Manufacturer: Cessna
Aircraft Model(s): TP206( ), P206( ), (T)P206A (replaces C58, C79, C90), TU206 (to S/N U20602199), U206 (to S/N U20604074), 206
Applicable Engines: IO-520-A,-F TSIO-520-C,-M
PDF: ( )206( ), P206(A), T( )206( ) 82″, 84″ & 86″
QTY | DESCRIPTION | ITEM # |
1 | 3-Bladed Propeller | HC-C3YF-1RF/F8468A-4R |
1 | Polished Spinner | A-2295-1P |
1 | STC Document Set | SA02752CH-D |
QTY | DESCRIPTION | ITEM # |
1 | 3-Bladed Propeller | HC-C3YF-1RF/F8468A-2R |
1 | Polished Spinner | A-2295-1P |
1 | STC Document Set | SA02752CH-D |
QTY | DESCRIPTION | ITEM # |
1 | 3-Bladed Propeller | HC-C3YF-1RF/F8468AR |
1 | Polished Spinner | A-2295-1P |
1 | STC Document Set | SA02752CH-D |
Applicable Models:
Floatplane Props (84 & 86″) 206, P206(A), U206-U206F & U206G thru s/n U206004074, TP206A, TU206A-TU206E & TU206F thru s/n U20602199
Landplane Prop (82″) 206, P206A, U206, U206A, TP206A, TY206A through TU206F through s/n 20602199
Note: Replaces short hub C58, C78, C79, C90, and C230 only.
Specifications:
84-86 inch diameter 3-bladed, short aluminum hub propeller
2400 hour / 6 year TBO
82.4 / 82.6 pounds (propeller and spinner)
Two inch diameter reduction allowable
Maximum RPM 2700
-TU206C,D,E and F using 86″ diameter prop are limited to 2690 RPM under this STC for noise certification.
-U206B thru U206G using IO-520-F engine, take-off and max continuous RPM is limited to 2700 RPM
**See below under notes for specific placard information
Replaces:
McCauley C58/C78 – 82-88 inch diameter 2-bladed prop
Oil fill requirement per AD 91-15-04
1200-1500 hour / 5 year TBO
McCauley C79/C90 – 80 inch diameter 3-bladed prop
Oil fill requirement per AD 91-15-04
1500 hour / 6 year TBO
Advantages:
vs. McCauley C58/C78 2-bladed models
Better take-off performance
Longer TBO
Current design, Mc threaded design obsolete
vs. McCauley C79/C90 3-bladed models
Better take-off performance
9.5% decrease in time to accelerate to 60 MIAS
Current design, Mc threaded design obsolete
vs. All models – 3% decrease in engine out glide distance
Notes:
Placard (normally aspirated engines):
“Continuous operation is prohibited above 26 inches MP between 2250-2450 RPM”. Applies to 86″ diameter propeller only.
Placard (turbo-charged engines):
“Continuous operation is prohibited above 28 inches MP between 2250-2450 RPM”. *Applies to 86″ diameter propeller only.
No Placards apply to 82″ or 84″ diameter propellers
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