P
ERFORMANCE AND
F
LIGHT
P
LANNING
AOA
A
NGLE OF
A
TTACK
.
I
NCIDENCE OF THE AERODYNAMIC
CHORD IN RELATION TO THE STILL AIR
.
C
LIMB
G
RADIENT
T
HE RATIO OF THE CHANGE IN ALTITUDE DURING A PORTION
OF A CLIMB
,
TO THE HORIZONTAL DISTANCE TRAVELED IN
THE SAME TIME INTERVAL
.
M
AX
.
D
EMONSTRATED
C
ROSSWIND
C
OMPONENT
T
HE DEMONSTRATED CROSSWIND COMPONENT FOR WHICH
ADEQUATE CONTROL OF THE AIRPLANE DURING TAKE
-
OFF
AND LANDING WAS ACTUALLY DEMONSTRATED
.
T
HE VALUE
IS CONSIDERED TO BE LIMITING
.
R
OUTE
S
EGMENT
P
ART OF A ROUTE
.
E
ACH END OF A LEG IS DEFINED BY A FIX
.
LPH
L
ITERS PER
H
OUR
F
UEL
F
LOW
GPH
G
ALLONS PER
H
OUR
F
UEL
F
LOW
Van’s RV7
Aircraft Flight
Manual
Rev 0.1
S/N 74141
Aircraft Flight
Manual
I-MKLK
GENERAL
I-MKLK AIRCRAFT FLIGHT MANUAL 1.0 11
