Daher-Socata TBM 700C2

Overview

The TBM 700 C2 variant features a substantial increase in tanks-full payload. Maximum take-off weight has been increased to 7,394 pounds allowing the C2 to carry three passengers with baggage with full fuel. The TBM 700C2 is a cabin-class single engine turboprop aircraft optimized for five passengers in addition to the pilot, but able to accommodate six passengers in a high-density configuration. The TBM 700C2 is powered by a single Pratt & Whitney Canada PT6A-64 reverse flow, axial-centrifugal turboprop engine flat-rated at 700 shp at ISA + 49C and driving a four-bladed, reversible, constant-speed propeller. Engine inspection interval is 3,500 hours.


Aircraft Specifications


Certified Crew

1

Typical / Maximum Cabin Passenger Capacity

5/6

Balanced Field Length [SL/ISA TMP] (FT)

2840

Length (FT)

34.11

Wingspan (FT)

41.7

Height (FT)

14.4

Cabin Height (FT)

4

Cabin Width (FT)

3.11

Cabin Length (FT)

14.11

Baggage Capacity Internal / External (CFT)

10/4

Powerplant

P&WC PT6A-64

Years Aircraft Manufactured

2003-2006

Estimated Retail Price Low

1,150,000

Estimated Retail Price High

1,500,000

Aircraft Category

SE Turboprop



Operating Cost Overview

Aircraft variable and fixed costs are important to determine before making a purchase decisions or planning annual budgets. Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization.



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Range Map

The Daher-Socata TBM 700C2 has a range of 1,565 nautical miles. Type in your city or airport identifier for a visual representation of the NBAA IFR Range (NM) for this aircraft.


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