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Twa 800

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Vik said:
This lame brain argument again.
No argument, just wondered what the general concensus was.

What's the matter, Vik? Do you have something to hide, hmm?

(Relax...kidding.)
 
I remember reading a book by Victor Belenko a couple of years ago. If I am not misstaken he said that the Russians brought this one down. I could be wrong however but for some reason I remember reading about this in his book.


Jimmy
 
fastandlow said:
Too many large Boeings with similar fuel systems been flying for 35+ years and only one "blowing up" in flight. Don't buy it.

Good, because it isn't true. As I mentioned, several KC-135's experienced the very same types of explosions with almost identical fuel systems. I lost a friend in such an explosion of a KC-135 at Loring AFB, ME.

Perhaps you should read this story about Boeing's belated concern over fuel pumps in empty tanks:

FAA Issues 3rd Warning on Fuel Pumps


EC/KC/RC-135 operators from that timeframe will remember SAC OPERATING PROCEDURE 90-1 that evolved out of the Loring event:

1. BACKGROUND: POTENTIAL EXISTS FOR HEAT BUILD-UP IN -135 AIR REFUELING/BODY PUMPS WHEN THE PUMPS ARE RUN DRY. THIS HEAT BUILD-UP MAY CAUSE CONDITIONS OF AN EXPLOSIVE NATURE IN THE BODY TANKS. DUE TO THE FUEL QUANTITY SYSTEM TOLERANCES AND DESIGN OF THE LOW PRESSURE WARNING LIGHT SYSTEM, IT MAY BE DIFFICULT TO DETERMINE WHEN A BODY TANK IS EMPTY. NORMAL SYSTEM TOLERANCES CAN RESULT IN A BODY TANK READING OF MORE THAN 500 POUNDS WHEN THE TANK IS IN FACT EMPTY.

2. PENDING ENGINEERING ANALYSIS AND INCORPORATION OF APPROPRIATE DATA INTO THE FLIGHT MANUALS, THE FOLLOWING PROCEDURES AND RESTRICTIONS WILL BE FOLLOWED. THESE PROCEDURES APPLY TO ALL -135 AIRCRAFT FLOWN BY SAC, ANG, OR AFRES AIRCREWS. ... THE PROCEDURES CONTAINED IN THIS OPS PROCEDURE TAKE PRECEDENCE OVER ANY PREVIOUS PROCEDURES.

A. FLIGHT CREWS WILL NOT ACCEPT AN AIRCRAFT FOR FLIGHT WITH LESS THAN 3000 POUNDS OF FUEL IN BOTH THE FORWARD AND AFT BODY TANKS ...

B. AIRCREWS WILL NOT ACCEPT AN AIRCRAFT FOR FLIGHT UNLESS BOTH THE FORWARD AND AFT BODY TANKS HAVE AT LEAST ONE GOOD AIR REFUELING/BODY PUMP. EACH OF THESE TANKS MAY CONTAIN ONE "SUSPECT" PUMP, ANNOTATED AS SUCH IN THE AFTO 781 ("DO NOT OPERATE PUMP OR RESET CIRCUIT BREAKER EXCEPT IN AN EMERGENCY") AND DEACTIVATED BY PULLING AND COLLARING THE 28V DC CIRCUIT BREAKER (CB) WITH A REMOVABLE COLLAR. ... IN AN EMERGENCY, CB COLLARS MAY BE REMOVED AND CIRCUIT BREAKERS RESET TO USE THOSE "SUSPECT" PUMPS. THEIR USE WILL BE LIMITED TO THAT NECESSARY TO SAFELY RECOVER THE AIRCRAFT. AIRCREWS WILL NOT ACCEPT AN AIRCRAFT FOR A PEACETIME FLIGHT WITH A REFUELING/BODY PUMP REMOVED OR AN INOPERATIVE /UNUSABLE PUMP INSTALLED WITHOUT A WRITTEN WAIVER FROM HQ SAC/LGM.

