https://upload.wikimedia.org/wikipedia/commons/thumb/a/a6/Mndnr-cl215-N266NR-071028-fox-tanker266-02-16.jpg/220px-Mndnr-cl215-N266NR-071028-fox-tanker266-02-16.jpghttps://upload.wikimedia.org/wikipedia/commons/thumb/4/4d/CL215-263.JPG/220px-CL215-263.JPG

 

***AIRCRAFT “Canadair - C215T/415/UD13”***

REFERENCE INFORMATION (by internet )

 

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

Wing position: High wing (winglets)

Engine position: Above wing pods

Tail configuration: Cruciform tail

Landing gear: Tricycle retractable/Floats fixed

Wing Span: 28.63 m

Length: 19.82 m

Height: 8.98 m

Power plant: 2 x 2.380 SHP P&W PW123AF turboprops with 4 blade propellers.

Flightcrew of two and two observers or 11 to 30 passengers.

 

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

000,000 lbs - 19.890 kg

VMO - Maximum Operating Speed 180 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:        M

Distance:   844 mt

V2 (IAS):   100 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        130 kt

ROC:        1500 ft/min

-(to FL150)

IAS:        150 kt

ROC:        500 ft/min

-(to FL240)

IAS:        nd kt

ROC:        nd ft/min

-(mach)

mach:       nd

ROC:        nd ft/min

 

*****Cruise*****

TAS:        180 kt

MACh:       no data

Ceiling:    FL180

Range:      1000 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        180 kt

ROD:        800 ft/min

 

*****Approach*****

IAS:        140 kt

MCS:        nd kt

ROD:        800 ft/min

 

*****Landing*****

Vht (IAS):  105 kt

APC:        B

Distance:   674 mt