Text book reject at MAN - A330
Moderators: sky's the limit, sepia, Sulako, North Shore
-
iflyforpie
- Top Poster

- Posts: 8132
- Joined: Tue Apr 15, 2008 12:25 pm
- Location: Winterfell...
Re: Text book reject at MAN - A330
I always thought reversers were a no-no on a reject.
-
DeltaHotel
- Rank 3

- Posts: 148
- Joined: Thu Mar 26, 2009 11:53 am
- Location: Montreal CYUL
Re: Text book reject at MAN - A330
Can't get credit for reverse thrust on takeoff performance calculations but the drill (ours anyways) is max reverse, max brake ....
Then if no reverse thrust is available to an engine the FO calls out NO REVERSE ON #1 (2)
Then if no reverse thrust is available to an engine the FO calls out NO REVERSE ON #1 (2)
-
iflyforpie
- Top Poster

- Posts: 8132
- Joined: Tue Apr 15, 2008 12:25 pm
- Location: Winterfell...
Re: Text book reject at MAN - A330
Oh, that's it. I guess assymmetric thrust isn't a huge deal on that aircraft.
Re: Text book reject at MAN - A330
Pie,
As Delta hotel said, "field length" calculations do not take reverse thrust into consideration, they also state "average pilot reaction time" in order to initiate the reject.
I've landed several times with 1 of the reverse systems inop (ours are hydraulically controlled in the E170/190). It doesn't have that much adverse yaw. A little bit of rudder is needed, but not as much as say a V1 cut.
As Delta hotel said, "field length" calculations do not take reverse thrust into consideration, they also state "average pilot reaction time" in order to initiate the reject.
I've landed several times with 1 of the reverse systems inop (ours are hydraulically controlled in the E170/190). It doesn't have that much adverse yaw. A little bit of rudder is needed, but not as much as say a V1 cut.



