***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