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DHC8 > OM-B NORMAL > Flashcards

OM-B NORMAL Flashcards

1
Q

Checklist trigger point
Preflight

A

Pre takeoff data received

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2
Q

Checklist trigger point
Start

A

W&B completed, Doors closed, and if possible, clearance/ traffic received

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3
Q

Checklist trigger point
After start

A

Both pilots flow complete

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4
Q

Checklist trigger point
Before Takeoff

A

Cabin Secure received and takeoff imminent

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5
Q

Checklist trigger point
Climb

A

Passing transition altitude*

*Short flights, ex. JEG-JAV, complete climb and approach checklist at an appropriate time

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6
Q

Checklist trigger point
Approach

A

Cleared for Descent below FL100 and no later than when cleared to altitude*

*Short flights, ex. JEG-JAV, complete climb and approach checklist at an appropriate time.

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7
Q

Checklist trigger point
Landing

A

Prop full increase or 1050

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8
Q

Checklist trigger point
Anti-collision lights - on

A

Upon entering the runway environment

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9
Q

Checklist trigger point
Landing lights - on, taxi lights - off

A

Cleared for takeoff or just prior to takeoff run

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10
Q

Checklist trigger point
Taxi light on

A

Cleared for landing / no traffic on the runway reported

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11
Q

PF phase of flight responsibilities (general)

A

Taxiing (normally performed by LP)
Flight path and airspeed control
Airplane configuration
Navigation

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12
Q

PM phase of flight responsibilities (general)

A

Checklist Reading
Communications
Task asked for by the PF
Monitoring taxiing, flight path, airspeed, airplane configuration, and navigation

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13
Q

Terms regarding power settings
Full power

A

Firewall power

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14
Q

Terms regarding power settings
Max power

A

Max. Certified power (5 min limit)
TORQUE: In-flight (107,5%)

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15
Q

Terms regarding power settings
Max Takeoff (MTOP) power

A

Max. Certified power (5 min. Limit)
TORQUE: (Static 109,5%) (In-flight 107,5%)

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16
Q

Terms regarding power settings
Normal Takeoff (NTOP) power

A

TORQUE: (Static 99,5%) (In-flight 97,5%)

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17
Q

Terms regarding power settings
Max Continuous power (MCP)

A

According to torque power chart
TORQUE: (In-flight 97,5%)

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18
Q

Terms regarding power settings
Max Cruise power

A

According to torque power chart
TORQUE: (In-flight 114,2%)

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19
Q

Terms regarding power settings
“Power set”

A

Confirmation that requested power is set, and engine instruments checked for normal indications

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20
Q

Terms regarding power settings
“Set power…(TQ)..”

A

Calculated power given in terms of torque

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21
Q

Automation callouts
Level 2 - Selecting modes

A

PF “Select <mode>”
PM “<mode> selected”
PF “Checked”</mode></mode>

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22
Q

Automation callouts
Level 2 - Selecting armed modes

A

PF “Arm <mode>”
PM “<mode> armed”
PF “Checked”</mode></mode>

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23
Q

Automation callouts
Level 2 - Armed mode automatically engages

A

PF “<mode> capture” or “<radial> capture” or “LNAV”
PM “Checked”</radial></mode>

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24
Q

Automation callouts
Level 2 - Changing parameters

A

PF “Set Heading/IAS/VS xxx”
PM “Heading/IAS/VS xxx set”

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25
Q

Automation callouts
Engagement of Autopilot

A

PF “Engage autopilot”
PM “Autopilot engage, <mode>”</mode>

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26
Q

Automation callouts
Level 3 or 4 - Selecting modes

A

PF “<mode> selected”
PM “Checked”</mode>

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27
Q

Automation callouts
Level 3 or 4 - Selecting armed modes

A

PF “<mode> armed”
PM “Checked”</mode>

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28
Q

Automation callouts
Level 3 or 4 - Changing parameters

A

PF “Heading/IAS/VS xxx Set”
PM “Checked”

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29
Q

Automation callouts
Level 3 or 4 - Armed mode automatically engages

A

PF “<mode> capture” or “<radial> capture” or “LNAV”
PM “Checked”</radial></mode>

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30
Q

Automation callouts
Setting course direct to a waypoint

A

PF “Direct <waypoint> set”
PM “Checked”</waypoint>

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31
Q

Calls for Altitude Changes and Transitions
Altitude changes

A

PF “<FL/ ALTITUDE> set - ALT SEL armed”
PM “Checked”

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32
Q

Calls for Altitude Changes and Transitions
1000 feet before selected altitude/ FL

