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56 Cards in this Set
- Front
- Back
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Icing Conditions |
Visible moisture, standing water, slush or snow and OAT or Sat is +5 or less. |
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Flap speeds |
Max ALT for use of flap is 14000ft 7 or 15 - 175kts 20 - 165kts 35 - 140kts |
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Gear retraction speed Vlor |
150kts |
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Gear extension speed Vloe |
200 |
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Gear emergency extension speed |
200 |
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Gear extended speed Vle |
200 |
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Vmcl flaps 20 and 35 (B and WT) |
106kts B 103 kts WT |
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Vmo, Max operating speed |
250kts upto 16000ft, above it decreases as indicated my Vmo pointer to approx 210kts at 25000ft |
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Va |
180kts |
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Vra |
190kts upto 21000, above which speed is Vmo pointer minus 30 |
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Wing span |
Without WT - 21.44m WT - 22.75m |
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Max Takeoff tail wind |
10kts |
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Max landing tail wind |
10kts |
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Max landing tail wind with AFMS 54/55 |
15kts |
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Max Operating Altitude |
25000ft |
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Max crosswind |
35kts |
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Yaw damper operation is not authorised for |
Take off Go around Landing |
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When must landing flap be set by |
300ft radio height Final flap setting must be called for at no less than 500ft AGL |
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Flap setting when holding in icing conditons |
Flap 0 |
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Cargo fire protection times |
60min 340B (WT) 35 Min all other models |
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Structural limits SF340B |
MTW - 13,740 MTOW - 13,605 MLW - 12,930 MZFW - 12,020 |
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Structural limits SF340B (WT) |
MTW - 13,290 MTOW - 13,155 MLW - 12,930 MZFW - 12,020 |
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Cabin altitude pressure in flight |
7.1 psi normal 7.5 psi max |
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Cabin differential pressure landing max |
0.3 psi |
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CABIN PRESS warning |
7.5 psi 10000ft |
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DC generator loads |
Voltage 27.5 Min 28 norm 29 max Normal load 400A Max load for 5 Min 600A |
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External power voltage |
Gpu 28-29.5 Battery cart - higher than a/c battery for engine start, Max 29.5 |
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External power amperage requirement |
600A max for normal operation 1400A Min 1600A Max for engine start |
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Minimum fuel Takeoff in each tank |
135kg |
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Max fuel imbalance between tanks |
90kg |
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Total usable fuel capacity |
2542kg @0.79 density |
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Windshield heating time in normal |
Switching direct from off to high is not authorised, must be in normal for a minimum of 7 mins |
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Time from switching STBY PITOT On until full ice protection is obtained |
5 min |
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Windshield wipers Max speeds |
In low position 130kts In high position 160kts |
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How many altimeters does the Saab have and require |
3. Serviceable to same standards are normal ifr |
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Max difference between two ASI |
+- 8kts |
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Number of brake applications of full charged accumulators |
11 |
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Max speed for use of brakes with anti skid inop/off |
40kts |
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Ng limitations for motoring start |
Max ng for motoring - 26% Min stabilised ng prior to condition lever to start - 17% Min Ng prior to tail wind start - 20% |
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Start duty cycle |
Two start attempts with 3 minutes cooling in between, then 25 mins cooling before subsequent starts |
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Starter motoring |
3 30 sec ventilations with 3 mins cooling inbetween, then 1 hour before subsequent starts or motor |
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Max time till light off on start (from initial Ng rotation to ITT rise) |
20 seconds |
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Max time with starter engaged |
70 seconds of which Max 30 seconds plain motoring |
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Auto Pilot not authorised |
Below 200ft on take off or go around Below 500ft during cruise Below 50ft on app Below 100ft for a non coupled app |
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Flight Director use not authorised |
In go around mode during take off |
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Low level fuel light |
135kg |
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CT7-9B Engine power |
1750 shp/ 1870 shp (APR) 1935 eshp |
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Max altitude for flap use |
14,000ft |
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Attitude/ heading reference system |
Aircraft must not be moved during initialisation. Takeoff not permitted till 2 mins after initialisation complete, both eadis show 3 degrees or less, and heading on Compass card not slewed from a/c heading. |
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B model APR 5min |
TRQ - 107 ITT - 940 RPM - 1396 |
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B Model APR 2min |
TRQ - 107 ITT - 950 RPM - 1396 |
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B model Take off power 5 min |
TRQ - 100 ITT - 917 RPM - 1396 |
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B model Take off power 2 min |
TRQ - 100 ITT - 927 RPM - 1396 |
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B model MCP |
TRQ - 100 ITT - 944 RPM - 1396 |
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B model transient power |
TRQ - 112 ITT - 965 RPM - 1572 |
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B model engine start ITT |
965 |
