Aerospatiale-Socata TBM 700

The TBM-700 is a high performance single engine turboprop powered light business and corporate transport.

The TBM-700 is mainly optimised as a business transport in competition with established twin turboprops, mainly Beech's C90 King Air series. Unlike the similarly sized C90 King Airs though, the TBM-700's single engine layout is a major conceptual difference. With its single PT6 turboprop, rather than two on the King Air, the TBM-700 offers significantly lower operating costs yet comparable performance.

The TBM-700 was originally developed in partnership between Socata (Aerospatiale's General Aviation division) in France and Mooney in the USA, hence the TBM designation. The two companies formed TBM SA to build and market the TBM-700, with development responsibility for the project divided on a 70/30 basis between Socata and Mooney respectively.

The first of three TBM-700 prototypes first flew on July 14 1988. French certification was granted in January 1990. Shortly after the delivery of the first production aircraft in December 1990, Mooney withdrew from the program, leaving Socata with full responsibility for the aircraft.

The pressurised TBM-700 is of conventional design and construction, with a small amount of composite materials used in some areas. Flight controls, flaps and most of the empennage and fin are made from Nomex honeycomb and metal sheets. Leading edges and undercarriage doors meanwhile are made from a carbon and fibreglass composite. Entry to the cabin is through a split upward/downward opening door in the rear port fuselage.

Apart from the base aircraft the TBM-700 is offered as the TBM-700C freighter with a freight door and separate port side cockpit door. Development of the stretched TBM-700S ceased in 1995.

More than 125 in service worldwide. Total of 25 ordered for the French air force and army.

Power Plant
- Manufacturer : Pratt & Whitney Canada
- Type : Free turbine, inverse flow PT6A-64
- Thermodynamic power : 1,570 SHP
- Flat rated power : 700 SHP
- Air intake : deiced, 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 automatic full feathering, reverse control
- Governor : Woodward 8210.007

Fuel

- Types : Jet A, A1, B (ASTM-D1655), JP4, JP5 (MIL-T-5624L), JP8 (MIL-T-83133A)
- Total tank capacity : 290,60 US gal (1,100 I)
- Usable fuel : 281,62 US gal (1,066 I)

Oil

- Type : MIL-L-23699C (Viscosity 5 cSt)
- Total oil capacity : 12,7 US quarts (12 l)
- Max. consumption : 0,3 US quart/h (0,29 l/h)

Operational characteristics

- Max. freight volume in cabin : 123.6 cu.ft (3.5 m3)
- Freight floor area : 33.9 sq.ft (3.15 m2)
- Loading through cargo door : 3.9 ft x 3.54 ft (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)

Dimensions

Loading

- Average empty weight : 4,100 Ibs (1,860 kg)
- Maximum take-off weight : 6,579 Ibs (2,984 kg)
- Maximum ramp weight : 6,614 Ibs (3,000 kg)
- Maximum landing weight : 6,250 Ibs (2,835 kg)
- Useful load : 2,514 Ibs (1,140 kg)
- Max payload 1.764 lbs (800 kg)
  refer to payload / range diagram)
- Luggage compartments :  
- Aft (pressurized) : 220 Ibs (100 kg)
- Non pressurized front bay :  
- Load : 110 lbs (50 kg)
- Hatch
 
1.21 ft x 1.67 ft (0.37 m x 0.51 m)
 
- Conversion from freight configuration to 6/7 passenger configuration available for cross-country flying with a quick change capability.

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)
- Economic 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 : 2133 ft (650 m)
with reverse 1,640 ft (500 m)

Range {ISA - 45 mn reserve}

- Full fuel :
- Maximum cruise : 1,350 NM (2,500 km)
- Economical cruise : 1,550 NM (2,870 km)
- 6 pax + luggage (6 x 90 kg) :
- Maximum cruise : 900 NM (1,667 km)
- Economical cruise : 1,080 NM (2,000 km)