The dominance of any branch of the Philippine government is a threat to both principle of separation of powers and independence of each body which may lead to a constitutional crisis. Seve…Full description
Lesson for f&e.
Mass and Balance QB
Material and Energy BalanceFull description
This pdf condenses in two pages the entire knowledge necessary to pass the JAR ATPL exams on Mass and Balance. Find more information and other subjects on www.ATPLessentials.com. Feedb…Descrição completa
R22 ALPHA, BETA AND BETA II CENTER OF GRAVITY LIMITS
Weight and Balance Worksheet Robinson R22 (Alpha, Beta and Beta II)
A CG Longitudinal
A
x CG/ARM (in) =
Basic Empty Weight
x
Passengers & Bags
x
79 C
(without fuel weight)
Box (C) to Graph (A)
=
2) Main Tank (19.2 gal)
x
108.6
=
3) Aux Tank (10.5 gal)
x
103.8
=
Total 1/2/3 W&M Only
D
(with fuel weight)
Box (D) to Graph (A)
WEIGHT (lbs)
x CG/ARM (in) =
Basic Empty Weight
x
Right Seat (+)
x
10.7
=
Left Seat
x
-9.3
=
(-)
E
(without fuel weight)
Box (E) to Graph (B)
5) Main Tank (19.2 gal)
x
-11
=
6) Aux Tank (10.5 gal)
x
11.2
=
B
F
(with fuel weight)
Box (F) to Graph (B)
Weight and Balance Info for R22 Alpha, Beta and Beta II
Max Gross Weight
MOMENT (in-lbs)
=
4) Total W&M Only
Total 4/5/6 W&M Only
MOMENT (in-lbs)
=
1) Total W&M Only
CG Lateral
B
WEIGHT (lbs)
Formulas 1370lbs.
Aircraft
WxA= M
Min Gross Weight
920lbs.
M / W = A (CG)
Max Per Seat & Bags
240lbs.
CG = ARM
Max Bags Under Seat
50lbs.
Min Mi n Sol Solo o Wei Weigh ghtt (wit (with h Au Aux x Tan ank) k)
135l 13 5lbs bs..
Main Tank (19.2gal)
x
6.0 lbs
=
Min Solo Solo Weight Weight (without (without Aux Aux Tank) Tank) 130l 130lbs. bs.
