North America:1 (800) 942-7767 International:+1 (937) 778-4200
Search

( )206( ), P206(A), T( )206( )

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″

82″ Kit (Landplane) Includes:

QTY DESCRIPTION ITEM #
1 3-Bladed Propeller HC-C3YF-1RF/F8468A-4R
1 Polished Spinner A-2295-1P
1 STC Document Set SA02752CH-D

84″ Kit (Floatplane) Includes:

QTY DESCRIPTION ITEM #
1 3-Bladed Propeller HC-C3YF-1RF/F8468A-2R
1 Polished Spinner A-2295-1P
1 STC Document Set SA02752CH-D

86″ Kit (Floatplane) Includes:

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

Interested in more information? Fill out the form below and we’ll contact you shortly.

Hartzell Propeller