Hi guys,
I'm finding it a great struggle to taxi with the A321. As far as I am aware, like the A319 and A320, after a short burst of power to get it rolling, the A321 should taxi comfortably under idle power.
With the PA model, I find that I need to increase the throttles slightly and keep them there in order to keep the aircraft moving. If I do return the throttles to idle, the aircraft will slowly come to a stop. This is the case, even with a reasonably lightly loaded aircraft (80-90% load factor, 30% fuel load and extremely light cargo load).
Is this desired, or is there an error?
Thanks for your help.
Jamie
Taxiing the A321
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Please read the pinned topics and search the forum before posting to make sure your question's not already been answered.
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Billster8724
- Posts: 74
- Joined: 09 Dec 2009, 22:40
Re: Taxiing the A321
The A321 is slightly underpowered, as it is in real life. Same powerplant options as the A319/A320, same wing, except the aircraft is significantly longer. The handling characteristics you're feeling are very realistic. I cheated and bumped up my power a little bit in the .cfg (nothing rediculous), but its realistic as you have it right now.
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scottecLEMG
- Posts: 8
- Joined: 26 Jul 2011, 07:31
Re: Taxiing the A321
It is true that the A321 is longer but although it uses the same powerplant series it does has a more powerful thrust version of both the CMF56 and IAE V2500.
Static Thurst for A320 aircraft
CMF56 - ranges from 22,000lbs to 27,000lbs
IAE V2500 - is 24,800lbs
Static Thrust for A321 aircraft
CFM 56 - ranges from 30,000lbs to 32,000lbs
IAE V2500 - ranges from 29,900lbs to 31,600lbs
Therefore the aircraft should not be underpowered.
The above details are taken from the Type Certificate Data Sheet EASA-TCDS-A.064
Ken
Static Thurst for A320 aircraft
CMF56 - ranges from 22,000lbs to 27,000lbs
IAE V2500 - is 24,800lbs
Static Thrust for A321 aircraft
CFM 56 - ranges from 30,000lbs to 32,000lbs
IAE V2500 - ranges from 29,900lbs to 31,600lbs
Therefore the aircraft should not be underpowered.
The above details are taken from the Type Certificate Data Sheet EASA-TCDS-A.064
Ken