*****AIRCRAFT
“Piaggio - P808”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft Features*****
Aircraft Features
Wing position: Low wing with wing tip tanks
Engine position: Both sides of rear fuselage
Tail configuration: Regular tail, high set
Landing gear: Tricycle retractable
Wing Span: 13.2 m
Length: 12.8 m
Height: 4.5 m
Power plant: 2 x 15.24 kN
R-R (Bristol Siddeley) Viper 525 turbojets.
Accommodation: Flightcrew of two and 7 passengers, 10 troops or 3 patients.
Notes: Commuter airliner and utility
transport aircraft.First prototype flew in August
1965. Operated by Italian Air Force as transport and EW (Electronic Warfare)
aircraft.
Alternative names:
PIAGGIO PD-808.
*****Total Flight
Simulator aircraft weight with full fuel*****
000,000 lbs - 8.170 kg
VMO - Maximum Operating Speed 380 KIAS
MMO - Maximum Operating Speed Mach 0.69 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: 900
mt
V2 (IAS): 100
kts
*****Climbing*****
-(to 5000 ft)
IAS: 130
kt
ROC: 1500
ft/min
-(to FL150)
IAS: 300
kt
ROC: 1500
ft/min
-(to FL240)
IAS: 300
kt
ROC: 1500
ft/min
-(mach)
mach: 0.70
ROC: 1000
ft/min
*****Cruise*****
TAS: 380
kt
MACh: 0.69 data
Ceiling: FL480
Range: 1300
NM
*****Descent
*****
- (to FL240)
mach: 0.75
ROD: 800
ft/min
- (to FL100)
IAS: 300
kt
ROD: 3000
ft/min
*****Approach*****
IAS: 250
kt
MCS: nd kt
ROD: 1500
ft/min
*****Landing*****
Vht
(IAS): 105 kt
APC: B
Distance: 800
mt