SOCATA TBM-850

Aircraft
Name: 
TBM-850
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
Regular tail, low set
WTC
L
APC
B
Type Code: 
L1T
Engine: 
Turboprop
Engine Count: 
Single
Position: 
Nose mounted
Landing gear: 
Tricycle retractable
Manufacturered as
SOCATA TBM-850

TBM8

The TBM 850 is the production name for the TBM 700N, an improved version with the more powerful Pratt & Whitney PT6A-66D engine flat rated at 850 shp (634 kW). The TBM 850 is limited to 700 shp (522 kW) for takeoff and landing, but in cruise flight the engine power can be increased to 850 shp (634 kW). This extra power gives it a higher cruising speed than the TBM 700 models, especially at high altitudes. The outside appearance of the TBM 850 has remained the same as that of the TBM 700. The TBM 850 has a typical range of 1520 nm.

Technical Data
Wing span: 
12.20 m
Length: 
10.40 m
Height: 
4.20 m
Powerplant: 

1 x P&W PT6A-66D engine flat rated at 850 shp (634 kW).

Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
870 m
MTOW: 
3400 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
250 kts
MACH: 
n/a
Ceiling: 
310
Range: 
1500 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
750 m

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