DELTA MATH UPDATED QUESTIONS WITH ANSWERS
VDP for distance - CORRECT ANSWER✅✅✅1. Divide HAT by 300
2. Subtract that amount from end of runway
VDP for descent point in time - CORRECT ANSWER✅✅✅1. Take 10% of HAT
2. Subtract that from FAF-MAP time
Descent rate on an ILS - CORRECT ANSWER✅✅✅Ground speed / 2, add a zero
Lead point - CORRECT ANSWER✅✅✅1. Lead point is 60/DME x Turn Radius
2. Turn radius = (TAS/60)-2
3. So 60/DME x (TAS/60)-2 = degrees to add to desired radial
Tstorm radar tops - CORRECT ANSWER✅✅✅Your altitude + distance x degrees
IAS in knots to TAS - CORRECT ANSWER✅✅✅KIAS + altitude/200
Mach to TAS - CORRECT ANSWER✅✅✅Multiply first # of Mach by 6 = XXX knots TAS
KTAS increase with temp change - CORRECT ANSWER✅✅✅1.2 kts/1 degree C
Bank angle: standard rate turn - CORRECT ANSWER✅✅✅(TAS/10) x 1.5
Drift correction - CORRECT ANSWER✅✅✅Xwind/(nm/min)
ex: 60Kts, 240 TAS = 60/4= 15 deg
VDP for distance - CORRECT ANSWER✅✅✅1. Divide HAT by 300
2. Subtract that amount from end of runway
VDP for descent point in time - CORRECT ANSWER✅✅✅1. Take 10% of HAT
2. Subtract that from FAF-MAP time
Descent rate on an ILS - CORRECT ANSWER✅✅✅Ground speed / 2, add a zero
Lead point - CORRECT ANSWER✅✅✅1. Lead point is 60/DME x Turn Radius
2. Turn radius = (TAS/60)-2
3. So 60/DME x (TAS/60)-2 = degrees to add to desired radial
Tstorm radar tops - CORRECT ANSWER✅✅✅Your altitude + distance x degrees
IAS in knots to TAS - CORRECT ANSWER✅✅✅KIAS + altitude/200
Mach to TAS - CORRECT ANSWER✅✅✅Multiply first # of Mach by 6 = XXX knots TAS
KTAS increase with temp change - CORRECT ANSWER✅✅✅1.2 kts/1 degree C
Bank angle: standard rate turn - CORRECT ANSWER✅✅✅(TAS/10) x 1.5
Drift correction - CORRECT ANSWER✅✅✅Xwind/(nm/min)
ex: 60Kts, 240 TAS = 60/4= 15 deg
