|
|
TIME / SPEED / DISTANCE
) e0 `) T% A# L7 H7 Z/ s4 aCalculate Speed# }1 \0 ]+ U3 K- @1 d$ E. {% A& |
Calculate Distance2 m4 ] @2 \, h; i0 q3 J
Calculate Time Enroute. v) H# I; q" ?# |: D
Calculate Fuel Endurance! m/ |: J7 X* {6 O4 _" x
Calculate Fuel Flow( Z. d# K( `) ~/ k
Calculate Fuel Needed
& i2 X( k1 |' ^3 q0 t/ B* n
' s" a8 N. L( r- QALTITUDE / AISRPEED8 S7 U+ z/ F8 O& s& K
Calculate Calibrated Airspeed
( u+ j! g7 \0 V6 c- i" l4 LCalculate True Airspeed
" H4 E2 D- r* K4 D$ CCalculate Density Altitude
% b. [* S t, ?4 p; YCalculate Mach9 S @' p$ x. f) X) V+ F
9 }% q3 w- [0 A) i# L9 WWIND
' S: X! n3 {$ J9 U Z4 {Calculate Wind Direction, Wind Speed
1 O+ U6 O* \6 h+ W8 qCalculate Ground Speed and Heading" D. d. l6 y" |# z+ q( s+ N
Calculate Wind Correction, Cross Wind Component, Tail Wind Component* ?- y$ s# R X5 a3 A- a- H
Calculate Runway Crosswind
2 Q; _# y& E% L) v$ ?* lCalculate Magnetic Variation7 b( U! \& L4 D$ W4 m
; h+ H" }( w) A3 |) x$ v/ ?
WEIGHT & BALANCE3 J0 V0 v$ C# d/ G+ R/ o# m9 Z d
Calculate Center of Gravity
\0 M# a+ K* V! j7 MCalculate Weight Shift
6 n) f/ k7 `- HCalculate Percentage Mean Cord% v ~8 V4 A$ a& {/ X- o
+ |2 }7 ~ J9 i: C5 nCONVERSIONS:8 R) q% _# |' c _8 V/ }
Volume: LTR, GAL, IPG
. P8 _ G. F K Q- T+ e! t* wWeight: KG, LB% v! R+ N( b: K% i, S" D
Weather: °C, °F, MB, HP, IHG, MHG4 q9 n& ^( E4 |" I; P# V2 J5 ]
Distance: MTR, YRD, KM, FT, IN, NM, SM
( u# o* C: \( r* A( E$ gTIMER, STOPWATCH8 z! N/ B5 Q# a* I0 h& ~
& d3 L' O/ l6 C
Local time / GMT time shown
' y8 _. V$ o8 U! F- r- u. [4 PCalculate time enroute
9 f: ^0 {1 F, P' ACalculate departure time
0 i4 B" }! Y( ^0 eCalculate arrival time# r+ u9 {8 c T6 [' u5 ?, J" f
Count up timer+ K( l, M. q/ t: c/ c
Count down timer
3 T' w% ^+ e; m6 |, U5 q# [* |, i( L- `) q2 A) r
Runway / Descent 0 P7 n& a' @# N: a& K4 ?2 \0 f
Landing Runway Length Needed
) o z) L( ^! E5 xTakeoff Runway Length Needed
. B! |( S, a' B5 mTailwind Landing Runway $ Y# [% Y5 o x& P" [) S
Descent Profile
( C; v0 D: Q& Q5 D! t! v% s( ]Descent Rate
0 U" Q' j: V: dBegin Descent Point
. E7 n& Q, p$ m% H* l
& o4 ?: h2 V$ w8 W8 J3 V& `, F m0 v! c- K- R
|
|