Piper PA-28-161 Pilot Operating Handbook page 106

PIPER AIRCRAFT CORPORATION
PA-28-161, WARRIOR II
SECTION 5
PERFORMANCE
12000
10000
1-
w
w
1'-
8000
I
w
0
~
1-
5
6000
"'
w
a:
~
Ill
Ill
4000
w
a:
II.
Example:
PA-28-161
GLIDE PERFORMANCE
AS SOCIA TEO CONDITIONS:
WEIGHT 2440 LBS. PROP WINOMILLING
FLAPS
o•
NO WIND
73 KIAS
Cruise pressure altitude: 5000 ft.
Terrain pressure altitude: 2000 ft.
Glide distance (9.5 miles minus 3.9 miles): 5.6 nautical miles
CRUISE
2000
T~RR
1.
SEA LEVEL
0
li
10
15 20
GLIDE RANGE - NAUTICAL MILES
GLIDE PERFORMANCE
Figure 5-33
ISSUED: AUGUST 13, 1982
25
REPORT: VB-1180
5·27