The CFM-56-5C was tested to 36,000+ lbs and I'm sure it would not have taken much to certify it at that rating. Obviously Airbus didn't feel that they needed to.
Jump to postDL loves their 717's and would buy more if they could. I do not see those exiting the fleet any time soon The C Series will be a great replacement for them over time. Seems like too many people think the C Series will descend on Atlanta in one great wave. The orders will be structured to arrive ove...
Jump to postWell, considering the GE90-90B (90k thrust variant) weighs 17,400 lbs and the GE CF6-80E1 weighs 11,200 lbs, I can see why Airbus would be rolling their eyes. Only a serious stretch of the 333 could make that weight penalty worth the fuel burn savings. Taller landing gear may also be required...
Jump to postBoeing is correct, Canada should be buying multi-engined fighters........like the Dassault Rafale and Eurofighter Typhoon. :stirthepot: :box: Typhoon would make a lot more sense than the F-35 for Canada given the core mission of Canadian/North American air defense. Harper was a hardcore neocon so o...
Jump to postWhere is this "767-400 has taller landing gear to fit the PW4000 94-inch fan" stuff coming from? The taller gear has absolutely NOTHING to do with the engines. The 767-300 uses exactly the same size engines (93 and 94-inch fans) as the 767-400. The only difference is the thrust rating, and...
Jump to postThe only course that really makes sense for Boeing is to address MOM with a version of their 737 replacement (NSA). This shouldn't be too hard as the optimum size for both the 737 and 320 keeps moving up. A318, A319, 737-600/7 are basically non-factors.. NSA will probably start with 738/A320 size an...
Jump to postI'd like to see a 767-200A NEO (GEnx-2b). That would have real promise for the MOM role. Forget the -300. Too big (and too ugly in my opinion)
Jump to postThe 777-8 is clearly too large for this mission, which calls for 300 seats, not 365. On the other hand a 772 length 777X would be perfect for this mission and should be able to meet all Qantas requirements without MTOW increases or a central bogey. It would also have superior CASM because its not ca...
Jump to postAre these two aviators still in junior high? If they are going to go through the effort, why not draw something that's actually funny for people older than 15.
Jump to postOr just use the An-225 for 560,000 lbs of bombs over a longer range (still short compared to typical bombers).
Stratolaunch would be perfect however for one huge 500,000 lb thermobaric bomb.
Given that the F135 has 28,000 lbs dry and will certainly get a larger fan for a better subsonic efficiency, I can see the derivative for the B-21 having 36-40,000 lbs thrust.
Jump to postI still think the best aircraft for this role would be a 772 fuselage length for the 777X, call it the 777-7X. The 772 can already seat 300 in 3 classes. With the wider interior it would have even more space. The 777-8 is too big for this niche. A 777-7X would offer superior performance to either t...
Jump to postI still think the best aircraft for this role would be a 772 fuselage length for the 777X, call it the 777-7X. The 772 can already seat 300 in 3 classes. With the wider interior it would have even more space. The 777-8 is too big for this niche. A 777-7X would offer superior performance to either th...
Jump to postBased on 767-200 non-ER max TO weight and engine thrust, I'd think a 150 ton MOM would need at least 50,000 lb engines unless the wing area is substantially larger than the 767's 3050 sq ft (which of course would add more weight)
Jump to postDominion301 wrote:I can't see DL ordering a Boeing narrowbody for a while after the CSeries debacle.
Well, if Qantas are looking for something to compete against the 321LR, Boeing's 260+ seat twin aisle NMA isn't going to be much help.
Jump to postI'm all for an A358 ULR (especially if it gets all the A3510 mods), but I had thought that the original A359 ULR proposal with the A3510 wings, etc had the range/payload required for this mission? Boeing could theoretically do a 777X at 772 length. With the wider interior that could do 300 pax at 10...
Jump to postCompared to the CF6-80 next to it, the GE9X cowl is extremely thick (not sure why)- lots of drag
Jump to postThey won't stop producing the 747-8F until there is a real one-for one replacement, which the proposed 777-8F is not. I'll bet even money that if they threaten to close the line before then, there will be a flurry of orders to "get one while they can", ...resulting in continued production.
Jump to postSupposedly the new NK-32-02 engines will add 1000 km range and more significantly, enable cruise at over 60,000 ft as opposed to ~50,000 ft for the current aircraft. That would require a significant increase in thrust (probably to 65,000 lbs or more), but so far there has been no information forthco...
Jump to postT-900 - 6246kg GP7200 - 6718kg (but will be out of production in 2018) T-1000 - 5936kg - 6114kg (Not sure if that includes the -TEN) T-XWB - 7549kg (XWB-97) T-7000 - 7750kg Trent 1000 - https://www.easa.europa.eu/system/files/dfu/TCDS%20E%20036%20issue%2008.pdf Trent XWB - https://www.easa.europa.e...
Jump to postI hated the seraph fonts introduced in the late 80's and early 90's right from the start. 60's and 70's fonts were the best.
Jump to postRWA380 wrote:The more I think of it, this was likely something coming out of testing in Nevada,
It was bad enough when I found out they weren't going to build an A318NEO, now the A319NEO is on the rocks. We are moving towards a world where not only are all aircraft going to be twins, but they are all going to be "stretch" versions as well. Bullocks.
Jump to postI doubt it was a NT-43A if it was outrunning other 737's, especially with all that added drag from the sensor blisters. Also, if that 750 knots figure is true, there would have been a sonic boom and someone would have heard it, even in that remote area. One item missing as well is was the unidentifi...
