FAA Grounds 787s
Joined: Jan 2008
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From: Los Angeles
glenbrook:
Do I incorrectly recall that the battery weighs some 65 lbs? Adding another 200 lbs doesn't seem significant. (Guessing that the APU battery was identical to the Main for spares commonality, I've not multiplied by two.)
I do think that lithium batteries do have other advantages e.g. low internal resistance that might make replacing them more than simply a weight-and-volume issue, though.
I would like to believe that, but I am not sure that plan B is all that simple.
Maybe you are right, perhaps they have a non-Lithium-ion replacement that will fit the slot. But if they do, it is going to be 4 times heavier and twice the volume
Maybe you are right, perhaps they have a non-Lithium-ion replacement that will fit the slot. But if they do, it is going to be 4 times heavier and twice the volume
I do think that lithium batteries do have other advantages e.g. low internal resistance that might make replacing them more than simply a weight-and-volume issue, though.
Joined: Apr 2011
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From: Cork, Ireland
Remember that the business case for the B787 was predicated on an increase in "point-to-point" journeys as compared to the traditional "hub-and-spoke" system. As such, it does not - at least initially - require ETOPS certification as it can fulfil that business case via intra-continental routes.
Joined: Jul 2002
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From: UK
A 787 without ETOPS is still grounded. Would Boeing even be able to deliver them?
Joined: Jun 2000
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From: Canada
The history of Lithium Ion batteries is not very flattering and their adverse effects in aircraft not that reassuring despite some positive characteristics.
If I might point to the volatility of these batteries whilst adding I acknowledge they were NOT connected to an electrical system at the time, they did bring down a B747-400 in Dubai in recent times.
Were lessons NOT learnt?
Is their lightness of weight, their ability to quickly recharge despite the residual heat they omit with such potential for disaster truly worth it?
Apparently.
This is what we get when manufacturers are pressurized by an industry that is so driven by the bottom line.
That's not news but that too is reality.
Willie
If I might point to the volatility of these batteries whilst adding I acknowledge they were NOT connected to an electrical system at the time, they did bring down a B747-400 in Dubai in recent times.
Were lessons NOT learnt?
Is their lightness of weight, their ability to quickly recharge despite the residual heat they omit with such potential for disaster truly worth it?
Apparently.
This is what we get when manufacturers are pressurized by an industry that is so driven by the bottom line.
That's not news but that too is reality.
Willie
Joined: Jan 2013
Posts: 2
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From: Triad, NC
I don't think it has been pointed out, but the power distribution and charging circuits seem to be made by Thales:
The batteries themselves are being made by Yuasa in Japan.
Joined: Jul 2002
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From: UK
Did they? The FAA released a precautionary bulletin and restriction on carrying consumer-grade Li-ion batteries following UPS006, but as far as I know there has been no confirmation that the batteries were the cause of the fire...
Joined: Mar 2002
Posts: 4,569
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From: Florida
The acceptable level of risk is one in a billion flight hours, not one in 25,000
I have yet to see what evidence applies in this case to the level of risk (either regulated by statue or to somebody's concept of safety).
All this re-quoting of the Special Condition is meaningless and pedantic unless expert assessments follow of what paragraphs were not met. In the end the means to unground will be made by corrective actions that bring it back into specific paragraph compliance and/or equivalent safety actions.
Neither the completion of these assessments has been made nor the proposed means of compliance, This then is the thorn that produces the delay and feeds the rampant uneducated discussions on the internet boards




Joined: Feb 2002
Aviation Qualifications: AME
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From: UK
The batteries are likely to be interchangeable to increase despatch reliability. (oh the irony!)
IE. If you have a main battery (or charger) go u/s away from main base then swap with the APU battery and away you go. MEL 49-1 refers.
IE. If you have a main battery (or charger) go u/s away from main base then swap with the APU battery and away you go. MEL 49-1 refers.
Joined: Aug 2007
Posts: 988
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From: Dublin
Although familiar with the long list of early in service problems with the 787, I'm finding it difficult to understand why the aircraft had to be grounded by the FAA rather than pilots or their representative bodies taking the initiative and refusing to fly them first.

Joined: Feb 2007
Posts: 134
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From: England
Something must be seriously wrong for FAA and EASA to ground the 787
I was quietly amazed that the FAA grounded the 787, which of course was followed too by EASA (Can I hear EADS applauding in the background) . I was in shorts the last time the FAA grounded an airliner (DC-10 I recall) in the mid 1970s.
I have been critical of the FAA and EASA before for not grounding other aircraft when lives have been lost in highly dubious circumstances (Rudder PCUs in Boeing 737s, and ADIRU/Pitot problems in Airbus A330s).
I wonder what has changed the approach of the FAA, unless there really is something that bad with the 787....
I have been critical of the FAA and EASA before for not grounding other aircraft when lives have been lost in highly dubious circumstances (Rudder PCUs in Boeing 737s, and ADIRU/Pitot problems in Airbus A330s).
I wonder what has changed the approach of the FAA, unless there really is something that bad with the 787....

Joined: Jan 2008
Posts: 17,729
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From: Reading, UK
Adding another 200 lbs doesn't seem significant.
Not so much for the impact on fuel burn, though it doesn't help, but for the effect on payload and therefore revenue potential over the life of the aircraft.
OTOH, if that's the price that has to be paid to get the type back in the air (and I suspect it will be) then that's what will happen.
Joined: Oct 2012
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From: toofaraway
DaveReidUK
Adding 200lbs to the OEW of a commercial airliner is not hugely significant.
200lb on the OEW equals 200lb off the payload, and only if the latter is already limited for some reason.
This means no revenue loss on almost all flights, and 200lb less cargo revenue on the remaining few.
200lb on the OEW equals 200lb off the payload, and only if the latter is already limited for some reason.
This means no revenue loss on almost all flights, and 200lb less cargo revenue on the remaining few.
Joined: Oct 2007
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From: brasil
APU only required for ETOPS beyond 180 min
Interval: C
Installed: 1
Required: 0
May be inoperative or removed
a) VFSG systems operate normally
b) ETOPS beyond 180 minutes not conducted
Installed: 1
Required: 0
May be inoperative or removed
a) VFSG systems operate normally
b) ETOPS beyond 180 minutes not conducted
Last edited by vaschandi; 23rd January 2013 at 12:04.

Joined: Feb 2007
Posts: 628
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From: Melbourne
Originally Posted by various
Adding 200lbs to the OEW of a commercial airliner is not hugely significant.
Hindsight is a wonderful thing, helps make all sorts of decisions easy to make. Only problem is it's a bit late by then...
Joined: Jun 2005
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From: position data invalid
The APU is required for the ETOPS certification, which by definition has to be very reliable and therefore needs a very reliable battery.
Wouldn't engine-driven generator be used as primary power source for APU in-flight lightup?



