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50 Cards in this Set
- Front
- Back
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Max Ramp Weight |
19,595 kg |
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MTOW |
19,505 kg |
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Max Landing Weight |
19,051 kg |
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MZFW |
17,917 kg |
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Maximum Baggage Compartment Weight |
1134 kg |
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Forward CoG limits |
Up to 13,608 kg =15% 13,608 - 19,505 kg = 15 - 21% |
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Aft C of G limits |
40% |
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Load Factors |
Flaps Retracted: +2.5g, -1.0g Flaps Extended: +2.0g, 0.0g |
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Maximum Operating altitude |
25,000ft ASL |
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Max Altitude for T/O and Landing |
10,000ft ASL |
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Maximum Altitude for gear/flap extension |
15,000ft ASL |
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Maximum Runway Slope |
+2% (uphill) -2% (downhill) |
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Max Tailwind Component |
10kt (Air Nelson is 20kt) |
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Max Crosswind |
36 kts |
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Maximum operating ambient temperature |
48.9 C or ISA +35 C |
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Minimum operating ambient temperature |
-54 C |
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VMO |
0 - 17,000ft = 243 kt 20,000ft = 232 kt 25,000ft = 214 kt |
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VFE |
Flaps 5 = 163kt Flaps 10 = 154kt Flaps 15 = 150kt Flaps 35 = 138kt |
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VA |
177kts |
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VLO (Landing gear operating speed) |
163kt |
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VLE |
173kt |
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VRA |
190kt |
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Alternate Gear Extension speed |
140kt |
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Max Tyre Speed |
165kt |
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Max altitude for air start |
20,000ft |
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MTOP |
Max Torque = 105.6% ITT = 800 C Max NH = 102.7% PRPM = 1212 Oil pressure = 55 to 65 Oil Temp = 45 to 115 |
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NTOP |
Max Torque = 92% ITT = 765 C Max NH = 101% PRPM = 1212 |
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Max Cont. |
Max Torque = 90% (96%) Max ITT = 800 C Max NH = 102.7% PRPM = 1212 (1125) |
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Starting |
950 C (900 C) 900 to 950 degrees for 5 seconds 840 to 900 degrees for 12 seconds |
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Transient |
Max Torque = 115% ITT = 840 C Max NH = 103.7% PRPM = 1320 Oil Temp = 125 MAX |
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Max Reverse |
Max Torque = 90% ITT = 765 Max NH = 101 PRPM = 1212 |
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Minimum flight idle NH |
66% |
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Oil Pressure between 40 and 55 psid is allowed below what NH%? |
75% |
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Normal oil temperature |
45 - 115 C 115 - 125 C is time limited to 20 mins |
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Oil temperature required prior to unfeathering propellers? |
0 C |
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Usable fuel tank capacity |
1287kg |
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Engine Start - Tailwind Limits |
GPU - 35kt APU - 20kt Battery Start - 0kt |
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Starter Cranking Time Limits |
START / Max time ON / Rest 1 1 min 2 min OFF 2 1 min 2 min OFF 3 1 min 30 min OFF |
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What propeller RPM is prohibited? |
500 - 780 rpm |
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DC generators |
Ground operation = 0.7 In flight = 1.0 |
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L TRU and R TRU |
Ground operation = 1.0 Flight Operation = 1.0 |
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AC Generators |
Ground operation up to +10C OAT = 1.0 Ground operation at or above +10C OAT = 0.33 In flight operation = 1.0 |
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Inverters |
1.0 (ground and in flight) |
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Normal cabin pressure differential limit |
5.5 +/- 0.3 psi |
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Maximum cabin pressure differential limit |
5.95 psi |
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Maximum cabin pressure differential limit during taxiing, take off and landing |
0.5 psi |
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Maximum Cabin Altitude |
8,000 ft |
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APP mode is not permitted with: |
Flaps 35 Flaps 5 and A/P engaged below 1500 ft AGL Flaps 0 and A/P engaged below 500 ft AGL |
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Speed Restrictions Class C or D airspace |
200kts when operating below 3000ft AAL within 5nm of the Aerodrome |
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Speed Restrictions Class G Airspace |
Below 9500ft AMSL 200kts At and Below 5000ft AMSL 160kts |
