TBM7
SOCATA TBM-700
SOCATA TBM-700
Aircraft
Name
TBM-700
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, mid set
WTC
L
APC
A
Type Code
L1T
Engine
Turboprop
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufactured as
TBM TBM-700
SOCATA TBM-700
TBM7
Single engine business aircraft. In service since 1990. High performance single turbo-prop light business and corporate aircraft. Partnership development of SOCATA, France, and MOONEY, United States. TBM-700C freighter version with a large freight door and separate/portside cockpit door. The French Air Force and Army are the main users of this type.
Technical Data
Wing span (metric)
12.20 m
Length (metric)
10.40 m
Height (metric)
4.20 m
Powerplant
1 x 700 SHP P&W PT6A-64 turboprop with 4 blade propeller.
Engine Model(s)
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2
85 kts
Distance
650 m
MTOW
3000 kg
Initial Climb (to 5000 ft)
IAS
115 kts
ROC
2000 ft/min
Initial Climb (to FL150)
IAS
200 kts
ROC
1000
Initial Climb (to FL240)
IAS
200 kts
ROC
1000 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
290 kts
MACH
0.46
Ceiling
300
Range
900 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
240 kts
ROD
1500 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
80 kts
Distance
500 m
