*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