This is long winded but I hope it helps to clarify some things.
There seems to be a lot of confusion about TCAS and Transponders here so I will try to clarify a bit.
The setup on an aircraft with two transponders is not like a small twin’s whereby the transponder is right in front of you and you dial in the code right on the transponder itself. On a large aircraft, you control the transponder via a control panel. The actual transponders are in the electronics compartment. Each one looks at the control panel’s settings to transmit the correct code and to see which one of them should be transmitting. It is much like the tuner on your TV. It just tells the guts what they should be doing.
They also don’t transmit at the same time, and on any aircraft I have ever flown, they don’t fail automatically to the second transponder, they just fail. ATC then calls you to say they lost your target and you switch to the second one.
The transponder in question has an AD, because of a bug which puts the transponder in standby mode all by itself.
Airworthiness Directive
Federal Register Information
Header Information
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24639; Directorate Identifier 2005-NM-171-AD;
Amendment 39-14761; AD 2006-19-04]
RIN 2120-AA64
Airworthiness Directives; Honeywell RCZ-833J/K, -851J/K, and - 854J Communication (COM) Units, Equipped with XS-852E/F Mode S Transponders; and Honeywell XS-856A/B and -857A Mode S Transponders;
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Honeywell COM units and transponders, installed on but not limited to certain transport category airplanes. … This AD results from the transponder erroneously going into standby mode if the flight crew takes longer than five seconds when using the rotary knob of the radio management unit to change the ATC code. We are issuing this AD to prevent the transponder of the COM unit from going into standby mode, which could increase the workload on the flight crew and result in improper functioning of the traffic alert and collision avoidance system.
Applicability
(c) This AD applies to the Honeywell parts identified in paragraphs (c)(1) and (c)(2) of this AD, approved under Technical Standard Order TSO-C112, installed on but not limited to…
…EMBRAER Model EMB-135BJ, -135ER, -135KE, -135KL, and - 135LR airplanes; EMBRAER Model EMB-145, -145ER, -145MR, -145LR, - 145XR, -145MP, and -145EP airplanes
The entire AD can be read at
http://www.airweb.faa.gov/Regulatory_an ... enDocument
This would explain why radar contact was lost and more importantly, why radar contact was re-established when the crew dialed in 7700. (They would take less than 5 seconds to dial 7700)
There is radar coverage over that area and it is the definition of "the middle of nowhere". Even so, they popped up on radar when they squawked 7700. They couldn’t find a usable frequency because they had lost situational awareness and didn’t know where they were. All the frequencies for a given sector are published on the Jepp. enroute charts for that area. They couldn’t find a useable airport by themselves as well ( they needed help from a passing cargo flight) even though where they landed is asphalt 8547 X 145 and has VOR and NDB approaches. It is a non English non sched. public airport as it is only used for medivacing indians out of the bush.
If their transponder went to standby, their TCAS would be inop according to the AD, as it would not be radiating nor processing any signal . The Legacy would therefore be invisible to the 737’s TCAS.
Contrary to popular belief, jet pilots are not scanning for traffic while in cruise flight. No-one is supposed to be there so why the hell look?
As to what happened: The initial clearance to maintain FL370 was correct as the airway was one way until Brasilia.
Either ATC just clean forgot about the flight after Brasilia, or the pilots upon hearing “Radar Contact, maintain FL370” turned down the volume of their radios too far because that sector has a lot of traffic/ chatter. (I fly it every week). That is WAY more common than people like to admit.
Brasilia center doesn’t normally change codes, but if they had given a new code to the Legacy and then lost radar contact, the Legacy should still be on frequency. (5 seconds)
My gut feeling is that they turned down the radios to play with the new toys in the aircraft and while messing with the transponder managed to trip it to standby. There were multiple calls to the aircraft registered on tape.
This in no way excuses ATC from not moving the 737. That was a blatant error.
As to what happened to the 737.
A friend of mine is part of the investigation and had access to the Flight Data Recorders and was on site.
The 737 was hit in the wing and started an immediate roll. It reached 6 G’s in the roll. The engines separated from their pylons. The main gear was ejected from the gear wells as the uplocks only withstand 4 G’s I am told. Catastrophic failure of the fuselage occurred below 10,000 feet. The aircraft remains are in a small area for a midair as everything went nearly vertical after the collision.
Time to impact from 37,000 feet was 2 minutes and 55 seconds.
He sent me pictures from the crash site, believe me you don’t want to see them. Bodies were found more than a meter under ground.
The crew of the Legacy were held because everyone, myself included, thought that they had been playing with their new toy and were relying on the Big Sky Theory to keep them out of trouble. As the airspace is all RVSM, that seemed at the time like criminal negligence causing death. In 1997 a flight for the company I flew for screwed up badly at LAX. There was not an accident but the crew were under house arrest (hotel) in LA for over 2 weeks, so it is not a third world thing.
We will just have to wait and see.
PS Do not believe anything that the papers publish here about the accident. I have NEVER seen so much drivel about aviation in my life as to what has been published here.