Kingair 200/350 Start up sequence
 

Hey guys

This question would mainly be directed towards kingair pilots who know the a/c well...My question is this:Why when a 200/350 starts up,the right condition lever is put into low idle first,and then into high idle when starting the left engine?
It may be a daft question to ask,but Im just curious...So..what would happen if you did not move the condition lever to High Idle when starting the left engine?
And What would happen if the left engine was started first?
These are just curious thoughts that crossed my mind today...
Thanks for helping out :ok:
Daniele

Daniele,

Whilst I am by no means experienced and I fly the King Air 90, we have exactly the same start sequence. I was taught that you start the right engine first and place the right condition lever into high idle after start to provide a greater electrical output from the generator to assist with starting the left engine.

So long as I have decent battery voltage I tend to alternate starting left and right engines first and have never had any issues. I have played about with this a bit and have typically found that after the first flight of the day I don't need run the RH engine up to high idle before starting the left, with no negative impact on the start and ITTs, although I definitely needed to run the RH engine up to high idle this morning as the aircraft had been left out in the cold all night!

Also, I was told that the checklist specifies the right engine to be started first as the battery compartment is in the right wing (at least on the King Air 90, not sure about the 200/350) and so there is less resistance due to the cable length being shorter to the right engine.

Hope this helps!

Kind regards,


Adrian

hey Adrian.

Your answer is kind of what I expected to hear.I just had no idea whether or not it would have a negative effect on the engines itself.But never the less,atleast I now know!;)
Thanks for your reply.:ok:

I have 4000+ hrs on the KingAir, mainly the B200, few on F90s, C90A and C90B...none on the 350.

IMO there is no need to place it to low and then go to high. I always put it directly to high idle. And doing so has indeed to do with the relatively great strain the generator puts onto the engine. In low idle this would mean higher ITT than in high. I also alternate the starters, I do have the impression to equalize the high stress the first starter/gen has to bear...although there are people that never do that and their genies last as well...

Never forget to check you current limiters on the 200 after start...

The only reason to start right first is the somewhat shorter way from the battery to the starter, this might play a role with very low temperatures, less voltage drop, thats the only time I´d use R/H first. (athough I think this is more or less academic...cause in very low temps one should use a GPU anyhow)

The last KingAir I flew a lot was 1478 (4-Blade-prop), that had already electric heat (not radiant) Electric heat uses something around 80 amps and if you use it in low idle you can actually see the difference in ITT (hotter). So going and staying in high not only gives you more bleed air then but also a cooler ITT.
When you start in hot conditions, the R/H engine provides for the A/C, therefore you´d need this one in high idle anyways (63% min IIRC). Taxiing with on in high and one in low I found not practicable, so both go to high.

I also land in high idle and props fully forward. Pros IMHO: already somewhat spooled engine in case of a G/A, more readily available reverse and the short field technique practised....

Regarding the 90...its a considerably smaller engine. I would not recommend use of low idle for cross starts.

The reason for starting the starboard engine first was historically more to do with cooling the battery than anything else. This reason has become obsolete due to modern batteries.

The modern 90 does not require high idle for cross starts.

goodday HD

Thanks for your input...SO I assume that with regards to the starts,If you engage the gen while on low idle your ITT will peak?I was reading an article (cant remember the site) which stated,"If you engage the generator and AC system while in low idle,you can expect the ITT to over temp."Not 100% clear on this if this is true or not..But it would make sense with regards to a higher fuel flow..?
Also,Is it recommended to start the 200 with props feathered?But then if so,you torque will definitely peak to its limits.Not so?
Daniele

...and perhaps the fact that the AC-compressor is powered by the starboard accessory gearbox. So if your cabin is a little to "toasty" you can cool it down while you wait for your pax. That's the story that was sold to us by FSI, although we operated in a not-so-tropical climate! :E

DK :rolleyes:

I engage the GEN when the engine has reached high idle.(I go direct from cut-off into high idle)
The whole idea basically is to have as little ITT spikes/transients as possible. If you´d go with the CL, you´d spike on the low idle niveau, engage the GEN, then go to high idle with another spike of ITT. These ideas stem from a former Beech engineer who was involved in the B200 development, later was (maybe still is) a freelance trainer for conversion on the airplane. The person that trained me was trained by this guy...

The AC system clutch won´t engage in low idle (n1 speed switch, below 62% -> triggers the AIR COND N1 LOW light). If it would the ITT would be higher for sure. Anything that draws power will increase the ITT.
The engine is made to work above 90% really, anything below means that the airflow is not optimal...thats why the compressor bleed valves (P2.5) are put on the engines.

Any power demand to the engine in lower n1 will result in a ITT raise, this raise will be higher the lower the engine n1 is.

No and no. The only time I ever started a KA with props in feather was on a very slippery apron. I do know some guys that do start regurlarly in feather but I don´t know the reason...
If you can feather the prop in regular idle without overstressing (too high torque) why should there be an overtorque situation when starting?

Another reason for starting RH first is the simple fact that the door is on the left, I was told once...

hi guys

Thanks for the replys...I am Learning alot more than I originally thought I would.BUT,here's another one:The auto feather switch:if armed,the minute you have an engine failure,will it automatically feather the props?
And another thing I read on a website,which stated,"Disengage the prop sync BEFORE adjusting throttles/power levers."If you do not disengage the prop sync and you increase/decrease power,what is the worst that can really happen?Maybe just damaging the prop sync?
Daniele:ok:

is it only me who always has to laugh when the first words of an reply are a proud report of its own virtual logbook without being asked for this ? :E

daniele - yes, autofeather will feather automatically and senses the torque drop, you will not damage the syncrophaser but it may try to regulate more or less violently when adjusting engine settings with prop synchro on.

cheers !

