EasyManuals Logo

Piper PA-38-112 User Manual

Piper PA-38-112
213 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #24 background imageLoading...
Page #24 background image
1.3 ENGINE
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model Number O-235-L2C (with Slick Mags.)or
O-235-L2A (with Bendix Mags.)
(d) Rated Horsepower 112
(e) Rated Speed (rpm) 2600
(f) Bore (in.) 4.375
(g) Stroke (in.) 3.875
(h) Displacement (cu. in.) 233.3
(i) Compression Ratio 8.5:1
(j) Engine Type Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
1.5 PROPELLER
(a) Number of Propellers 1
(b) Propeller Manufacturer Sensenich
(c) Model 72CK-0-56
(d) Number of Blades 2
(e) Propeller Diameter (in.)
(1) Maximum 72
(2) Minimum 70
(f) Propeller Type Fixed Pitch
1.7 FUEL
(a) Fuel Capacity (U.S. gal.) (total) 32
(b) Usable Fuel (U.S. gal.) (total) 30
(c) Fuel Grade, Aviation
(1) Minimum Octane 100/130-Green
(2) Specified Octane 100/130-Green
100-Green
100LL-Blue
(3) Alternate Fuels* 115/145-Purple
*Alternate Fuels refers to military grade with 4.6 ml of TEL. See Section
8.25, Fuel System.
PIPER AIRCRAFT CORPORATION SECTION 1
PA-38-112, TOMAHAWK GENERAL
ISSUED: JANAURY 20, 1978 REPORT: 2126
REVISED: MARCH 1, 1979 1-3
1.3 ENGINE
(a) Number of Engines 1
(b) Engine Manufacturer Lycoming
(c) Engine Model Number O-235-L2C (with Slick Mags.)or
O-235-L2A (with Bendix Mags.)
(d) Rated Horsepower 112
(e) Rated Speed (rpm) 2600
(f) Bore (in.) 4.375
(g) Stroke (in.) 3.875
(h) Displacement (cu. in.) 233.3
(i) Compression Ratio 8.5:1
(j) Engine Type Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
1.5 PROPELLER
(a) Number of Propellers 1
(b) Propeller Manufacturer Sensenich
(c) Model 72CK-0-56
(d) Number of Blades 2
(e) Propeller Diameter (in.)
(1) Maximum 72
(2) Minimum 70
(f) Propeller Type Fixed Pitch
1.7 FUEL
(a) Fuel Capacity (U.S. gal.) (total) 32
(b) Usable Fuel (U.S. gal.) (total) 30
(c) Fuel Grade, Aviation
(1) Minimum Octane 100/130-Green
(2) Specified Octane 100/130-Green
100-Green
100LL-Blue
(3) Alternate Fuels* 115/145-Purple
*Alternate Fuels refers to military grade with 4.6 ml of TEL. See Section
8.25, Fuel System.
PIPER AIRCRAFT CORPORATION SECTION 1
PA-38-112, TOMAHAWK GENERAL
ISSUED: JANAURY 20, 1978 REPORT: 2126
REVISED: MARCH 1, 1979 1-3

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Piper PA-38-112 and is the answer not in the manual?

Piper PA-38-112 Specifications

General IconGeneral
BrandPiper
ModelPA-38-112
CategoryAircrafts
LanguageEnglish

Related product manuals