C. THE MINIMUM FUEL LEVEL IN THE FOREWARD AND AFT BODY TANKS IS 3000 POUNDS FOR ALL GROUND AND FLIGHT OPERATIONS. A NON-STANDARD FUEL LOAD WAIVER HAS BEEN GRANTED FOR ALL FUEL LOADS TO MEET THIS REQUIREMENT. THE 3000 POUND FUEL MINIMUM IN BOTH TANKS WILL BE TREATED AS TRAPPED/UNUSABLE FUEL. AS SUCH, IT WILL NOT BE CONSIDERED AVAILABLE FOR DIVERSION OR DELAY. ONLY AN ACTUAL EMERGENCY WARRANTS THE RISK OF DECREASING BODY TANK LEVELS BELOW 3000 POUNDS.


WARNING


AIR REFUELING/BODY PUMPS SHOULD NOT BE RUN DRY. IF PUMPS OPERATE DRY FOR A PERIOD EXCEEDING TWO MINUTES, DAMAGE TO PUMPS, FIRE AND EXPLOSIONS MAY RESULT.


D. FOR NORMAL OPERATIONS, AIRCREWS WILL TERMINATE OPERATION OF THE AFT PUMP IN EITHER BODY TANK WHEN THE QUANTITY IN THAT TANK REACHES 5,500 POUNDS. TERMINATE OPERATION OF THE FORWARD PUMP IN EITHER BODY TANK WHEN THE QUANTITY IN THAT TANK REACHES 3000 POUNDS. WHEN THE LIMIT IS REACHED, OPEN THE APPLICABLE 5 AMP 28V DC PUMP CONTROL CB ON THE SBCBP. ...

E. ... FLIGHT CREWS OPENING PUMP CIRCUIT BREAKERS AS PRESCRIBED BY THE MODIFIED FUEL BURN PROCEDURES WILL MAKE THE FOLLOWING ANNOTATION IN THE AFTO 781A (INFLIGHT DISCREPANCIES): "NOTE: AR/BODY PUMP CIRCUIT BREAKERS OPENED IAW HQ SAC FUEL BURN PROCEDURE." ...


There have been no further mid-air explosions of -135s.


It's too bad the 747 operators didn't get this message.
 
Whale Pilot said:
Being typed on the 747 and very familiar with the systems of the 747, I am sure that it didn't blow up on it's own. Go ahead and throw a match on a pool of jet a. The match will be extingushed. The fuel must be vaporized to attain the flashpoint for ignition.

The tank was empty. (No Jet-A, just a tank full of vapors.) Does that change your mind?
 
My understanding, although it may in fact be incorrect, is that the fuel pumps are not actually in the tank.

As far as TWA wanting to scream for further investigation, if you will remember they were just out of a bankruptsy at the time. Within 6 months of this event they announced that they would be purchasing 1 new aircraft every month for 6 years. Kinda funny sequence, considering they were still in pretty bad financial trouble on July 17, 1996. How did they suddenly get all the money for all those new airplanes?
 
atrdriver said:
As far as TWA wanting to scream for further investigation, if you will remember they were just out of a bankruptsy at the time. Within 6 months of this event they announced that they would be purchasing 1 new aircraft every month for 6 years. Kinda funny sequence, considering they were still in pretty bad financial trouble on July 17, 1996. How did they suddenly get all the money for all those new airplanes?

Probably the same way USAirways found financing for 135 RJs just out of bankruptcy...Some moron lent them the money. Stupid people working in the financial industry does not make for a cover-up. It just makes business as usual in the airline world.

Skeezer
 
fastandlow said:
Too many large Boeings with similar fuel systems been flying for 35+ years and only one "blowing up" in flight. Don't buy it.

And if you don't wanna take my word for it, try browsing through this FAA Notice regarding Fuel Tank Ignition Prevention Measures.

Including the KC-135 I mentioned from October 1989, this document lists are 13 civilian and 13 military accounts of fuel tank explosions. All but 4 were Boeing products.

1982: Air Canada DC-9 center wing fuel tank exploded on the ground during maintenance - - Dry running of pumps is the suspected cause.

1990: Phillipine Airline B-737 during taxi - - empty center wing tank exploded.

1970: USAF B-52 during maintenance - - explosion of fuel tank, most likely ignition source traced to arcing or overheat of fuel pump shaft or fuel quantity probe.

1971: Spain Air Force B-707 - - #1 main tank exploded during descent through 17,000'. USAF determined chafing of boost pump wires located in conduits as possible ignition source.

1982: KC-135A near Chicago descending through 12,000' - - forward body tank exploded, initial cause listed as VHF antenna.

