P32R

PIPER PA-32R

Aircraft
Name
PA-32R
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
Low wing
Tail
Regular tail, low set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tricycle retractable
Manufacturered as
PIPER Lance
PIPER Turbo Saratoga SP
PIPER PA-32R-301T Turbo Saratoga SP
PIPER Saratoga 2 HP
PIPER Saratoga 2 TC
PIPER Saratoga SP
PIPER Cherokee Lance
PIPER PA-32R-301T Saratoga 2 TC
PIPER PA-32R-300 Cherokee Lance
PIPER PA-32R-300 Lance
PIPER PA-32R-301 Saratoga 2 HP
PIPER PA-32R-301 Saratoga SP
NEIVA Sertanejo
NEIVA EMB-721 Sertanejo
EMBRAER EMB-721 Sertanejo
EMBRAER Sertanejo
CHINCUL PA-A-32R-300 Cherokee Lance
CHINCUL PA-A-32R-300 Lance
CHINCUL Cherokee Lance
CHINCUL Lance
AICSA Lance
AICSA PA-32R-300 Lance
AICSA PA-32R-301T Turbo Saratoga SP
AICSA Turbo Saratoga SP

P32R

Light aircraft. In service since 1977. Retractable gear development of PA-32 Cherokee six. Replaced by Lance series in 1979 and later by Saratoga SP. Licence production by CHINCUL, Argentina, AICSA, Columbia, and by EMBRAER/NAIVA, Brazil, as EMB-721 Sertanejo.

Technical Data
Wing span (metric)
11.00 m
Length (metric)
8.60 m
Height (metric)
2.60 m
Powerplant

1 x 300 HP Lycoming IO-540-K1G5 piston engine with 2 or 3 blade propeller.

Engine Model(s)
Lycoming O-540
Indicative Performance Data
Take-Off
V2
n/a
Distance
293 m
MTOW
1633 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
1100 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
177 kts
MACH
n/a
Ceiling
200
Range
950 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
223 m

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