*****AIRCRAFT “Mitsubishi - MU2”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Wing position: High wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle retractable

Wing Span: 11.9 m

Length: 10.1 m

Height: 3.9 m

Power plant: MU-2: 2 x 605 SHP Garrett TPE331-25A or

2 x 724 SHP Garrett TPE331-G-251M turboprops with 3 blade propellers.

Marquise: 2 x 715 SHP Garrett TPE331-10-501M turboprops with 4 blade propellers.

Accommodation: One or two pilots and 7 passengers (11 in Marquise).

Notes: Utility transport aircraft. In service since 1964 (MU-2G since 1978). Light twin turboprop transport aircraft development, built in several versions. Also used by Japan Air Self Defence Forces as SAR aircraft. MU-2G Marquise stretched more powerful export version built by Mitsubishi International in San Angelo, Texas.

Production ceased in 1986. Marquise: Length 12,01 m MTOW 5250 kg.
Alternative names:
Marquise
MITSUBISHI MU-2,Marquise,Solitaire (LR-1), MU-2,Marquise,Solitaire (LR-1), Solitaire, MU-2,Marquise,Solitaire
.

 

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

000,000 lbs - 4.050 kg

VMO - Maximum Operating Speed 280 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:         650 mt

V2 (IAS):         120 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 150 kt

ROC:               1800 ft/min

-(to FL150)

IAS:                 260 kt

ROC:               1500 ft/min

-(to FL240)

IAS:                 260 kt

ROC:               1000 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                280 kt

MACh:             no data

Ceiling:            FL290

Range:            1100 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 270 kt

ROD:               1500 ft/min

 

*****Approach*****

IAS:                 230 kt

MCS:               nd kt

ROD:               1500 ft/min

 

*****Landing*****

Vht (IAS):        110 kt

APC:                B

Distance:         600 mt