Pseudo Memory Items Flashcards

1
Q

What are limitations on climb power?

   - Outside Icing conditions 
   - Inside Icing conditions
A

Less of 90% or climb power chart

Climb charts TRQ in icing

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2
Q

When checking landing weight from FMS and comparing it to FLaPs program. What must it be inside ?

A

250kg. If outside this figure. Crew must investigate why

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3
Q

Descent Calculation ?

Effects of HW & TW

A

3 x feet to lose

HW subtract 1nm per 10kts

TW add 1nm per 10kts

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4
Q

Signal to cabins 2 chimes indicates what ?

A

5 minutes until landing - or

5 minutes to the commencement of an instrument approach

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5
Q

When selecting Gear Down - what must you also select?

A

Taxi Light and

Auto coarsen

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6
Q

What are the speed tolerances before the PNF must call “SPEED” ?

A

+/- 10kts

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7
Q

When must prop sync be switched on and off?

A

Must be switched:

ON - during climb scan action flow after CL’s are set to 1230rpm

OFF - prior to selecting CL’s to Max for an approach or Landing.

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8
Q

On landing Vfa must be bugged.

If two bugs Vfa and Venroute will both be set. If only 1 bug available what must you set.

A

If Vfa is less than Venroute than you will set Vfa

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9
Q

What occurs at:

80kts

40kts

A

80kts - your ailerons

40kts - Gust Lock

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10
Q

If a go around is initiated prior to the FAF or prior to 1000ft Visual.

What power setting do you set ?

A

Manually set approx 80% and adjust as required.

As CTOT valve is calculated at aerodrome level you may risk over temp/TRQ at a higher altitude.

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11
Q

What is MCP?

A

MCP is 944 degrees ITT and initially no greater than 100% TRQ until referring to MCP table.

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12
Q

In icing conditions Normal operations what Venroute speed shall be adapted as recommended by SAAB?

A

160kts

If 160kts and an average of 500fpm cannot be maintained considering leaving current icing conditions.

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13
Q

On a cold day why may:

ENG OIL BYPASS illuminate ?

FUEL TEMP LOW illuminate ?

A

ENG OIL BYPASS - due to high oil viscosity

FUEL TEMP LOW - as the PGB oil is not acting as a heating medium for the fuel heater as yet.

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14
Q

What power condition shall be used in icing conditions ?

A

Rated Power

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15
Q

What is a precautionary method of determining the accretions of ice on the ACFT?

A

Bug your current Speed and any deterioration from this speed may indicates accumulation of ice on the ACFT surfaces

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16
Q

What should you consider when climbing AEO in mod/sev turb ?

A

Should consider increasing speed by 10-15kts as the alpha vanes are sensitive to fluctuations in load factor

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17
Q

What climb speeds relate to the segments below:

  • T/O to Acceleration Altitude
  • Acceleration Altitude to MMA/MSA/LSA
  • MMA to further
A
  • V2 safety speed
  • Venroute +10 (icing). +20 icing and 1/2 bank off if (OEI)
  • Further acceleration above MSA/MMA/LSA
    160kts or into L,M,H climb
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18
Q

Why must L,M,H climb modes not be used in icing conditions ?

A

As there is no IAS protection, the autopilot logic will try and maintain a min 100fpm rate of climb regardless of IAS

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19
Q

What are L,M,H climb modes?

A

Low - Best rate of climb outside icing conditions

Medium - compromise between Low and High

High - gives optimum distance/altitude ratio

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20
Q

If a TIMER master caution is experienced what must be done?

A

Increase TRQ up to 25-30% to achieve sufficient LP bleed air, once extinguished reactive boots.

If illuminates again refer QRH

A ruptured boot may also indicated a torn or ruptured boot. Landings with this shall be conducted at Flap 0

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21
Q

Low Vis take off requirement if below 550RVR?

A

LP take off only

Commands from PM - Steer Left/Right. PF - checked

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22
Q

Selecting HP’s on the ground with feathered props ?

A

PL - 77%
HP Bleeds - OPEN
PL - Restore 77%

consider X-VALVE for increased airflow

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23
Q

Descent speeds HIGH & LOW ?

A

LOW - 220KIAS

HIGH - 250KIAS

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24
Q

What is defined as a stabilised approach ?

