*****AIRCRAFT “Beech - T50 Bonanza”*****

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: 14.0 m

Length: 9.6 m

Height: 3.5 m

Power plant: 2 x 295 HP Lycoming GO-480-G2F6 or

2 x 340 HP Lycoming IGSO-480-A1B6 or

2 x 400 HP Lycoming IO-729-A1A piston engine with 3 blade

propellers.

Accommodation: One pilot and 5 to 6 passengers.

Notes: Light twin-engined utility aircraft. In service since 1950. J50 more powerful development for higher speed, higher service ceiling and extended range. Again more powerful development Excalibur by SWERINGEN, USA. Mil. type: U-8 Seminole. J50: MTOW 3310 kg. Excalibur: MTOW 3450 Kg.
Alternative names:
BEECH 50 Twin Bonanza, BEECH U-8D/E/G,RU-8 Seminole, Excalibur, EXCALIBUR Excalibur, RU-8 Seminole, SWEARINGEN Excalibur, Twin Bonanza, U-8D/E/G
.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 2.680 kg

VMO - Maximum Operating Speed 160 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):   95 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        125 kt

ROC:        1000 ft/min

-(to FL150)

IAS:        125 kt

ROC:        500 ft/min

-(to FL240)

IAS:        nd kt

ROC:        nd ft/min

-(mach)

mach:       nd

ROC:        nd ft/min

 

*****Cruise*****

TAS:        160 kt

MACh:       nd

Ceiling:    FL200

Range:      600 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        160 kt

ROD:        800 ft/min

 

*****Approach*****

IAS:        160 kt

MCS:        nd kt

ROD:        500 ft/min

 

*****Landing*****

Vht (IAS):  80 kt

APC:        A

Distance:   300 mt