EKQ Flashcards

1
Q

Maximum flap extension / extended speed

A

Approach - 202
Full Down - 158

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2
Q

Maximum landing gear operating speed

A

Extension - 182
Retraction - 164

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3
Q

Air minimum control speed - Propeller feathered

A

Flaps up - 101
Flaps Approach - 98

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4
Q

Maximum operating speed

A

Sea level to 24,000ft - 245

24,000 - 35,000ft - 245 to 192 / 0.58M

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5
Q

One engine inoperative best rate of climb speed

A

135 kts

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6
Q

Max operating alt with yaw damper inop?

A

15,000ft

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7
Q

Max cabin diff pressure?

A

6.6 PSI

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8
Q

Is the Shadow cleared for RVSM operations?

A

No

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9
Q

Max normal cabin alt

A

8,000ft

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10
Q

Maximum OAT

A

Sea Level to 25,000ft - ISA +37°C

Above 25,000ft - ISA +31°C

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11
Q

Maximum loading (G’s) - Up to 16,500 lb?

A

Clean: -1.21g to +3.01g
Flaps extended: +0g to +2g

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12
Q

Maximum loading (G’s) - above 16,500lb up to 17,500 lb?

A

Clean: -1.08g to +2g
Flaps extended: +0g to +2g

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13
Q

Max crosswind for take off and landing?

A

20kts including gusts

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14
Q

Max tailwind for take off and landing?

A

10 kts

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15
Q

Max tailwind for touch and go?

A

5kts

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16
Q

Max crosswind for coupled approach?

A

32 kts

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17
Q

Aircraft approach category

A

B

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18
Q

Single engine approach VCH (below 16,500 lb)

A

Not below 200 ft agl

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19
Q

Single engine approach VCH (above 16,500 lb)

A

Not below 300 ft agl

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20
Q

Arrester Gear Trampling - Max speed over rigged supported and unsupported cable?

A

Walking speed at 90°

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21
Q

How many cycles are the landing gear limited to?

A

one ever five minutes for a total of 6 cycles followed by a cooling down period of 15 mins

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22
Q

Autopilot minimum engagement height after take off

A

400 ft agl

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23
Q

Autopilot min use height during cruise?

A

1000 ft agl

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24
Q

Autopilot min use height during an approach?

A

79 ft agl

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25
Q

Autopilot min use height during a steep approach?

A

160 ft agl

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26
Q

Can you depart with the auto feather inop?

A

No it must be operable for all flights and must be armed for take off, climb, approach and landing.

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27
Q

Max ITT on Start?

A

+1000°C (time limited to 5 seconds)

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28
Q

Max ITT at Idle?

A

+750°C

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29
Q

Min Prop RPM at Idle?

A

1050RPM

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30
Q

Oil Temp limits

A

-40°C to +110°C

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31
Q

Min N1 at Idle

A

64%

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32
Q

Limits during Take off
(TRQ, ITT, N1, Prop RPM)

A

TRQ - 100%
ITT - +850°C
N1 - 104%
Prop RPM - 1700

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33
Q

Limits for Max Cont and Cruise Climb
(TRQ, ITT, N1, Prop RPM)

A

TRQ - 100% (Trq values vary with alt and temp in climb)
ITT - +840°C
N1 - 104%
Prop RPM - 1700

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34
Q

Limits for Max Reverse
(ITT, N1, Prop RPM)

A

ITT - +760°C
N1 - 104%
Prop RPM - 1650

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35
Q

Limits for Transient
(TRQ, ITT, N1, Prop RPM, oil PSI)

A

TRQ - 156% (limit to 20 secs)
ITT - +870°C
N1 - 104%
Prop RPM - 1870
Oil PSI - 200

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36
Q

What prop RPM indicates a failure of the primary governor?

A

RPM above 1700. Flights may continue with a prop overspeed up to 1768 RPM with the torque limited to 96%

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37
Q

External power V and A’s

A

28.0V to 28.4V and can generate a minimum of 1000A momentarily and 300A continuously

38
Q

Icing limitations: Minimum ambient temp for operation of the de-icing boots

39
Q

Minimum airspeed for sustained flight in icing below 16,500 lb

40
Q

Minimum airspeed for sustained flight in icing above 16,500 up to 17,500 lb

41
Q

Maximum airspeed for flight with windshield icing

42
Q

Total usable fuel quantity

43
Q

Max fuel in each main fuel tank

44
Q

Max fuel in each aux tank

45
Q

Max fuel in each ER tank

46
Q

Max wing fuel imbalance

47
Q

Min fuel tank quantity for take off

A

265 lb per side

48
Q

When is Crossfeeding of fuel permitted

A

When one engine is inop

49
Q

Different Classes of Airspace

A

Class A - Airways (IFR only)
Class C - Above FL195 (IFR and VFR)
Class D - Aerodrome areas, CTR’s and CTA’s
Class E - Some Scottish Airways
Class G - uncontrolled

50
Q

What class of airspace is a MATZ?

