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APU Operations

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400A

Well-known member
Joined
May 26, 2003
Posts
1,760
I am looking for some advice on APU operation. I would like thoughts from Hawker and Non-Hawker Operators. Ours is available in flight, so here are the questions I have.

Start up and Shut down Altitudes?

Generator on or off?

Shut down Loaded? Gen, or Gen and Bleed?

Any other tips are welcome. Thanks
 
A lot of that stuff is very specific to the APU and the airframe; your plane's manual is where I'd start for that.

On the Excel, we can start it at or below 20,000, run it at or below 30,000, and we're supposed to start it and shut it down totally unloaded.
 
A lot of that stuff is very specific to the APU and the airframe; your plane's manual is where I'd start for that.

On the Excel, we can start it at or below 20,000, run it at or below 30,000, and we're supposed to start it and shut it down totally unloaded.

I am very aware of the Limitations, but there are different schools of thought even from the instructors as far as daily ops. The Generator for example. After start up on the Hawker you do a Gen Amps/Volts check that requires you to trip the APU Generator. Some say leave it off to protect it in the event of a spike, and some say put it back on line.

Hawkers take of with the APU Bleed for Pressurization and then you open the Main Air Valves. They can only all three be on for 1 minute. Some people are just shutting the APU down at that point (Loaded) and others including myself, close the apu bleed valve, insuring I do not get a bleed valve fail, and then shut the APU down later.

We ave the same APU as the Excel, I think, (GTCP-150) and the Manufacturer recently sent out a "recommendation" to shut it down fully loaded.

These are the kind of tips I am looking for.
 
The Hawker 800a I fly has the old 30-92c model. That thing won't run in the air so no question. As soon as weight is off wheels it shuts down. We shut it down unloaded. Wish I had one of those 150's. Have a good day everyone.
 
Challenger 604
APU bleed on/open for takeoff, generator off, shut down once flaps up (unloaded).
After landing we start the APU and transition to APU bleed and generator, as our packs are high flow with the APU. We shut the APU down (post flight) loaded with bleeds open as per Bombardier.
 
Hawker
APU GEN TRIP, APU BLEED AIR ON
DEPART
MAIN AIR VALVES TO LP
APU BLEED AIR OFF
LARGE RUSH OF AIR (TO AVOID BUMP)
MAIN AIR VALVES TO HP
CLIMB CHECKS, SHUT DOWN APU
 
Falcon 2000:

Push the green button and let the ECU do the rest!

Never operate it in flight, although you can below FL350 (yea, right!)
 
CE 750 Typically turn off climbing through 10,000 and on descending through 10,000. The ECU does the job wait for the amber bleed air light, then bleed air off.
 
Lear 60, push the start button, and let the computer do the rest. Shutdown, press the stop button.

Ground-only unit.

Previous life in the airlines, start was automatic, and shutdown was on a load-shed timer...so that unit would shutdown after unloading and cooling.

Inflight use of that unit was at our discretion and subject to the needs at a particular gate or airport and or length of taxi, etc...

Always used to take off and landings in low vis/auto land environment.

But in the end, we did what the checklist told us to. We never re-thought that sort of stuff. Changes to SOP's came several pay-grades above ;-)
 
XP via the checklist FOM limitations and transition in the early part of the flight

800A apu goes off during the line ups and valves come on right after takeoff. Now, if it's super, super hot I have knows pilots that'll takeoff with the main air valves open and have a hair trigger there to close them in the event... The Solar will run in flight but it's easier to explain the air valves on oops than a burping, smoke blowing, mis adjusted apu on takeoff.
 
Gear Up! has it right on. Also, I would never start the APU on descent because if something were to go wrong during the start (which happens quite frequently) it can take your attention away during a critical phase, as well as put alot of fire and hot air in the tail section during approach (apu fire on short final once, not fun).

You have plenty of time to start the APU on the ground after landing.

