TCDS P-861

Type certificate data sheet · Sensenich Propeller Manufacturing Company Inc. · Propeller

Holder
Sensenich Propeller Manufacturing Company Inc.
Revision
6
Revised
November 1, 1968
Status
Current
Product
Propeller
Models
3

The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.

On this page

Models · 3

ModelAlso known asNote
CS-2FM4
CS-2FM6
CS-2FM5

Airworthiness directives · 2

ADs whose products are models on this data sheet, matched by model and maker.

What the data sheet says

From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.

Page No. 1 2 Rev. No. 6 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION P-861 Revision 6 SENSENICH CS-2F November 1, 1968 TYPE CERTIFICATE DATA SHEET NO. P-861 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate No. P-861) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations/Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Sensenich Corporation Lancaster, Pennsylvania 17604 Type Hydraulically controllable, two-position manual (see Note 3) Hub material Steel Blade material Vertical laminated birch with steel ferrule fastened to shank with leg screws. Plastic covered with metal tipping. Number of blades Two Hub models eligible CS-2FM4, CS-2FM5, CS-2FM6 Blades Eligible Maximum Continuous Takeoff Diameter Limits Hub and Blade Weight (See Note 2) HP RPM HP RPM (See note 2) Max. Dia. PC-276A6-0 to PC-276A6-6 112 2665 115 2875 76" - 70" (-0 to -6) 27 lb. PC-276A7-0 to PC-276A7-6 112 2665 115 2875 76" - 70" (-0 to -6) 27 lb. Certification basis Type Certificate No. P-861 dated September 8, 1947 Date of application for Type Certificate August 1, 1947. Production basis Production Certificate No. 1 NOTE 1. Hub Model Designation Hub model designation CS - 2 F * 1 - 1 First minor design change First major design change * B indicates SAE No. 1 flange * M indicates SAE No. 2 flange Flange type of engine shaft adaptation Sensenich blade shank size Constant speed Hub details P-861 2 Model Bolt Circle Diameter No. of Bolts Bolt Hole Diameter Bolt Diameter CS-2FM4 4-3/4" 6 41/64" 5/8" (bushing) CS-2FM5 4-3/4" 6 41/64" 5/8" (bushing) CS-2FM6 4-3/4" 6 41/64" 5/8" (bushing) NOTE 2. Blade Model Designation Blade model designation P C - 2 76 A 6 - 6 Number of inches cut off (or added to) basic propeller diameter. Dash for subtraction from basic diameter (plus sign for addition to basic diameter. Sixth major change Type of blade centerline arrangement. Basic propeller diameter in inches. Sensenich blade shank size. Controllable pitch Plastic covered blade NOTE 3. Pitch Control (1) Eligible as manual two-position; or manual controllable with Sensenich Model L-2160 hydrocontrol valve. (2) For constant speed use only Woodward Governor Models X662-04 and X662-010, Weight 2.0 lb. NOTE 4. Feathering Not applicable. NOTE 5. Left-Hand Models. The letter "L" preceding the hub and blade designations indicates left-hand models which are eligible at the same rating and diameter limitations as listed for the right-hand models. NOTE 6. Interchangeable Blades. All blade models contained in this data sheet are interchangeable, but only identical models can be paired in the same hub for reason of balance. NOTE 7 & 8. Not applicable. NOTE 9. Approved Installations. Intentionally left blank. NOTE 10. The word "eligible" as used herein does not signify approval. For approval, compliance with the applicable aircraft airworthiness requirements is necessary. ....END.....