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特点:8 R }3 n3 N4 s) t5 `' Y, b% \
TIME / SPEED / DISTANCE
6 i9 A0 h5 h! o( FCalculate Speed
3 V2 X+ J2 g/ Z9 O( U, n5 hCalculate Distance
+ w, H0 q! I# C# JCalculate Time Enroute: t) P# p) s! |$ u) E- b8 u! u6 t* X
Calculate Fuel Endurance" D* M1 M/ m* ~3 B
Calculate Fuel Flow
6 D/ @( S$ A2 R# ECalculate Fuel Needed
, S+ N; m2 R0 d6 `2 e: h2 MALTITUDE / AISRPEED" w% x1 R( X8 I
Calculate Calibrated Airspeed
( H2 r0 y e+ v2 ECalculate True Airspeed
7 D7 o& `* |8 \4 fCalculate Density Altitude) Z4 [8 E8 Y0 B u. a
Calculate Mach
: t' f' G0 R$ Z; wWIND
4 i" S# r+ o$ o1 l4 P$ {( rCalculate Wind Direction, Wind Speed
- M( Y" n. [, F6 y! }* [Calculate Ground Speed and Heading
" S/ S% F- r# H! H# l# K( t; p2 tCalculate Wind Correction, Cross Wind Component, Tail Wind Component3 ?' Q3 N5 F/ h- k
Calculate Runway Crosswind
4 y6 D O6 R" m8 |* dCalculate Magnetic Variation
7 g; Y( Z9 ~. L% X& ^$ QWEIGHT & BALANCE3 B2 G7 B. d, I6 f, J4 x
Calculate Center of Gravity( k S) U% g0 U- A- F
Calculate Weight Shift. p8 T. V4 \3 ^* N: y, }# K
Calculate Percentage Mean Cord
+ b* P9 }* A/ p9 p. mCONVERSIONS:
0 `, `4 I5 u1 b; q! H9 h8 h; kVolume: LTR, GAL, IPG; i R+ d7 x1 Q8 t
Weight: KG, LB
2 w( }/ z/ B" E3 w& f% cWeather: °C, °F, MB, HP, IHG, MHG/ i9 \( ~; V, G( K+ Q; s; @! q
Distance: MTR, YRD, KM, FT, IN, NM, SM! T# a& s# ^: w( F
TIMER, STOPWATCH
* z0 v3 X; t9 M; pLocal time / GMT time shown
- H, ~( L$ y/ ?& U2 z1 ICalculate time enroute4 p+ O9 L6 D2 x, }
Calculate departure time9 M! L5 ^( |* D. @/ ~
Calculate arrival time' T4 [2 C- x; U1 m/ {) z
Count up timer( P! C2 b* d/ B I8 |
Count down timer
, n$ h4 {/ e( h% ?0 ]8 d! t/ M' W5 z% aRunway / Descent 7 {6 F6 W3 e1 R5 f. l4 ^3 r
Landing Runway Length Needed 7 H; h1 Q1 }+ \0 G) P
Takeoff Runway Length Needed
' Q1 Q2 F- v) q- Z: qTailwind Landing Runway
$ z6 }( F) @- _* sDescent Profile 5 ?6 `2 D. c" ^: H- I$ G' r1 ]
Descent Rate ( d, q/ |: p- ~* y" V( x
Begin Descent Point
* X- V3 L/ ` b4 j/ f& Q
& U6 C1 V5 t3 T3 `- I百度网盘:+ P& a( @$ x8 l8 e: ~" r
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