Also, another rule of thumb learned from experience is never leave the airplane with the APU air on. Sitting on the ramp one time, pop, pop, pop, I notice a bunch of breakers popping. Go outside and open up the hell hole and bang, a bleed air leak is basically melting the tail cone. I shutdown the APU before any real damage occurred. If I hadn't been there, it would have been a total loss of the airplane due to fire. Lesson learned.
 
Doi you wash your airplane? if so, turn the APU off below 4000msl, or the tail will turn black. Also, if you have the APU on, turn on the gen. That wat if you lose a generator on t/o, you will not load shead. Our APU doesn't pressurise the cabin as well as the engine bleads, so in flight, your ears pop a little faster. Use your own judgement when to turn it off.
 
XP
Descending through 4000 FT
APU ON (Let spool up)
CABIN RATE SET TO ZERO
MAIN AIR VALVES CLOSE, (AT SAME TIME) APU BLEED AIR ON
(THIS TAKES CARE OF ANY CABIN DUMP)
 
DA-900B and 50EX, APU approved for ground operation only. We start it 45 minutes prior to departure (start unloaded), usually shut it down on the after start checklist (shut it off loaded).

We start it again on the after landing checklist.
 
I am looking for some advice on APU operation. I would like thoughts from Hawker and Non-Hawker Operators. Ours is available in flight, so here are the questions I have.

Start up and Shut down Altitudes?

Generator on or off?

Shut down Loaded? Gen, or Gen and Bleed?

Any other tips are welcome. Thanks

APU is shutdown after takeoff once main air valves are fully open
APU is started around 10 minutes out on descent

Generator is off for takeoff (tripped before bus tie check and stays tripped)
Generator is on for landing

Shutdown loaded, GEN & Bleed.
 
APU is shutdown after takeoff once main air valves are fully open
APU is started around 10 minutes out on descent

Generator is off for takeoff (tripped before bus tie check and stays tripped)
Generator is on for landing

Shutdown loaded, GEN & Bleed.

For Hawker specifics, There was a debate during school, and I am still leaning away from shutdown with the bleed on, because if you get a bleed valve fail light during the shut down it was my understanding from school that you could not leave the main air valves on with that valve stuck open and therefore now you are committed to unpressurized flight. If the Valve was stuck open then you could at least continue below 30,000 ft pressurizing with the APU. Thus I always make sure to close the valve and make sure it closed before killing the APU. As you know, this is not covered in the checklist. I do not have the APU section of the AFM here at the house. Did I Misunderstand something? Back to back initials is enough to confuse anyone.
 
I love those school debates. It got so bad on Falcon 2000 that Honeywell sent out a letter telling everyone not to mess with it.

Just push the grren button and let ECU do the rest.
 
I love those school debates. It got so bad on Falcon 2000 that Honeywell sent out a letter telling everyone not to mess with it.

Just push the grren button and let ECU do the rest.

No Green Button on the Hawker. Not that simple in my opinion.
 
For Hawker specifics, There was a debate during school, and I am still leaning away from shutdown with the bleed on, because if you get a bleed valve fail light during the shut down it was my understanding from school that you could not leave the main air valves on with that valve stuck open and therefore now you are committed to unpressurized flight. If the Valve was stuck open then you could at least continue below 30,000 ft pressurizing with the APU. Thus I always make sure to close the valve and make sure it closed before killing the APU. As you know, this is not covered in the checklist. I do not have the APU section of the AFM here at the house. Did I Misunderstand something? Back to back initials is enough to confuse anyone.


If you get the APU bleed valve fail light DURING APU ops you're not supposed to open the main air valves. This is because you dont know the position of the APU bleed valve (could be open, closed, or partially open) which could cause damage...same reason why there is the 1 minute limitation of having the main air valves open and the APU bleed on.

When you shut it down loaded you'll get the bleed valve fail light, but because it's not running anymore producing air, you wont cause any damage. Then when you go to start it on the other end of the flight you will be good to go because you will have turned the APU master off, then on, the APU GEN switch off, and the APU bleed switch off.

I think the AFM recommends it to be shut down loaded but I dont have it with me.
 

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