CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Weight and
Balance Data
Original
6
−
5
Reissue 2
BASIC WEIGHT
AND BALANCE RECORD
(CONTINUOUS HIST
OR
Y
OF CHANGES IN STRUCTURE OR EQUIPMENT
AFFECTING WEIGHT
AND BALANCE)
AIRCRAFT MODEL
MD900
SERIAL
NUMBER
900
−
000XXX
MD Helicopters, Inc.
DA
TE
ITEM NO.
IN
OUT
REGISTRA
TION NUMBER N9XXXX
P
AGE 4 OF 4
DESCRIPTION OF
AR
TICLE
WEIGHT
CHANGE
RUNNING T
O
TA
L
BASIC AIRCRAFT
ADDED (+)
REMOVED (-)
WEIGHT
LONG
ARM
WEIGHT
LONG
ARM
Form HOQ014 (rev 5/00)
12/23/xx
01/09/xx
01/09/xx
X
ACTUAL
BASIC WEIGHT
REVISED
CALCULA
TED BASIC WEIGHT
FIXED
BALLAST
IN NOSE
5.0
87.6
438
3277.8
210.2
689103
210.4
3272.8
688665
f92
−
054
A
OR MOCIFICA
TION
LA
T
ARM
LONG
MOMENT
LA
T
MOMENT
WEIGHT
LONG
ARM
LA
T
ARM
LONG
MOMENT
LA
T
MOMENT
LA
T
ARM
LONG
MOMENT
LA
T
MOMENT
0.4
1465
0.4
1309
Figure 6
−
4. Sample Weight and Balance Record
Summary of Contents for MD900 Explorer
Page 4: ......
