Take a look, can we build one?

[GWSimulations]

This is lookin great!

Thanks.

[Alphajet_Enthusiast]

When will this one be ready GW?  :)

[Skligmund]

That is looking great, I can't wait to see the final project.

What else do you need, I was kept from going to Kenai last weekend, and MIGHT go this weekend. If there is anything I can do, let me know, I'll tell you if I can do it.

[GWSimulations]

That is looking great, I can't wait to see the final project.

What else do you need, I was kept from going to Kenai last weekend, and MIGHT go this weekend. If there is anything I can do, let me know, I'll tell you if I can do it.

I really need internal photos, of absolutley everything inside. Especially the cockpit.

If there are any still flying, then a recording of it's engine sounds on startup, running, and on shutdown would be great.

Also, as many pictures of the different liveries as possible.

When will this one be ready GW?

I don't really know. It's just the inside to do. How's the panel, Alphajet?

[Skligmund]

I'll see if I can contact Cape Smythe Air, they still fly 3 or 4 of them. I might be able to get interior pictures from them. As for the audio, it is basicly the same as a Cheyenne less than the IIXL (I, IA and II), so I can probably come up with something there.

If anybody out there has any of this, lease feel free to acknowledge.

[Skligmund]

Engines:

Number of engines: 2
Engine manufacturer: Pratt and Whitney of Canada
Engine model number: PT6A-11
Rated Horsepower: 500
Propeller speed (RPM): 2200


Propellers:

Propeller manufacturer: Hartzell
Blade model: T10173K-8
Number of blades: 3
Hub model: HC-B3TN-3B
Propeller diameter: 93"
Propeller type: Hydaulically operated, constant speed, full feathering, reversible


Fuel:

Fuel capacity (U.S. gal)
With tip tanks: 366
Without tip tanks: 300


Oil:

Oil tank capacity  (each engine) (U.S. gal): 2.3


Maximum weights (lbs):

Maximum ramp weight: 9050
Maximum takeoff weight: 9000
Maximum landing weight: 9000
Maximum zero fuel weight:
With tip tanks: 7600
Without tip tanks: 7800
Maximum weights in baggage compartments:
Foward: 300
Aft with 10th and 11th seats: 100
Aft without 10th and 11th seats: 440
Nacelle (each): 150


Standard airplane weights (lbs):
Standard empty weight: 4729
Maximum useful load (including ramp fuel): 4321


Cabin and entry dimensions (in.):
Cabin width (max): 50
Cabin length (max): 151
Cabin height (max): 51.5
Entry width: 28
Entry height: 46


Specific loadings:
Wing loading (lbs. per sq. ft.): 39.30
Power loading (lbs. per hp): 9.00

[Skligmund]

Airspeed limitations (kias):

Maximum operating speed (Vmo): 227
Design maneuvering speed (Va): 183
Maximum flaps extended speed (Vfe):
15 degrees flap: 174
40 degreesflap: 142
Maximum gear extended speed (Vle): 156
Air minimum control speed (Vmca): 87
Best single engine rate of climb speed: 118
Stall speed (full flaps) (power off): 78
Best multi-engine rate of climb speed (15 degrees flaps): 110
Best multi-engine angle of climb speed (15 degrees flaps): 87
Twin engine approach speed:
With tip tanks: 109
Without tip tanks: 106


Airspeed indicator markings (kias):

Green arc (normal operating range): 86 to 227
White arc (flaps extended range): 78 to 142
Radial red line (minimum control speed): 87
Radial blue line (best rate of climb speed single engine): 118
Maximum operating limit speed (Vmo) shown by red needle

[Skligmund]

Powerplant intsrument markings:

(a) Tachometer (propeller)
Green arc (normal operating range): 1800 to 200 RPM
Yellow arc (caution): 2000 to 2200 RPM
Radial red line (maximum): 2200 RPM
(b) Tachometer (gas generator)
Green arc (normal operating range): 51 to 101.5%
Radial red line (maximum): 101.5%
(c) Fuel pressure
Green arc (normal operating range): 15 to 50 PSI
Yellow arc (caution): 5 to 15 PSI
Radial red line (minimum): 5 PSI
(d) Fuel flow
Green arc: .5 to 5 PPH x 100
(e) Oil Pressure
Green arc (normal operating range): 80 to 100 PSI
Yellow arc (caution): 40 to 80 PSI
Radial red line (maximum): 100 PSI
Radial red line (minimum): 40 PSI
(f) Oil temperature (dual guage)
Green arc (normal operating range): 55C to 99C
Yellowarc (caution): 0C to 55C
Radial red line (maximum): 99C
(g) Inter turbine temperature
Green arc (normal operating range): 500C to 685C
Radial red line (maximum): 700C
(h) Engine torque
Green arc (normal operating range): 0 to 1194 LB-FT
Radial red line: 1194 LB-FT


Let me know if you want CG limitations


Flight maneuvering load factor limits
Positive load factor (flaps up): 3.36 G
Negative load factor (flaps up): -1.35 G
Positive load factor (flaps down): 2.00 G

[Alphajet_Enthusiast]

How's the panel

I started it on my PC back home but I can hardly make out which gauge is which from these distant photographs of the flightdeck... Bigger photos would be great...  ;)

[Skligmund]

I don;t have bigger photos, but I have gauge placement diagrams from the information manual.

Give me a minute, I'll post them in another thread like T-1040 Panel.

[Skligmund]

Also, I'll be out for the next couple of days. My back-up computer let the smoke out, so I'm rebuilding this one, and my better old one. I have parts for almost 4 computers, one blew up, so now I have parts for 3, and I'm rebuilding this one in a new case, and my next slowest one in this case. All hard drives are to be wiped ect.

[GWSimulations]

Alphajet, Please can I include your panel with my model?

[GuitarFreak]

i was wondering if you have the plane done yet

[cspyro21]

Hey GW your model is coming along great. It's a good representation of a nice plane (I see why you like it Skligmund!!)
    I was wondering GW, did you download any program to be able to make the aircraft you make and if so what is it called?
   Thanks
    cspyro21

[GWSimulations]

[quote]I was wondering GW, did you download any program to be able to make the aircraft you make and if so what is it called?