1987: KC-135A during landing rollout at Altus AFB, OK - - an explosion and fire occurred following copilot transmission on UHF radio. The UHF wire run near the right aft wing root in the fuselage was melted due to an electrical fault. Fuel vapors in the area of the aft body tank were ignited.

1988: B-52H at KI Sawyer AFB, MI during touch-and-go landing - - at 20 ft AGL the empty aft body tank exploded. Pump num [sic] operating in the aft body tank was cause. Evidence of arcing a [sic] overheat was found.

Sept 1989: KC-135A at Loring AFB, ME, parked following flight - - during system shutdown, explosion in the aft fuselage tank occurred. Source of ignition was believed to be a hydraulically driven fuel pump mounted inside the aft body fuel tank.

Oct 1989: KC-135A at Loring AFB, ME, in local traffic pattern - - explosion in the aft body fuel tank caused hull loss. (Oh, and by the way, the loss of lives - added) Aft body f hydraulically driven pump implicated as source of ignition.

1993: KC-135R at Mitchell Field, Milwaukee during ground maintenance - - center wing tank exploded. Center wing fuel tank fuel pump implicated as source of ignition.
 
There was also a Thailand government 747 that blew up at on the ramp shortly after TWA 800 went down.
 
Vik said:
I think there was an Iran Air 747 that also blew up due the center tank issue.

The above cited report mentions a "special investigation of the May 9, 1976, explosion and in-flight separation of the left wing of an Iranian Air Force Model 747-131, as it approached Madrid, Spain, following a flight from Iran. Witnesses reported seeing a lightning strike to the left wing, followed by fire, explosion, and separation of the wing." The wreckage revealed evidence of an explosion that originated near a fuel valve installation in the left outboard main fuel tank.
 
Typhoon1244 said:
It's unorthadox in an airplane that's neither certified nor stressed for it.

just curious (yes i do not like caps)....

at 90deg bank, what would you do with the ailerons/rudder keeping in mind you have the benefit of hindsight and not .5sec to do something. the poor fo is a scapegoat. all i said was he did a "standard" recovery in terms of basic aerodynamics.
 
TonyC,

I read the accident summaries and the excerpt from 90-1 you posted with great interest. I'm almost convinced that the official explanation for this incident makes sense, except for one major issue...but I'll come back to that in a second.

One thing I noticed in 90-1 is that the main issue they seem to have been concerned about was heat, not arcing.
US Air Force said:
POTENTIAL EXISTS FOR HEAT BUILD-UP IN -135 AIR REFUELING/BODY PUMPS WHEN THE PUMPS ARE RUN DRY. THIS HEAT BUILD-UP MAY CAUSE CONDITIONS OF AN EXPLOSIVE NATURE IN THE BODY TANKS.
Does anyone know whether or not the center tank pumps on N93119 were running as it climbed out on July 17th?

In any case, it's my understanding that for a given quantity of Jet-A to ignite, it must be heated and misted. I didn't think "fumes" were enough to cause an explosion, regardless of what the ignition source is. But when you read about all those lost Stratotankers...perhaps I'm mistaken.

Now, back to the major problem I have with the official explanation: if TWA 800 was brought down by an accidental explosion in the center tank, then what exactly did all those witnesses see?

I don't buy the CIA's "zoom climb" story. The aerodynamics and radar data don't support that. And the Agency's story about people being misled by the differing speed of sound and light doesn't apply to those who were looking up at 800 before the explosion.

As I said, eyewitness accounts are notoriously misleading, particularly when it comes to aircraft accident investigation. But are we really supposed to believe that two hundred people--including a handful of military pilots--all got it wrong?
 
TonyC said:
And if you don't wanna take my word for it, try browsing through this FAA Notice regarding Fuel Tank Ignition Prevention Measures.

Including the KC-135 I mentioned from October 1989, this document lists are 13 civilian and 13 military accounts of fuel tank explosions. All but 4 were Boeing products.

1982: Air Canada DC-9 center wing fuel tank exploded on the ground during maintenance - - Dry running of pumps is the suspected cause........
Lot more instances that I was aware of, but the point remains that there are an awful lot of 747 series AC that have and are still flying and this scenario is just too rare, making me suspect something else. But this is based on intuition and limited experience with this equipment.

