Nyttige tommelfingerregler - Skybrary

Definition

Used correctly, rules of thumb (sometimes know as “heuristics") can assist significantly in pilot decision making and understanding. A rule of thumb is a principle with broad application that is not intended to be strictly accurate or reliable for every situation. It is an easily learned and easily applied procedure for approximately calculating some value. It is particularly useful as a means of cross-checking or confirming the validity of information being displayed by aircraft navigation systems and flight management systems.

1 in 60 Rule

A 1 degree offset angle at 60 nm equates to 1 nm of displacement.

Distance off track = (number of degrees off course x distance to station)/60

Speed/Distance/Time

Flying speeds that simplify mental arithmetic can help you in many ways, such as keeping retaining situational awareness during radar vectoring.

120Kts = 2nms/min

180Kts = 3nms/min

240Kts = 4nms/min

300Kts = 5nms/min

The 1 in 60 rule combined with Speed/Distance/Time assumptions is the basis of many other ‘rules of thumb’ that can be useful in pilot navigation (or to check that an FMS-calculated track makes sence. For example:

At 120 kt groundspeed, the aircraft travels 60nm in 30 minutes. A 10 kt wind blows the aircraft 5 nm in 30 minutes At 120 kt groundspeed, a 10 kt crosswind will cause 5 degrees of drift

Maximum drift angle (Max Drift) = Windspeed divided by Groundspeed in miles per minute

Crosswind Component

Useful for evaluating runway crosswind from reported wind, the crosswind is a function of the SINE of the angle between the runway and the wind direction. Therefore, crosswind can be estimated as follows:

Angle between wind and runway (degrees)	Crosswind component (% of wind strength)	Sine of angle between wind direction and runway in degrees
0	0	0
15	25	0.26
30	50	0.5
60 or more	100	0.87

A similar process can be used to estimate wind effect on groundspeed

Combining Max drift and Crosswind component:

Flying at 420 kt groundspeed (7 nm/min) in the vicinity of a 60 kt wind (approx. 8½ degrees max drift) headwind from 30 degrees off track, the expected drift angle is just over 4 degrees.

Flying at 420 kt airspeed in the vicinity of a 60 kt wind from 30 degrees off track, groundspeed will be approximately 360 kt (~6 nm/min) so max drift is 10 degrees and the expected drift angle will be 5 degrees.

Slant Range

Overhead a DME the indicated range will be equal to the altitude of the aircraft. One NM is approximately 6,000’ (actually 6,076’)

Slant Range Overhead DME = Altitude in feet/6000

Descent Range

Different types will have different performance so pilots must establish and check any ‘rule’ for their own aircraft.

30 per 10 plus 10…

For many older jet transports, a normal descent from cruise altitude descent required about 30 nm for each 10,000ft of height loss and a further 10 nm to slow down. Therefore:

30,000’ cruise = (3 x 30) + 10 = 100 nm descent

35,000’ cruise = (3.5 x 30) + 10 = 115 nm descent

Although not strictly accurate, it provided a good first guesstimate.

Modern, more efficient aircraft, will need greater distances but similar rules of thumb can often be defined from a review of performance figures and line experience. You may find that (e.g.) “40 per 10 plus 15” works better for your type. The important point here is that well practiced rules of thumb may need to be revised dramatically when changing from one type to another.

Similarly, to confirm that a descent profile is going well:

30 out at 10 and 250….

Thirty miles from the airport at 10,000' and 250 knots.

If at 30 nm from destination, the aircraft is still above either 10,000’ or 250 kt (or both!) getting down and reducing speed to achieve a stabilized approach will be a real challenge in many jet transports.

Diagram showing Descent range rules of thumb

Final Approach

3 degree glideslope = 300’/nm to touchdown

Again from the 1 in 60 rule, 3 degrees at 60 nm ~ 3 nm ~ 18,000’ so 3 degrees at 6 nm ~ 1,800’ and 3 degrees at 1 nm ~ 300’)

This is not exact – and approach plates will show precise figures for any approach - but it provides a simple way to spot any gross errors.

Rate of Descent on Final Approach

For a 3 degree glideslope, required rate of descent in feet per minute is approximately equal to ground speed in knots multiplied by 5.

From the above, at 120 knots GS, the rate of descent to maintain a 3 degree glideslope is approximately 600 fpm

Payload

It is always useful to check mentally that loading figures make sense. While it may not be true for every situation (so pilots must review the circumstance of their own operation before using this), many pilots find the following rule of thumb effective:

100 pax equates to 9 tons.

If you have any other rules of thumb that you find useful then please send the information to the Editor