AC11
COMMANDER 112
COMMANDER 112
Aircraft
Name
112
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, mid set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufactured as
ROCKWELL 112 Alpine Commander
ROCKWELL Commander 112
ROCKWELL Commander 114
ROCKWELL Gran Turismo Commander
ROCKWELL Alpine Commander
ROCKWELL 114 Commander 114
ROCKWELL 112 Commander 112
ROCKWELL 114 Gran Turismo Commander
NORTH AMERICAN ROCKWELL Commander 112
NORTH AMERICAN ROCKWELL 112 Commander 112
COMMANDER Commander 114
COMMANDER Commander 115
AC11
Light aircraft. In service since 1972. Light aircraft development orginally by ROCKWELL. Commander 112 replaced by turbocharged 112TC Alpine Commander with wingtips and more powerful 114 in 1976. Commander Aircraft Company incorporated in 1988, resulting new developed Commander 114B (since 1992) and turbocharged 114TC (since 1995). New high performance model (since 2000): Commander 115. Commander 114TC has a ceiling of 25000 ft.
Technical Data
Wing span (metric)
10.00 m
Length (metric)
7.60 m
Height (metric)
2.60 m
Powerplant
112: 1 x 200 HP Lycoming IO-360-C1D6 piston engines with 2 blade propeller. 114/115: 1 x 263 HP Lycoming IO-540-T4B5 piston engine with 3 blade propeller.
Engine Model(s)
Lycoming O-360
Lycoming O-540
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
1480 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
160 kts
MACH
n/a
Ceiling
165
Range
700 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a
