Bj Memory Flashcards
Service ceiling
45,000
Vlo vle Vww
200 knots
Max takeoff weight
Max landing
16,300 lbs.
15,700 lbs.
Icing conditions are defined as :
RAT below 10 C and visible moisture
Icing conditions around convective activity are destined by what criteria ?
Above 20,000 feet with RAT below 10C and within 5000’ vertically or 10 NM horizontally of convective activity.
Is there a lower temperature limit for the operation of anti icing equipment ?
No, engine icing may occur at high altitude with temperatures down to -30C with no airframe icing.
If leaving an aircraft outside overnite in snow at a temperature below what value would you expect the snow to not adhere ?
Below -10C it most likely won’t stick.
What should the flap position be for depicting ? Should the ECS be on or off ?
Flaps up, ECS off. Operation of ECS off and engine anti ice on is approved for ground operations, not flight.
To mitigate the risk of premature type 4 anti ice fluid breakdown what can you do ?
Delay extending flaps to takeoff for as long as practical.
In what section of the GOM are holdover timetables found ?
Section 7
A per takeoff, tactile check must be conducted when ? Two conditions.
When HOT has been exceeded and then it must be within 5 minutes of departure.
What is the difference between a pretakeoff check and a pretakeoff contamination check ?
A pretakeoff check is required when in ground icing conditions but a pretakeoff contamination check must be conducted when HOT has been exceeded.
What do the items on the beech jets all have in common ?
They are all located in the back of the aircraft.
What is the minimum battery voltage for start ? Minimum to close the battery relay ?
22 volts for start, 18 to close batt. Relay
What are the tree things you should see when conducting the battery feeder test ?
Feeder fault light
No power to the aircraft
Standby power items on
What are the GPU limitations for start ?
28 volts, 1000-1500 amps
When are four times when you would use the generator master switches (guarded) ?
Dual generator failure
Electrical smoke or fire
Starter does not disengage
Emergency evacuation
If we are forced to place the battery switch to EMER what can we expect to lose ?
EFC's off Engine anti ice ON No flaps, speed breaks , TR's, normal trim, no anti skid (40% more runway needed) Alternate gear extension required Ahrs aux battery
What equipment is available on the standby battery bus ?
Standby attitude indicator. RTU 1
Standby altimeter vibrator. COMM 1
Standby instrument lights. Left ITT
Light for magnetic compass. EFC for start
Pilot and copilot headsets and hand mics, no intercom.
The “L/R feeder fail” light illuminates inflight, what does this mean ?
That one of the two lines feeding power from the main to the load bus has failed and a third line is supplying power. If this third line fails the light extinguishes,the light gets its power from this third line.
What are the starter limitations ?
30s on / 5 min. Off
30s on / 15 min. Off
30s on / 60 min. Off
Which battery bus powers the EFC’s for engine start ? Why ?
Standby bus, to prevent power dropping offline due to power surges.
What items are AC powered ?
Pitch trim position AC bus shed annunciator Flap position LH, RH oil pressure EGPWS
What are the sources of power for the number 2 inverter ?
The right load bus, if it fails the inverter is automatically powered by the EMER bus.