Very interesting - sounds like the last step before a completely un-manned
drone airliner -  "The controller can uplink speed, heading, and altitude
changes to the airplane. These show up on a  second line right under the
speed, heading and altitude displays on the mode control panel. If you
pilot wants to use them, he can press a XFR button next to each window. The
controller can even uplink a conditional clearance, like - After passing
point XYZ, climb to FL390. If you accept this, it will do it automatically."


On Wed, Jul 25, 2012 at 11:59 PM, <relng...@aol.com> wrote:

> Over the last ten years there have been many posts here and elsewhere
> bewailing "all them electronics" in late model MBs which make the
> ownership of
> one a nightmare when the cars get a few years on them. So they think.
>
> So take warning because the following post will may bring on a fainting
> spell.
>
> From a pilot friend.
> > ------------------------------
> >
> >
> > I just completed the first pilot training class on the
> > 787 at United Airlines, an airplane which is destined to replace the 767
> > and live for many years after I retire. Here's what I've learned in 787
> > training so far. By the way, last night we passed our MV (maneuvers
> > validation) check ride, with emergency after emergency, and the FAA
> > observing. Tonight was our LOE (line-oriented evaluation), again with
> > FAA - this time 2 FAA observers. It's 0200 and I just got back to the
> > hotel and poured a well-earned glass of wine to celebrate. I now have a
> > type rating in the 787. Phew. I'm pretty confident this will be the last
> > one for me.
> >
> >
> >
> > I've summarized some of the major differences and unique
> > features of the 787 versus more traditional "old school" airplanes like
> > the 777 (not kidding) - from the pilot's viewpoint. Our "Differences"
> > course takes 11 days to gain an FAA type rating, which is a "common"
> > type rating with the 777. The course has been like drinking from a fire
> > hose, but has finally come together. Some of our pilots attended
> > Boeing's 5-day differences course, and deemed it unacceptable. The FAA
> > approved the Boeing 5-day course, but our guys decided it lacked too
> > much information. FAA is observing our checkrides now, and taking our
> > course as well, to certify the training. We're just the guinea pigs.
> >
> > A computer nerd would describe the 787 as 17 computer servers
> > packaged in a kevlar frame. The central brains is the Common Core System
> > (CCS). Two Common Computing Resources (CCRs) coordinate the
> > communications of all the computer systems, isolating faults and
> > covering failed systems with working systems. When battery power is
> > first applied to the airplane in the morning, it takes about 50 seconds
> > for the L CCR to boot up. After this, a few displays light up and you
> > can start the APU. If there is a major loss of cockpit displays, this
> > may require a CCR reboot, which would take about a minute. Here are a
> > few of the major features and differences from the 777.
> >
> > Electrics - Though a smaller plane, the 787 has 4 times the
> > electric generating power of the 777 - 1.4 gigawatts. Generators produce
> > 235 VAC for the big power users. Other systems use the traditional 115
> > VAC and 28 VDC. There are 17 scattered Remote Power Distribution Units
> > which power about 900 loads throughout the plane. The big power
> > distribution system is in the aft belly, along with a Power Electronics
> > Cooling System (PECS). This is a liquid cooling system for the large
> > motor power distribution system. There's also an Integrated Cooling
> > System (ICS), which provides refrigerated air for the galley carts and
> > cabin air, and a Miscellaneous Equipment Cooling System for Inflight
> > Entertainment Equipment.
> >
> >
> >
> > If 3 of the 4 engine generators fail, the APU starts itself. The APU
> > drives two generators, and can be operated up to the airplane's max
> > altitude of 43,000 feet. If you lose all 4 engine generators, the RAT
> > (ram air turbine) drops out (like a windmill), powering essential buses.
> > (It also provides hydraulic power to flight controls if needed).
> >
> > If you lose all 4 engine generators and the two APU generators (a really
> > bad day), you are down to Standby Power. The RAT will drop out and
> > provide power, but even if it fails, you still have the autopilot and
> > captain's flight director and instruments, FMC, 2 IRSs, VHF radios, etc.
> > If you're down to batteries only, with no RAT, you'd better get it on
> > the ground, as battery time is limited. Brakes and antiskid are electric
> > - 28V - so you don't lose brakes or antiskid even when you're down to
> > just standby power.
> >
> > Normal flight controls are hydraulic with a couple exceptions. Engine
> > driven and electric hydraulic pumps operate at 5000 psi (versus normal
> > 3000 psi) to allow for smaller tubing sizes and actuators, thus saving
> > weight. If you lose all 3 hydraulic systems (another bad day), you still
> > have two spoiler panels on each wing which are electrically powered all
> > the time, as is the stabilizer trim. You can still fly the airplane (no
> > flaps, though). If you're having an even worse day and you lose all
> > hydraulics and all generators, flight control power is still coming from
> > separate Permanent Magnet Generators (PMGs) which produce power even if
> > both engines quit and are windmilling. If the PMGs fail, too, your
> > flight controls will be powered by the 28 V standby bus.
> >
> > If you lose all 3 pitot/static systems or air data computers, the
> > airplane reverts to angle of attack speed (converts AOA to IAS), and
> > this is displayed on the normal PFDs (primary flight displays) airspeed
> > indicator tapes. GPS altitude is substituted for air data altitude and
> > displayed on the PFD altimeter tapes. Very convenient.
> >
> > If you lose both Attitude and Heading Reference Units (AHRUs), it
> > reverts to the standby instrument built-in attitude & heading gyro, but
> > displays this on both pilot's PFDs for convenience.
