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Socata Aircraft TBM 700 Details
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Type:
TURBOPROP
Specifications
Powerplant(s)
|
Pratt
& Whitney
|
Model
|
PT6A
|
hp/shp (lbst)
|
700
|
TBO
|
3,000 hrs
|
Propeller(s)
|
Hartzell
|
Diameter
|
91
in
|
Length
|
35
ft 0
in
|
Height
|
14
ft4
in
|
Wingspan
|
41
ft 7
in
|
Wing
Area
|
194
sq ft
|
Wing
Loading
|
34
lb/sq ft
|
Power
Loading
|
9.4
lb/hp
|
Seats
|
6/7
|
Cabin
-Length
|
13
ft 4
in
|
-Width
|
4
ft 0
in
|
-Height
|
4
ft 0
in
|
Empty
weight
|
4,167
lb
|
Ramp
weight
|
6,614
lb
|
Gross
weight
|
6,579
lb
|
Useful
load
|
2,447
lb
|
Payload
(full fuel)
|
558
lb
|
Max.
TO wgt
|
6,579
lb
|
Max.
LDG wgt
|
6,250
lb
|
Zero
fuel wgt
|
6,001
lb
|
Fuel
capacity
(std)
290
gal
|
282 (usable)
|
Oil
capacity
|
12.7
qt
|
Baggage
capacity
|
330
lb19
cu ft
|
Limiting
and Recommended Airspeeds
All measurements
given in: Kts
Vx(best angle of climb)
|
95 |
Vy
(best rate of climb)
|
123 |
Va
(design maneuvering)
|
158 |
Vfe
(max flap extended)
|
178 |
Vle
(max gear extended)
|
178 |
Vlo
(max gear operating)
-Extend
|
178 |
-Retract
|
122 |
Vno
(max structural cruising)
|
266 |
Vne
(never exceed)
|
266 |
Vr
(rotation)
|
85 |
Vs1
(stall, clean)
|
75 |
Vso
(stall, in landing
configuration)
|
61 |
|
|
|
Performance
Takeoff
distance, ground roll
|
1,378
ft |
Takeoff
distance over 50-ft obstacle
|
2,133
ft |
Maximum
demonstrated crosswind component
|
20
kt |
Rate
of climb, sea level
|
2,100
fpm |
Maximum
level speed, sea level
|
220
kt |
Maximum
level speed , 26,000
ft
|
300
kt |
Cruise
speed/endurance w/45-min reserve
|
|
|
@75%
power, best economy
|
|
end
4:30 hr
|
range
1,305 nm |
speed
290 kt
|
fuel
53 gph |
|
alt
26,000 ft
|
|
Maximum
operating altitude
|
30,000
ft |
Service
ceiling
|
30,000
ft |
Landing
distance over 50-ft obstacle
|
2,133
ft |
Landing
distance, ground roll
|
1,215
ft |
ICAO
flight plan identifier |
TBM7 |
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