*********10********20********30********40********50********60
***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:
Length:
Height:
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*****
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
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