A

PM “Pre level”
PF “ALT SEL armed, QNH xxxx”
PM “Checked”

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33
Q

Calls for Altitude Changes and Transitions
Approaching selected altitude

A

PF “Altitude capture”
PM “Checked”

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34
Q

Calls for Altitude Changes and Transitions
Transition Altitude

A

PM “Transition Altitude”
PF “1013 FL…”
PM “Set and crosschecked”

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35
Q

Calls for Altitude Changes and Transitions
Transition Level

A

PM “Transition Level”
PF “QNH…..FT”
PM “Set and crosschecked”

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36
Q

Deviation Calls, Different Phases of Flight
Approaching torque limit for current configuration

A

PM “Torque”
PF “Correcting”

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37
Q

Deviation Calls, Different Phases of Flight
Bank angle exceed 30 degrees

A

PM “Bank”
PF “Correcting”

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38
Q

Deviation Calls, Different Phases of Flight
Any deviation from lateral or vertical flight path

A

PF - Explain why deviation is made
PM - Verify and accept deviation

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39
Q

Deviation Calls, Different Phases of Flight
Any improper FGC or FMS selection

A

PM - Bring attention of the improper selection mode
PF - Correct the improper selection

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40
Q

Deviation Calls, Different Phases of Flight
1 dot localizer or 5˚ VOR/NDB/ deviation

A

PM “Track”
PF “Correcting”

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41
Q

Deviation Calls, Different Phases of Flight
1 dot glide slope deviation

A

PM “Above/ Below glide slope”
PF “Correcting”

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42
Q

Deviation Calls, Different Phases of Flight
Altitude deviations +/- 100 ft

A

PM “Altitude Above/ Below”
PF “Correcting”

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43
Q

Deviation Calls, Different Phases of Flight
Speed deviation +/- 10 kts

A

PM “Speed high/ low”
PF “Correcting”

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44
Q

Deviation Calls, Different Phases of Flight
Briefed Vref -0 / Vtrgt +10 kts

A

PM “Speed high/ low”
PF “Correcting”

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45
Q

Deviation Calls, Different Phases of Flight
Fast/ slow indicator deviating +/- 0.1

A

PM “Speed high/ low”
PF “Correcting”

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46
Q

Deviation Calls, Different Phases of Flight
@300 ft AGL and below

A

If aircraft not within criteria for stabilized approach configuration
PM “Go Around”
PF “Go Around, Set power Flap 15”

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47
Q

Deviation Calls, Different Phases of Flight
Passing runway threshold, for Short field; runway edge

A

If aircraft not within criteria for stabilized landing configuration
PM “Go Around”
PF “Go Around, Set power Flap 15”

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48
Q

Deviation Calls, Different Phases of Flight
Circling

A

PM - Call any deviation from speed/ altitude
PF “Correcting”

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49
Q

Landing Pitch Deviation Call Out
Pitch attitude 8˚ or more during landing

A

PM “Pitch….” - State actual pitch attitude
PF “Correcting”

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50
Q

Four basic methods of flying the DHC-8
Level 1

A

BASIC
Where the pilot manually flies the a/c without using the FD

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51
Q

Four basic methods of flying the DHC-8
Level 2

A

GUIDED
Where the pilot manually flies the V-bar of the FD

52
Q

Four basic methods of flying the DHC-8
Level 3

A

DIRECTED
Where the AP flies the commands of the FD

53
Q

Four basic methods of flying the DHC-8
Level 4

A

MANAGED
Using LNAV/ VNAV commands from the FMS

54
Q

Summary of actions before a flight
First Officer

A

Check the A/C shelf for revisions to be inserted in the aircraft documentation
Update personal and the shared EFB from crew lounge
Charge the Apple Pencil of the shared EFB

55
Q

Walk-Around
Entering flight deck

A

Engage all pulled circuit breakers
Hydraulic pump handle stowed
Smoke goggles, Crew oxygen masks and oxygen quantity
Emergency equipment

56
Q

AC TEST
XXX/XXX
VOLTS: XXX LOAD X.XX
After 2 seconds
VOLTS: XXX+/-X LOAD X.XX+/-X

A

INVERTER / VARIABLE FRQUENCY
VOLTS: 188 LOAD 1.88
After 2 seconds
VOLTS: 150+/-3 LOAD 1.05+/-3

57
Q

DC POWER
NORM VOLT: XX-XX Volt
MAX: XX,X Volt
MIN: XX Volt

A

DC POWER
NORM VOLT: 24-29 Volt
MAX: 31,5 Volt
MIN: 22 Volt

58
Q

DC TEST
VOLTS XX.X LOAD M.B. X.XX GEN/TRU A.B X.XX LOAD X.XX
After 2 seconds
VOLTS XX.X+/-X.X LOAD X.XX+/-X,X

A

DC TEST
VOLTS 88.8 LOAD M.B. 1.88 GEN/TRU A.B 1.88 LOAD 1.88
After 2 seconds
VOLTS 30.5+/-0.3 LOAD 1.05+/-0,3

59
Q

When parking brake set
Minimum pressure indicated?

