***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