Evacuated!
The 90 passengers and 4 crew fled the plane.
In 57 seconds:
http://www.flightglobal.com/news/articles/arj21-passes-emergency-evacuation-test-376827/
A380 needed 79.
I think JT442 is right, and the requirement envisages a worse case scenario where all the exits on one side of the fuselage are unusable after an accident.
Yes. And 737 seats are limited by the small service doors on right side.
Then why doesn´t A320 have larger exit limits?
Sorry – slip of keyboard! C130 used to be meant for 130 seats but of course renaming it CS300 did not include stretching it to 300 seats!
But there is real talk of stuffing in 160 seats. What are the allowed ways to exceed 145?
How could CS300 be modified for 300 seats?
Testing water injection
Which tests are done, which are remaining?
Incidentally, does this Challenger come with Gama infant seat/s?
http://www.ainonline.com/aviation-news/aviation-international-news/2012-06-05/gama-launches-infant-safety-seat-bizav-market
Regarding fin and rudder – fin obviously will provide a returning torque against yawing into sideslip.
Is it needed?
Is Taube dangerously yawing?
Taube could turn by banking via aileron application (actually wing warping, but the control effects are equivalent).
What is a rudder for? For “coordinated” turns.
What is the problem with uncoordinated turns by ailerons alone – with rudder either idle or nonexistent?
Not quite sure about the fin either – Etrich Taube certainly has no fin whatsoever.
But does have horizontal stabilizer.
Now, what is the use of the horizontal stabilizer? Concorde does without.
The use is stabilizing the plane against pitching.
The angle of attack must decrease backwards. Accordingly, a tailplane must have smaller angle of attack than main wing, whereas a canard must have bigger angle of attack.
When a plane with tailplane pitches up so far as to stall the main wing, the wing falls – but the tailplane at lower angle of attack is as yet unstalled, keeps the tail up and therefore drops nose, releasing the main wing from stall;
when a plane with canards pitches up, the canard having higher angle of attack stalls first, drops nose and thus prevents main wing from stalling.
So either way the stabilizer prevents sustained stalls – and also changes of pitch short of stall.
Then how does Concorde fly without any horizontal stabilizer at all?
Note how big the wing chord is.
You can move the tailplane closer to main wing and still keep the plane stable – if the tailplane is made bigger on account of the smaller leverage.
Accordingly, a plane with big chord could completely merge the stabilizer into the trailing edge of the main wing.
With some obvious disadvantages.
I’m a bit confused by your actual question, as you already know the answer to the ‘detailed cabin capacity’
So they can’t actually fit in any more passengers…..
Yes. But as I pointed out above, it is the exit limited capacity – 440 seat 747SP and 777-200 may equally be unable to add more seats, but this does not mean those 440 are in equal comfort.
No, it isn´t. Point at specific, detailed cabin capacity data at the upper link.
What the lower link gave (checked before your unhelpful suggestion) is:
Seating capacity 331 (28 first, 303 economy)
However, this kind of standard suggested capacity is notorious for not being comparable. There is simply no guarantee that a comparable suggestion for 777-200 capacity would use exactly the same distribution of cabin space between classes, pitches and widths of business and first classes, galley and toilet area etc….
So. Any real apples to apples comparison?
Hydraulic ready for tests
Hydraulic systems of Aircraft 0 test rig are ready for tests:
http://www.bombardier.com/wps/portal/en/aerospace/media-centre?docID=0901260d8020c129
It seems that A318OEO – defined as any A318 which is not the nonexistent NEO – has a total of 4 orders.
In January-April 2012, net orders +1. 1 cancellation, 2 gross orders – both from private customers.
E195 simply will not approach the performance of A318, with its mere 2200 nm range and needing 2200 m runway for that. As well as being 95 cm narrower than A318, while CSeries is mere 41 cm narrower.
How does the takeoff distance of an abused/lightly loaded A319 compare against 318? I have not heard of 319 having steep approach capability.
I am not sure I quite understand what you’re asking? YOu want us to compare the C series against a plane that Airbus has not even proposed (neither Boeing for the 600MAX)? Both the A318s and the B736s are lemmons. Neither Airbus nor Boeing will go through the trouble of redesigning them. There´s a reason why already several A318s have gone to the scrapper!
No. Against the OEO, which in contrast to NEO, exists and flies.
And Airbus will at least put sharklets on A318 – but not new engines.
How much range boost (or runway cut at constant range) shall A318OEO get from the sharklets? Because CSeries shall be competing against the sharkletted A318OEO, not the existing one.
Furthermore the A318 is restricted to operate from LCY with lower MTOW, indeed BA operates the A318 in all-busines 32-seat configuration on the LCY-JFK route.
No, they don´t and cannot. A318 only gets as far as Shannon, even with the 32 seats.
A318OEO
How does CSeries compare against A318OEO – considering no A318NEO is offered (and no 737-600MAX either)?
Seat count – no frills maximum:
CS100 125
A318 132
Seat count – manufacturer “typical”:
CS100 110
A318 107
MTOW, highest
CS100ER 58,1
A318 68
Range at maximum TOW and “typical” payload
CS100ER 2950 nm
A318 3200 nm
But at lower TOW-s:
CS100 non-ER at 54,9 t 2200 nm
A318 weight variant at 63 t 2200 nm
Takeoff distance at ISA sea level:
CS100ER in 1500 m, and range 2950 nm
A318 in 1800 m
but A318 at 63 t in 1500 m.
How far would Better on a Camel CS100ER fly out of London City?