- Holder
- McCauley Propeller Systems
- Revision
- 0
- Status
- Current
- Product
- Propeller
- Models
- 1
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| 2C36C9 | Formerly Cessna Aircraft Co. |
Airworthiness directives · 1
ADs whose products are models on this data sheet, matched by model and maker.
STCs approved under this data sheet · 2
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MacCauley 2C36 Propeller T.C. 895
Type Two-position; hydraulic (See NOTE 3)
Engine shaft SAE No. 4 flange
Hub material Alaminum a. loy
Blade material Aluminum alloy
Number of blades
Hub models eligible 2C36C9 (See NOTE 1) Approx. Maximum
Maximum Diameter Weight Complete (1b.)
Blades Eligible (See NOTE 2) HP Continuous RPM Takeoff RPM (See NOTE 2) Limits (For reference (See NOTE 3) only)
90M-0 225 2600 225 2600 90" - 80" (-0 to - 10) 85
90M-10
Certification basis: Type Certificate No. 895 (Expired September 24, 1958. No propeller of this model
manufactured after that date eligible for use on certificated aircraft.)
NOTE 1: Hub Model Designation. A dash and a letter added to the hub model designation indicates a minor change
NOTE 2: Blade Model Designation. which does not affect the eligibility. ndicates that the propeller diameter is reduce dash and a number (specifying inches) added to the blade model designatior from the design basic diameter specified by the number
of inches indicated. Self-contained hydraulic unit with magnetic control.
NOTE 4, 5, 6, Not applicable.
rable of Propeller-Engine Combinations
Approved Vibrationwise for use on Single-Engine Tractor Aircraft
The maximum and minimum propeller diameters that can be used for a vibration standpoint are shown below.
No reduction below the minimum diameter listed is permissible since this figure includes the diameter
reduction allowable for repair purposes.
Min. Diameter
_(in.)
86