特点：9 [& X7 P2 v1 V3 M
- TIME / SPEED / DISTANCE
- l; H( j( A4 p, W- Calculate Speed2 l" b- i0 A9 Q9 n V
- Calculate Distance( G/ U# h1 v; d( O& F/ M
- Calculate Time Enroute/ h- m6 L+ k) u2 }; w; f( c
- Calculate Fuel Endurance
! ?+ F, C* r; }- Calculate Fuel Flow- f; Y( a! S0 s: R2 }
- Calculate Fuel Needed/ u0 `, F# d! R5 m( N
- ALTITUDE / AISRPEED
9 c( A/ B& c; B/ ~8 X& G0 r- Calculate Calibrated Airspeed
0 K4 c3 A: H% {& a5 n- Calculate True Airspeed
% |" H/ C) w# a' ]! o" ^& P- Calculate Density Altitude
: z" C' x/ P, A x) y- Calculate Mach
2 `+ u- ^' b5 c9 O* Q- x- WIND
7 |) D2 j6 }" g; w- Calculate Wind Direction, Wind Speed
- ?4 R# ?' R$ h7 B8 h1 S6 l% ? {$ _- Calculate Ground Speed and Heading+ Q* d j+ t6 ^* N) `' s, D4 A
- Calculate Wind Correction, Cross Wind Component, Tail Wind Component; [8 f; ~& `/ }* w* J
- Calculate Runway Crosswind6 \% _, ?) f5 W# a
- Calculate Magnetic Variation- W3 W$ K& {1 V7 Z. f; C* ?: I& f
- WEIGHT & BALANCE
# J( {% ^1 Z8 P- Calculate Center of Gravity& j7 J0 {; q# s& w e( D z
- Calculate Weight Shift( \: z& u8 R6 }' g8 n
- Calculate Percentage Mean Cord9 W: B% y3 U1 v
- Volume: LTR, GAL, IPG
: k& y9 j/ Y( A( x$ z! F- Weight: KG, LB* H; B# }' R5 k
- Weather: °C, °F, MB, HP, IHG, MHG4 x9 B$ x4 \% p$ w- b! H* |
- Distance: MTR, YRD, KM, FT, IN, NM, SM/ b$ J/ v! [# r! {
- TIMER, STOPWATCH
1 ?$ H, p, l. y/ W1 \- Local time / GMT time shown
4 M- s$ V6 u w6 e; [2 {- Calculate time enroute, Q7 F! X0 H M5 M, c
- Calculate departure time
# r8 I7 [0 ]8 {. d! o, S+ Z9 @, q p- Calculate arrival time
* }9 x+ m0 x, k/ H: H9 @1 B% j- Count up timer) ?9 I8 u" `2 _) g8 T/ Z
- Count down timer
4 a' `* l& T2 `5 D- Runway / Descent
0 s) C4 H( ?. g/ y$ |$ D- Landing Runway Length Needed
+ Q: u5 [ I* _- Takeoff Runway Length Needed ! `, n6 c0 [$ m) Z7 s, U* N8 h
- Tailwind Landing Runway
; e, F! T! o6 D8 B% F% a- Descent Profile 9 O( J d" O* ]9 a. l3 V
- Descent Rate
/ n) R; b% ]/ U5 ^' a- Begin Descent Point
$ I4 T# P M! d! d% [& S' Z5 y* j: O9 V
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