*****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