*****AIRCRAFT
“Piper - PA31 Navajo”*****
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
Wing Span: 12.4 m
Length: 9.9 m
Height: 4.0 m
Power plant:
PA-31: 2 x 310 HP Lycoming TIO-540-A turbocharged piston engines
with 3 blade propellers.
Chieftain: 2 x 350 HP Lycoming TIO-540-J2BD
turbocharged piston engines
with 3 blade propellers.
Accommodation: One pilot and 5 passengers (9 in Chieftain).
Notes: Corporate twin and commuter aircraft. In service since 1965
(Chieftain since 1973). Commuter and airliner development. Basic for a large
series of developments
that led to
Cheyenne 400LS. PA-31-350 Chieftain improved, stretched version for 9
passengers with more powerful counter rotating engines. Production of the
Navajo ceased in 1983 (1800 aircraft built) and of the Chieftain in 1984 (1825
aircraft built). Pressurized versions PA-31P Pressurized Navajo and PA-31P-350
Mojave. The PA-31-310 Navajo has 3 square and one rounded cabin windows, the
PA-31-350 has 4 square cabin windows. Chieftain: Length 10,6 m MTOW 3200 Kg.
Alternative names:
COLEMILL Panther Navajo,Panther 2/3, EMB-820
Navajo, EMBRAER EMB-820 Navajo
Navajo, Navajo
Chieftain, NEIVA EMB-820 Navajo, PA-31 Navajo,Navajo, Chieftain,Chieftain, Panther
2/3, Panther Navajo, PIPER PA-31 Navajo,Navajo Chieftain,Chieftain, PA-31
Navajo, Chieftain.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 2.950 kg
VMO - Maximum Operating Speed 190 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: 400
mt
V2 (IAS): 90
kts
*****Climbing*****
-(to 5000 ft)
IAS: 120
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 140
kt
ROC: 800
ft/min
-(to FL240)
IAS: 140
kt
ROC: nd ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 190
kt
MACh: nd
Ceiling: FL270
Range: 1000
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
mach: 190
ROD: 800
ft/min
*****Approach*****
IAS: 190
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 90 kt
APC: A
Distance: 6O0
mt