I leave prop sync engaged while making power changes, but I move the levers slowly enough that I can manually keep in sync during the change.

Prior to start I set the L. volt/ammeter to volt, and the R. V/Ammeter to Amps after checking Voltage. I start the R. engine first because it's closest to the battery and minimises voltage drop. I go straight to High Idle after a very low idle and then switch on the R. Gen. High idle is to keep temps as low as possible. Then I wait for <50% load (125 Amps), but preferably under 90-100A. If environmental temps aren't pleasant then I also run the aircon (it's on the R. engine) while waiting. Can't put the aircon on with <62% so that's another reason for high idle.

Then R. Gen OFF, start the left engine with R. Gen ON after light-off. Before switching the L. Gen ON, I check for 28V on the L. bus. That way I can tell if the current limiter is still OK.

There are 2 synchrophasing systems, the type 1 installed on airplanes up to BB-935 and the type II installed afterwards. Basically you can leave the type II on all the time, although its probably good airmanship to switch it of off for starting, takeoff and landing. Certainly if you fly both systems, cause thats what the checklist says for the type I.
Generally speaking, the type I manipulates only the R/H props RPM which is considered the slave, and the type II works on both props, adjusting whichever is the slower one to match the faster (within a limited range of course). So the type I makes the prop slower or faster, the type II only can make the slower one faster. When there is an engine failure on the left (master), then - when switched on - the type I will decrease the RPM of the right engine by its modulating range, trying to follow the dropping RPM of the master. Hence it should be off on the ground, durning T/O and LDG and one should manually synchronize before switching it on.

Regarding autofeather, it will start to work when the non-operating engines torque drops below 200ft/lbs -> then a valve is openend and dumps the oil from the prop -> thus feathering it. Before that, at 400 ft/lbs, the opposite site is disarmed (the Auto Feather light extuinguishes), the light of the auto - feathered engine goes out passing the 200ft/kbs threshold. So if you have an autofeather happening, there is no indication other than the prop windmills...

Regarding starting, there is a few things to be considered:

first of all, what type of battery is installed:

1) NiCad, used to be the standard up to.... BB1631, but there are aircraft that were converted to:
2) lead- acid, standard an BB1632 and on.

The converted ones should have the battery charge light removed and also the cooling intake below the battery on the R/H wings underside might be removed.

There are also 2 types off generators put on the airplane, the standard being 250 Amps gens and optional 300 Amp gens. (Note: the amp meter reading is always 100%=250Amps)
The regular procedure for NiCad batteries used to be: start first engine, switch generator on, load battery to below 50%, switch the gen off again, start second engine and going through 12% n1 switch gen back on.

Later models did not require the first gen to be switched off. (not sure an the serial number there...have a look in the checklist, if its properly updated you should see it in there. Definitely not required on BB1476 and on)

So start first engine, switch on gen, load to 50%, then start second engine. Perform current limiter check before switching on second gen (push for Voltage on second side and check for 28 V, if readout is 24 V -> opposite side CL blown, if 0 -> onsite CL blown)

On the lead acid battery I was told you start one after the other and also leave the gen of the first one on, no need to wait. The main reason for that is as far as I know that the temperature rise in the lead acid does not mean anything vs. the possible thermal runaway of a Nicad. One should not take off with a load of more than 10 amps on lead acid batteries or a BATTERY CHARGE light on with Nicads.

the gents who state they start up their king air 200 pt6 going entirely to high idle from cutoff . could you just for interest report how much fuel flow you read , when and how the fuel flow develops and whatkind of temps you read on such a startup ? thanks much

I must agree. I've got 10,000+ hrs but none of it on the King Air. I do have nearly 300 hours on PPRuNe ;)

I think you only start the right engine first if you're in the northern hemisphere with your back to the wind.

Thanks for the replies everyone...
This Has helped alot..I'll be posting a few more questions on pprune sometime soon,so keep a lookout.
Thanks again everyone.
Daniele:ok::ok:

Hi Dudeness correctly points out that later models do not require the Gen to be turned off before second engine start, permitting a Generator Cross Start. I believe this only applies to aircraft with the 5 bus electrical system. However on the 90 I fly, this puts extremely high loads on the operating generator which I doubt does it any favours.

According to at least one guy (to whom I think His Dudeness referes in an earlier post... wrote a book, no?) on models with the older electrical system you can do Generator Assisted starts, whereby you turn off the Generator after charging the battery, get the second engine turning on the starter, then switch on the generator of the already running engine.

h

thats basicly correct on any pt6a driven aircraft, not only kingair.but his dudeness , really should describe us how he starts a pt6a with going from cutoff to high idle immediately. i questioned him but somehow memory seems to fade here. i,m wondering how fuel flow and ITT devolop in such a startup :ok:

In Response to aerobat77
On the PT6 the FTG contains Py putting pressure on the pneumatic bellows allowing fuel through the FCU, on initial startup, you are on the Min Flow valve/FCU bypass. As Py builds the bellows allow some flow through the FCU, through approx 40-45% the secondaries open, and "at least on the -67" at about 60% N1 allow full operation of the FCU. At least that is my experience.

As far as the OP's question, the start gen has a limit for internal cooling. I will have to dig out the book, but something like more than 50% load on the -67 requires 72%N1

yeah right, but the question to the other guy with his cutoff-high idle immediately startup what readings on fuel flow he has on the gauge.

does the flow rise steadily as the engine spools or does the needle jump from zero to idle flow when you put in the condition lever ...?

cheers