FS98 Piper Seneca V
Model by Dana McGee
atocane@c2i2.com

This is a new version of the Piper Seneca V using the fuselage of the Saratoga to get a more realistic version of the windows of the new version. Best cruise altitude is 12,500 ft.

Known problems are the flaps which tend to disappear from a lower forward view, this is caused by the large file size and the limits of AF99 to handle it. Still working on getting the problem fixed.

Piper 2000 Seneca V

SPECIFICATIONS
Base price :
$519,900
Engine make/model:
Continental
TSIO-360-RB
Horsepower@altitude:
220
Horsepower for takeoff:
220
TBO hours:
1800
Fuel type:
100/100LL
Propeller Type:
Hartzell CS
Landing gear type:
Tri/Retr.
Max ramp weight (lbs.):
4773
Gross weight (lbs.):
4750
Landing weight (lbs.):
4513
Std. empty weight (lbs.):
3413
Useful load std. (lbs.):
1337
Payload - full std. fuel
(lbs.):
605
Usable fuel - std. (gals.):
122
Wingspan:
38 ft. 10 in.
Overall length:
28 ft. 7 in.
Height:
9 ft. 11 in.
Wing area (sq. ft.):
209
Wing loading (lbs./sq. ft.):
22.7
Power loading (lbs./hp):
10.8
Wheel base (ft.):
7
Wheel track:
11 ft. 1 in.
Wheel size (in.):
6.00 x 6
Seating capacity:
6
Cabin doors:
2
Cabin width (in.):
49
Cabin height (in.):
47
Baggage capacity (lbs.):
100 (F), 85 (R)
PERFORMANCE
Cruise speed (knots):
75% power:
197
65% power:
190
55% power:
180
Max range (with reserve) (nm):
75% power:
730
65% power:
800
55% power:
828
Fuel consumption (gph):
75% power:
29.0
65% power:
23.3
55% power:
18.7
Estimated endurance (65%)
(hrs.):
5.5
Stall speed (gear, flaps up)
(kts.):
65
Stall speed (gear, flaps
down) (kts.):
61
Best rate of climb SL (fpm):
1550
Best rate of climb, 8000 ft.
(fpm):
1250
Max operating altitude
(ft.):
25,000
Single-engine service
ceiling (ft.):
16,500
Takeoff ground roll (ft.):
1143
Takeoff over 50-ft.
obstacle (ft.):
1707
Landing ground roll (ft.):
1400
Landing over 50-ft.
obstacle (ft.):
2180