2011 DAHER-SOCATA TBM850 S/N569 D-FRAS Garmin 1000 Avionics / MT 5-blade propeller
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1 2011 DAHER-SOCATA TBM850 S/N569 D-FRAS Garmin 1000 Avionics / MT 5-blade propeller If you want to stay in your comfort zone, but while cruising at 31,000 feet and with an approach speed slow enough to land on most runways, the TBM850 from DAHER-SOCATA is for you. Nearly as quick as a light jet, but at a fraction of the cost, the TBM850 offers substantially more payload and range. Featuring outstanding dependability and ease of handling, the TBM850 is powered by the Pratt & Whitney PT6A turbine engine and equipped with state-ofthe-art Garmin 1000 avionics. The TBM850 s luxuriously-appointed cabin and distinctive European styling raise the bar even further. We invite you to take the controls for an unforgettable experience, flight after flight.
2 STANDARD DEFINITION (2011 MODEL) Certified ceiling 31,000 ft (Gazeous oxygen system) PREMIUM EDITION FITTINGS INCLUDING 6 fabric seats with adjustable backrests and folding armrests Fully adjustable (3-axis) pilot and co-pilot seats and adjustable rudder pedals Ultraleather upper cabin side panels, leather covered lower cabin side panels, wool carpeting Individual fresh-air vents and reading lights Pilot and co-pilot sun visors Front and rear 24 V outputs (one in cockpit, one in passenger cabin) Ship-powered headset jacks behind each seat Baggage compartment with straps, baggage net and coat rack 2008 standard Paint scheme DELUXE LEATHER PACKAGE 6 genuine leather seats with adjustable backrests and folding armrests in replacement for fabric Genuine leather upper side panels Satinbrass trimming of individual fresh-air vents and reading light ring
3 STANDARD AVIONICS PACKAGE 2 GMA 1347C Dual digital audio controller with integrated marker beacon receiver, intercom and public address capability on outer side for pilot and co-pilot side 1 Sennheiser HMEC25 noise attenuating headset with ship-power connection 2 GDU 1040A, 10'' PFD display with three axis flight dynamics, air speed, altitude, vertical speed, HSI w/ perspective modes, turn, bank side slip, NAV/COM frequencies indication and AP annunciation 1 GDU '' multi-function display with engine (w/ optimum TRQ setting display), pressurization, electrical, fuel, flaps and trim indication, Crew Alerting Systems (CAS), checklist, aircraft synoptics and super large navigation mapping system 2 GIA 63W Nav/Com/ILS/WAAS GPS 2 GEA 71 Engine and airframe interface unit 2 GRS 77 Attitude and Heading Reference System (AHRS) 2 GMU 44 tri-axial magnetometer 2 GDC 74B digital air-data computers w/ dual probe system 1 GTX33 Mode S transponder 1 GCU 475 remote FMS control panel conveniently located on the central consol 1 GMC 710 autopilot mode controller located in upper central panel 4 GSA 81 torque flight servos (yaw, pitch, pitch trim and roll) 1 GTA 82 adapter for yaw auto trim device Backup instrumentation with pneumatic attitude, airspeed and altimeter indicators similar to photo
4 ADVANCED POSITION AND TRAFFIC AWARENESS PACKAGE RVSM data package GTX 33 Mode S transponder (#2) KRA 405 B Radar Altimeter displayed on GDU 1040As TAWS-B, class B TAWS worldwide database KTA 810 Traffic Advisory System (TAS) KN 63 DME displayed on GDU 1040As (****) Electric pitch and rudder trims on co-pilot control wheel Co-pilot side map light and approach plate holder ON-BOARD WEATHER PACKAGE WX 500 Stormscope displayed on G1000 displays GWX 68 digital four color weather radar - 10'' antenna similar to photo MISCELLANEOUS GTX 33D Enhanced (EHS) Mode S with diversity antenna transponder (#1) in replacement for GTX 33 mode S (****) Chart view option for GDUs Front and rear 14V DC power outlets (replacement for 24V outputs) Synthetic Vision Technology to be displayed on both of PFD GDU1040As Wood trim central upper panel, wooden insert exterior table cover
5 MT 5-BLADE PROPELLER (*) More Ground Clearance due to reduced propeller diameter. Less FOD possibility The highest noise requirements are fulfilled for unlimited operation without any restrictions At 1800 propeller rpm increased speed by 3 to 5 kts with reduced cabin noise 5 % shorter Take-off Run Improved Climb Performance Reduced Cabin Noise by 3 to 4 db(a) depending on location Reduced Vibration Level due to the Composite Blade Design with High Damping Characteristics Unlimited Blade Life protected with Stainless Steel Leading Edge Ramp Appeal due to the 5-bladed Scimitar Composite Design (*) Technical details according to statement of MT Propeller
6 FOR MORE INFORMATION PLEASE CONTACT OUR SALES DEPARTMENT Frank Prochaska Sales Manager DAHER-SOCATA TBM850 T: M: Rheinland Air Service GmbH Flughafenstrasse 31 D Mönchengladbach
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