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F100 NAA Memory Items > Memory items # FCOM > Flashcards

Memory items # FCOM Flashcards

1
Q

MZFW

A

36,740 KG

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2
Q

MRW

A

46,040

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3
Q

MTOW

A

A / T: 45,810 KG
G: 44,450 KG

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4
Q

MLW

A

39,915 KG

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5
Q

RTO Captain Actions

A

“STOP”
Thrust levers - Idle
Monitor ABS (if fitted) or Full Brakes
> 80 Kts max reverse thrust
Forward pressure on control column
< 60 It’s reverse thrust idle
Check MFDU Alert/Warning “Confirmed”
“Cabin Crew remain seated”
Or
“Cabin crew to your stations”

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6
Q

Emergency Evacuation

A

Park Brake - Set
Flaps - Fully Down
Reverse Thrust Levers - Fully down
Lift Dumpers - Disarm
Both Fuel Levers - Shut

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7
Q

RTO First Officer actions

A
  • Lift dumpers out / Reversers Green / Decel
  • 60 kts
    “Net link stopping”
    Read MFDU procedure or consult QRH
    Monitor captains actions
  • “ net link evacuating on runway / taxiing to the gate”
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8
Q

Emergency Descent

A

ATS - Disconnect
THRUST LEVERS - Idle
SPEED BRAKE - Out
FMP - 10,000 or MEA / LVLCH / Vmo

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9
Q

Both Engine Flame Out

A

Ignition - Relight

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10
Q

Hot Start

A

Fuel Lever - Shut

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11
Q

Min and max pressure altitudes for takeoff and landing

A

-1000 feet and up to 8000

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12
Q

Air con operative max temp T/O, flight, LDG

A

ISA +35c

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13
Q

Max cabin diff
Excessive cabin altitude alert
Max pax oxy mask drop

A

7.65 psi
10,000
14,500

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14
Q

Max crosswind

A

35 kias

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15
Q

Maximum tailwind

A

10 knots

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16
Q

Vmo / MMO

A

320 / 0.77

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17
Q

Max flap extension
8
15/25
42
Max altitude

A

250 / 0.5
220 / 0.45
180 / 0.36
FL200

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18
Q

Turbulence penetration speed

A

250 / 0.65

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19
Q

Autopilot altitudes
Minimum after takeoff
Cruise modes
Non-precision approach
ILS approach

A

35
700
250
80

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20
Q

APU start attempts
Min battery volts for APU start
APU Bleed pressure for engine starts

A

Up to 3 attempts allowed, 2 mins between then 15 mins
24 volts
20 psi

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21
Q

Fuel conversion

A

1 litre = 0.8kg

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22
Q

Fuel asymmetry max in flight

A

1000kg

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23
Q

Hydraulic min dispatch quantity

A

70%

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24
Q

Brake system alternate accumulator minimum

A

1000 psi

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25
Q

Power plant limitations
During start
During relight
Max takeoff
Max reverse thrust
Max continuous
Max over temperature

A

740 - 2 seconds
780 - 2 seconds
850 - 5 minutes
850 - 60 seconds
795 - unrestricted
870 - 20 seconds

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26
Q

Power plant start limitations
Power plant light up limitations
Power plant warm up limitations

A

4 starts 2 mins each with 30 seconds between
Must light up within 20 seconds of fuel lever open
Oil temp
40-20: 2 mins
0 - 20: 3 mins
-20 - 0: 4 mins

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27
Q

Oil pressure min for takeoff

A

30 psi

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28
Q

Max pax

A

109
(100 adults / 9 infants)

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29
Q

Load factors
Flaps up
Flaps down

A

-1 to 2.5
0 to 2

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30
Q

Crosswind limitations

A

Double aileron fault 15 kias
Total hydraulic failure 10 kias
Fuel asymm > 20 kias

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31
Q

Minimum temp in flight

32
Q

Flex shall not be used when?

A

Icing conditions exist
Runway contaminated with water, slush snow or ice
Windshear or temp inversions
Lift dumpers inop
One or more anti skid units inop
Wing anti ice on
Tail anti ice on

33
Q

Dry operating weight

A

Approx 27 tonne

34
Q

Category C speeds

A

Initial 240 - 160
Final 160 - 115
Missed - max 240
Reversal - no restriction

35
Q

Holding speeds

A

Up to FL140 - 230 kias
FL140 to FL200 - 240 kias
Above FL200 - 265 kias

36
Q

Missed approach requirements

A

Straight in landing cannot be affected from approach
Not visual at MDA or DA
Raim warning past IAF
Outside tolerances on final segment
Failure of navaid
Loss of visual reference below during visual circling

37
Q

Air Conditioner and Px
Cabin rate of change climb and desc
Ground ops without aircon

A

500fpm climb / 300fpm descent
Not permitted is OAT >40

38
Q

Automatic flight:
Min / Max Glide Slope Angles

A

Minimum 2 / Maximum 4

39
Q

Opening and closing window / doors

A

40 knots / 60 knots once opened
L1 / L2 operations not to be operated above 64 knots

40
Q

Fuel
Max assym on ground at or below 39,900 / above 29,900?
How much fuel can be added to centre tank for trimming purposes?

