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68 Cards in this Set
- Front
- Back
Minimum Crew for flight |
2 Pilots |
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The Emb - 145 is certified in transport category in the following conditions? |
VFR IFR Icing Conditions |
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Max runway slope |
+-2% of runway length |
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Runway surface |
Paved |
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Max tailwind |
10kts |
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Max temperature for aircraft |
52C |
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Min/max takeoff and landing pressure altitude |
Minimum -1000ft Maximum LR 8000ft XR 10000ft |
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Min/max SAT at FL370 |
Min -65C Max -21.5C |
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Min/max SAT for Takeoff |
Minimum -40C Maximum 52C |
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Min TAT above FL250 |
Total air temperature in cruise flight flight above FL250 is limited to -45C. However, if momentary deviations occur down to -50C no maintenance action required |
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Min SAT below FL250 |
-54C |
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MX inspection needed when landing below |
-40C |
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Vlo for gear retraction/extension |
Retraction 200KIAS Extension 250KIAS |
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Vle |
250KIAS |
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Maneuvre speed Va |
200KIAS |
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Max flap extension speed for flaps 9 |
250KIAS |
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Max flap extension speed for flaps 18 |
200 KIAS |
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Max flap extension speed for flaps 22 |
200 KIAS |
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Max flap extension speed for flaps 45 (LR) |
145 KIAS |
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Max flap extension speed for flaps 45 (XR) |
160 KIAS |
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Above 10000ft with YD disengaged, max speed for flaps 22 (XR) |
180 KIAS |
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Above 10000ft with YD disengaged, max speed for flaps 45 (XR) |
145 KIAS |
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For LR, when flaps are extended to/retracted from 45, momentary airspeed deviations between 145 and ______ will not require a MX inspection. |
160 |
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For LR, when flaps are extended to/retracted from 22, momentary airspeed deviations between 200 and ______ will not require a MX inspection. |
210 |
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Max airspeed after T/O without retrimming |
160 KIAS |
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Max airspeed for turbulent air penetration below 10000 _____ and above 10000 ______ |
200 KIAS 250 KIAS/0.63 M, whichever is lower |
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Min/max fuel tank temperature |
Min -40C Max 52C |
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Max N1 |
100% |
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For all models, min/max oil pressure < 88% N2 |
Min 34 PSI Max 110 PSI (may be exceeded during engine start if oil temperature is below 21C. The engines must remain at idle until the oil pressure is less than 110 PSI. Oil pressure in the 111 to 115PSI maximum 5 minutes in the 116 to 155PSI maximum 2 minutes) |
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On LR min/max oil pressure > 88% N2 |
Min 50 PSI (operations between 34 and 50 PSI permitted on takeoff and go around) Max 110 PSI (operation between 111 and 115 for 5 minutes. 116 to 155PSI for 2 minutes)
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On XR, mim/max oil pressure > 88% N2 |
Min 48 PSI (operation between 34 and 48PSI permitted during takeoff and go around) Max 110 PSI (operation between 111 and 115 for 5 minutes. 116 to 155PSI for 2 minutes) |
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On XR, operation between 34 and 48PSI is permitted for. |
For take off and go around |
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Max oil pressure may be exceeded during start if oil temp is below ______. The engine must remain at Idle until oil pressure is less than: ______ |
21C 110PSI |
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All aircraft will display oil pressure <= _______ in green |
110PSI |
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All aircraft will display oil pressure in range ______ in amber and permitted in all operation modes. Limited to ______. Operation in the oil pressure amber range between ________ in amber and permitted in all operation modes. Limited to ______. However, total over-pressure time may not exceed_____. |
111-115 PSI 5 minutes 116 - 155PSI 2 minutes 5 minutes |
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Min oil temp for start |
-40C |
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To increase N2 above _____, the engine oil temp must be _____. Or, run the engine for at least ______, allow the engines to stabilise and ensure that the oil pressure is<= ______. |
83% 40C 8 minutes 83 PSI |
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LP and HP spool virbration limits maybe exceeded up to ______ for ______ during takeoffs and go arounnds. Else _______. |
2.5IPS 5 minutes 10 seconds |
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Max ITT for start on all engines |
800C |
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All ER/LR takeoff thrust rating/ITT limits (948) are time limited to ________. |
5 minutes |
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All XR, takeoff thrust rating/ITT between ______ are time limited to _______. Takeoff thrust rating/ITT up to______ are permitted up to max of_____. |
971 to 992 90 seconds 970 5minutes |
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Any engine exceedance or peak must be monitored and logged by crew. |
True |
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Min battery temp for APU start |
-20C |
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Start cycle for APU: After 1-2 attempts:______ after 3rd attempt_____. |
1 minute off 30 minutes off |
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Max APU generation above FL300 |
300A |
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Min AP engagement height |
500ft |
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So disengagement height is ____ for visual approaches. For CAT 1, ____ for CAT II and __________ for non precision. |
200 ft AGL 200 ft AGL 85 Ft AGL Before leaving MDA |
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Max ISIS duration when operating only on batteries is ____. Maybe exceeded to _____ if pitot 3 is turned off in non icing conditions. |
40 minutes 45 minutes |
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The airplane must not be moved during power-up initialisation do not cage attitude in turning flight. |
? |
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Max altitude for flap extension |
20000ft |
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Max differential pressure |
7.8PSI |
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Max differential over-pressure |
8.1PSI |
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Dry monitoring continuous operation |
5 minutes on 5 minutes off |
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Max differential negative pressure |
-0.3PSI |
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Minimum temperature for manual anti ice operation |
-40C |
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Max operation for manual anti ice operation |
10C |
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Hold configuration in icing |
Landing gear ——- up Flaps ——- 0 Minimum airspeed—200KIAS |
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The airplane must not be moved during power-up initialisation do not cage attitude in turning flight. |
True |
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After start, the engines must run at idle or taxi thrust for _____ for cold engines. Or _____ for warm engines. |
4 minutes 2 minutes |
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Engine is considered cold, if it’s been shut down for at least |
90 minutes |
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Engines must run for at least _____ at idle or taxi thrust before shut down. |
2 minutes |
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Max altitude for starting APU |
30000 |
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Max operation altitude for the APU |
37000 |
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The APU will automatically shutdown at _____ rotor speed. |
104% |
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APU May exceed _______ for a maximum of______. |
680C up to 717C 5 minutes |
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Max windshield wiper operating speed |
170KIAS |
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Do not operate windshield wiper |
Dry windshield |
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Max imbalance allowed between tanks. |
800Lbs |