Piper PA-38-112 User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-20 REVISED: JANUARY 15, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-20 REVISED: JANUARY 15, 1981
(g)
Engine
and Engine Accessories
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
1:nstl.
(Pounds)
Aft
Datum
(Lh-In.)
89
Engine Primer Pump**
Essex K2406-SAE-2
0.4
24.4
10
90
Oil Cooler Instl.
Piper Dwg. 77896-2
4.0
33.5
134
(h)
Propeller and Propeller Accessories
(Optional Equipment)
Item
Mark if
Weight
Arm (In.)
Moment
No.
Item
Instl.
(Pounds)
Aft
Datum
(Lh-In.)
(i)
Landing Gear and Brakes
(Optional Equipment)
Item
Mark if Weight Arm (In.) Moment
No. Item
Instl. (Pounds)
Aft
Datum
(Lh-In.)
103
Toe Brakes (Dual),
Piper Dwg. 77825-3
& 77918-3
7.6* 49.4
375
*Right and Left
**Optional
on aircraft with serial nos. 38-78AOOO I through 38-78A0844. All aircraft included the engine primer

Piper PA-38-112 Specifications

General

Brand	Piper
Model	PA-38-112
Category	Aircrafts
Language	English