How to use it
- Type the Altitude to lose in feet and your Ground speed in knots.
- Choose Descent path given as: an angle such as 3 degrees, or a gradient in feet per NM.
- Read Start the descent this far out and Vertical speed needed, then compare them with the 3 to 1 rule under them.
- Open Working to see each step, and the Comparison of descent paths table for 2.5, 3.0 and 3.5 degrees.
How the top of descent is found
A descent path has a fixed gradient: the feet of descent for each nautical mile flown. A three degree path is about 318 ft per NM, which the FAA Instrument Procedures Handbook gives for a STAR as about 318 ft/NM, or about three degrees. The distance to start is the altitude to lose divided by the gradient.
The vertical speed follows from the gradient and the ground speed: at 120 kt a three degree path needs about 637 ft per minute, because 318 feet per NM at 2 NM per minute is 637 feet per minute.
gradient = tan(angle) × 6,076.1 ft per NM
distance = altitude to lose ÷ gradient
time = distance ÷ ground speed × 60
vertical speed = gradient × ground speed ÷ 60
- A descent angle of 3 degrees gives 318.4 ft per NM, and the gradient in feet per NM gives the angle back with atan.
- The check of the IPH for an approximate three degree glidepath is 300 feet to 1 NM: at 10 NM the height is 3,000 ft above the touchdown zone.
The 3 to 1 rule
The IPH gives a rule of thumb for initial IFR descent planning in jets: it takes 3 NM to descend 1,000 feet. Multiply the altitude to lose in thousands of feet by 3 to get the distance to start. The rule is a planning check: it gives a gradient of about 333 ft per NM, a little steeper than the three degree path.
distance (NM) = 3 × altitude to lose (ft) ÷ 1,000
- The IPH example: from FL 310 to an approach gate at 6,000 ft is 25,000 ft of descent, so the descent starts 75 NM out.
- The IPH adds 2 NM for each 10 knots of tailwind and takes 2 NM off for each 10 knots of headwind, for jets at idle thrust and a speed of Mach 0.74 to 0.78.
What this planner does not cover
- Wind along the route, which changes the ground speed and the distance to start.
- The aircraft's own descent profile, its speed limits and the idle-thrust performance in the flight manual.
- The altitude restrictions and the descent gradient that a published arrival sets. Those replace the figures here.
- This page is for training and planning practice, not for real flight.
Worked example: 30,000 ft to lose at 240 kt on a three degree path
A three degree path is 318.4 ft per NM. The distance to start is 30,000 ÷ 318.4 = 94.2 NM, which takes 23.6 minutes at 240 kt.
The vertical speed is 318.4 × 240 ÷ 60 = 1,274 ft per minute. The 3 to 1 rule gives 3 × 30 = 90.0 NM, a little later than the three degree path (closer to the target), because its gradient is steeper.
| Output | Value |
|---|---|
| Start the descent this far out | 94.2 NM |
| Vertical speed needed | 1,274 ft/min |
| 3 to 1 rule: distance to start | 90.0 NM |
Frequently asked questions
What is the top of descent?
It is the point, measured as a distance before the target, where the descent must begin so that the aircraft reaches the target altitude on the chosen path. Starting later means a steeper descent than planned.
Why is a three degree path about 318 feet per mile?
The tangent of 3 degrees is 0.0524, and a nautical mile is about 6,076 ft long, so the path drops about 318 ft for each NM flown. The IPH gives the same figure as about 318 ft/NM for a STAR.
What is the 3 to 1 rule?
The IPH gives it as a rule of thumb for jets: 3 NM to descend 1,000 ft. It is a quick check on the start of the descent, not a published procedure.
How much vertical speed do I need for a three degree path?
The vertical speed is the gradient times the ground speed divided by 60. At 120 kt it is about 637 ft per minute, and at 240 kt about 1,274 ft per minute.
Can I use these distances for a real approach?
No. Use the published descent gradient, the altitudes of the procedure and the aircraft's own profile. The page is for training and planning practice.
Sources
- FAA Instrument Procedures Handbook FAA-H-8083-16B (STARs at about 318 ft/NM, the 3 to 1 formula, the 300 ft to 1 NM check)
- NIST Guide for the SI, Appendix B: Conversion Factors (foot and nautical mile)
Figures and text last checked on Tuesday, November 10, 2026.