Daher TBM 960 - Page 573

Figure 6.4.1 - Example of Weight and Balance Report and Basic Airplane
Characteristics (m, kg)
SAMPLE
REGISTRE INDIVIDUEL DE CONTRÔLE
INDIVIDUAL INSPECTION RECORD
WEIGHT AND BALANCE REPORT
6-SEAT CONFIGURATION
TBM 700
S/N :
F :
8
Re f. 0
d
0
d
1
d
2
P
1
P
2
/ P
3
d
1
= 2.985 m (117.5 in)
d
2
= 5.297 m (208.5 in)
Levelling : Seat rails
Front wheel
Left and right
Wheel points
LIMITATION
ONLY FOR INFORMATION, REFER TO
LIMITATIONS SECTION 2 OF POH
Maximum takeoff weight : 3,454 kg
Maximum landing weight : 3,225 kg
H
Balance
( landing gears down and flaps up )
2,835 kg 18 to 35.5 %
3,186 kg 23.8 to 35.4 %
3,354 kg 23.8 to 35 %
3,454 kg 34.4 to 34.7 %
H
WEIGHING CARRIED OUT ON JACK POINTS
Painted airplane
With engine oil
Gross
Weight ( kg )
Tare
( kg )
Net
Weight ( kg )
Left point
Right
point
Front point
785.8
825.0
507.7
P2
P3
P1
Weight P0 ( kg ) = 2,1
18.5
DISTANCE FROM C.G.
T
O REFERENCE
d0 =
( P1 x d1 ) + ( P2 + P3 ) x d2
P0
d0 =
(507.7 x 2.985) +
(785.8 + 825) x 5.297
2,118.5
= 4.743
CORRECTIONS
Weight
( kg )
Arm
( m )
Moment
( m * kg )
Weight P0
Paint
(2)
Engine oil
(3)
Unusable fuel
2,118.5
30.0
11.2
27.2
4.743
4.873
2.090
4.700
10,048.0
146.2
23.4
127.8
RESULTS W: 2,145.7 D0: 4.742 M: 10,175.89
BALANCE
MAC ( % )
CG =
D0 - 4.392
1.51
x 100
CG =
4.742 - 4.392
1.51
x 100 = 23.2
BASIC INDEX CALCULATION
See section 6 of Pilot's Operating Handbook
Empty weight ( W ) : 2,145.7 kg
Balance ( CG ) : 23.2 %
Moment ( M ) : 10,175.89 m*kg
(1a)
(1c)
(1b)
DESCRIPTION OF 6-SEAT CONFIGURATION :
• Application of Modificati
ons described in the chapter F11 (Modification Status) of this
RIC.
• Application of Options described in the chapter F5 (Description of optional
equipment) of this RIC
• Aircraft ground equipement kit installed in the front baggage compartment.
• Seats protections and carpet protections not installed.
• Freight nets and freight carpets not installed.
• Kit for 4-seat configuration not installed.
1 - Scratch useless mention.
2 - V
alues not taken into account if the airplane was painted
when weighed.
3 - Values not taken into account if the oil tank was full when the airplane was weighed.
DATE : INSPECTION VISA :
C4080000AABCMA8000
NOTE
The airplane's original report shall be kept with the airplane's POH.
Section 6
Weight and Balance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 6.4.5
PIM - DO NOT USE FOR FLIGHT OPERATIONS