> >
> > If you lose both Inertial Reference Units, it will substitute GPS
> > position, and nothing is lost.
> >
> > If someone turns one or both IRSs off in flight (I hate it when they do
> > that), you can realign them - as long as one of the GPSs is working!
> >
> > There is no pneumatic system. The only engine bleed is used for that
> > engine's anti-ice. Wing anti-ice is electric. Each of two air
> > conditioning packs control two CACs, which are electric cabin air
> > compressors. The four CACs share two air inlets on the belly. Each pack
> > controller controls two CACs, but if a pack controller fails, the
> > remaining pack controller takes over control of all 4 CACs.
> >
> > There are no circuit breakers in the cockpit. To check on them, or if
> > you get a message that one has opened (more likely), you select the CBIC
> > (circuit breaker indication and control) display on one of the MFDs
> > (multi function displays). There you can reset the virtual C/B if it is
> > an "electronic" circuit breaker. You can't reset a popped "thermal"
> > circuit breaker.
> >
> > If you have an APU fire on the ground or inflight, the fire
> > extinguishing bottle is automatically discharged. If there is a cargo
> > fire, the first two of seven bottles will automatically discharge also.
> >
> > There's a Nitrogen Generation System which provides automatic full-time
> > flammability protection by displacing fuel vapors in the fuel tanks with
> > nitrogen (Remember TWA 800?).
> >
> > Like the 767 and 777, the 787 also has full CPDLC capability
> > (controller-to-pilot datalink communications). In addition, its full
> > FANS capability includes ADS-B in & out. The controller can uplink
> > speed, heading, and altitude changes to the airplane. These show up on a
> > second line right under the speed, heading and altitude displays on the
> > mode control panel. If you pilot wants to use them, he can press a XFR
> > button next to each window. The controller can even uplink a conditional
> > clearance, like - After passing point XYZ, climb to FL390. If you accept
> > this, it will do it automatically.
> >
> > Fuel system - like the 777, the 787 has a fuel dump system which
> > automatically dumps down to your maximum landing weight, if that is what
> > you want. In addition, it has a Fuel Balance switch which automatically
> > balances your L & R main tanks for you. No more opening crossfeed valves
> > and turning off fuel pumps in flight. No more forgetting to turn them
> > back on, either.
> >
> > Flight Controls - An "Autodrag" function operates when the airplane is
> > high on approach and landing flaps have been selected. It extends the
> > ailerons and two most outboard spoilers, while maintaining airspeed, to
> > assist in glidepath capture from above, if you are high on the
> > glideslope. The feature removes itself below 500 feet.
> >
> > Cruise flaps is an automated function when level at cruise. It
> > symmetrically moves the flaps, ailerons, flaperons, and spoilers based
> > on weight, airspeed and altitude to optimize cruise performance by
> > varying the wing camber, thus reducing drag.
> >
> > Gust suppression - Vertical gust suppression enhances ride quality when
> > in vertical gusts and turbulence. It uses symmetric deflection of
> > flaperons and elevators to smooth the bumps. This should result in fewer
> > whitecaps in passengers' coffee and cocktails. Lateral gust suppression
> > improves the ride when on approach by making yaw commands in response to
> > lateral gusts and turbulence.
> >
> > Instrument Approaches - The airplane is actually approved for autoland
> > based not only on ILS but on GLS approaches - GPS with Ground based
> > augmentation system, which corrects the GPS signals. GLS minimums are
> > the same as CAT I ILSs - 200' and 1/2 mile visibility. Our airline is
> > not yet approved for GLS autolandings yet, though we will be doing GLS
> > approaches.
> >
> > Special Cat I & II HUD approaches - These allow lower than normal
> > minimums when the Heads Up Devices are used at certain approved airports
> > (HUDs). The HUDs include runway centerline guidance which helps you stay
> > on the centerline on takeoff when visibility is greatly reduced. It uses
> > either ILS or GLS for this.
> >
> > Cabin - Pressurization differential pressure maximum is 9.4 psid, so the
> > cabin altitude is only 6000 feet when at the max cruising altitude of
> > 43,000 feet. There is a cockpit humidifier switch, and cabin air
> > humidification is fully automatic. Cabin windows are larger than other
> > airplanes, and window shading is electronic. The passenger can select 5
> > levels of shading, from clear to black. The flight attendants can
> > control the cabin lighting temperature - mood lighting - to aid in
> > dealing with changing time zones (evening light after dinner, morning
> > light to wake up, etc.).
> >
> > Much of the cockpit seems like it was designed by Apple. The Control
> > Display Units (CDUs) are virtual, so you can move them from one MFD to
> > another. In fact, you can configure the displays in 48 different ways, I
> > think, though we have found a few favorites we will use to keep it
> > simple. To move the cursor from one MFD to another, you can either use a
> > button, or you can "flick" your finger across the trackpad (Cursor
> > Control Device) to fling the cursor from one screen to the next - much
> > like an iPad.
> >
> > I'm going home this morning, and will return for a 777 simulator ride
> > before I go back to work. They want to make sure we've still got the
> > old-fashioned legacy airplane in our brain before we fly the 777 again,
> > even though it shares a "common type rating". We won't get the first 787
> > until October, and begin operations in November or December. At that
> > time I'll return for at least 4 days refresher training before beginning
> > IOE - initial operating experience in the airplane - with passengers.
> >
> > What a ride. It may be "fuel efficient", but I'm glad someone else is
> > paying for the gas.
> >
> >
> _______________________________________
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-- 
OK Don
2001 ML320
2012 Passat TDI DSG
1997 Plymouth Grand Voyager
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