Daher TBM 960 - Maximum Certificated Weights; Standard Airplane Weights; Cabin and Entry Dimensions

Table 1.3.2 - Recommended Engine Oil Types [Reference: P&WC Engine
Maintenance Manual, latest revision]
Nominal viscosity Specification NATO code
5cSt MIL-PRF-23699
O-156 (STD)
O-154 (HTS)
Maximum Certificated Weights
Maximum airplane weight:
Maximum Ramp Weight (MRW)
7,430 lbs to 7,650 lbs *
(3,370 kg to 3,470 kg) *
Maximum Takeoff 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)
* Depending on the C.G. position – see Figure 2.5.2
Baggage weight:
- For weight and C.G.
limits, refer to
Paragraph Weight Limits in Subsection
2.5.
- For cargo loading instructions, refer to Subsection 6.3. Baggage Loading
Standard Airplane Weights
Standard empty weight: 4,784 lbs (2,170 kg)
Maximum useful load: 2,831 lbs (1,284 kg)
Cabin and Entry Dimensions
Maximum cabin width: 3.97 ft (1.21 m)
Maximum cabin length: 13.29 ft (4.05 m)
Maximum cabin height: 4 ft (1.22 m)
Number of cabin entries: 1 (standard) + 1 pilot door (if installed)
Entry width (standard): 3.54 ft (1.08 m)
Section 1
General
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 1.3.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS