I have always felt that, since the 777 was reworked 6 years ago, it has been far more powerful during the climb than the real thing. I understand that the developers won’t and can’t update the performance characteristics of an aircraft based on feelings or assumptions, so I have done my best to accumulate some real data. This includes data from a LATAM 777-300ER Flight Crew Operations Manual (link below) and a video from inside the cockpit of a real departure. Hopefully the data provided in this thread is enough to update the performance of the 777 to make it as accurate as possible.
Part 1 :
Data from the FCOM of a LATAM 777-300ER :
https://studylib.net/doc/25610915/fcom-v1v2-b777-latam-brasil-rev24–tpr-41-rev-1-
This table from the FCOM shows us the maximum climb thrust available at given altitudes and temperatures. I have highlighted the figures significant to this test.
The table below shows us the climb rate, speed and pitch we should expect at full climb thrust at given altitudes and temperatures. Once again I have highlighted the relevant data for this test.
Therefore if we combine the two we are able to get the maximum climb rate we should expect at each weight and at each altitude.
The weight was set to 310t.
10,000ft : TAT is 10 degrees C
93% N1 set as per the chart
Expected climb rate : 2700ft/m pitching at 9.5 degrees and stable at 270kts
IF climb rate : 4400ft/m with speed increasing
Difference : 1700ft + speed should have not have been increasing :
To maintain the rate of climb and speed expected I had to lower the nose to 6/6.5 degrees (3 degrees lower) and the N1 to 78% (15% lower than expected.) :
20,000ft : TAT is -5 degrees C
96% N1 set as per the chart
Real expected climb rate : 1900ft/m pitching at 7.5 degrees and stable at 270kts
IF climb rate : 3900ft/m pitching at around 7.5/8 degrees with correct speed
Difference : 2000ft/m
30,000ft : TAT is -15 degrees C
100% N1 set as per the chart
Real expected climb rate : 1200ft/m pitching at 4.5 degrees at 280kts
IF climb rate : 2300ft/m at 4.5 degrees and speed correct
Difference : 1100ft/m
How much higher is IF 777 climb performance than reality :
10,000ft : 63% too high
20,000ft : 105% too high
30,000ft : 92% too high
This shows that during the climb the 777 is between 60%- over 100% too capable and too powerful, depending on the altitude.
Part 2 :
Video of Turkish Airlines 777-300ER departure.
I matched all weight, weather and power information seen in the video to a departure I did in IF to track the difference. You can see these values below with time stamps for when they are visible in the video.
Temperature : 11 degrees on departure (22:00)
Weight : 324.5t (28:00)
Performance vs IF
Real 777 : climbing at 2400ft/m at 10,000ft and at 250kts when pitching at 10 degrees with 93% n1 (37:50)
IF 777 : climbing at 3600ft/m at only 88% n1 at same speed and altitude
Difference : 1200ft/m at 5% less N1
Real 777 : Climbing at 2300ft/m at 15,000ft and at 320kts whilst pitching at ~6/6.5 degrees (39:50)
IF 777 : climbing at 3500ft/m at only 88% n1 (if you match the n1 to the video the IF version can do over 4000ft/m)
Difference : 1200ft/m at 8% less N1
Conclusions :
It’s clear to see that the 777 on IF has much better climb performance than the real counterpart. The pitch when climbing isn’t too dissimilar so it appears to be a mixture of producing too much lift, and the engines being too powerful (or the aircraft not producing enough drag.) I understand that differences of 1000-2000ft/m don’t seem too big, but that represents between 62% and over double what the 777 is actually capable of. The 777 is a great airliner capable of carrying some incredible weights, it would be great if it could feel like the heavy airliner that it is in the sim.
Before anyone accuses me of moaning or hating, that is not the purpose of this topic. The 777 is a great aircraft and is one of the most popular in the simulator, I want to help make it as accurate as possible. I hope this is useful in that cause!









