CHECK, FOUND A CRACK IN THE DORSAL FIN ATTACH ANGLE AT LONGERON 2L. REPAIRED ANGLE (P/N 5939711-1), PER EA 91-99249. ## Other aircraft with N94S - [Registered now](https://openairdocs.org/aircraft/N94S): Beech 65-A90-1, S/N LM-133, built 1971 --- 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.