Piper PA-38-112 User Manual

PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: NOVEMBER 2, 1981 6-27
PIPER AIRCRAFT CORPORATION SECTION 6 PA-38-112, TOMAHAWK WEIGHT AND BALANCE ISSUED: JANUARY 20, 1978 REPORT: 2126 REVISED: NOVEMBER 2, 1981 6-27
(m)
Radio Equipment
(Optional Equipment) (cont)
Item Mark if Weight
Arm (In.)
Moment
No. Item
Instl.
(Pounds)
Aft
Datum
(Lb-In.)
227
Transponder Instl., Piper Dwg.
09197-2
or 08388-4
2.2
58.8
129
229
Transponder Instl., Piper Dwg.
09184-2
or 08327-4
3.3
57.2
189
231
Transponder Instl., Piper Dwg.
09191-2
or 08421-4
2.5
61.9
155
233
ADF Instl., Piper Drawing
09191-2
or 08421-3
5.7
84.1 479
235
ADF Instl.. Piper Drawing
09452-2 or 08388-3
5.1
87.4
446
237
ADF Instl., Piper Drawing
09185-2
or 08327-3
6.3
84.1 530
239
Glide Slope/
Marker Beacon
Instl.. Piper Dwg. 09193-2
(Exchange for Nav I Indicator)
0.2*
63.0
13
*Weight and moment difference between Nav I Indicator and Glide Slope Installation.

Piper PA-38-112 Specifications

General

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