UPS MD-11 crash at SDF

And it's not from lack of trying on Boeing's part either. They would want nothing more than to sell the replacement. One day while sitting at my desk in the Airport Compatibility group I get asked to make a drawing of the ramps at MEM and SDF, re-pitching every Group IV wingspan parking spot for Group V, then stick a 777F there and see how many spots they would lose. If I had time they also wanted the smaller hubs like IND and ONT. Apparently it was in support of a sales campaign to replace the MD-11. Then they asked me to lay out the regular ramps but everywhere an MD-11 could park, put a 767-400. I did a double take. A 767-400, that hasn't been in production since 2005, not -300F? My lead engineer confirmed that he did not stutter. Some crazies much higher up were willing to offer a 767-400F, re-engined with GEnX engines, if they could get FDX and UPS to commit to get rid of the MD-11s. Something about having a closer cargo capacity and the -300F being too small. I did the study but it ultimately went nowhere. Either they didn't get interest or figured spending all that design capital for such a niche product wasn't worth it even if they could sell it 1:1. Although I'm sure Southernjets would have ordered 100 if they offered a passenger version, they love a niche, orphaned aircraft that nobody else wants.

Sorry to derail the discussion on this tragic incident. It hit me hard too, and today was my first day back on a trip after it happened, but this anecdote suddenly popped into my mind seeing all the MD-11 replacement talk.
Interesting about the -400. My understanding is any viable alternative ( not a 763) has such a bigger wing span that both shops simply don't own the real estate to make it happen.
 
And it's not from lack of trying on Boeing's part either. They would want nothing more than to sell the replacement. One day while sitting at my desk in the Airport Compatibility group I get asked to make a drawing of the ramps at MEM and SDF, re-pitching every Group IV wingspan parking spot for Group V, then stick a 777F there and see how many spots they would lose. If I had time they also wanted the smaller hubs like IND and ONT. Apparently it was in support of a sales campaign to replace the MD-11. Then they asked me to lay out the regular ramps but everywhere an MD-11 could park, put a 767-400. I did a double take. A 767-400, that hasn't been in production since 2005, not -300F? My lead engineer confirmed that he did not stutter. Some crazies much higher up were willing to offer a 767-400F, re-engined with GEnX engines, if they could get FDX and UPS to commit to get rid of the MD-11s. Something about having a closer cargo capacity and the -300F being too small. I did the study but it ultimately went nowhere. Either they didn't get interest or figured spending all that design capital for such a niche product wasn't worth it even if they could sell it 1:1. Although I'm sure Southernjets would have ordered 100 if they offered a passenger version, they love a niche, orphaned aircraft that nobody else wants.

Sorry to derail the discussion on this tragic incident. It hit me hard too, and today was my first day back on a trip after it happened, but this anecdote suddenly popped into my mind seeing all the MD-11 replacement talk.
Wouldn't the 777 be a nice replacement for the MD-11?
 
I’ve always sort of wished that time to V1 was a thing routinely calculated, as it is probably the most accurate way to measure degraded acceleration.

Sort of a normal thing in seaplanes, as you don't have any runway distance references. The seaplane can also do a "confined area take-off" though - you can always just turn in a circle building airspeed.
 
Dassault uses a calculated minimum G and during takeoff displayed a G meter during takeoff for an acceleration check once T/O thrust was set. At least for the EASy 900.
Some of the fancier later Airbus airplanes are all “ACCELERATION DEGRADED” and you reject then and there.
 
What happened to Kalitta and 777-300 freighters? I was flying with a former Connie pilot and they claimed it would have the same capacity as a 747.
 
Only airplane I’ve ever done this in, but in the T-45, we calculated line speed checks on the takeoff roll. It’s been so long i cant remember any of the details, but it was something like “at the 5 board you need to be at XXX knots to continue” kind of thing. I guess maybe the 1/4 mile trap version of what you are saying
Marine Herks did it on short field takeoffs. We had a spaghetti chart to figure out the time/distance. We also didn’t use V1 and Vr. The charts were built for VMCa and T/O refusal speeds. Under normal circumstances those numbers coincided with each other. Only when you got into extreme weights or density altitude or short runways did they start to separate.
 
Too much wingspan.
At this point it sounds more like an excuse.

From a short term perspective it is valid but I imagine it has been known for a couple decades now that these planes aren't going to have an equivalent any time soon (if ever) and they will have an expiration date. Ramp design and route structure are going to need to change in order to accommodate the loss of the fleet. FedEx finally figured that out and took advantage of their downturn. Not sure if UPS had an exit plan yet or not.
 
Not sure if UPS had an exit plan yet or not.

None is in evidence that I can see. It could be that the plan was to "shrink to (even more) profitability" with 76s replacing MDs as routes "right-sized", but if that was the case, I think you'd have seen more Pratt MDs retired more quickly as 76s were acquired. I think the more likely case is that Atlanta did their normal "step over a dollar to pick up a penny" routine and just assumed that they could "sweat the assets" and duct-tape the remaining GE MDs until they could get a steal-of-a-deal on...who knows, your guess is as good as mine.

In any case, if that was the plan, I think we can see some glaring weaknesses in it now...
 
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