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TIME / SPEED / DISTANCE
u- G& Y, ]; HCalculate Speed
3 F, I- s9 L. e: @& KCalculate Distance
! Y/ i0 A( f* U1 ~' D% @Calculate Time Enroute
; Z M; w9 C0 r: Z7 X' I/ R* Z; X8 T3 _Calculate Fuel Endurance
2 L$ ]* H+ U! J' o& HCalculate Fuel Flow. }7 G3 Z9 }; e+ t
Calculate Fuel Needed1 _8 H; J6 F$ j, d1 W
0 @5 E/ y* P$ @7 t6 B: h5 X
ALTITUDE / AISRPEED" y5 U- @. z6 n, C" C- n) H8 Y
Calculate Calibrated Airspeed
4 A5 T, U$ g* Q0 ~0 a6 u2 tCalculate True Airspeed2 t+ _4 \! f3 q1 \
Calculate Density Altitude6 B9 I7 N8 o, B/ {) Q
Calculate Mach5 [, \6 r2 P) i+ y: s6 ?. _
3 D$ j0 J$ {7 x) L tWIND
& [; Y; E1 ~1 _! D4 p, g& Q* RCalculate Wind Direction, Wind Speed
, O9 p: J& \/ T! B4 \/ q' JCalculate Ground Speed and Heading' X) {" o8 h f* K
Calculate Wind Correction, Cross Wind Component, Tail Wind Component
0 L ^: M, L0 s/ @ W0 r- Z; cCalculate Runway Crosswind% {& h/ n7 [! i1 K7 R
Calculate Magnetic Variation- I9 N! D- {8 H4 N% b1 ~7 E3 g
- B5 ~& g8 o3 k, z9 S" ?
WEIGHT & BALANCE- }$ { |2 E; v# ?# r, T% v
Calculate Center of Gravity
1 S* a" `! Y' M P$ O( XCalculate Weight Shift
- Y: e# ]( d, }# i( h7 ?Calculate Percentage Mean Cord
2 ?9 {7 y5 I1 v& ^; G e. o6 k0 n L/ H
CONVERSIONS: W9 C! u: z; a( m4 R- ?7 Y0 a% E
Volume: LTR, GAL, IPG
) D* j% m* n$ e$ B5 v- d1 aWeight: KG, LB
% a2 K$ t/ Q: n* wWeather: °C, °F, MB, HP, IHG, MHG
( E% x5 o, T0 VDistance: MTR, YRD, KM, FT, IN, NM, SM+ N" @' i2 K( R
TIMER, STOPWATCH9 N W& [; J6 q; d' F# V L* g
) `1 e. ?0 i$ t8 j% z8 d! {& J: @) fLocal time / GMT time shown# E1 i, k2 ]+ h1 t6 j
Calculate time enroute
0 z9 s' i8 z) O( q! z2 HCalculate departure time; _+ k8 n9 o; s) f. c
Calculate arrival time5 C; ?/ @0 v; N# d H4 O+ K+ c
Count up timer
! |$ _ B3 q' JCount down timer( q% S O J' u$ U
: }5 b. o$ S! r9 \Runway / Descent
( w1 `5 H* x5 o; c+ r6 T9 t& FLanding Runway Length Needed
" z/ L" J1 v! J7 iTakeoff Runway Length Needed
8 `' x# C1 V0 @# u4 q- A2 d6 uTailwind Landing Runway $ n7 P' ]' r1 H
Descent Profile 6 c, z/ y# }- L
Descent Rate
/ P% ^* H9 s) u% F: b# T( ~1 j: mBegin Descent Point
4 f- R# {" X9 o; W, d
+ k' {6 ?& P5 y9 Q, ~! A, Y: t9 v, K5 W |; f, R, z
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