Assuming it was a fuel tank explosion, where does the oxygen come from? I'd think, even though it's not very volitile, the jet fuel vapors would displace any oxygen in a partially or even empty fuel tank.
 
"...In congressional testimony and in statements repeatedly made in the media, the NTSB leadership cited the loss of an Air Force 707 and three KC-135 air to air tanker aircraft, to fuel tank explosions as examples of mishaps similar to TWA Flight 800. Col. Dougherty’s office of the Air Force’s safety center says, “there is no record of a 707 loss and all three KC135’s were fueled with JP4, a fuel as volatile as automobile gasoline”. “Since switching to the military equivalent of...Jet-A fuel the Air Force has not had a problem.”
This is from Commander William Donaldson's report to the Congressional Subcommittee on Aviation two years after TWA 800 went down.
 
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Whale Pilot said:
Just a little info from someone there!

AA Airbus flight crashed b/c the "God Pilot" F/O was trained that use of rudder to help regain the proper attitude is the proper procedure.

Who is claiming that the F/O was a "God Pilot"? What the heck does that mean?

Whale Pilot said:
He would have been trained because at the time American was training this. I know because I was a former TWA pilot who saw the video with 2300 other TWA pilots.

Let me get this straight. All 2300 TWA pilots saw the AAMP together and at the same time? (Question asked in a sarcastic manner.)

Whale Pilot said:
Many of us were amazed that AA was teaching this "unorthadox" and dangerous procedure.

I have been through the program as well. None of what the AAMP taught is, was or will ever be dangerous or unothadox. If it was or had been then why did the FAA as well as other airlines use and still use all and parts of the program to train pilots? Can you answer that for me?

Whale Pilot said:
As far as 800, I was flying back from KBOS to KJFK that evening. It didn't just blow up. I too, like many others saw the "streak" heading skyward from the ocean.

It has been shown many times that that "streak" was most likely TWA 800 flying in a near vertical manner after exploding with the wings still attached. The streak you saw was probably the plane itself.

Whale Pilot said:
Being typed on the 747 and very familiar with the systems of the 747, I am sure that it didn't blow up on it's own. Go ahead and throw a match on a pool of jet a. The match will be extingushed. The fuel must be vaporized to attain the flashpoint for ignition.

That statement alone shows you have no clue what you are talking about. After TWA 800 Boeing came out with an AD for all operators of the B-747, B-767 and I think the B-757 to leave a certain amount of fuel in the center fuel tank to prevent such an explosion that happened on TWA 800.
 
Typhoon1244 said:
One thing I noticed in 90-1 is that the main issue they seem to have been concerned about was heat, not arcing.Does anyone know whether or not the center tank pumps on N93119 were running as it climbed out on July 17th?

In any case, it's my understanding that for a given quantity of Jet-A to ignite, it must be heated and misted. I didn't think "fumes" were enough to cause an explosion, regardless of what the ignition source is. But when you read about all those lost Stratotankers...perhaps I'm mistaken.

fastandlow said:
Assuming it was a fuel tank explosion, where does the oxygen come from? I'd think, even though it's not very volitile, the jet fuel vapors would displace any oxygen in a partially or even empty fuel tank.

From the FAA Notice:

"Evidence indicates that as the airplane was
climbing near 13,800 feet mean sea level (msl), an in-flight explosion occurred in the center wing fuel tank (CWT). (The flight engineer from the previous flight remembered having left about 300 pounds, or about
50 gallons, of fuel in the approximately 13,000 gallon capacity tank. The recovered fuel gauge indicated slightly more than 600 pounds (about 100 gallons) of fuel remaining in the CWT.) The CWT was nearly empty."

"Portions of the airplane have been reconstructed, including the CWT, the passenger cabin above the CWT, and the air conditioning packs and associated ducting beneath the CWT. The reconstruction thus far shows outward deformation of the CWT walls and deformation of the internal components of the tank that are consistent with an explosion originating within the tank. Airplane parts (includes portions of the fuselage structure from above, air conditioning packs and ducting from below, wing structure from both sides, all tires from behind, and numerous components that included the large fiberglass water and cargo fire extinguisher containers from forward of the CWT) from in and around the CWT recovered and identified to date contain no evidence of bomb or missile damage."

