特点：! F* v1 b' w* d- t& t/ x
- TIME / SPEED / DISTANCE; p9 u: m+ E/ {. b
- Calculate Speed
! ]" f7 _, Y8 ~* W7 X; H$ m+ `- Calculate Distance
9 H9 p. g- A7 m$ }( b- Calculate Time Enroute( q) S I1 F6 E( p3 c. k
- Calculate Fuel Endurance8 e- ]3 a: s0 H" {; W" L% Y
- Calculate Fuel Flow5 T# H0 O/ k! R4 @
- Calculate Fuel Needed
$ q4 ~- b V U- ALTITUDE / AISRPEED
8 e( n' Y+ d& t1 Z+ m- Calculate Calibrated Airspeed
4 z. O9 d7 @$ X ^) t1 j- Calculate True Airspeed4 t# q/ F, e3 H
- Calculate Density Altitude
+ ~" y- O9 W8 A5 k- U y- Calculate Mach9 h* r+ y0 V8 l5 M
- WIND$ E; u m: T! ?+ h
- Calculate Wind Direction, Wind Speed# N; r2 B* s# u
- Calculate Ground Speed and Heading
# O! g3 d% h2 J! Q0 h7 G- Calculate Wind Correction, Cross Wind Component, Tail Wind Component
8 Y1 B% E* b, {. B& u- Calculate Runway Crosswind6 X$ e" M$ t- ]7 Q- D4 a
- Calculate Magnetic Variation
; ^# @( m/ p& g. H) ^- WEIGHT & BALANCE
9 E( M7 J: @7 X' M8 ^# G E( z5 Q- Calculate Center of Gravity" v I1 t" M+ o( q1 u1 u
- Calculate Weight Shift2 x& U, Y0 R1 E9 `4 B1 b! R" w1 \, p
- Calculate Percentage Mean Cord
/ l( h( m9 r0 Y8 t" }; F. y- Volume: LTR, GAL, IPG5 g7 o2 e/ _* D9 F' N/ E0 v
- Weight: KG, LB
3 o* J' k6 P3 p& s5 B- Weather: °C, °F, MB, HP, IHG, MHG' ~" v. e) b' g9 y, G
- Distance: MTR, YRD, KM, FT, IN, NM, SM# j/ \3 J. ], M, n. I
- TIMER, STOPWATCH% [# [- `5 }* f$ J, R
- Local time / GMT time shown
+ Z, R8 s. f/ J5 X, A- Calculate time enroute. l# \" {2 x2 ~( ?/ q1 A
- Calculate departure time
4 ?+ i: {& l' `% C& K- Calculate arrival time0 b' U# m6 m, b, v. x S. N
- Count up timer; Y3 w1 q( \) Y2 |) J
- Count down timer- J* A/ p7 B2 |4 I) o8 i
- Runway / Descent & M/ j% i$ f7 `3 G6 l' x9 B0 b' r
- Landing Runway Length Needed ( S# k* Q' J+ L9 J0 L( a3 ` w! F
- Takeoff Runway Length Needed * t' ?0 B! k$ @+ k
- Tailwind Landing Runway # t1 s* n! Q4 ~, p4 F
- Descent Profile / W: h1 P) u. K3 U3 @2 `
- Descent Rate 7 Y1 _' c' Y, y( o
- Begin Descent Point
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