TBM 940

Max range 1,305 nm
Max cruise speed 300 kts
Max passengers 6 persons
Useful load 1,347 lbs
Takeoff field length 2,133 ft

Releases | OCT

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History

Released in 1990
Released in 1990
  • In 1990 the TBM 700 was the first pressurized single-engine turboprop certified. The original model (TBM 700A) was followed by the B model, featuring a large access door to allow easy passenger and baggage loading, as well as newly designed seats to improve comfort. A new interior sported rich leathers and elegant woodwork finished in high gloss with black chrome or gold inlays.
LEGENDARY PERFORMANCE
LEGENDARY PERFORMANCE
  • Since its introduction, the TBM 700 has kept its promise: delivering jet-like performance on a pistontwin budget, as well as turbine safety and superb handling throughout the flight envelope. Its short field performance is legendary. The TBM 700 slips into 2,800 ft (860 m) strips or mountain airports where business jets dare not follow.
TBM C model
TBM C model
  • The TBM 700 C model is the culmination of 10 years of fine-tuning, making it the most capable of all TBM 700s. Its airframe has been strengthened, its avionics upgraded, it is equipped with a new luggage compartement aft of the passenger cabin and with a new cabin environment control system setting a new reference in travel standard.
TBM C2 variant
TBM C2 variant
  • The TBM 700C2 variant is mainly characterized by wheels and tires reinforced and by a cabin equipped with 20 G seats, allowing to take off at an increased MTOW of 7,394 lbs (3354 kg), with a maximum payload of 1,347 pounds (611 kg). This increase in maximum weight translates into a stall speed of 65 KTAS (120 km/h), which meets the rules of FAR Part 23 Amendment 44.

TBM 700 technical details

Specifications

PowerPlant
  • 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
Operational characteristics
  • Max. freight volume in cabin
    123.6 cu. ft.
  • Freight floor area
    33.9 sq. ft.
  • Loading through cargo door
    3.9 ft.
    3.54 ft.
  • Optional pilot door dimensions
    3.34 ft.
    2.56 ft.
Loading
  • Average empty weight
    4,100 Ibs
  • Maximum take-off weight
    6,579 Ibs
  • Maximum ramp weight
    6,614 Ibs
  • Maximum landing weight
    6,250 Ibs
  • Useful load
    2,514 Ibs
  • Max payload
    1.764
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)

TBM Operating Costs

COST OF OWNERSHIP

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Jet A1 cost per gallon :

Direct operating cost per NM ($)

TBM 910/940

Annual fixed costs ($)

TBM 910/940

Minutes flight (min)

TBM 910/940

Cost/seat mile ($)

TBM 910/940
Source : Conklin & Decker june 2019; Aircraft cost evaluator Engine overhaul costs based on JSSI datas for turbines and estimated for jet engines Disclaimer : DOC for TBM is calculated with the 5 Year TBM Total Care Program included.