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***AIRCRAFT “British Aerospace - ATP”***
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: Low wing
Engine position:
(Front) Wing leading mounted
Tail
configuration: Regular tail, mid set
Landing
gear: Tricycle retractable
Length:
Wingspan:
Height:
Wing
area:
Powerplant:
ATP: 2 x 2.653 SHP P&W PW
6 blade propellers.
JS61: 2 x 2.050 SHP P&W PW 127 D turboprops
with 6
blade propellers.
Accommodation:
Flightcrew of two and typical 64 passengers
(70 in Jetstream 61).
Notes: Turboprop regional airliner. In
service since 1988.
Modernized and stretched development of HS 748,
also used in a
freighter version. A total of 62 ATPs were
built before the
production ended in 1994. A newer development
was the Jetstream 61
but it was not put into production.
Alternative names:
British Aerospace
ATP, Jetstream 61.
*****Total Flight Simulator aircraft weight
with full fuel*****
Empty
weight:
Max.
takeoff weight:
VMO -
Maximum Operating Speed 000 KIAS
MMO -
Maximum Operating Speed Mach .00 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*****
Takeoff
flaps 15 (2 notches) Some up-elevator trim
MTOW:
WTC: M
Distance: 1351 mt
V2
(IAS): 105 kts
Vr 105 kts
*****Climbing*****
Ascent
VS 1500-1200 f/m
-(to
IAS: 140 kt
ROC: 1000 ft/min
-(to
FL150)
IAS: 185 kt
ROC: 600 ft/min
-(to
FL240)
IAS: 185 kt
ROC: 600 ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
Cruise
speed:
Range:
Service
ceiling:
TAS: 266 kt
MACh: no data
Ceiling: FL250
Range: 1000 NM
*****Descent *****
Descent
1200-1500 f/m
- (to
FL240)
mach: nd
ROD: nd ft/min
- (to
FL100)
IAS: 230 kt
ROD: 1500 ft/min
*****Approach*****
IAS: 180 kt
MCS: 140 kt
ROD: 800 ft/min
*****Landing*****
Vref: 105
kts at full flap
Vht
(IAS): nd kt
APC: B
Distance: 1128 mt