What do you mean it wasn't Southwest's fault...Salk

[scoreboardII]

Wow, you win the "hate filled and biased yet unaccountable" post of the week at FI.

Well done.

Please, don't let the fact the manufacture has already publicly declared these cracks shouldn't have happened sway you from poking at windmills.

 

[luckytohaveajob]

Hate filled. SWA has lost its niche status and is preparing to play the real game. You guys are not the underdogs and do not get any special consideration.

Blame shifting Boeing is for pussies.

 

[LeeRoyJenkins]

I have not flown the B737 in years now.

Ahhhhhhh more back peddling.

But it is a slow piece of crap. The 37 is an airway blocker. Clogs up the pipes. Widebodies all run at .82 or better and fly 250 below 10k doing stabilized approaches.

No comes the tired justification for being wrong.

The limitation is 250k below 10k whether you like it or not. And the reason is debatable. Birds, separation, whatever.

It is not a design limitation!! It is an FAA REGULATION. You must still be embarrassed by making stupid statement. However if you have forgotten I will remind you:

I will write real slow for the SWAPA pilots who need the tutoring.

250 k below 10k is a design limitation. period. end of discussion. fact

Who is it now that needs the tutoring?

But you RJ pilots still got that little issue of following the rules. Stabilized approaches, de-icing in winter ops, overspeeding by 40+ knots, making crossings, knowing what the nearest suitable means, using drag devices appropriately, and flying the advanced systems as Boeing designed them.

The irony here is very rich, however you are too stupid to grasp it.

 

[redflyer65]

I'd say he's in the running for the monthly award.

Look out when Delta and others screw up. We'll see Lucky and the General spin machine at full tilt. I wouldn't throw too many stones gentlemen. Kharma is a real b'tch.

There's already plenty of incidents at other carriers of poor decisions and I'd rather not start a long laundry list. I honestly hope for safe practices at all carriers, I don't find any pleasure in another pilot's screw up. Every carrier has their 1 percenters. Every single one.

 

[luckytohaveajob]

Irony. You literary fellow. Get back to watching Pride and Prestigious with your wife.

Did those issues happen at SWA? You know the answer is yes. Your paxs deserve better and it is not Boeing's fault.

 

[Amish RakeFight]

Look out when Delta and others screw up. We'll see Lucky and the General spin machine at full tilt. I wouldn't throw too many stones gentlemen. Kharma is a real b'tch.

There's already plenty of incidents at other carriers of poor decisions and I'd rather not start a long laundry list. I honestly hope for safe practices at all carriers, I don't find any pleasure in another pilot's screw up. Every carrier has their 1 percenters. Every single one.

You mean like landing on a taxiway? :laugh:

 

[LeeRoyJenkins]

Irony. You literary fellow. Get back to watching Pride and Prestigious with your wife.

Did those issues happen at SWA? You know the answer is yes. Your paxs deserve better and it is not Boeing's fault.

Still don't want to admit that you were wrong I see.

I guess you think UAL 585 was not Boeing's Fault either?

 

[CA1900]

Looks like I caught a nerve exposing the corndogs shenanigans. Limitations are limitations and they are not up for debate.

Aircraft limitations and government regulations are not the same thing. Until you can understand that, it's impossible to have a meaningful conversation with you.

My particular airplane is limited to 305 above 8000, and 260 at or below 8000. That's its limitation per the manufacturer. Both of those speeds are higher than the 250 below 10,000 required by regulation in the US.

Do you understand the difference?

 

[stalker]

The only thing he understands is what daddy tells him before he pats him on the butt when hes getting on the school bus!

 

[scoreboardII]

Hate filled. SWA has lost its niche status and is preparing to play the real game. You guys are not the underdogs and do not get any special consideration.

Blame shifting Boeing is for pussies.

Well, I guess we can see who has found their inner child.

 

[densoo]

(AP) Investigators trying to determine why the roof of a Southwest Airlines jet cracked open in flight have issued preliminary findings suggesting there may have been flaws in the riveting work when Boeing built the plane 15 years ago.

The National Transportation Safety Board said Monday that some of the rivets used to bind the Boeing 737's aluminum panels together were sunk in holes larger than the rivet shafts. The holes weren't lined up correctly and were misshapen, not round, the board said.

 

[scoreboardII]

