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TIME / SPEED / DISTANCE9 O3 A( G) a9 U$ \/ m E( k
Calculate Speed
3 G. a5 O8 \( gCalculate Distance0 B5 J- X4 t9 s* J
Calculate Time Enroute
6 R' r% m _1 R) Y1 @8 ~Calculate Fuel Endurance# i) q( N0 D$ I/ L
Calculate Fuel Flow5 @$ R, k8 s$ K, U2 _- D
Calculate Fuel Needed6 O+ v. @' r' A9 j# X5 m0 P
/ L. t6 o, i& y3 n, [ALTITUDE / AISRPEED
% H2 [6 n9 s$ X% QCalculate Calibrated Airspeed
& U# l0 j$ k( D% j) {) \0 iCalculate True Airspeed* X5 \0 V/ E3 n0 H1 J% X3 n! Y( G* g
Calculate Density Altitude
0 ?# [; \. s& Y& p' f4 }Calculate Mach: |( c& j3 h7 B& I& A
! H ]. t2 y( S2 \! w
WIND, w7 I7 n7 e5 N7 V* J# d
Calculate Wind Direction, Wind Speed
" a& {: A, T1 D" q5 H8 V6 T. H7 _ GCalculate Ground Speed and Heading: s1 v5 G. r8 r" y, x: G
Calculate Wind Correction, Cross Wind Component, Tail Wind Component9 n, B4 f3 q* j+ G; Z
Calculate Runway Crosswind" l6 j) u& o$ g, R/ W& b
Calculate Magnetic Variation& m( n$ a3 h. f, m5 [4 i! e
7 [$ K3 a- I9 ^) \
WEIGHT & BALANCE* U7 V0 e+ ^+ m: A, N+ G
Calculate Center of Gravity) p5 X& H# ~( g
Calculate Weight Shift
+ r8 w3 I3 E; aCalculate Percentage Mean Cord
0 y n" y. z; d9 J' l
) ~7 l5 U$ R, U. ~: PCONVERSIONS:, i- I$ w% i0 a& _8 s
Volume: LTR, GAL, IPG
1 x4 {$ r( w3 Q( E# u- {Weight: KG, LB$ \: u! ~! E- w0 c8 @* S- R) ^$ o
Weather: °C, °F, MB, HP, IHG, MHG
5 H5 l& k4 a: i8 t/ T3 [8 v `/ T1 y5 h" gDistance: MTR, YRD, KM, FT, IN, NM, SM
& J2 T5 n/ l; A6 iTIMER, STOPWATCH a) e) \# i3 a8 q/ Q4 s z( _1 A/ C
' L8 \' @( b8 SLocal time / GMT time shown4 [% y# @! z& Q' p
Calculate time enroute
, a# `& z4 Q+ W" ECalculate departure time" o1 o+ x2 L# P. V* V5 Y$ T
Calculate arrival time6 I$ [, }$ y$ y4 H3 P. F, q g
Count up timer
; O# X$ O! W9 BCount down timer
5 S0 w0 j& r( d/ {) l' K4 g
7 N) M: n& i: `) _& KRunway / Descent
. g7 S* _, |$ k, g2 a' m9 XLanding Runway Length Needed ) u3 q4 c, u% A5 g, h6 g
Takeoff Runway Length Needed 7 B8 u9 u! Q! X9 Y/ E0 A5 g- N
Tailwind Landing Runway
7 g. z& m& H3 G3 d& GDescent Profile
# P8 M0 k1 k/ f' ]( xDescent Rate
. }! [; q% p& q9 {4 {Begin Descent Point9 B: k! U: n$ q8 e, F
7 v+ a1 I0 F P: l: f! p
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