Cessnaflyer
Wooooooooooooooooooooooooooooooo
Is there an STC out there to put a +200 HP engine into a 172RG to make it a high performance aircraft?
Its the perfect opportunity for you to develop the STC for one. Spend about $1M doing the engineering and testing, then sell the STC for $10k a copy and you'll only end up losing about $990,000 on the deal when its all said and done.Shoot! It's a perfect opportunity to finally get a HP airplane without having to buy one. I am surprised there isn't anything.
Is there an STC out there to put a +200 HP engine into a 172RG to make it a high performance aircraft?
I have flown a C-172 with 210 HP, no shoot about it.
Its the perfect opportunity for you to develop the STC for one. Spend about $1M doing the engineering and testing, then sell the STC for $10k a copy and you'll only end up losing about $990,000 on the deal when its all said and done.![]()
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By the time you waste money doing that why not just get a 177RG/182RG/early210???? Assuming you love cessna products that much.
182 or a 210 wouldn't be easier to obtain?
But a 172RG is not really 172. It is actually typed as a 175.
Well there has been a little incident by a renter and we need a new engine and prop...
182 or a 210 wouldn't be easier to obtain?
what about an stc for a turbocharger?
From the Type Certificate Data Sheet:
IX. Model 172RG, Skyhawk RG, 4 PCLM (Normal Category) (cont'd)
Propeller and propeller 1. McCauley constant speed propeller
limits (a) B2D34C220 hub with 80VHA - 3.5 blades
Diameter: not over 76.5 in., not under 75.5 in.
Pitch settings at 30 in. sta.:
Low 12.0°, high 26.5°
(b) Governor
(1) McCauley C290D3/T18
(c) Spinner, Cessna Dwg. 2450002
*Airspeed limits Maneuvering 106 knots
(IAS) Maximum structural cruising 145 knots
(See Note 7 on use of IAS) Never exceed 164 knots
Flaps extended 100 knots
Landing gear extension 164 knots
C.G. range Normal Category
(+39.5) to (+46.5) at 2650 lbs.
(+36.0) to (+46.5) at 1950 lbs.
Straight line variation between points given.
Moment change due to retracting landing gear +2424 in.-lbs.
Empty weight C.G. range None
*Maximum weight 2650 lbs.
Ramp weight 2658 lbs.
Number of seats 4 (2 at +34 to +46, 2 at +73)
Maximum baggage 200 lb. (+95)
Fuel capacity 66 gal. (two 33 gal. tanks in wings at +48.0) (62 gal. usable)
See Note 1 for weight of unusable fuel.
Oil capacity 8 qt. (-17.4) (5 qts. usable)
Control surface movements Wing flaps Up 0° Down 30° +0°, -2°
Ailerons Up 20° ± 1° Down 15° ± 1°
Elevator tab Up 28° + 1° -0° Down 23° + 1° -0°
Elevator Up 28° + 1°, -0° Down 23° + 1°, -0°
(Neutral position measured
with the bottom of the balance
area flush with the bottom of
the stabilizer)
Elevator tab Up 22° + 1°, -0° Down 19° + 1°, -0°
Rudder Right 16° ± 1° Left 16° ± 1°
(Measured parallel to W.L.)
Serial numbers eligible Model 172RG: 172RG0001 through 172RG0570 (1980 Model)
691, 172RG0571 through 172RG0890 (1981 Model)
172RG0891 through 172RG1099 (1982 Model)
172RG1100 through 172RG1144 (1983 Model)
172RG1145 through 172RG1177 (1984 Model)
172RG1178 through 172RG1191 (1985 Model)
I'm sure you can go over to Felts and use their C182RG