A

The aircraft is on track

Aircraft is on an slope

The aircraft is in proposed landing config (Flap 35 may be delayed until 500’)

Speed is within limits

ROD not more than 1000fpm

Appropriate power setting is selected

Requires no more than normal corrections to stay on profile

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25
Q

Bank angle shall not exceed what below 300ft ?

A

15 degrees

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26
Q

When can the approach checklist be conducted ?

A

Only once the FA has been alerted of the 5 minute to landing or start of an IAP

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27
Q

When must you commit to the briefed speeds? Eg. with EAI on

A

The approach checklist is the commit point for briefed speeds. Even if EAI comes off and ICE SPD XXLD after the approach checklist you just still comply with Original speeds

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28
Q

Max roll trim tolerance for dispatch ?

A

+/- 0.5 unit from neutral

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29
Q

If anti-skid is off for takeoff or Landing, what must be consulted ?

A

Takeoff and landing performance data relating to anti skid inop

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30
Q

What does a series of - - - - - - indicate on a checklist ?

A

That checklist item must not be completed until that stage in checklist.
Command Item

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31
Q

Tailwind start min Ng and ITT?

A

20% and 150 degrees

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32
Q

If engine RPM increases prior to what Prop rpm must you put CL to fuel off ?

A

A model - 581prpm

B model - 830prpm

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33
Q

If EAI is selected on and even if ICE SPD has been canceled what time frame will it activate after takeoff ?

A

6 minutes

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34
Q

If making a non standard circuit turn what height shall it be conducted ?

A

2000ft AGL

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35
Q

When climb setting is set you must compare delta TRQ valves with placard.

Above what temp range must you apply QRH procedure ?

A

If the delta TRQ is out by more than 30 degrees the QRH must be consulted

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36
Q

After reaching final or intermediate climb level what must the PF call?

A

PF calls - maintaining FL ….

PNF - Checked

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37
Q

Descent TRQ setting.

A

KIAS - 100/ 2 + 5% for level flight torque

Then subtract 10% TRQ for every 500pm

Eg: 200KIAS level flight for descent at 200KIAS

200-100/2 = 50 + 5 = 55%

Descent 1500fpm = 55 - (30%) = 25%

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38
Q

Crew must not descend below 1000ft AGL or commence an IAP until ?

A

Cabin is secure

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39
Q

When setting climb power and ITT limits below 150 or above 150 are exceeded before tabulated TRQ what must you do ?

A

In this case you may exceed ITT limits by reducing tabulated torque by 5%.

Eg 80%
When setting ITT limit gives 73%

Use TRQ of 80-5 = 75%

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40
Q

What are the calls when EAI is selected off in regards to ICE SPD ?

A

PNF will deselect the ICE SPD button and call “ICE SPD OFF”

The PF will then confirm and reply “CHECKED”

41
Q

After exiting icing conditions how long must EAI remain on for ?

A

5 minutes

42
Q

Once EAI is selected on, the PNF (or crew member who selected it on) to say “ICE SPD ON”

The PF will then do what ?

A

Set relevant Ice speeds and call “SPEED BUGGED”

The PNF will confirm and bug his side and say “CHECKED”

43
Q

What speed is hydroplaning in the SAAB?

A

95kts

44
Q

If the FMS is switched off for engine start how long will data be stored for ?

A

7 minutes

45
Q

What takes precedence in order if the following:

TCAS
STALL
TAWS

A
  1. STALL
  2. TAWS/GPWS
  3. TCAS
46
Q

In EMERGENCY/ABNORMAL procedures what must be done prior to descending below the MSA?

A

All emerg/abnormal checklists and briefings should be completed before descent below the MSA or leaves a holding pattern for the applicable approach

47
Q

When restoring power on a failed engine what must you ensure ?

A

Must ensure autocoarsen switch is OFF until power levers are at the same PLA

48
Q

In the case of a major failure eg: EFATO, double engine flame out, engine fire, what is priority memory items or master warnings and cautions ?

A

If your in a critical stage and the failure is one of the above you will identify the failure without reference to master warnings or cautions.

Conduct memory items then when time permits master warnings should be identified followed by cautions

49
Q

Criteria for Rejected Take-off :

A
  • Failure to achieve predicted T/O power
  • 944 exceeded
  • Engine failure/fire
  • illumination of MSTR WARNING
  • Structural Failure
  • Directional Control issue
50
Q

If there is an engine fire on TO with no power loss when shall Memory Items be conducted?

