Search
Notices

717 phase out?

Thread Tools
 
Search this Thread
 
Old 02-01-2021, 04:26 PM
  #101  
Gets Weekends Off
 
Trip7's Avatar
 
Joined APC: Dec 2007
Posts: 5,414
Default

Originally Posted by tennisguru View Post
That tweet also shows that JetBlue dumped 6 A321's. I seriously doubt that is meant to show permanent retirements, but instead probably a temporary operational reduction due the normal post Christmas lull. The AE that closed today is supposed to add 70 717Bs, so it's not like the category is shrinking.
They are adding FOs to backstop the bleeding that will occur from that position when the May AE drops. Similar to how nearly all NYC narrow bodies had a significant amount of positions added

Sent from my SM-N986U using Tapatalk
Trip7 is offline  
Old 02-01-2021, 04:49 PM
  #102  
Gets Weekends Off
 
Joined APC: Mar 2020
Posts: 537
Default

Originally Posted by sailingfun View Post
The Max is stable throughout its flight envelope without MCAS. MCAS was added to insure a common type rating and that there would be no required sim training for transition. The A321NEO on the other hand has actual stability issues in its flight envelope discovered after the Max issues. Currently that’s being managed with CG restrictions however a software fix is in the works. Some operators have to block aft seats.
MCAS was added because the stick force gradient in high power, high alpha situations was not adequate for it to be certified under applicable certification standards. It has nothing to do with a common type rating. Even if it were its own type rating, it would still need MCAS, or an aerodynamic fix, which they couldn’t effectively engineer, so they went with MCAS.
copy is offline  
Old 02-01-2021, 05:07 PM
  #103  
Gets Weekends Off
 
notEnuf's Avatar
 
Joined APC: Mar 2015
Position: stake holder ir.delta.com
Posts: 10,033
Default

Originally Posted by copy View Post
MCAS was added because the stick force gradient in high power, high alpha situations was not adequate for it to be certified under applicable certification standards. It has nothing to do with a common type rating. Even if it were its own type rating, it would still need MCAS, or an aerodynamic fix, which they couldn’t effectively engineer, so they went with MCAS.
This MCAS, the forward CG from underslung engines being pushed forward and in front of the wing along with the complimentary tail stand and the extendo gear is the result of over engineering an obsolete airframe in the interest of cost control. But I don't really care. Flown right, respecting all of its quirks, it can be operated safely. Even the Wrights, who had no frame of reference, abandoned the flyer for more suitable designs.
notEnuf is offline  
Old 02-01-2021, 06:29 PM
  #104  
Gets Weekends Off
 
Joined APC: Dec 2005
Posts: 8,898
Default

Originally Posted by copy View Post
MCAS was added because the stick force gradient in high power, high alpha situations was not adequate for it to be certified under applicable certification standards. It has nothing to do with a common type rating. Even if it were its own type rating, it would still need MCAS, or an aerodynamic fix, which they couldn’t effectively engineer, so they went with MCAS.
Got a source for that claim?
ShyGuy is offline  
Old 02-02-2021, 04:56 AM
  #105  
Gets Weekends Off
 
Joined APC: May 2012
Posts: 1,126
Default

Originally Posted by ShyGuy View Post
Got a source for that claim?
https://www.seattletimes.com/seattle...st-safeguards/

pretty straightforward article. FAA would require it regardless
waldo135 is offline  
Old 02-02-2021, 06:35 AM
  #106  
Gets Weekends Off
 
GyroNole's Avatar
 
Joined APC: Jun 2016
Position: First Officer
Posts: 234
Default

Originally Posted by Lifeisgood View Post
Are 717s being aggressively retired?
The latest aircraft fleet information file on DLnet dated 01 January shows 50 717s in the fleet.
I thought we had around 92?
Thx

49 Tails going forward per the Fleet LLCA (skyhub)....I am on the fleet and I do not know if the ones that were flown west were the tails that we owned and the remaining are the leases from Boeing or not...

I have flown with a technical pilot on the fleet twice and both times we discussed FMS constraints going forward and the amount of money required to comply with future FAA airspace restrictions...There were also some non-airspace airworthiness directives requiring expensive modifications that probably were not cost effective either...can’t remember what they were.

I have also heard there may be some white-tail MAXs being looked at (amount/timeline UNK)....maybe in conjunction with lease turn-ins?...

I do know that I won’t be told what’s going to happen until it does nor will my opinion be solicited.

I don’t suspect the 717 fleet will be around in the same numbers beyond two years from now...but have zero evidence or sources for that summation.


