TCDS ATC 197 Menasco: Menasco Manufacturing Super Buccaneer C6S-4

Holder: Menasco Manufacturing Co.
Revision: 0
Status: Current
Product: Engine
Models: 1

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

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Models · 1

Model	Also known as	Note
Super Buccaneer C6S-4

Airworthiness directives · 0

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

No ADs matched this data sheet’s models

STCs approved under this data sheet · 1

STC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.Andrew D. Humphrey

PMA parts · 2

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this data sheet’s models, so check the FAA record before relying on it. Newest first.

UREM40ESpark PlugAero Accessories Inc · PMA PQ1206CE · Replaces Allied Signal (Autolite) Part No. SH… · For Super Buccaneer C6S-4 · Jun 10, 2010 UREM40E URHM40ESpark PlugSlick Aircraft Products, Division of Unison Ind · Replaces SL 20A SL200A Allied Signal (Autolite) · For Super Buccaneer C6S-4 · Jul 1, 1999

What the data sheet saysOCR

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

MODEIS: Menasco Super Buccaneer C6S-4 1.C. NUMBER: ATC 197 Model Super Buccaneer C6S-4 CLAI Fating: Maximum continuous, nf. Ipm, in.Hg., at: Rated pressure altitude (ft.) 260-2300-39 172-7500 s.1. pressure altitude 260-2300-40 1/2-S.L. Take-off (one minute), he, Ipm in.Hg- 290-2400-44 Fuel (minimum octane aviation gasoline) 80 (87 required for take-off (one minute)) Pore and stroke, in. 4.750 × 5.125 [isflacement, cu. in. height (dry), Its. 550 Crankshaft gearing None Supercharging (impeller gear ratio) 10.9:1 Fropeller shatt, SAE NO. CarDuretion stromterg NA-RIA carburetor with 2-7/16 in. venturi Ignition, dual Scintilla MN6-3/4DF magnetos Certification tasis Approved Iype Certificate No. 197 NOTE 1. Maximum permissible cylinder head, barrel and oil inlet temperatures, 550 degrees F., 300 degrees F.r and 200 degrees F.. respectively. NOTE 2. Approval expired 10/7/41. No engines of this model manufactured after this date or with serial nimbers above 6133 eligible for use in certificated aircraft.