A

Min 1500 psi

60
Q

Hydraulic Qty. Check
Min #1 og #2?

A

1 1,5 US Quarts

#2 3,0 US Quarts

61
Q

TAKE-OFF ELEVATOR TRIM VS CG
Forward CG:
Aft CG:

A

Forward CG: AFT END (15% MAC)
Aft CG: FWD END (38% MAC)

62
Q

USE OF HEADSET
On the ground
1:
2:

A

1: When receiving the ATC departure clearance via voice communication
2: When engines are running

63
Q

USE OF HEADSET
In Fligth
1:
2:
3:

A

1: During climb out until passing 10.000 ft
2: When receiving oceanic ATC clearance via voice communication
3: Whenever deemed necessary by either pilot

64
Q

When should the DEPARTURE BRIEFING be conducted?

A

By the PF between the preflight og start checklist

65
Q

PF shall before departure briefing:

A

Have selected departure routing from the FPL/MENU/DEPART if applicable

66
Q

During NORM ENG START
F/O tasks:

A

1: Check side clear (if ENG #2)
2: Start timing
3: Observe oil pressure and hydraulic pressure rising
4: Observe starter cut out above 60% NH

67
Q

Oil pressure below 75% NH during NORM ENG START is allowed between:

A

40 and 55 PSI

68
Q

Altimeter checking
The altimeter shall not be used is the difference btwn true alt and indicated is:

A

More than 60 ft apart

69
Q

Altimeter checking
Two altimeters Max difference

A

90 ft
Most exact altimeter should be used

70
Q

Maximum speed during taxi

A

Depending on surface conditions
15 kts, except 30 kts during backtracking on rwy

71
Q

Quiet Taxi mode, the RPM is limited to:

A

785 RPM

72
Q

Flight control unluck and check should only be performed in:

A

Headwind

73
Q

Nose When Steering
Steering range:

A

High-speed: 5˚ (Rudder pedals)
Low-speed: 60˚ (Steering control handle)
Unpowered (caster) mode: 120˚

74
Q

The Autopilot shall not be engaged below?

A

1000 ft

75
Q

Autopilot and FMS three-step:

A

1: Anticipate - Understand system/ modes and know what to expect
2: Execute - Perform action on FGC or FMS
3: Confirm - X-check modes and entries. After each action in FGC verify ADU

76
Q

Takeoff in icing condition
Overall concept?

A

MAKE IT CLEAN AND KEEP IT CLEAN

77
Q

Takeoff in icing conditions
Before takeoff (3 items)

A

1: Check for stable engine operation before releasing the brakes
2: Observe Ice-speed increments as per TOLD card
3: Oil temp. Must be maintained above 45˚C to ensure adequate air inlet splitter anti-icing

78
Q

Climb procedure
Type 1

A

210 KIAS Up to FL100, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS

79
Q

Climb procedure
Type 2

A

170 KIAS Up to FL180, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS

80
Q

Climb procedure
Type 3

A

130 KIAS

81
Q

Climb procedure
Company flight plan calculation is basen on which climb type?

A

Type 2 due to cost factors
This should be used when conditions and terrain separation allow

82
Q

If final level is FL190 or lower, propeller RPM may be reduced to:

A

900 RPM

83
Q

Climb to cruise transition
PF will Call “?” And PM will ?

A

PF “Setting Cruise Power” - adjust pwr and condition levers
PM: Monitor torque gauges

84
Q

Climb to cruise transition
Use of synchrophaser

A

With synchrophaser on, move conditionlevers slowly and in sync.
If more than 20 RPM in diff. With conditionlevers at min, deactivate synchrophaser, adjust within 20 RPM and re-engage

85
Q

Passenger briefing should include?
7 items

A

1: Statement of dest. And route
2: Cruise alt
3: Wx at dest.
4: Wx enroute
5: Special info regarding connections
6: Wx at Ultimate dest.
7: Relevant changes

86
Q

Cruise torque setting
Approx. Minimum cost?

