ARP237A: Propeller Control Clearance - Single Acting System Single Rotation Propeller Shaft Reciprocating Engines - Recommended Practice

Features

Issuing Committee: E-25 General Standards for Aerospace and Propulsion Systems

Scope

Content: No Scope available

Rationale

Content: This document has been reaffirmed to comply with the SAE 5-year Review policy.

REFER TO ARP 244 FOR FLANGE INSTALLATION CLEARANCE.

OUTLINE SHOWN COVERS BASIC PROPELLER CONTROL PARTS ONLY. ADDITIONAL CLEARANCE AND ACCESS MUST BE PROVIDED FOR ELECTRICAL, MECHANICAL AND HYDRAULIC CONNECTIONS REQUIRED BY DETAIL PROPELLER EQUIPMENT SPECIFIED.

DIMENSIONS SHOWN REPRESENT MAXIMUM ENVELOPE OF PROPELLER PARTS AS DEFINED ABOVE.

THIS ENVELOPE APPLIES TO CONTROLS FOR USE ON REDUCTION GEAR SECTIONS DESIGNED AFTER DATE OF ISSUE.

Meta Tags

Topics: Propellers and rotors
Technical review
Gears
Parts
Documentation
Tools and equipment

Details

DOI: https://doi.org/10.4271/ARP237A

Pages: 2

Citation: SAE International Recommended Practice, Propeller Control Clearance - Single Acting System Single Rotation Propeller Shaft Reciprocating Engines, SAE Standard ARP237A, Reaf. Nonc. May 2006, Noncurrent August 1973, Issued April 1950, https://doi.org/10.4271/ARP237A.

Additional Details

Publisher: SAE International

Published: May 11, 2006

Product Code: ARP237A

Content Type: Recommended Practice

Status: Reaffirmed

Language: English

Historical