Rules Of Thumb Flashcards
Level attitude
2-3 deg nose up
1% pitch up vs power to maintain speed
2.5% N1 = 1/4 knob
+250 pph
Gear down or flaps extension per 10 deg, N1 adjust
N1 + 2.5%
Descent gradients
Idle clean high 280/.77 3-3.5 deg 2000fpm
Idle clean 250ft/nm 2.5 deg low (250kt) 1250fpm
Gear down 100-200 ft/nm
Speed brakes 400-500ft/nm
Flaps (each 10) 100ft/nm
Power + 3%N1 100ft/nm
Speed brakes impact on descent gradient
Approx doubles
Thrust for taxi
40-45% 2 knob width
Line inside thigh
Lead with rudder
Beware Swing of wings
Rate of descent ; gs and degrees
5/3 * degrees * GS = ROD
2 = 3.3xGS (x3 +10%)
3 = 5xGS (5.2 précise)
4=6.6xGS (x6 + 10%)
5=8.3xGS
SRT radius
SRT bank
Lead degrees for arc to radial
Radius (nm) = nm/min / pi
AoB = TAS/10 + 7
Lead degrees = TR x 60/DME
TAS from IAS
TAS = IAS + (2% IAS per 1,000ft)
TAS = IAS + FL/2
Max range mach number
99% max range (4 Eng)
AoA
M0.76
M0.777
0.27 +/- 0.05
Glide / best range descent
M0.76 or IAS charted (approx GW/1000)
1:15 or 3.8 degree… 380ft/nm
Descent profile
Clean
Idle ~2000 fpm , 260 ft/nm, 2.5-3 deg
Distance = 3 x Alt
M0.77 -> 31,800
280 KIAS -> 10,000 350 ft/nm 3.5 deg
250 KIAS -> SFC
Tactical Descent A
ROD, Angle HI and LOW
Distance to lose 1,000ft
Speedbrake, Idle: 4,300fpm / 540ft/nm / 5 deg
Dist = 2 x Alt (conservative)
M0.8 -> 30,600
300 KIAS -> 10,000 - 800 ft/nm 8 deg
250 KIAS -> SFC
Turn radius at 30 AoB
TR for SRT
(Dont seem very helpful)
IMN squared x 10 (best)
(IMN x 10) - 2
Most useful:
(nm/min = IMN x 10 )
SRT TR = nm/min / pi
Approx = TAS / 200 (60pi)
300kts
TR chart low alt DFM = 1.6 nm
Formula = 5/pi = 1.57 or 300/200 = 1.5
220klb
Vapp
Vth
Vtd
Vapp = 163kts
Vth = 157kts
Vtd = 147kts