TBM-700 Dimensions & Specifications:

CONFIGURATION
Low wing, metal construction, pressurized cabin, certified to FAR Part 23 amendment 34 (type certificate A60EU) Single pilot IFR, authorized in known icing conditions
DIMENSIONS
Overall length:	34.92 ft (10.645 m)
Height:	14.29 ft (4.355 m)
Wing span:	41.6 ft (12.68 m)
Horizontal tail span:	16.36 ft (4.988 m)
Cabin length:	13.29 ft (4.050 m)
Cabin width:	3.97 ft (1.210 m)
Maximum cabin height:	4.00 ft (1.220 m)
Wing area:	193.75 sq.ft (18.00 m2)
POWER PLANT
Manufacturer:	Pratt & Whitney Canada
Type:	Free turbine, inverse flow PT6A-64
Thermodynamic power:	1,580 ESHP
Flat rated power:	700 SHP
Air intake:	Foreign Object Damage (FOD) Protection with inertial separator
PROPELLER
Manufacturer:	Hartzell
Model:	HC-E4N-3/E9083S (K)
Diameter:	91 in (2.31 m)
Type:	All metal, four blade, hydraulic, constant speed, reverse control and automatic full feathering
Governor:	Woodward 8210.007
FUEL
Types:	Jet A, A1, B (ASTM-D1655), JP4, JP5 (MIL-T-5624L), JP8 (MIL-T-83133A)
Total tank capacity:	290 US gal (1,100 l)
Usable fuel:	282 US gal (1,066 l)
OIL
Type:	MIL-L-23699C (Viscosity 5 cSt)
Total oil capacity:	12.7 US quarts (12 l)
Maximum Consumption:	0.3 US quart (0.29 l/h)
OPERATIONAL CHARACTERISTICS
Maximum freight volume in cabin:	123.6 cu.ft (3.5 m3 )
Freight floor area:	33.9 sq.ft (3.15 m2)
Cargo door dimensions:	3.9 ft x 3.54ft (1.19 m x 1.08 m)
Optional pilot door dimensions:	3.34 ft x 2.56 ft (1.02 m x 0.78 m)
LOADING
Operating empty weight:	4,100 lbs (1,860 kg)
Maximum take-off weight:	6,579 lbs (2,984 kg)
Maximum ramp weight:	6,614 lbs (3,000 kg)
Maximum landing weight:	6,250 lbs (2,835 kg)
Useful load:	2,514 lbs (1,140 kg)
Max payload (refer to payload / range diagram)	1,764 lbs (800 kg)
Luggage compartments:
Aft (pressurized):	220 lbs (100 kg)
Fwd (unpressurized) Load: Door:	110 lbs (50 kg) 1.21 ft x 1.67 ft (0.37 m x 0.51 m)
PERFORMANCE (ISA)
Time to climb to (maximum weight):	20,000 ft: 11 mn 45 s 30,000 ft: 20 mn 30 s
Maximum cruise speed at 26,000 ft:	300 KTAS (555 km / h)
Maximum cruise speed at 30,000 ft:	243 KTAS (450 km / h)
Certified ceiling:	30,000 ft
DISTANCE (ISA - 50 ft)
Take-off:	2,133 ft (650 m)
Landing:	2,133 ft (650 m) with reverse 1,640 ft (500 m)
RANGE (ISA - 45 nm reserve)
Full fuel:
Maximum cruise:	1,350 NM (2,500 km)
Economical cruise:	1,550 NM (2,870 km)
6 pax + luggage (29 lbs per pax):
Maximum cruise:	900 NM (1,667 km)
Economical cruise:	1,080 NM (2,000 km)
SYSTEMS
Flight controls:
Ailerons and spoilers, actuated by push / pull rods and cables Conventional empennage with movable part actuated by push / pull rods Electrical trim on the three control surfaces Slotted flaps with electrical actuation Autopilot and vertical speed / altitude preselector
Landing gear:
Retractable gear with hydraulic actuators Emergency actuation with manual hydraulic pump Steerable front wheel Hydro-pneumatic shock absorbers Hydraulic brakes with discs
Fuel system:
One structural fuel tank per wing Engine driven mechanical fuel pump Emergency electrical fuel pump Automatic or manual fuel tank selector with sequencer unit Capacitive fuel gauge system
Electric generation and distribution:
Starter generator 56 kW - 28 V Auxiliary alternator NiCad battery (40A.h) NATO external electrical power plug Bus Distribution
Air conditioning and pressurization:
Environmental Control System (ECS) provided by engine bleed air and bootstrap system Pressurization with two regulation valves [p max = 6.2 psi (427 mb)] Cabin altitude below 8,000 ft (2,440 m) up to aircraft altitude of 28,500 ft (8,690 m)
Emergency oxygen:
3 bottles located under the seats Passenger masks 2 masks with microphone on front seats
Deicing:
Pneumatic deicing of wings and impinges leading edges Electrical deicing of windshield Electrically heated pitots Electrical deicing of propeller Engine air intake deiced by exhaust gases
Specific equipment:
Metal reinforced floor (option) Tie-down points in floor rails customized according to type of freight Pilot door (option)
Conversion from freight configuration to 6 / 7 passengers configuration available for cross-country flying with a quick-change capability.
All Socata aircraft fleet are designed with low maintenance cost in mind. The direct operating cost for the TBM aircraft is also less expensive than those of the competitors and offers an unequalled price-to-performance ratio much appreciated by the users.