*****AIRCRAFT
“Piper – 600 AEST”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Mid wing
Engine position: (Front) Wing leading mounted
Tail configuration: Regular
tail, mid set
Landing gear: Tricycle retractable
Wing Span: 11.2 m
Length: 10.6 m
Height: 3.9 m
Power plant: 600A: 2 x 290
HP Lycoming IO-540-K1J5 piston engines with 3 blade propellers. 700P: 2 x 350
HP Lycoming TIO-540-K2A turbocharged piston engines with 3 blade propelle.
Accommodation: One pilot and 5 passengers.
Notes: High performance light
aircraft. In service since 1968. Developed as response to the AERO COMMANDERS
twins. Exists in several versions, last more powerful and turbocharged model
PA-60-700P. Built first by TED SMITH (later AEROSTAR) INSERT INTO tblaircraftdatasupp VALUES United States, transfered to PIPER as PA-60 Aerostar
in 1982.
Alternative names:
Aerostar
AEROSTAR (1) 600,601, AICSA Aerostar, MACHEN Superstar, PA-60,Aerostar, PIPER PA-60,Aerostar, TED SMITH Aerostar
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 2.860 kg
VMO - Maximum Operating Speed 230 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 degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: L
Distance: 550
mt
V2 (IAS): 95
kts
*****Climbing*****
-(to 5000 ft)
IAS: 125
kt
ROC: 1500
ft/min
-(to FL150)
IAS: 180
kt
ROC: 1300
ft/min
-(to FL240)
IAS: 180
kt
ROC: 800
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 230
kt
MACh: nd
Ceiling: FL290
Range: 1200
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 230
kt
ROD: 2500
ft/min
*****Approach*****
IAS: 160
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 100 kt
APC: B
Distance: 350
mt