# N952AR: 1992 Mcdonnell Douglas MD-11F, registration cancelled 2020-10-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 3, 2020 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600) - Engine: [Pratt & Whitney PW4460](https://openairdocs.org/engine/pratt-whitney-pw4460) (registry code 51673) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (OpenAirDocs) - Serial number: 48497 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 18, 2010 - Certificate issued: June 16, 2014 - Last registry action: April 25, 2017 - Mode S code: AD3C25 - Owner when cancelled: [Sky Lease I Inc](https://openairdocs.org/faa-owner/SKY%20LEASE%20I%20INC) - Location: [Miami Springs, FL](https://openairdocs.org/faa-place/FL/Miami%20Springs) - Owner type: Corporation - Owner's area on the map: 25.8166° N, 80.3105° W: Placed by OpenAirDocs at the center of ZIP code 33166, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N952AR - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=952AR - Page: https://openairdocs.org/deregistered/N952AR-2020-10-03 From the FAA registry file of November 4, 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 MD-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md ## Service difficulty reports (15) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR WRNA201301270017](https://openairdocs.org/sdr/WRNA201301270017), Jan 21, 2014: ENGINE. FAILED. DURING TAKEOFF ROLL, CREW DISCOVERED THE ACFT SUFFERED AN AUDIBLE ENGINE STALL AND FAILURE. CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. - [SDR WRNA201312270016](https://openairdocs.org/sdr/WRNA201312270016), Dec 22, 2013: CABLE. BROKEN. DURING APPROACH, CREW EXPERIENCED A SLAT DISAGREE INDICATION. TOOK APPROPRIATE PECAUTIONS AN LANDED WITHOUT INCIDENT. AFTER VISUAL INSPECTION BY MAINTENANCE, PR - [SDR WRNA201300015](https://openairdocs.org/sdr/WRNA201300015), Oct 21, 2013: PILOT VALVE. OVERTEMP. AFTER DEPARTURE, APPROX 45 MINUTES, CREW HAD A LEVEL 3 ALERT FOR BLEED AIR TEMP HIGH. NR 1 AIR SYS AUTO SHUTDOWN AND NR 2 SYS WAS ON DMI. CREW FOLLOWED QRH PROC - [SDR WRNA201308070011](https://openairdocs.org/sdr/WRNA201308070011), Aug 2, 2013: OIL SYSTEM. OVERHEATED. ON DEPARTURE, "OIL TEMP HIGH" ANNUNCIATION WITH OIL TEMP ON THE NR 1 ENGINE AT 166 DEGREE C. REDUCED POWER ON NR 1 IAW THE QRH. IDLE POWER WAS REQUIRED TO KEEP - [SDR WRNA201300010](https://openairdocs.org/sdr/WRNA201300010), Apr 21, 2013: BATTERY. DEFECTIVE. DURING TOP OF CLIMB, CREW NOTICED AIRCRAFT BATTERIES NR 1 & 2 INDICATING LOW VOLTS. THEY WERE INSTRUCTED BY MAINTENANCE CONTROL TO RETURN SINCE THEY WERE 45 MIN - [SDR WRNA201300009](https://openairdocs.org/sdr/WRNA201300009), Apr 16, 2013: CARBON SEAL. BROKEN. NR 1 ENGINE OIL QTY LOW, TEMP AND PRESSURE NORMAL. DURING CLIMBOUT FROM MIA TO LIM. PILOTS NOTICED NR 1 ENGINE HAD LOSS OIL QUANTITY WITH TEMP AND PRESSURE NORM - [SDR WRNA201300008](https://openairdocs.org/sdr/WRNA201300008), Apr 12, 2013: HOUSING. DAMAGED. DURING FLIGHT FROM IQQ TO MIA PILOTS NOTICED NR 1 ENGINE HAD LOSS OF OIL PRESSURE AND OIL QUANTITY. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE. ON SHUTDO - [SDR WRNA201300006](https://openairdocs.org/sdr/WRNA201300006), Mar 21, 2013: SEAL. LEAKING. DURING FLIGHT FROM CCS TO SCL PILOTS NOTICED NR 1 ENGINE HAD LOSS OF OIL PRESSURE AND OIL QUANTITY. CREW FOLLOWED SHUTDOWN PROCEDURES FOR NR 1 ENGINE. ON SHUTDO - [SDR WRNA201300005](https://openairdocs.org/sdr/WRNA201300005), Mar 2, 2013: WHEEL. DEPARTED. DURING TAXI FOR DEPARTURE TO MIA, CREW NOTICED LOW TIRE PRESSURE INDICATION LIGHT ILLUMINATED AND SAW NOSE WHEEL DEPARTED ACFT AND WAS ROLLING OFF TAXIWAY. CREW - [SDR WRNA201200014](https://openairdocs.org/sdr/WRNA201200014), Nov 16, 2012: ENGINE. BIRD INGESTION. AFTER TAKEOFF FROM SUMU, HAD HIGH VIBRATION NR 3 ENGINE. DUMPED FUEL TO MAX LANDING WEIGHT AND RETURNED TO FIELD FOR A SAFE LANDING. AFTER LANDING ENGINE NR 3 W - [SDR WRNA2012100500012](https://openairdocs.org/sdr/WRNA2012100500012), Oct 5, 2012: TRIM MOTOR. CRACKED. DURING CLIMB AROUND 8000FT, 'HYD 3 ELEV OFF' ALERT ILLUMINATED. SYNOPTIC PAGE SHOWED 4.5 GAL IN HYD 3 QTY. PLACED HYD SYS IN MANUAL AND TURNED PUMPS OFF TRYING - [SDR WRNA201100006](https://openairdocs.org/sdr/WRNA201100006), Jun 10, 2011: ACTUATOR. MALFUNCTIONED. AFTER T/O DURING FLAP AND SLAT RETRACTION LEVEL 2 ALERT "AIL DEFLECT DISAG" ILLUMINATED. FOLLOWED PROCEDURE ESTABLISHED IN VOL I (QRH). DUMPED APPROX 63000 KGS - [SDR WRNA201100005](https://openairdocs.org/sdr/WRNA201100005), Jun 9, 2011: SWITCH. OBSTRUCTED. DURING CLIMB, CETNER CARGO DOOR OPEN "A" ALERT MESSAGE. CREW FOLLOWED EMERGENCY PROCEEDURES AND RETURNED TO AIRFIELD. LANDING NORMAL. MAINT CHECKED CARGO DOOR I - [SDR WRNA201000008](https://openairdocs.org/sdr/WRNA201000008), Dec 21, 2010: TRANSMITTER. FAULTY. AT 2500 FT DURING CLIMBOUT SPEED 200KTS, LANDING GEAR HORN ON, UNABLE TO SILENCE IT. `NO ABNORALITIES ON GEAR INDICATION. CYCLED GEAR, WITH HORN OUT WHEN GEAR S - [SDR WRNA201000007](https://openairdocs.org/sdr/WRNA201000007), Dec 20, 2010: COMPUTER. UNSERVICEABLE. CLIMBING THRU 12K FT, AURAL WARNING "LANDING GEAR" THEN THE INDICATIONS WERE THAT THE GEAR WAS UP AND RETRACTED, HOWEVER, THE AURAL WARNING "LANDING GEAR" NEVER --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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