Relationship between temperature and Maximum Take-off Weight (MTOW)

In general, as ambient temperature increases, air density decreases and take-off thrust becomes weaker. As a result, the allowable take-off weight is reduced. Therefore, lower temperatures provide greater margin for take-off.

On the other hand, when the ambient temperature exceeds 86°F, and the rate of decrease accelerates sharply at approximately 97°F and above. For aircraft types and routes that normally operate close to MTOW, temperature rise is already a significant operational constraint. Under abnormally high temperature conditions, the impact is likely to extend to a wider range of aircraft types and routes.

1. Payload Reduction

Due to the decrease in allowable take-off weight, the following measures may be required.

・Limiting the number of passengers, even if seats are available.

・Reducing cargo weight, even if there is available space in the cargo hold.

Such measures may be necessary on many routes.

2. Fuel Load Reduction

The following relationship applies.

Allowable Payload = Max T/O weight - Aircraft Operating Weight - T/O Fuel Weight

Even if the maximum take-off weight decreases, the aircraft operating weight does not change. Therefore, it becomes necessary to reduce either payload (passengers + cargo), fuel, or both.

The main methods to reduce fuel load compared to normal operations are as follows.

①Not carrying excess fuel

 ※However, this may be difficult to apply under adverse weather conditions.

②Cancelling direct flights and making an en-route stop for refueling

③Operating under a reclearance flight planning method

All of these methods have significant operational impacts, so payload reduction is typically prioritized.

3. Changes in Operating Time Windows

From a temperature perspective, this may be an effective measure. However, other constraints may arise, such as airport and airspace operating time restrictions.