Sent from my iPhone using Tapatalk
GyroNole is offline  
Old 02-02-2021, 02:56 PM
  #107  
Gets Weekends Off
 
Joined APC: Apr 2014
Posts: 1,101
Default

Originally Posted by GyroNole View Post
49 Tails going forward per the Fleet LLCA (skyhub)....I am on the fleet and I do not know if the ones that were flown west were the tails that we owned and the remaining are the leases from Boeing or not...

I have flown with a technical pilot on the fleet twice and both times we discussed FMS constraints going forward and the amount of money required to comply with future FAA airspace restrictions...There were also some non-airspace airworthiness directives requiring expensive modifications that probably were not cost effective either...can’t remember what they were.

I have also heard there may be some white-tail MAXs being looked at (amount/timeline UNK)....maybe in conjunction with lease turn-ins?...

I do know that I won’t be told what’s going to happen until it does nor will my opinion be solicited.

I don’t suspect the 717 fleet will be around in the same numbers beyond two years from now...but have zero evidence or sources for that summation.


Sent from my iPhone using Tapatalk
I agree with all of what you said. I have also noticed lately, that the 717 is doing a lot more longer leg segments, and fewer short flights now too. More DAL, PHL, EWR, IAH, BDL, MKE and ORD type legs.
3 green is offline  
Old 02-02-2021, 03:06 PM
  #108  
Gets Weekends Off
 
GyroNole's Avatar
 
Joined APC: Jun 2016
Position: First Officer
Posts: 234
Default

Originally Posted by 3 green View Post
I agree with all of what you said. I have also noticed lately, that the 717 is doing a lot more longer leg segments, and fewer short flights now too. More DAL, PHL, EWR, IAH, BDL, MKE and ORD type legs.

Could be seasonal...I used to commute from PNS and we got 7-9 88s daily in the winter...with a mix of 739 and even 757 turns in the summer.

So to go there now (at least turns) to me is indicative of low traffic count.

PHL and ORD...MKE too are maybe from lower loads...


Sent from my iPhone using Tapatalk
GyroNole is offline  
Old 02-02-2021, 03:42 PM
  #109  
Gets Weekends Off
 
Joined APC: Dec 2005
Posts: 8,898
Default

Originally Posted by waldo135 View Post
https://www.seattletimes.com/seattle...st-safeguards/

pretty straightforward article. FAA would require it regardless
This is an old article, before the media reported correctly on MCAS. MCAS was required to mimic current NG pitching behavior at higher AOA. The MAX could have been certified without MCAS, but at the expense of needing a new type rating.
ShyGuy is offline  
Old 02-02-2021, 04:20 PM
  #110  
Gets Weekends Off
 
Joined APC: Oct 2019
Posts: 414
Default

Originally Posted by ShyGuy View Post
This is an old article, before the media reported correctly on MCAS. MCAS was required to mimic current NG pitching behavior at higher AOA. The MAX could have been certified without MCAS, but at the expense of needing a new type rating.
The media has not once, ever, reported correctly on MCAS.

Title 14

SECTION 25.203 Stall characteristics.

§ 25.203 Stall characteristics.(a) It must be possible to produce and to correct roll and yaw by unreversed use of the aileron and rudder controls, up to the time the airplane is stalled. No abnormal nose-up pitching may occur. The longitudinal control force must be positive up to and throughout the stall. In addition, it must be possible to promptly prevent stalling and to recover from a stall by normal use of the controls.

I am not going to go dragging out the Advisory Circular guidance (AC 25-7D) on flight test. It is written for engineers and basically says stick force per G has to be constant approaching a stall. Because of the bigger engines, they created a lifting force close to stall, in accelerated stall testing. Not high AOA, which is why MCAS is only active with Flaps up. No adverse characteristics with flaps down stalls. MCAS makes the stick force per G constant in accelerated stalls, that is a requirement for Part 25 Aircraft certification, has nothing to do with a common type rating. Common type rating only refers to the amount and type of training required.

The DC-10 and MD-11 do not have the same stall characteristics and they have a common type rating, as do many other aircraft.
Texasbound is offline  
Related Topics
Thread
Thread Starter
Forum
Replies
Last Post
marcal
Delta
42
05-11-2018 10:04 AM
Turboprop
Regional
16
02-28-2014 11:51 AM
nerd2009
Major
586
05-31-2012 04:02 AM
shado
Southwest
268
09-09-2011 03:08 PM
bjsmith
Technical
9
04-16-2009 09:18 PM

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are On
Pingbacks are On
Refbacks are On



Your Privacy Choices