A

After the AEO flap retraction altitude (400ft)

51
Q

Prior to shutting down a gas generator what must you ensure speed wise ?

A

You must be at a minimum Venroute+10 prior to shut down

Once engine is secured, speed must be adjusted to OEI best angle climb = Venroute and 1/2 Bank ON

52
Q

When should master warnings and cautions be confirmed and cancelled ?

A

Once the PF has the ACFT stabilised and prior to the acceleration altitude time permitting

53
Q

Prior to initiating a OEI go around what must you ensure ?

A

Both LP and HP bleeds are closed to ensure maximum power is available

When calculating CTOT setting ensure the ECS OFF figure is used

54
Q

What timeframe should MCP be set after setting TO power on a OEI go around ?

A

MCP shall be set within 5 minutes

55
Q

During a double engine flameout what attitude shall you achieve ?

A

5 degrees nose up to prevent rapid decay in IAS this will also aid the 130KIAS

56
Q

What are the limits that apply to a RA to do with Pitch and Speed?

A

AEO - pitch: +/- 15 degrees
speed: V2 or Venroute+10 in icing

OEI - pitch: +6.5 and -15 degrees
speed: V2 or Venroute+10 in icing

57
Q

What will the PNF and PF call during an over speed condition ?

A

PNF - over speed warning

PF - checked

*overspeed warning occurs @ Vmo +1.5kts

58
Q

What speed should you maintain once airborne in take off windshear ?

A

V2+25

59
Q

TCAS symbols:

  • RA
  • TA
  • PROXIMATE TFC
  • OTHER TFC
A

RA - Red filled square (15-35 seconds)

TA - Solid Amber Circle (20-48 seconds)

Proximate - solid white/cyan diamond (+/-1200ft & 6nm)

Other - open white/cyan diamond

60
Q

How to get TAWS displayed on MFD?

A

Select WX on MFD and then press DISP on glareshield

61
Q

How to get TAWS display on EHSI ?

A

Select RR on DSP and press DISP.

ENSURE RADAR IS ON

62
Q

In regards to TAWS what significance is the colours:
GREEN
YELLOW
RED

A

GREEN - terrain is below the aircraft

YELLOW & RED - terrain displayed is at or above aircraft level. Therefore operational significance

63
Q

What do the ECCL colours and symbols indicate?

PINK 
WHITE 
BLUE 
* 
S
A

PINK - read and do

WHITE - challenge and response

BLUE - procedures for X-feed operations. Read and do

    • Memory Items

S - operationally significant items. Confirmation from PF must be obtained before actioning

64
Q

When will the LP call for engine start checklist ?

A

After the park brake is checked on and chocks removed. Also when both pilots are seated the LP will call “engine start checklist”

65
Q

When will the LP call for “set flap 0 (or 15) taxi checklist” ?

A

LP will call this once commenced taxi and clear of congested areas

66
Q

When shall the PF call for the climb checklist ?

A

PF will call the climb checklist when:

  • The departure report has been given
  • The aircraft is above the MSA/LSA
  • Established on track or on the SID if applicable
67
Q

When will the transition checklist be called by the PF ?

A

The transition checklist will be called after the transition scan has been completed by the PNF.

68
Q

When will the descent checklist be completed ?

A

The descent checklist will be complete after the descent scan action flow.

The PNF and PF will set altimeters as part of the scan close to the transition.
Then the descent checklist will be called for

69
Q

When will the approach checklist be called for ?

A

???? Finding out

70
Q

When will the final checklist be called for ?

A

It will be PF discretion. May call it after IAF and compete up until flaps.

PNF will say flaps next….

Then once flap 20 is selected can call it again.
Or hold off on the checklist until the aircraft is fully configured.

Personally I would call for it after selecting Flap 20 ?

71
Q

When should the after landing checklist be completed ?

A

The after landing scan will be completed once the aircraft is backtracking or clear of the active runway.

Once scan is complete the checklist may be called for by the LP

72
Q

Class C

Airways clearance ?