NTSB CONTINUES INVESTIGATION OF SOUTHWEST AIRLINES FLIGHT 812

As part of its continuing investigation of the April 1, 2011 accident involving Southwest Airlines flight 812 that experienced a rupture in the fuselage while in flight, the National Transportation Safety Board releases the following update.
On April 1, 2011, Southwest Airlines flight 812, a Boeing 737-300 registration N632SW, experienced a rapid depressurization caused by a rupture in the fuselage. The flight was at 34,000 feet when the depressurization occurred. The flight crew conducted an emergency descent and diverted the flight to Yuma International Airport, Yuma, AZ. At the time of the accident, the aircraft had accumulated 48,740 hours of service and 39,781 cycles (a cycle is a takeoff and landing). The accident aircraft was delivered to Southwest Airlines on June 13, 1996.
On-scene inspection by NTSB investigators revealed an approximately 9-inch wide by 59-inch long rectangular-shaped hole in the fuselage crown on the left side of the airplane, aft of the over-wing exit. The 59-inch longitudinal fracture occurred in the aluminum fuselage skin along the lap joint at stringer-4 left (S-4L) between body station (BS) 666 and BS 725. At S-4L, the crown skin overlaps the lower skin forming a lap joint. The two skins are connected at the lap joint by three rows of rivets (referred to as lower, middle, and upper row of rivets.) The fracture was through the lower skin and connected 58 consecutive rivet holes in the lower row of lap joint rivets. The exterior surface of the skin in the area of S-4L is painted blue. Evidence of blue paint was also found inside the joint between the upper and lower skin and on several areas of the skin fracture surface.
Following an on-scene examination of the accident aircraft, a portion of the fuselage skin that contained the hole and another portion of the skin located forward of the hole (total size 116 inches by 19 inches) were excised from the accident aircraft and transported to the NTSB Materials Laboratory in Washington, DC. The airplane was then released back to the operator.
At the NTSB Materials Laboratory, microscope examination of the fracture faces of the ruptured skin revealed fatigue cracks emanating from at least 42 of the 58 rivet holes connected by the fracture. Electrical conductivity measurements, hardness tests, and X-ray energy dispersive spectroscopy elemental analysis of the skin in the area of the fracture revealed that the aluminum skin material was consistent with the specified material. The skin was the specified thickness.
Non-destructive eddy current inspections conducted around intact rivets on the removed skin section forward of the rupture revealed crack indications at nine rivet holes in the lower rivet row of the lap joint. To assess the condition of the intact rivets and the skin rivet holes, X-ray inspections were performed on the skin located forward of the rupture location. This inspection revealed gaps between the shank portions of several rivets and the corresponding rivet holes for many rivets associated with S-4L. Upon removing selected rivets, the holes in the upper and lower skin were found to be slightly offset relative to each other and many of the holes on the lower skin were out of round.
In this ongoing investigation, the NTSB Materials Laboratory work is actively conducting additional inspections and examinations in the following areas:

1. Removal of rivets and examination of rivet hole dimensions, rivet dimensions, and rivet hole alignment between upper and lower skins.
2. Detailed fractographic analysis of the skin fractures emanating from the rivet holes using optical and scanning electron microscopes.
3. Fatigue striation analysis using a scanning electron microscope of specific skin fractures to determine the rate of crack propagation.
4. Additional portions of the lap joints from the accident aircraft.

Following the depressurization accident and on-scene examination of the accident aircraft, Boeing issued Alert Service Bulletin SB 737 53A1319-00 on April 4 instructing operators of certain Boeing 737-300, 400, and 500 aircraft to inspect the lower row of fasteners at stringer S-4R and S-4L, from BS 360 to BS 908 for cracking in the lower skin of the lap joint on airplanes.
The Federal Aviation Administration issued Emergency Airworthiness Directive AD 2011-08-51 on April 5 mandating the inspections in the Boeing Service Bulletin. To date, the NTSB has been informed that 136 airplanes have been inspected worldwide in accordance with the Service Bulletin and Airworthiness Directive including all U.S. registered airplanes covered by the Directive. As stated in a previous release, four of these airplanes were found to have crack indications at a single rivet and one airplane was found to have crack indications at two rivets. These airplanes had accumulated between 40,000 and 45,000 total cycles. The lap joints from these areas of the subject airplanes have been removed and will be fully documented as part of the NTSB investigation.
Photograph showing the interior and exterior surfaces of the ruptured section of the fuselage:
Click for full-sized image

OYS, LTHAJ, this is why it's best to let the investigators investigate before you emotionally speculate like an ammature.

 

[tankerhead]

Lucky,

You should prolly just stick to the Firebird or Camaro or whatever gets your rocks off when you're not flying the heavies. These jets are gonna bite ya. (plus you're gonna deep-six whoever's unLUCKy enough to be riding in the back) Just sayin'.

TH

 

[redflyer65]

OYS, LTHAJ, this is why it's best to let the investigators investigate before you emotionally speculate like an ammature.

Gotta love it. Thanks for playing...

 

[iflyhigh72]

Irony. You literary fellow. Get back to watching Pride and Prestigious with your wife.

Did those issues happen at SWA? You know the answer is yes. Your paxs deserve better and it is not Boeing's fault.

It's Pride and prejudice MO-RON

6 million sperm and your the one that made it through?

 

[LeeRoyJenkins]

It's Pride and prejudice MO-RON

6 million sperm and your the one that made it through?

That one sperm had retard strength.

 

[CA1900]

Never go full retard.

 

[imacdog]

It's Pride and prejudice MO-RON

6 million sperm and your the one that made it through?

It never fails.

 

[iflyhigh72]

It never fails.

Thanks for the correction imac. I was wrong. Whew!! feels real good to get that off my chest. Hey LTHAJ!!! Give it a shot.

 

[imacdog]

Don't get me wrong though; LTHAJ has been bumping the power up to full retard all thread.