Piper PA-38-112 User Manual

SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-28 REVISED: JUNE 30, 1981
SECTION 6 PIPER AIRCRAFT CORPORATION WEIGHT AND BALANCE PA-38-112, TOMAHAWK REPORT: 2126 ISSUED: JANUARY 20, 1978 6-28 REVISED: JUNE 30, 1981
(m)
Radio Equipment
(Optional Equipment) (cont)
Item
Mark if
Weight
Arm (In.) .
Moment
No.
Item
Instl.
(Pounds) Aft Datum
(Lb-In. )
241 Glide Slope Instl. (Collins),
Piper Dwg. 09199-2 (Exchange
for Nav 1 Ind.)
2.3*
48.1 III
243 Marker Beacon Instl., Piper Dwg.
09187-2
or 09598-2 or 08327-2
Q.6
63.0 38
245 Marker Beacon InstL Piper Dwg.
09201-2
or 08388-2
0.7 63.0
44
247
Encoding Altimeter Instl., Piper
Dwg. 09127-0
or -2 (United) or
08331-2 or 08331-4 or 08331-6
1.9
63.0
120
249 Encoder Instl. - Blind
Piper Dwg. 09612-2 (United)
or
08331-3 or 08331-5 or 08331-7
1.5
47.0 71
*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