A

Sydney delivery,
REX6166
To ORANGE
Request clearance

73
Q

Class C

Taxi clearance

A

SYDNEY GROUND
REX6166
INFO ALPHA
REQUEST TAXI

74
Q

Class C airborne report

A
SYDNEY DEPARTURES 
REX6166
Left heading 280 
Passing 3000
On climb 5000
75
Q

Class C first contact with approach

A
SYDNEY APPROACH 
REX6166 
Cleared to 9000
Information ALPHA
(Visual)
76
Q

Class D clearance report

A

ABX GND
REX6767
TO SYDNEY
REQUEST CLEARANCE

77
Q

Class D Taxi

A

ABX GND
REX6767
INFO APLHA
REQUEST TAXI

78
Q

Class D departure report

A

ABX TWR
REX6767
TRACKING 020
Climbing 8000

79
Q

Class D inbound

A
ABX TWR 
REX6767
SAAB 340 
INFO ALPHA 
25nm inbound on the 020 radial descending to 6000 
(visual)
80
Q

Class G departure report with Surveillance coverage

A
MELB CENTRE 
REX6161 
5nm east of orange 
Passing 5500
On climb FL130
MEEGA at 04
81
Q

Class G inbound call to centre

A
MELB CENTRE and all stations Orange 
REX6166
SAAB340
35nm east of orange 
Leaving FL120 inbound 
Estimating circuit 52 
Centre and all stations Orange
82
Q

MAYDAY format

A
MAYDAY x3 
MELB centre 
REX6161
Emergency or any other situation 
Intentions 
Position and level 
Any other info
83
Q

PAN CALL format

A
PAN PAN x3
MELB centre 
REX6161
Medical emergency, controlled engine failure etc 
Intentions 
Level and position 
Any other info
84
Q

AC Duct over temp occurs at ?

AC unit
Distribution Duct

A

AC unit - 225 degrees

Distribution- 82 degrees

85
Q

BLD FAULT LIGHT

A

Occurs if

Bleed air temp too high - 228 degrees

Pressure is too high. 43.5psi
Or
Bleed valve is not closed after a closed position

86
Q

HP HIGH LIGHT

A

Will illuminate if fails to close after a closed signal

87
Q

Tail pipe hot occurs at what temp ?

A

235 degrees

88
Q

Wake turb questions AIP

A

We are classified as medium:

Heavy to Medium -
arrival = 2 mins,
departure full length = 2 min,
intermediate = 3 mins

Super to Medium -
arrival = 3 mins,
departure full length = 3 mins,
intermediate = 4 mins

Heavy to medium - 5nm
Super to medium - 7nm

89
Q

Wind increment to Vref ?

A

Half wind speed, plus the gust

90
Q

De icing boots.

A

Must be operated in CONT -

  • In icing conditions
  • any I’ve observed on aircraft
  • if not certain of ice accumulation

If SAT is below -40 use boots only if ice is accumulating.

They can be switched off:

  • SAT warmer than +5
  • no visible moisture and 3 de-ice boot cycles are complete (9 minutes in CONT)
  • if entering below -40, turn boots off prior to completion of 3 cycles
91
Q

Missed approach gradient and terrain clearance ?

A

2.5% (152fpm) and guarantees 100ft obstacle clearance

92
Q

What obstacle clearance does 10 and 25nm MSA’s give ?

A

1000ft

93
Q

What does the bustie connection do ?

A

Connects L and R bus together and allows external power (or a single gen) to power both sides of the bus

94
Q

How do you get to RAIM PREDIC on FMS ?

A

FLIGHT PLAN - MENU - RAIM

95
Q

How to get to BARO AID on FMS ?

A

DATA - DATA - ADC - BARO

96
Q

What are checks prior to instrument approach ?

A
B - BARO 
R - RAIM 
A - APP ARMED 
C - CONFIDENCE CHECK 
E - EFIS (lowest range on knob ? ) 
D - DME DESELECT 
5 - 5 min warning cabin.
97
Q

What certification must the SAAB meet for depressurisation timing

A

Must be able to descend to FL140 in 4 minutes

98
Q

When must you use rated power ?

A

ENG ANTI ICE ON
VIS LESS THAN 1000M
TURB/WINDSHEAR
ANTISKID INOP
GEAR DOWN DISPATCH
NOSEWHEEL STEERING INOP
GROUND DEICING
CTOT SYSTEM INOP

99
Q

How long must wait between bat cart or bat starts ?

A

1 minute starter gen cool down