B400 OPC Flashcards

1
Q

What does “warning” mean in the POH

A

If not followed could lead to personal injury, death, or severe damage to equipment

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2
Q

Go through B400 flash cards

A

Go through B400 flash cards

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3
Q

What does “caution” mean?

A

may result in damage to equipment if not followed

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4
Q

What does “note” mean?

A

procedure or technique considered essential to emphasise

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5
Q

How much thrust does the FJ44 -3ap develop

A

3031LBS at sea level and 25 degrees C

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6
Q

Whats the max fuel we can practically upload

A

4800lbs can do 4900lbs but requires cool temps and overnight refuel

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7
Q

When should you check the oil level

A

within 15min of shutdown

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8
Q

When checking FMS legs, should you read from navlog and check CDU or read from CDU and read navlog?

A

Read from Navlog and check CDU

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9
Q

How should Genises calcs be done between the two pilots?

A

Either independently and then compared OR completed together

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10
Q

Whats the landing factor for a dry runway

A

May only use 60 percent of LDA

May reduce in flight to:
Must have 115percent LDA of LDR eg LDR is 1000m LDA must be 1150M

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11
Q

Whats the landing distance required on a wet runway

A

LDA must be at least 115 percent of the 60 percent available for a dry runway EG. get dry runway figures and add 115percent

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12
Q

When does a Genesis EO DP end

A

When Aircraft is above applicable MSA (usually 25nm)

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13
Q

Are the GPS ‘s in OVS PBN compliant or Deemed, and what does it mean?

A

Compliant - aircraft are fitted with avionics including GNSS equipment that satisfies all requirements for
PBN airworthiness. The AFM or applicable supplement will clearly state that the aircraft is capable of the
required PBN elements for departure, enroute, arrival and approaches (RNP 10, 4, 2, 1, LNAV, Baro
VNAV, etc)

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14
Q

How do you set the park brake in the B400

A

Pull handle down and out, then apply brakes (one way valve)

must be set from pilot side if engines not running

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15
Q

What should the alt select be set to when on or cleared a visual approach

A

at least 2000ft AAL to avoid sporadic audio warnings

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15
Q

Do we have a PEC for the B400

A

No, standby altimeter only, correction can be found in AFM

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16
Q

When does thrust have to best by for a rolling start takeoff?

A

60kts

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17
Q

how often should fuel checks be conducted enroute?

A

Every 30min if fuel critical (less than 30min holding) otherwise, every 60 min

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18
Q

Whats the min airspeed in cruise?

A

180kts

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19
Q

Whats the fuel efficient climb profile?

A
  • no more than 200kts to 5000ft(advise ATC)
  • 220kts from 5000ft to 10,000ft
  • either 250kts or 220kts(long range) into M.64
  • When not flying in the general direction of destination - 170kts
  • Passing fl350, can accelerate to .70
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20
Q

Whats the single engine service ceiling at max weight

A

Fl140

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21
Q

For a flap zero landing, what speed do we use and how much extra runway can we expect to use over normal flap 30 vref

A

Up to 40 percent more runway and use flap 30 vref plus 20kts

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22
Q

Whats the average fuel usage figure for the 400xt

A

1200lbs 1st hour, then
900lbs
850lbs

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23
Q

Whats the OEI cruise speed and fuel flow

A

300kts TAS, FL210, 15,00lbs and ISA plus 10
-820lbs/hr
- Best to check Nextant POM

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24
Q

Whats the DP rough fuel usage

A

Long range cruise at 10,000ft is rounded 1100lbs a hour.
- TAS 260kts
- ISA plus 20

25
Q

What could happen if you exceed the tailwind limit for starting?

A
  • Hot start
  • ND annunciator
26
Q

Whats the maximum oil consumption for the FJ44

A

0.023Qrts/hr

27
Q

What the Min N2 for single engine gen operations in icing?

A

80 percent N2

28
Q

What do you get when you are down to standby power only?

A

-Standby instruments
- RTU and Comm 1
- Headphones and hand mic - interphone wont work

29
Q

What is the maximum altimeter split in the afm for entering RVSM airspace

A

Ground - 80ft
Flight - 200ft

30
Q

Can we disconnect the autopilot or flight director on a LNAV/VNAV approach?

A
  • Autopilot or FD must be used
    -so can disc AP but have to use FD
31
Q

What are the icing condition above 20,000ft associated with convective activity defined as

A
  • 5000ft above
  • Within 10nm horizontally
  • Visible moisture
32
Q

which power lever syncs to which and what are the parameters

A

left is master, must be within 3 degrees TLA
- inhibited for TO and LDG
- both engines must be in same bleed state

33
Q

what pressure should the hydraulic accumulator be

A

900psi +- 50-psi

34
Q

whats the max leakage rate for the hydraulics

A

one drop every 25 cycles or 2 drops a minute in the pressurised condition or 1000 to 1500psi

35
Q

when does the LH or RH pump press low annunciator come on (hydraulics)

A

15sec after system pressure dropped to 750 psi +- 100psi

36
Q

how many oxygen masks do we have onboard

A

12

37
Q

what the rough measurements for the wingspan and height

A

wingspan - 13.3m
tail - 4.3m

38
Q

how long is the aircraft nose to tail

A

14.8m

39
Q

when should the starter cut out on start

A

between 35 and 45 N2, if not:
thrust levers to cutoff, batt to emer, masters emer

40
Q

What does the inverters power

A

-pitch trim indicators
-EGPWS
-flap position
ac shed indicator

41
Q

What speed should we fly for autopilot couples approaches

A

vref plus 5

42
Q

which trim motor does the autopilot use

A

emergency trim motor

43
Q

whats the lowest we can use the autopilot

A

200ft agl

44
Q

What n2 should you introduce the fuel if the crosswind or tailwind component exceeds 5kts

A

equal to or greater than 12 percent

45
Q

what should you do if after takeoff if taking off from slush or snow covered runway

A

cycle gear once or twice

46
Q

when will the wing anti-ice lights come on

A

after the wing anti-ice has come up to temp

47
Q

Whats the min n2 for wing anti ice

A

80 percent

48
Q

Whats the min N2 for the anti ice test

A

78 percent, check for rise in ITT and Check ignition light come on

49
Q

how much sweep does the b400 wing have

A

20degrees, 2.5 degrees dihedral

50
Q

whats the green arc for the nitrogen level

A

1350 to 1500psi

51
Q

When will the L or R BUS FDR FAIL illuminate

A

When one, feeder cable between main and load bus fails. Extinguishes when all 3 fail

52
Q

What happens to the no2 inverter when you lose the right load bus?

A

automatically received power from emer bus

53
Q

How long does the standby battery power its equipment

A

min of 30min

54
Q

How can the landing lights be retracted and switched off

A

automatically with gear retraction and can use switch

55
Q

What powers the emergency lights?

A

2 lead acid batteries. charged by emer bus when switch is in off or arm

56
Q

what kind of tanks are the fuselage tanks

A

non self healing bladder tanks in steel boxes

57
Q

Whats the flow rate of the mid fusalage transfer pumps

A

2,200lbs per hour each

58
Q

How many fuel probes do we have

A

12
4 in each wing tank
1 aft fus tank
2 mid fus
1 right forward tank

59
Q

how much oil between the fill and add level on the FJ44

A

approx 1 quart

60
Q

how many ignitors do we have and where are they located

A

2, at the 1oclock position

61
Q
A