"Fuel tank explosions require an energy source sufficient for ignition and temperatures between the lower explosive (flammability) limit (LEL) * and upper explosive limit (UEL), which will result in a combustible mixture of fuel and air.

* (Marks' Standard Handbook for Mechanical Engineers, Eighth Edition, states, ``The lower and upper limits of flammability indicate the percentage of combustible gas in air below which and above which flame will not propagate. When a flame is initiated in mixtures having compositions within these limits, it will propagate and therefore the mixtures are flammable.'' Marks' states further, ``The autoignition temperature of an air-fuel mixture is the lowest temperature at which chemical reaction proceeds at a rate sufficient to result eventually (long time lag) in inflammation.'' In the TWA800 CWT, the LEL was about 115 deg.F, and the autoignition temperature was about 440 deg.F.)"

"However, a 1990, Society of Automotive Engineers technical paper comments, ``. . . if the ignition source is sufficiently strong (such as in combat threats), it can raise the fluid temperature locally and thus ignite a fuel that is below its flash point temperature. This is particularly true with a fuel mist where small droplets require little energy to heat up.''

"... on August 26, 1996, Boeing conducted flight tests with an instrumented Model 747 airplane that carried about the same small amount of fuel in the center wing tank as that carried aboard TWA800. All three air conditioning packs were operated on the ground for about 2 hours to generate heat beneath the CWT. The airplane was then climbed to an altitude of 18,000 feet msl. The temperature of the fuel in the center tank of the test airplane was measured at one location, and the air temperature within the tank was measured at four locations. In this test, the fuel-air mixture in the CWT ullage was stabilized at a temperature below the LEL on the ground. However, as the airplane climbed, the atmospheric pressure reducing the LEL temperature and allowing an explosive fuel-air mixture to exist in the tank ullage."


Now, fastandlow, you have touched on a very important concept, that of the existence of oxygen in the tank. No, fuel vapors do not displace oxygen. At the altitude the explosion occurred, there was more than sufficient oxygen to sustain an explosion. But there is a recommendation to equip airplanes with systems to replace oxygen with nitrogen.

"Without oxygen in the fuel-air mixture, the fuel tank ullage could not ignite, regardless of temperature or ignition considerations. The military has prevented fuel tank ignition in some aircraft through the creation of a nitrogen-enriched atmosphere (nitrogen-inerting) in fuel tank ullage, there by creating an oxygen-deficient fuel-air mixture that will not ignite. Although this technology could be applied to civil aircraft, there are no transport category airplanes of which the Board is aware that currently incorporate nitrogen-inerting systems to reduce the potential for fuel tank fires and explosions."


I could go on and on copying and pasting, but you really should take the time to read the whole thing yourself. It's quite educational.



Typhoon1244 said:
Now, back to the major problem I have with the official explanation: if TWA 800 was brought down by an accidental explosion in the center tank, then what exactly did all those witnesses see?

...

As I said, eyewitness accounts are notoriously misleading, particularly when it comes to aircraft accident investigation. But are we really supposed to believe that two hundred people--including a handful of military pilots--all got it wrong?

I don't know what they all saw, or even what one of them saw. I do find eyewitness testimony to be, at best, suspect. Given that the airplane has been almost entirely reconstructed, and that the physical evidence is overwhelming, I believe the eyewitnesses, once again, got it wrong.
 
Dangerkitty said:
That statement alone shows you have no clue what you are talking about. After TWA 800 Boeing came out with an AD for all operators of the B-747, B-767 and I think the B-757 to leave a certain amount of fuel in the center fuel tank to prevent such an explosion that happened on TWA 800.

No, the FAA has NEVER issued AD's that were either unnecessary or suspect for some reason. There are a lot of inconsistancies in the TWA800 case. If you want to believe that it blew up by itself, fine. There are still a LOT of people,and will always be a lot of people, who believe otherwise.
 
Ladies and Gentlemen:


I apologize for any misleading statements I may have made above. Please disregard all of my previous comments on this subject.

I have just been informed via PM that somebody knows somebody else at the CIA, in fact two somebodies at CIA that don't even know each other, that both know for a fact TWA 800 was shot down.


Sorry for the inconvenience! :rolleyes:
 
Well, that settles it. I hope we can all put this behind us... :D
 
no apology needed.

