*****AIRCRAFT
“Piper - PA27 Atzec”*****
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: 11.4 m
Length: 9.5 m
Height: 3.1 m
Power plant: 2 x 235 HP Lycoming O-540-B1A5 piston
engines or
2 x 250 SHP Lycoming TIO-540-C1A turbocharged piston
engines
with 2 blade propeller
Accommodation: One pilot and 5 passengers.
Notes: Light twin aircraft. In service since 1960. PA-23-250 Aztec
more powerful turbocharged development of PA-23-150/160 Apache. Production
ceased in 1982
after 4929
aircraft were built including a small number for military operators.
Alternative names:
CHINCUL PA-A-23-250 Aztec, E-19, PA-23-235/250
Aztec,Turbo Aztec
PIPER PA-23-235/250 Aztec,Turbo
Aztec, PIPER
U-11,E-19,UC-26, Turbo Aztec,
U-11, UC-26, PA-23-235/250 Aztec.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 2.360 kg
VMO - Maximum Operating Speed 170 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
***************************************************************
SPEEDS:
STALL CLEAN 76 MPH / 66 KT
DIRTY 70 MPH / 61 KT
MIN CONTROL SE (Vmc/Vr) 80 MPH
/ 70 KT (RED LINE-Lower)
FLAP 1/4. 160
MPH / 139 KT
1/2. 140
MPH / 122 KT
FULL (Vfe) 125
MPH / 109 KT
GEAR EXTENSION (Vle) 150 MPH / 130 KT
CLIMB RATE (Vy) 120 MPH / 102 KT
S.E. (Vyse) 102
MPH / 89 KT (BLUE LINE)
ANGLE (Vx) 107
MPH / 93 KT
S.E. (Vxse) 97
MPH / 85 KT
MANEUVERING SPEED (Vra) 149 MPH / 129 KT
NEVER EXCEED SPEED (Vne) 249 MPH / 216 KT (RED LINE-Upper)
***************************************************************
*****Maximum
Flap Placard Speeds*****
Flaps degrees KT
1/4 139
1/2 122
full 109
*****Take-off*****
WTC: L
Distance: 300
mt
V2 (IAS): 75
kts
*****Climbing*****
-(to 5000 ft)
IAS: 105
kt
ROC: 1000
ft/min
-(to FL150)
IAS: 120
kt
ROC: 500
ft/min
-(to FL240)
IAS: nd kt
ROC: nd ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 170
kt
MACh: nd
Ceiling: FL170
Range: 800
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 170
kt
ROD: 800
ft/min
*****Approach*****
IAS: 170
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 70 kt
APC: A
Distance: 500
mt