Jump to postDisappointing to not see any A319NEO orders, especially for F7. Sadly, it looks like the A319NEO has become what the A318 was in terms of orders.
Jump to postI can understand why Clark would not be interested in the A380-Plus as compared to an NEO, but compared to the CEO? I don't get it. 4% better than CEO is still pretty significant.
Jump to postNot sure if this has been posted already, but from ATWonline: Emirates rejects A380plus concept as order negotiations continue http://atwonline.com/airframes/emirates-rejects-a380plus-concept-order-negotiations-continue Emirates Airline is rejecting the proposed Airbus A380plus concept in spite of i...
Jump to postThen the new engine disturbs wing flow, so new corrections will be done around the engine. Wasn't the MAX engine integration declared perfect and Boeing excelling over itself here? :-) "perfect" meaning the best they could do without designing taller landing gear. They basically just cram...
Jump to postI'm hoping for either 3-3 or a 2-2-2 that cannot be expanded to 2-3-2. MOM sweet spot is 762 (or 752.5) per the airlines. Boeing would be better off just NEO-ing the 762 (NOT the 763) and covering the A321/752 replacement with single aisle NSA. No way it will be 2-2-2. That configuration just makes...
Jump to postI'm hoping for either 3-3 or a 2-2-2 that cannot be expanded to 2-3-2.
MOM sweet spot is 762 (or 752.5) per the airlines. Boeing would be better off just NEO-ing the 762 (NOT the 763) and covering the A321/752 replacement with single aisle NSA.
Saving the 748 (beyond the -8F) would in my opinion require a GEnx-2b using GE9X technology and giving 5% better sfc, a reduction of OEW to original promised spec (466,000lb) or lower, and full implementation of Project Ozark improvements (higher MTOW, improved wing-body fairing, improved wingtips. ...
Jump to postThe disappointment that is the 747-8 program is a direct result of two factors: 1.The failure of GE to provide an engine that met promised specifications (and still doesn't, by the way) The -2b67 was like 4-5% over spec at service entry. 2. Boeing's stealing of resources from the 748 program to deal...
Jump to postTrent1000, GenX significantly overstepped targets at their EIS ( even more when you look at the initially projected EIS date.) Trent1000 seems to traverse initial spec with the TEN, 13years after .. , I haven't followed GenX. The GEnx is still slightly above promised spec I believe (like 1/2%). The...
Jump to postThat's strange, I thought earlier they were offering the BR715 which makes much more sense both in terms of fuel efficiency and thrust. The BR725 would actually offer less thrust than the TF-33 and higher fuel consumption than the BR715. The BR715's thrust margin would help with hot and hi too witho...
Jump to postI've seen the ~1mm holes on the inside pax window pane too and always assumed they were there to prevent condensation buildup...
Jump to postKeesje addressed this question a long while back with the proposed Ecoliner double decker twin with thrusting APU. Optimized fuselage shape and engine layout. Google it or find the old posts here on A-net...
Jump to postA very basic NEO of the 767-200A with slightly de-rated GEnx-2b's, APB split scimitars and nothing else would cut fuel burn by 12-15% The -200A is right in the NEO capacity sweetspot and with the GEnx/winglets would easily have 5000 nmi range without the added structural weight of the 200ER The 200E...
Jump to postSo, because the 204 has two engines under the wings and a similar capacity it's a copy? You guys have no idea how hard it is to actually copy something one for one. At best, the Russians said "hey, it seems like this configuration is economical, let's make an airplane similar to that as well&q...
Jump to postIf the're talking MOM stopgap, then they should be producing the 767-200, not the 300ER and not the 200ER. 200ER and 300ER have too much range, carry extra weight and the 300ER is too big for MOM size according to airline desires. Boeing is the one who for some reason wants MOM to be larger than wh...
Jump to postIf the're talking MOM stopgap, then they should be producing the 767-200, not the 300ER and not the 200ER. 200ER and 300ER have too much range, carry extra weight and the 300ER is too big for MOM size according to airline desires. Boeing is the one who for some reason wants MOM to be larger than wha...
Jump to postOpen rotors are fascinating. Just remember the slower cruise speed than a GTF. They're benefit is they give you a higher bypass ration without the weight of a nacelle. But without a nacelle, blade tip mach number is limited which means cruise speed is limited more than with a nacelle. Business jets...
Jump to postActually, they were 14,000 dollar toilet seats. And everyone forgets that on 9/10/2001 Rumsfeld said there was 2.3 trillion dollars unaccounted for in the department of defense. It was conveniently "forgotten" the next day. DOD and US military contractors make the mafia look like second-ra...
Jump to postI have a very hard time believing that the A350's windows are smaller than the standard 23 year old 777 windows.
Jump to postThat was from Flight Global a few years ago when John Ostrower was still there. The Split scimitar is good for 2-3% over the normal APB blended winglet while the Boeing ATW was initially pegged at 1% and then was upgraded to 1.5% better than the APB blended winglet. Here is the article. https://www....
Jump to postThe Split Scimitar is superior to Boeing's design by .5%. Never understood why Boeing decided to make its own design in the first place. Plus its fugly compared to the split scimitar, mainly because the bottom element is splayed out so far. Ruins the looks of the MAX in my opinion.
Jump to postGood! ...Forget the short-sighted "Clean Sky" leadership. Safran knows this is the future. Damn the torpedoes and full speed ahead! (hopefully)
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