Mahindra GIPPSAERO GA8-TC 320 - Weight and Centre of Gravity Limits

C01-01-08 5 Feb 2009 Page 2-5
Section 2
Model GA8-TC 320 Limitations
2.4.5. Propeller
Manufacturer: Hartzell Propeller Inc.
Model: HC-C3YR-1RF/F8068
Type: Metal, Constant Speed
Number of blades: 3
Diameter: 2083 mm (82 in)
2.5. ENGINE INSTRUMENT MARKINGS
Instrument
Red Line
Minimum Limit
Green Arc
Normal
Operating
Yellow Arc
Precautionary
Range
Red Arc/Line
Maximum Limit
Tachometer - 575 - 2500 RPM - 2500 RPM
Manifold Pressure - 10 - 38 in Hg 38 - 40 in Hg 40 in Hg
Oil Pressure 25 psi 55 - 95 psi
25 - 55 psi
95 - 115 psi
115 psi
Oil Temperature - 60 - 118°C - 118°C
Fuel Pressure 12 psi 27-65 psi 12 - 27 psi 65 psi
Fuel Quantity 0 0 - F - -
2.6. WEIGHT LIMITS
Maximum Take-Off and Landing Weight: ....................... 1814 kg (4000 lb)
Maximum Weight in Main Cargo Area: ............................ 680 kg (1500 lb)
Maximum Weight on Cabin Baggage Shelf: ................... 113 kg (250 lb)
Maximum Weight in Aft Luggage Bin: ............................. 22 kg (50 lb)
2.7. CENTRE OF GRAVITY LIMITS
Forward Limit: 1219 mm (48 in) aft of datum at 1089 kg (2400 lb) and below;
1422 mm (56 in) aft of datum at 1814 kg (4000 lb), linear variation
between these points.
Aft Limit: 1626 mm (64 in) aft of datum at all weights
Datum: Firewall (Fuselage Station 0)
[located 1057 mm (41.63 in) forward of wing leading edge]
01 Aug 2011