# N95S: Douglas DC9-15, registration cancelled 1999-09-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 22, 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: 47205 - Type of aircraft: Fixed wing multi engine - Last registry action: September 22, 1999 - Mode S code: AD33DE - 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/N95S - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=95S - Page: https://openairdocs.org/deregistered/N95S-1999-09-22 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 Douglas DC9-15: https://openairdocs.org/model/douglas-dc9-15.md ## Service difficulty reports (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 9809679105](https://openairdocs.org/sdr/9809679105), Jun 29, 1998: CONTROLLER. FAILED. AT FL290, THE CABIN PRESSURE BEGAN CLIMBING 1500 FEET PER MINUTE. THE FLIGHT CREW CLOSED THE OUTFLOW VALVE, CHECKED FOR CLOSED CROSSFEED VALVES, FOLLOWED EMERGE - [SDR 9800799105](https://openairdocs.org/sdr/9800799105), Jan 11, 1998: CIRCUIT BREAKER. TRIPPED. PRIMARY TRIM FAILED AFTER TAKEOFF. SECONDARY SYSTEM OPERATED NORMALLY. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A PHASE CIRCUIT - [SDR 9721279105](https://openairdocs.org/sdr/9721279105), Oct 29, 1997: FRAME. CRACKED. DURING L-CHECK, FOUND A CRACK IN CANTED FRAME AT FS 895, LONGERON 4L. REPAIRED PER EA 91-151790. - [SDR 9720309105](https://openairdocs.org/sdr/9720309105), Oct 27, 1997: PANEL. CRACKED. DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT LEFT OUTBOARD VERTICAL SUPORT FS 106. REPAIRED PER EA 91-151781. - [SDR 9720299105](https://openairdocs.org/sdr/9720299105), Oct 25, 1997: PANEL. CRACKED. DURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE PREVIOUS REPAIR FS 83. REPAIRED PER EA 91-151780. - [SDR 9707309105](https://openairdocs.org/sdr/9707309105), Apr 7, 1997: CLIPS. OUT OF ADJUST. DURING LINE CHECK, FOUND EXCESSIVE FORCE REQUIRED TO REMOVE INTERNAL TAIL CONE RELEASE HANDLE FROM CLIPS. CLEANED AND LUBED LATCH PIN ASSEMBLIES AND INTERNAL HA - [SDR 9701589105](https://openairdocs.org/sdr/9701589105), Jan 24, 1997: DOOR JAMB. DIRTY. AFTER TAKEOFF, THE CABIN WOULD NOT PRESSURIZE. APPROXIMATELY SIX MINUTES AFTER TAKEOFF, AFT CARGO DOOR LIGHT ILLUMINATED FOR APPROXIMATELY TWO MINUTES. FLIGHT R - [SDR 9700599501](https://openairdocs.org/sdr/9700599501), Jan 11, 1997: FUEL CONTROL. MALFUNCTIONED. DURING CLIMB, APU AUTO SHUTDOWN. NR 1 ENGINE GENERATOR ON MEL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE APU FUEL CONTROL, LEAK CHECK GOO - [SDR 9700599105](https://openairdocs.org/sdr/9700599105), Jan 11, 1997: FUEL CONTROL. MALFUNCTIONED. DURING CLIMB, APU AUTO SHUTDOWN. NBR 1 ENGINE GENERATOR ON MEL. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE APU FUEL CONTROL, LEAK CHECK GO - [SDR 9626609105](https://openairdocs.org/sdr/9626609105), Dec 16, 1996: ENGINE. FAILED. DURING CLIMB AT 1000 FEET AGL, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS AND A CONTAINED FAILURE OF THE LEFT ENGINE. CREW FOLLOWED COM EMERGENCY PROCEDURES. RETU - [SDR 9621549105](https://openairdocs.org/sdr/9621549105), Sep 13, 1996: BULKHEAD DOUBLER. CRACKED. DURING H-CHECK, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD -13 DOUBLER UPPER DOOR JAMB. REPAIRED DOUBLER (P/N 5910130-13) PER EA 91-111229. - [SDR 9619469105](https://openairdocs.org/sdr/9619469105), Sep 6, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND THE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED LEFT AND RIGHT POWER SUPPLIES. OPERATIONAL CHECK OK. - [SDR 9619459105](https://openairdocs.org/sdr/9619459105), Sep 6, 1996: BATTERIES. DISCHARGED. DURING LINE CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERIES. OPERATIONAL CHECK OK. - [SDR 9614489105](https://openairdocs.org/sdr/9614489105), Jun 27, 1996: FRAME. CRACKED. DURING LINE CHECK, FOUND A CRACK EXTENDING APPROXIMATELY HALF WAY THROUGH THE FS 180 FRAME BETWEEN LONGERONS 6L TO 7L. REPAIRED FRAME PER SRM 53-03 FIG 36, SHEE - [SDR 9608239105](https://openairdocs.org/sdr/9608239105), Apr 11, 1996: BATTERY PACK. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERATIONAL CHECK GOOD. - [SDR 9605189105](https://openairdocs.org/sdr/9605189105), Feb 26, 1996: FITTING. CRACKED. DURING H-CHECK, FOUND A CRACK IN THE RIGHT KEEL FITTING FS 642 OUTBOARD OF LONGERON 29R. REPLACED FITTING REF 51-30. - [SDR 9605179105](https://openairdocs.org/sdr/9605179105), Feb 25, 1996: FITTINGS. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE FS 642 LEFT KEEL FITTINGS AT LONGERON 30 AND OUTBOARD OF LONGERON 29L. REPLACED BOTH FITTINGS PER SRM 51-30-5. - [SDR 9605149105](https://openairdocs.org/sdr/9605149105), Feb 20, 1996: FITTING. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE LEFT LAVATORY FITTING ON THE AFT SIDE OF THE FS 817 FRAME. REPLACED FITTING PER SRM 51-30-3. - [SDR 9600129105](https://openairdocs.org/sdr/9600129105), Jan 4, 1996: UNSAFE LIGHT. ILLUMINATED. DURING APPROACH INTO FAR, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. EXECUTED GO-AROUND AND RECYCLED GEAR. ALL INDICATIONS WERE NORMAL - [SDR 9520409105](https://openairdocs.org/sdr/9520409105), Dec 13, 1995: TRANSPONDER. MALFUNCTIONED. STALL WARNING AND STICK SHAKER ACTIVATED AFTER TAKEOFF. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT STALL WARNING TRANSDUCER, FLAP PO - [SDR 9514769105](https://openairdocs.org/sdr/9514769105), Sep 16, 1995: CLIPS. OUT OF ADJUST. DURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERNAL TAILCONE HANDLE FROM THE CLIPS. ADJUSTED THE CLIPS, CHECKED OK. - [SDR 9513519105](https://openairdocs.org/sdr/9513519105), Aug 30, 1995: SKIN. DELAMINATED. DURING LINE CHECK, FOUND DELAMINATION IN THE RIGHT INBOARD SPOILER. REPLACED SPOILER PER CITEXT 90-2760-1-9901. - [SDR 9507729105](https://openairdocs.org/sdr/9507729105), May 5, 1995: RIB. CRACKED. DURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD SPOILER FITTING (RIB CAP). REPLACED RIB CAP. - [SDR 9504799105](https://openairdocs.org/sdr/9504799105), Mar 26, 1995: SKIN. LOOSE FASTENERS. DURING LINE CHECK, FOUND APPROXIMATELY 40 - 50 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS. - [SDR 9502929105](https://openairdocs.org/sdr/9502929105), Feb 18, 1995: INTERCOSTAL. CRACKED. DURING LINE CHECK, FOUND ONE .5 INCH CRACK IN VERTICAL INTERCOSTAL, FORWARD CARGO DOOR JAMB FS 351. REPLACED INTERCOSTAL PER EA 91-096933. - [SDR 9502669105](https://openairdocs.org/sdr/9502669105), Feb 11, 1995: DNLOCK SW. MALFUNCTIONED. DURING APPROACH INTO MSP, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON GEAR EXTENSION. CONFIRMED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOC ## FAA accident and incident reports (9) 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 19961216043349I](https://openairdocs.org/incident/19961216043349I), Dec 16, 1996: Doug DC915 (N95S), Minneapolis, MN, Minor damage. Narrative: during climb at 1000 feet AGL, a noise was heard followed by vibrations and a contained failure of the left engine. Crew followed com emergency… - [Incident 19940712026599I](https://openairdocs.org/incident/19940712026599I), Jul 12, 1994: Doug DC915 (N95S), Wichita, KS. Tail compartment high temp light came on. Returned.segment high temp ducting broken at flange. - [Incident 19870718044839I](https://openairdocs.org/incident/19870718044839I), Jul 18, 1987: Doug DC915 (N95S), Memphis, TN. Vibration on rotation. Replaced brake assembly and anti-skid control. - [Incident 19850210007519I](https://openairdocs.org/incident/19850210007519I), Feb 10, 1985: Doug DC915 (N95S), Memphis, TN. Flight diverted after unsafe gear lights. Landed without incident. Repinned two wires at left down lock switch. - [Incident 19821128066259I](https://openairdocs.org/incident/19821128066259I), Nov 28, 1982: Doug DC915 (N95S), New Orleans, LA, Minor damage. Pilot incurred a bird strike during takeoff. Returned to airport. - [Incident 19810612039449I](https://openairdocs.org/incident/19810612039449I), Jun 12, 1981: Doug DC915 (N95S), Atlanta, GA, Minor damage. Aircraft wing tip hit jetaway during taxi turn on ramp. Taxi director misjudged. - [Incident 19801228088169I](https://openairdocs.org/incident/19801228088169I), Dec 28, 1980: Doug DC915 (N95S), Chantilly, VA. Za zg zl zh emergency descent after grew unable to control pressurization. - [Incident 19801214084519I](https://openairdocs.org/incident/19801214084519I), Dec 14, 1980: Doug DC915 (N95S), Chicago, IL. Requested and received descent clearance due to rise in cabin altitude. Crew ignored altitude restriction. - [Incident 19800422050419I](https://openairdocs.org/incident/19800422050419I), Apr 22, 1980: Doug DC915 (N95S), Memphis, TN. Flight experienced vibration in left engine. No cause found. ## Other aircraft with N95S - [Registered now](https://openairdocs.org/aircraft/N95S): Beech 65-A90-1, S/N LM-125, 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.