***AIRCRAFT “Rockwell – AC6L Grand Commander”***

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position: High wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail (Anhedral)

Landing gear: Tricycle retractable

Wing Span: 14.4 m

Length: 13.5 m

Height: 4.6 m

Power plant: 2 2 x 380 HP Lycoming IGSO-540-B1C piston engines with 3 blade propellers.

Accommodation: One pilot and 4 to 6 passengers.

Notes: Light utility corporate aircraft. In service since 1964. Piston engines powered version of 690 Turbo Commander. Developed from 1964 to 1967 on base of the 580 series.
Alternative names:
685 Courser Commander, Commander 685, Grand Commander, NORTH AMERICAN ROCKWELL 680FL,685.

 

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

000,000 lbs – 4.650 kg

VMO - Maximum Operating Speed 170 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):         80 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 110 kt

ROC:               1000 ft/min

-(to FL150)

IAS:                 130 kt

ROC:               500 ft/min

-(to FL240)

IAS:                 nd kt

ROC:               nd ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                170 kt

MACh:             nd data

Ceiling:            FL200

Range:            1200 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 170 kt

ROD:               800 ft/min

 

*****Approach*****

IAS:                 170 kt

MCS:               nd kt

ROD:               500 ft/min

 

*****Landing*****

Vht (IAS):        75 kt

APC:                A

Distance:         400 mt