51
Q

VMC minima for VFR in Class G airspace above 140kts?

A

5km vis, 1500m horizontally, 1000ft vertically

52
Q

Difference between QFE AND QNH?

A

QFE - Pressure at airfield level
QNH - sea level plus airfield elevation

53
Q

CDFA - Why was it introduced?

A

Continuous Descent Final Approach - To prevent level off, improving fuel efficiency, noise and pilot workload.

54
Q

What is TORA? ASDA? TODA?

A

TORA- Take off run available - Runway not inc stopway
ASDA - Accelerate Stop Distance Available - TORA plus stopway
TODA - Takeoff Distance Available - TORA plus clear way (area beyond the runway that is clear of obstacles)

55
Q

Crew Duty Time - What is it?

A

14 Hours

12 hours with no extra training just one landing.
After 9 hours CDT consideration for training plus no asymmetric training.

56
Q

Crew Duty Time - Who can extend and for how long?

A

Captain - 1 hour
Sqn Cdr - 1 hour
DDH - 1 hour
AOC - 1 hour

57
Q

What is mandatory Crew Rest Period?

A

12 hours

Plus an additional hour for every extra hour of CDT or every 4 hour time zone change.

58
Q

Min de-ice boot operation temp

A

-40 degrees C

59
Q

Anti ice off temp

A

More than 10 degrees C

60
Q

Maximum OAT?

A

37 degrees

61
Q

Max ramp weight?

A

17,600 lbs

62
Q

Max ZFW?

63
Q

Max weight in baggage area?

64
Q

Max fuel imbalance?

65
Q

Starter limits - what are they?

A

30secs on 5 mins off - 30 secs on 5 mins off - 30 secs on 30 mins off

66
Q

TRQ is time limited between 100% and 102% for how long?

67
Q

TRQ max transient is 156% for how long?

68
Q

N1 max SOP and N1 limit?

A

102% for SOP and 104% for limit

69
Q

Max prop RPM is 1700-1730 for how long?

70
Q

Max transient RPM is between 1730 and 1870 for how long?

71
Q

Oil pressure maximum?

72
Q

Oil pressure operating range?

A

90-135 psi

73
Q

Minimum oil temp?

A

-40 degrees

74
Q

Operating oil temp?

A

0-110 degrees

75
Q

External power supply volts and amps?

A

28-28.4 volts, 300 amps continuously, 1000 amps momentarily

76
Q

Refueling tanks order

A

Mains - Aux - ER

77
Q

Contingency fuel

A

600 lbs (Break it down)

78
Q

Flare order

A

Fwd left - Green
Fwd right - green
Aft right - brown/white
Aft left - white

79
Q

Flare safety interlocks

A

WoW switch
Mass
SDU pin

80
Q

DAS ground safety arcs

A

25 degrees off the nose - 20 degrees aft of the dispensers for a safety distance of 525 ft

81
Q

Oxy system SOP psi’s?

A

UK - 1000 psi
Transit/operational - 1500 psi

82
Q

When do L/R Ignition on activate?

A

Engine start switch or with auto ignition on below 17% TRQ

83
Q

When is it normal for L/R No Fuel XFR to activate?

A

When ignition is activated (delayed 11 +- 2 secs) or when crossfeeding fuel (the side receiving fuel closes)

84
Q

How does the rudder boost work?

A

Senses TRQ in both engines, when the difference exceeds 30% the yaw servo activates up to maximum deflection with 80% TRQ difference

85
Q

Describe the flap system

A

Fowler-type flaps which is controlled by a single electric motor

86
Q

Asymmetrical flap protection - how does it work?

A

Asymmetrical flap switch system will disable the flap motor when 3-6 degrees of split occurs between both flaps on the same wing. This causes the cam to slip off the switch and will remove power from the flap motor.

87
Q

How does the ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) work?

A

It provides pitch, bank and magnetic heading data.

Magnetic heading is provided by separate magnetic sensors in opposite sides of the horizontal stabiliser

Attitude is from two attitude and heading computers (AHC) Each system has an inertial measurement unit. The AHC has a primary and secondary power supply, if the secondary power fails the primary continues to power for 10 mins then fails. If the primary fails it will be instant. No indication maybe a tripped circuit breaker. If failed, AHRS reversionary can be used.

88
Q

Where does the Air Data Computers (ADC’s) get input?

A

-Ram air pressure from pitot mast
-Static pressure from static ports
-Air temp

Left pitot + left top and right bottom static ports supplies ADC 1 (PFD + MFD)

Right pitot + left bottom and right top static port supplies ADC 2 (Right PFD + ESIS)

90
Q

Why is RVS NOT READY activated?

A

When the props are not fully forward but the gear is down. Reverse can still be used but the fuel topping governor would limit the amount available.