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 Characteristics


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

General Information


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

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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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