A

1000kg / 500kg
1000kg and must be included to zfw

41
Q

Max altitude for fuel suction feed

42
Q

Limitation for front window heat inop

A

Max 300 kias < 10,000 ft

43
Q

Field elevation vs PFD and stby ALT

A

+/- 40 ft PFD
+/- 120ft STBY

44
Q

CAPT vs FO PFD altitude

45
Q

CAPT vs FO ASI when above 250kts
CAPT vs FO ALT when above FL250

A

+/- 2kts
+/- 100ft

46
Q

Maximum brake temp for T/O

A

Top of green band

47
Q

Minimum Oil temp for Start / Taxi

48
Q

Minimum oil Px to complete flight

A

16 - 25 psi

49
Q

Minimum Px for external air start

50
Q

Maximum guaranteed restart altitude

51
Q

N2 required for “Stabilised”

52
Q

MTL

A

Maintenance Technical Log

53
Q

CRS

A

Certificate of Release to Service

54
Q

NAD

A

Not Airworthiness Defective
(Mx to apply when at maintenance base)

55
Q

CDL

A

Configuration Deviation List

56
Q

Determining rainfall rate in last 10 mins

A

Light < 0.4 mm
Moderate 0.4 - 1.6 mm
Heavy > 1.6 mm

57
Q

Landing on other than dry runways

A

Light = No problem
Moderate = only in CTA if LDR < LDA
Heavy = only in CTA if LDR < LDA

58
Q

Contaminated runway

A

Standing water more than 3mm deep covering more that 25% of the runway surface to be used.
Assessed by flight crew after lining up on takeoff runway.

59
Q

Damp runway

A

Surface is not dry, but moisture on it does not give shiny appearance. Considered to be wet for performance calculations

60
Q

Inbound altitudes V distance CTA

A

9000 until 36 DME
5000 until 22 DME
4000 until 18 DME
2500 until 11 DME

61
Q

Earliest point after takeoff that tail anti ice can be selected?

A

After climb thrust is set

62
Q

Wing and tail anti ice test

A

Prior to descent into Perth on the last flight of a calendar day inbound to Perth, select wing and tail anti ice on for a minimum of 30 seconds then off. Report MFDU faults to MTL. Not required if used previously on that flight

63
Q

When exiting icing conditions with only engine anti ice on, wait how long before turning off?

A

1 minute, or in any case, after the MFDU icing alert has ceased

64
Q

Shut down APU, when can you turn off battery?

A

After 70 seconds to allow for self test unless GPU is available and on

65
Q

Cost index

A

Represents the time cost of operating the aircraft per hour divided by the fuel cost of operating the aircraft. 0 cost index provides a minimum fuel burn per unit time.

66
Q

Minimum fuel on arrival

A

2400 kg planned
2000 kg for alternate
Less than 2000 kg captain discretion for alternate if TAF indicated CAVOK

67
Q

Wake turbulence arriving aircraft

A

Medium behind super - 3 minutes
Medium behind heavy - 2 minutes
Does not apply if on visual approach and pilot reports following aircraft in sight

68
Q

Wake turbulence departing aircraft

A

Medium following heavy - 2 mins / 3 mins for intersection or 5NM
Medium following super - 3 mins / 4 mins for intersection or 7NM

69
Q

TIBA

A

Traffic Information Broadcast by Aircraft

70
Q

Brake temps after RTO

A

5 min for max temp accurate reading
10 mins for subsequent TO

71
Q

TCAS TA
Alerts:
Inhibited:

A

Within 40 seconds
Below 400 RA on descent and 600 RA on climb or if higher priority warning exists
Solid amber dot

72
Q

Proximate traffic

A

Non threat traffic within 6nm and 1200. Solid blue diamond

73
Q

TCAS RA
Too close within?
Inhibits

A

25 seconds
Below 900 RA descent and 11 RA climb

74
Q

Maximum fuel loads

A

A / T: 10,692kg
G: 10,256kg

75
Q

Fuel quantities wing and centre

A

A / T: Wing - 7615 Centre - 2942
G: wing 7647 Centre - 2480
Total 10557 / 10127

76
Q

Approach type selection order

A

ILS
RNP
LOC
RWY ALIGNED VOR
RWY ALIGNED

77
Q

Takeoff segments

A

Ground roll
First segment: liftoff to v2
Second segment: v2 to 400ft
Third segment: accelerate
Final segment: up to 1500 flaps up MCT

F100 NAA Memory Items (2 decks)

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