Balance tab vs Anti-balance tab
Balance tab is NOT Trim tab! balance tab’s movement is linked to the primary surface’s position, while a trim tab stays in a fixed position until adjusted. Balance tabs are rigged to operate automatically with application of the elevator and assist the pilot in reducing the control force necessary to move the elevator. They work in much the
What’s Speed Instability, region of reverse command, backside of the power curve ?
Introduction – why pilot should know these phases? What Is “Speed Instability”? Speed Instability, region of reverse command, backside of the power curve are just different terms to describe same topic! reverse command is encountered at low airspeed. It is also known as the back of the power curve, and is normally situated below the
Spiral Dive v.s Spin v.s Dutch Roll
好耐無溫書…係時候準備! 今日朋友講起呢兩個TOPIC…就睇下啦~ XDDD Spin Stall -> Spin (autorotation) BOTH wing stall, but one wing stall more -> i.e uncoordinated stall / imbalanced stall 3 Phases (2 mins 36 sec) Incipient Spin Fully developed Recovery Feature slow airspeed at fully developed stage + high AOA Factors affecting spin recovery Weight & Balance -> CG aft, more
What’s coffin corner?
Reference:https://airwaysmag.com/coffin-corner-aviation/ , https://www.boldmethod.com/learn-to-fly/aerodynamics/coffin-corner-where-vne-and-mmo-meet/ Ans: Coffin Corner can be explained by using below illustration. It is talking about when when the aircraft fly to an altitude where the aircraft reduces the speed, it will stall while the aircraft increase its speed, it will over the Mmo. Therefore, the margin for error is low.The coffin corner is
What’s CAVOK , What’s NCD, NSC
Reference source: https://skybrary.aero/articles/weather-observations-aerodromes CAVOK The visibility, RVR, weather and cloud groups are replaced by CAVOK (Cloud And Visibility OK) when the following conditions exist simultaneously: If there is no cloud below 5000 ft or below the highest minimum sector altitude (whichever is greater) and there is no towering cumulus or cumulonimbus, ‘NSC’ is reported. Note:
Service ceiling v.s Absolute altitude
Service ceiling 指飛機無再多MAP for climb; Critical altitude 指turbocharged engine 發揮最大壓縮空氣能力既高度 As a normally aspirated aircraft climbs, it eventually reaches an altitude where the MAP is insufficient for a normal climb. This altitude limit is known as the aircraft’s service ceiling Critical altitude is the maximum altitude at which a turbocharged engine can produce its rated
Six pack
Reference: https://www.airpowerinc.com/six-pack-aircraft-instruments Six pack: is a terms referring the six basic instruments that a pilot must know! From the top, on the most left is the Airspeed indicator (ASI), the Attitude indicator (AI) is in the middle, and the Altimeter (Alt) on the right At the bottom, on the most left is the Turn coordinator
What’s Wing Camber, What’s Chord line?
What’s Wing Camber? Ans: curvature of the aerofoil (wing) maximum distance between the mean camber line and the chord line Mean camber line : imaginary line equidistance between the upper and lower surface of the wing, joining from the leading edge to trailing edge. What’s Chord line? Ans: imaginary line joining from the
點樣知機場QNH? 點樣知Local Pressure? How to know the QNH? How to know local pressure?
今日上完堂再唸左成個下午先好D 通左D, 所以一定要記底佢…小喇叭, 呢個Concept 好難明! Anyway, mark 低佢先! Reading (in feet) = (Set QNH – Actual pressure level) * 30 For example, if the aerodrome is 30 feet Elevation and 當時QNH是1013, then Reading (in feet) = (Set QNH – Actual pressure level) * 30 30 = ( 1013 – Actual pressure level )* 30 30/30
Why “Fly to low, watch below ; High to cold, watch below” ?
Ref Ace the technical pilot interview 2/E Ans: Always remember : aneroid barometer is working based on MSL pressure (i.e pressure height) ! 1. FL formula Flight Level (Pressure Height) in feet = Height @ QNH + (1013 – QNH) * 30 Example: Now say 300 feet @ 1025 PH = 300
Maximum Glide Range?
Ans : two manoeuvre factors – 1. optimal angle of attack 2. minimum drag speed 當上面兩樣野做到又吾計wind , 理論上隻機就會飛 @ max L/D ratio 記著: 重量同max glide range 無關! 取決上面說的兩個操作factors – 大機同細機glide range 一樣 !
Pilot math
計數係惡夢 但方法還是有 🤭 Ref skybrary: https://skybrary.aero/articles/rules-thumb 時間 Time 6 mins 0.1 hour 3 mins 0.05 hour 方位 Reciprocal Heading = HDG +200 – 20 or = HDG – 200 + 20 大過200就- 先 ; 細過200就+ 先 e.g 090 : 90 + 200 – 20 = 270 270 : 270 – 200 + 20
Ground effect 對不同flight status 的影響? (就Ground Effect 有咩係機師要知, 有咩要做?)
Ref Ch5 Ans: 機師要記著 – T/O phase not attempt to force the acft T/O with not sufficient takeoff speed (due IAS 假象!) never retract the landing gear or flaps prior to establish +ve rate of climb never retract the landing gear or flaps prior reaching MSA (minimum safe altitude) Landing phase reduce power to
Ground effect 有咩影響? Significance of ground effect?
Ref Ch5 Ans: Upwash↓ , downwash ↓ –> Wingtip vortices ↓ –> induced drag ↓ –> AOA need to be reduced for same CL Local pressure on static source [position (installation) error] –> airborne IAS reduce 假象 Induced Drag 成因? What’s ground effect?
What’s ground effect?
Ref Ch5 Ans: air cushion phenomenon The reason of ground effect is that the air that is trapped between the wing and the landing surface, as if there were an air cushion. When the plane is very close to the surface (say just before touchdown), it would suddenly feel like the plane did not want
Strategy to avoid wake turbulence?
Ref Ch5 Ans: 飛緊 : avoid similar flight path with 1000 ft vertical separation T/O : rotate before the point at which preceding acft rotated LAND : approach above preceding acft’s flight path LAND : touch down after the point where other’s wheel contact If doubt, 用 3 mins margin time (rule of thumb) For