A

75% Torque

87
Q

After cruise torque has been set….

A

Adjust the friction knob

88
Q

Assigned FL or altitude shall be within an indicated tolerance of:

A

+/- 50 ft

89
Q

Performance calculations
Should not be calculated earlier than?

A

30 min. Prior estimated time of landing

90
Q

Standard target descent rate V/S

A

1800 ft/min

91
Q

Non-turbulent conditions normal descent profile
Maximum speed

A

Vmo -10kt or 220 KIAS which ever is lover
Using no more than 42-45% torque

92
Q

To take advantage of higher TAS at high altitude
Planned TVS and torque?

A

2200 Ft/min and 20-25% Torque

93
Q

OFP Fuel and time calculations are basen on ____ during descent

A

AFM Type 1 descent profile

94
Q

Temperature corrections

A

-5˚C to -25˚C - 10% of height above AD
-25˚C to -40˚C - 20% of height above AD
Below -40˚C - 30% of height above AD

95
Q

Recommended holding airspeed

A

150 KIAS with flaps up

96
Q

To avoid cycling of the outboard Roll spoilers, do not hold at precisely ____ KIAS

A

140 KIAS

97
Q

Approximate fuel consumption in holding and conditions

A

PWR as required
900 RPM
400 Kgs/Hr @FL100, ISA, 125 KIAS

98
Q

Minimum holding speed in icing conditions

A

160 KIAS
More than light icing, its recommended to set condition levers fully forward

99
Q

Callouts during climb

A

PF: Set 70% torque - “Climbing, Set climb power”
PM: Adjust power to climb power - “Climb power set, your power levers”
PF: “My power levers”

100
Q

Stabilized approach parameters
Speed @1000 ft AAL

A

Lower limit: Vref -5
Upper limit: Vtrgt +20

101
Q

Stabilized approach parameters
Speed @300 ft AAL

A

Lower limit: Vref -5
Upper limit: Vtrgt +10

102
Q

Stabilized approach parameters
ROD @1000 ft AAL

A

Precision and non-precision: Max 1500 ft/min
Visual and circling: Max 2000 ft/min

103
Q

Stabilized approach parameters
ROD @300 ft AAL

A

Precision and non-precision: Max 1000 ft/min
Visual and circling: Max 1000 ft/min

104
Q

Stabilized approach parameters
Configuration

A

Flaps for landing, gear down

105
Q

Stabilized approach parameters
Precision approach

A

1 dot LOC/GP

106
Q

Stabilized approach parameters
Non-Precision approach

A

1 dot/ 5˚NDB

107
Q

Stabilized approach parameters
Visual and circling

A

Wings level

108
Q

Max ft/min during steep approach

A

1450 ft/min

109
Q

Unstabilized approach callouts
Airspeed outside stabilized LIMITS from briefed Vtrgt or
Airspeed -5 from flaps Max limit speed

A

PM: “Airspeed”
PF: “Go-around” or “Correcting”

110
Q

Unstabilized approach callouts
Rate of descent in excess of stabilized approach parameters

A

PM: “Descent rate”
PF: “Go-Around” or “Correcting”

111
Q

With PROP’s not at MAX RPM
What to look for?

A

An engine overtorque can occur if a sudden climb or go-around is performed

112
Q

Minimum descent altitude during a visual app

A

500 ft AAL

113
Q

DH setting shall be set no later than

A

2500 ft AAL

114
Q

DH setting for visual approach

A

0 ft

115
Q

DH setting for precision approach

A

200 ft AAL (or applicable minima if higher)

116
Q

DH setting for non-precision

A

300 ft

117
Q

During proceedures with procedure turn
VNAV shall not be armed until

A

The a/c is established on the final approach track

118
Q

RNAV/ GNSS approach must be discontinued
When one of the following occurs

A
  1. SATTELITE POS ALARM (Indicated on FMS)
  2. GPS accuracy downgraded INTEG annunciation
119
Q

Normal minimum torque setting during approach

A

15% torque

120
Q

Max pitch during flare

A

6˚ to 8˚ nose up

121
Q

Landing with 1050 NP may only be performed

A

To runway longer then 1000 meters

122
Q

Prior setting T/O power on wet and contaminated runway

A

Confirm AUTO IGNITION prior setting T/O power

123
Q

Prior T/O in ice conditions or where icing is likely
Minimum oil temp

A

45˚

124
Q

Propeller de-icing may be enhanced by periodically selecting condition levers….

A

To maximum (1200 RPM)

125
Q

Torque setting for approximate minimum cost

A

75% torque

DHC8 (3 decks)

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