***AIRCRAFT
“Embraer - PA34 Seneca III”***
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Front) Wing leading mounted
Tail configuration: Regular tail, mid set
Landing gear: Tricycle retractable
Wing Span: 11.9 m
Length: 8.7 m
Height: 3.0 m
Power plant: 2 x 200 HP Lycoming IO-360-A1A piston
engines or
2 x 200 HP Continental TSIO-360-E turbocharged piston
engines with
2 blade propellers.
Seneca 4: 2 x 220 HP Continental TSIO-360-KB
turbocharged piston engines
with 3 blade propellers.
Accommodation: One pilot and 5 passengers.
Notes: Light twin aircraft. In service since 1971. Twin-engine
development of PA-32R. First version PA-34-200 Seneca replaced by 200T Seneca
II in 1974. Further development 210T Seneca III introduced in 1981, replaced by
220T Seneca IV in 1994. Licence production by
CHINCUL, Argentinia, AICSA, Columbia, and by
EMBRAER/NAIVA, Brazil, as EMB-810 Seneca. Seneca II built by PZL-MIELEC,
Poland, as M-20 Mewa, Gemini. Latest model Seneca V
(introduced in 1998) with Continental TSIO-360-RB engines and five seats.
Alternative names:
PA-34 Seneca,
PIPER PA-34 Seneca, Princess, PZL-MIELEC
M-20 Mewa,Gemini
SEGUIN Princess, Seneca, TM-20 Flamingo 3, U-7 (PA-34).
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 2.160 kg
VMO - Maximum Operating Speed 180 KIAS
MMO - Maximum Operating Speed Mach nd
Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: L
Distance: 300
mt
V2 (IAS): 80
kts
*****Climbing*****
-(to 5000 ft)
IAS: 110
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 140
kt
ROC: 500
ft/min
-(to FL240)
IAS: 140
kt
ROC: ND
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 180
kt
MACh: nd data
Ceiling: FL250
Range: 800 NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 180
kt
ROD: 800
ft/min
*****Approach*****
IAS: 180
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 80 kt
APC: A
Distance: 400
mt