MU2

MITSUBISHI LR-1

Aircraft
Name
LR-1
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Regular tail, mid set
WTC
L
APC
B
Type Code
L2T
Engine
Jet
Engine Count
Single
Position
(Front) Wing leading mounted
Landing gear
Tricycle retractable
Manufacturered as
MITSUBISHI Marquise
MITSUBISHI LR-1
MITSUBISHI MU-2 Marquise
MITSUBISHI MU-2
MITSUBISHI MU-2 Solitaire
MITSUBISHI Solitaire

MU2

The Mitsubishi MU-2 is a high-wing, twin-engine turboprop, and has a pressurized cabin.

Technical Data
Wing span (metric)
11.90 m
Length (metric)
10.10 m
Height (metric)
3.00 m
Powerplant

MU-2: 2 x 605 SHP Garrett TPE331-25A or 2 x 724 SHP Garrett TPE331-G-251M turboprops with 3 blade propellers.

Engine Model(s)
Garrett AiResearch TPE-331
Indicative Performance Data
Take-Off
V2
120 kts
Distance
650 m
MTOW
4050 kg
Initial Climb (to 5000 ft)
IAS
150 kts
ROC
1800 ft/min
Initial Climb (to FL150)
IAS
260 kts
ROC
1500
Initial Climb (to FL240)
IAS
260 kts
ROC
1000 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
280 kts
MACH
n/a
Ceiling
290
Range
1100 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
270 kts
ROD
1500 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
110 kts
Distance
600 m

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