Jeez, after reading brightspark's well thought out responses I assumed the entire group here would for sure be convinced it was a problem with the fuel tank..

bummer- just when you had everyone certain this happens !.

3 5 0
 
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You put 50 people in a room, they give you 50 different answers as to why it blew up..., my belief is we will probably never know the true facts......too many liars and black mailers out there. They tell you what you want to hear to keep you quite.

There is more questions then factual answers, none of us where there, all we have is info passed on from one person to another ... kinda defeats the whole purpose and most likely a complete waste of time,kinda like this thread
 
So the center wing tank is filled with a mix of air and kerosene fumes, which by the NTSB's own findings do not become flammable until after takeoff (and discounting the fact that the day the NTSB's test was conducted was 16 degrees warmer than July 17th). Somehow, a large amount of flammable vapors build up, even though the ullage was right at or below the critical temperature. Then a spark ignites the mixture- possibly from the CWT scavange pump, even though the pump was not running at the time, and was recovered and found not to have any problems. The resulting explosion is violent enough to blow the forward half of the fuselage off and eject debris out the right side which radar estimates is travelling at 2000 FPS.
The majority (98%) of the CWT is then recovered- all in the easternmost part of the debris field. Highly unlikely.

The NTSB's report details an experiment they performed with a scale model of the 747's CWT to investigate the nature of fuel vapors. When they heated the Jet-A to the vapor point and tried to ignite it, nothing happened. They eventually had to add propane and hydrogen to get a reaction, because the kerosene fumes would do nothing more than burn off and then self-extinguish.
You have to realize that when fuel vapors burn, it is a low velocity explosion. It's more of a "whump" that may deform or even rupture the tank, but can't do the kind of damage that was observed on the TWA 800 airframe. Much of the physical evidence, radar data, and eyewitness accounts, is indicitive of a high velocity explosion. That cannot be caused by fuel vapors of any kind- only high explosives.

Interesting side note:
Does anyone remember that Muslim wall calendar found in Europe that was in the news just after 9/11? It showed an airliner crashing in flames near New York City, and the media suggested it showed that the 9/11 plot was widely known enough to allow calendars to be printed even before the attack.
The calendar definitely depicts New York City- the Statue of Liberty is visible in the background. Two interesting things though: the airliner is a 747, and it is shown crashing into the water! Hmmm....
 
C601 said:
There is more questions then factual answers, none of us where there, all we have is info passed on from one person to another ... kinda defeats the whole purpose and most likely a complete waste of time,kinda like this thread

True, but I think it's our duty as pilots to see the true cause for this crash determined, and the associated threat addressed. To date, the investigation has been the strangest and most unconvincing accident investigation in history.
The book First Strike makes a good point about the evidence. It mentions Occhams's Razor- the idea that the simplest explanation is usually the correct one. So much of the evidence in this crash points to a missile attack, but the government seems determined to pursue far-fetched elaborate theories to avoid acknowledging it.

If I had lost a loved one on the plane, you can bet I'd be determined to know the cause of the crash! I think the family members have a right to be upset at how the investigation has been conducted so far.
 
One of the biggest questions that was always left in my mind was why did the CIA produce the video of what supposedly happened. The NTSB obviously has the capability to do so, as does the FBI. Why, AFTER they supposedly determined that foul play was not involved, was the CIA commissioned for the video?
 
dash8driver said:
this sounds like a job for Mythbusters!

Or the Dallas police.
 
atrdriver said:
No, the FAA has NEVER issued AD's that were either unnecessary or suspect for some reason. There are a lot of inconsistancies in the TWA800 case. If you want to believe that it blew up by itself, fine. There are still a LOT of people,and will always be a lot of people, who believe otherwise.

ATRDRIVER,

I used a poor choice of words. Boeing issued information asking operators to not run the center tanks dry and to keep a certain amount of Jet-A in them. I never said anything about the FAA but since I stated AD I guess thats what was implied. Sorry for the confusion.
 
atrdriver said:
Come on...The F-117A was in sqadron service for almost 10 years before anyone outside the program knew that it existed. Don't tell me that the government can't keep a secret if they want it kept.

I think there is a slight difference between working a classified project and being involved in a friendly fire incident.
 
Typhoon1244 said:
See how quickly I'm adapting to living in Tennessee?

Sigh....
Everyone knows that "y'all" is singular, while "y'alls" is plural.
 

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