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***AIRCRAFT “Aerospatiale - ATR42-500”***

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position: High wing

Engine position:  (Front) Wing leading mounted

Tail configuration: T-tail

Landing gear: Tricycle retractable

Wing Span: 24.6 m

Length: 22.7 m

Height: 7.6 m

Power plant: 2 x 1.900 SHP P&W PW121A Turboprops with 6 blade

propellers.

Accommodation: Flightcrew of two and typical 42 passengers,

up to 50 in high density configuration.

Notes: Twin turboprop regional airliner. In service since 1998. Development of ATR-42-320 with six blade propellers.

Only 2 aircraft built for Czech Airliner CSA.

 

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

000,000 lbs - 17.900 kg

VMO - Maximum Operating Speed 260 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 degr  KIAS

10°         157

15°         140

22°         125

30°         134

gear down   126

 

*****Take-off*****

WTC:        M

Distance:   1100 mt

V2 (IAS):   115 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        140 kt

ROC:        1900 ft/min

-(to FL150)

IAS:        210 kt

ROC:        1200 ft/min

-(to FL240)

IAS:        210 kt

ROC:        1000 ft/min

-(mach)

mach:       nd

ROC:        nd ft/min

 

*****Cruise*****

TAS:        260 kt

MACh:       nd

Ceiling:    FL250

Range:      1700 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        250 kt

ROD:        1500 ft/min

 

*****Approach*****

IAS:        250 kt

MCS:        170 kt

ROD:        1500 ft/min

 

*****Landing*****

Vht (IAS):  120 kt

APC:        B

Distance:   1000 mt