*AIRCRAFT
“Rockwell – AC11/112 Commander”*
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Nose
mounted
Tail configuration: Cruciform
tail
Landing gear: Tricycle
retractable
Wing Span: 10 m
Length: 7.6 m
Height: 2.6 m
Power plant: 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.
Accommodation: One pilot and 3 or 4 passengers.
Notes: 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.
Alternative names:
114 Commander 114,
Alpine Commander, Commander
112, Commander 114
COMMANDER Commander 114,
Gran Turismo Commander,
NORTH AMERICAN ROCKWELL 112, ROCKWELL 112 Commander 112, ROCKWELL 114 Commander 114.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 1.480 kg
VMO - Maximum Operating Speed 150 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: 350
mt
V2 (IAS): 70
kts
*****Climbing*****
-(to 5000 ft)
IAS: 100
kt
ROC: 800
ft/min
-(to FL150)
IAS: 110
kt
ROC: 200
ft/min
-(to FL240)
IAS: nd kt
ROC: nd ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 150
kt
MACh: nd data
Ceiling: FL160
Range: 750
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 140
kt
ROD: 500
ft/min
*****Approach*****
IAS: 140
kt
MCS: 67
kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 70 kt
APC: A
Distance: 220
mt