Tecnam P92-JS, Руководство по эксплуатации самолета

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F
LIGHT
M
ANUAL
Date : Issue 3: 25
th
May 2010
P92-JS
SECTI ON 6
WEIGHT & BALANCE
6-3
WEIGHING REPORT
Model P92-JS S/N : ________ Weighing n °____ Date :_________
Datum : Propeller support flange w/o spacer. –Equipment list, date: _____
MAC: 1400 mm
Kg meters
Nose wheel weight W
1
= Plumb bob distance LH wheel A
L
=
LH wheel weight W
L
= Plumb bob distance RH wheel A
R
=
RH wheel weight W
R
= Average distance (A
L
+ A
R
)/2 A =
W
2
= W
L
+W
R
= Bob distance from nose wheel B =
Empty weight
(1)
We = W
1
+ W
2
=
D
W A W B
We

  

2 1 m
D
D
%
.
  
14
100
Empty weight moment: M = [(D+1.405)
.
We] = Kg
.
m
Maximum takeoff weight W
T
= 550 kg W
T
= 600 kg
Empty weight We = We = Sign: ____________
Maximum payload W
T
- We Wu = Wu =
1 - Including unusable fuel (2.3 kg).
B
W1
Plumb
L
in
e
A
W2=WL+WR
1405
DA
TU
M
D
Horizontal
Reference