Daher TBM 960 - Weight and C.G. Limits; 2.5 - Weight and C.G. Limits

2.5 -
Weight and C.G. Limits
W
eight Limits
Maximum airplane weight:
Maximum Ramp W
eight (MR
W)
7,430 lbs to 7,650 lbs *
(3,370 kg to 3,470 kg) *
Maximum T
akeoff Weight (MTOW)
7,394 lbs to 7,615 lbs *
(3,354 kg to 3,454 kg) *
Maximum Landing Weight (MLW)
7,110 lbs
(3,225 kg)
Maximum Zero Fuel Weight (MZFW)
6,252 lbs
(2,836 kg)
* Depending on the C.G. position – see
Figure 2.5.2
NOTE
The Maximum Takeoff Weight of 3,454 kg is valid only for C.G. between 34.4%
and 34.7%.
The Maximum Takeoff Weight of 3,354 kg is valid only for C.G. at 23.8%.
The Maximum Takeof
f Weight increases linearly from 3,354 kg to 3,454 kg
between 23.8% and 34.4% of C.G.. For example, MTOW = 3,394 kg for C.G. at
28% – see
Figure 2.5.2.
Maximum baggage weight:
- in the front baggage compartment (non pressurized): 110 lbs (50 kg)
>> With 6-seat accommodation
-
in rear part of pressurized cabin: 220 lbs (100 kg)
>> With 4-seat accommodation
- in rear part of pressurized cabin: 396 lbs (180 kg), with small or large net –
see
Figure 2.5.1
Pilot's Information Manual
Section 2
Limitations
PIM TBM 960 - Edition 0
Rev. 00
Page 2.5.1
PIM - DO NOT USE FOR FLIGHT OPERATIONS