N87NY - MORANE SAULNIER MS 760 PARIS JET

MORANE-SAULNIER

MS 760 PARIS JET

87

N87NY

Used

TYPE A SINGLE PILOT APPROVED, four-place pressurized, high performance twin jet. POWER PLANT Two TURBOMECA MARBORE VI J engines with 1,060 lbs. thrust each. PERFORMANCE Maximum Take-Off Weight . . . . . . . . . . . . . . 8,650 lbs. Maximum Landing Weight . . . . . . . . . . . . . . . . 6,960 lbs. Average Useful Load . . . . . . . . . . . . . . . . . . . . . 3,850 lbs. Take-Off Distance, Sea Level, Standard Day at Maximum Weight . . . . . . . . . . . . . 3,000 ft. at 7,090 lbs. . . . . . . . . . . . . . . . . . . . 1,580 ft. Take-Off to 50 ft. Sea Level, Standard Day at Maximum Weight . . . . . . . . . . . . . . 5,410 ft. at 7,090 lbs. . . . . . . . . . . . . . . . . . . 3,500 ft. Normal Climb Speed . . . . . . . . . . . . . . . . . . 200 kts. Rate of Climb, Sea Level, Standard Day at Maximum Wt. and 17* Flaps @* 140 kts. . . . . . . . . . . . . . . . . . . . . . 1,575 ft./min. at Maximum Wt. and *Flaps*Up @ 200 kts. . . . . . . . . . . . . . . . . . . . 2,575 ft./min. Rate of Climb With One Engine at Maximum Wt. Gear and Flaps Up @ 160 kts. and without Dumping Fuel. . .512 ft./min. Stall Speed at Max. Landing Wt. . . . . . . . . . . .82 kts. Cruise up to . . . . . . . . . . . . . . . . . . . . . . . . . . 352 ktsTAS Range (Optimum with no Reserve) . . . . . . . 800 nm Ceiling (Certified to) . . . . . . . . . . . . . . . . . . . 25,000 ft. Service Ceiling on One Engine at Max. Wt. . 9,000 ft. Fuel Consumption (High Altitude Cruise) . . . 118 GPH Fuel Capacity . . . . . . . . . . . . .. 370 gals. (Can be extemded to 486 gals. ) BAGGAGE Baggage Compartment . . . . . . . . . . . . . . . . . . . Capacity 66 lbs. Cabin Compartment . . . . . . . . . . . . . . . . . . . . . Capacity 33 lbs. LANDING GEAR Tricycle type with steerable nosewheel equipped with knee-action which offer the softest and smoothest of landings. COCKPIT INSTALLATION Flight Instruments and Radio Navigation Wingtip and Tail Position Lights Fire Warning Light Test Fire Warning Lights Tip Tank Dump Valves Fuel Gauge Wing Tip-Tanks Transfer Lights Fuel Flow meter Dual Tachometer Warning Light for the last 26 gallons in main tank Dual Tailpipe Temperature Indicators Warning System Indicating Entry Stairs not Stowed Dual Starter/Generators (Latest factory modification) Voltmeter Right Pedals Adjustment and Disconnecting Device Emergency Oxygen System Dual Inverters Nose Wheel Clutching Mechanical Emergency Landing Gear and Speed Brake Control Fuel Cocks and Igniter Switches Taxi and Landing Light Pilot's Rudder Adjustment and Parking Brake Control Electric Stabilizer and Aileron Trim Tab Controls Landing Gear Squat Switch Override Selector Landing Gear Position Indicator Outside Air Temperature Pressurization Warning Lights Trim Indicator (Aileron Trim Tab and Stabilizer) Clock (Chronograph) Electric Canopy Open and Close Red Instrument and Panel Lights White Instrument and Panel Lighting Cabin Altimeter Warning Light "Speed Brakes Open" Selector for Windscreen or Feet Heating Pressurization and Air-Conditioning Control Canopy Inflatable Seals Cock Mechanical Canopy Opening Control Landing Gear /safety Switch Speed Brakes Cabin Altimeter Canopy Emergency Jettisoning System Dual Rotating Beacons DIMENSIONS Wing Span . . . . . . . . . 33'3" Stabilizer Span . . . . . . . 11' Length . . . . . . . . . . . . 32'11" Height to Top of Fin . . . 8'6" Landing gear Width . . . 7' 11" PRESSURIZATION Differential - 3.8 Cabin Altitude - Actual Aircraft Altitude Sea Level - 8,200 ft. 6,500 - 16,500 ft. 10,000 - 21,000 ft. ELECTRICAL EQUIPMENT 24-Volt System with Nickel Cadmium Battery Electrically Operated: Landing Gear, Flaps, Aileron, Elevator and Rudder Trim Tabs, Speed Brakes, Dual Heated Pilots, Cockpit Canopy, Fuel Dump Valves All Circuits Protected by Circuit Breakers Marbore II Engines, 1992.7 SAFOH, 328.7/353.7 Since Hot Section Overhaul, New Paint