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DHC8 > OM-B NORMAL > Flashcards

OM-B NORMAL Flashcards

(125 cards)

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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
Automation callouts Engagement of Autopilot
PF “Engage autopilot” PM “Autopilot engage, ”
26
Automation callouts Level 3 or 4 - Selecting modes
PF “ selected” PM “Checked”
27
Automation callouts Level 3 or 4 - Selecting armed modes
PF “ armed” PM “Checked”
28
Automation callouts Level 3 or 4 - Changing parameters
PF “Heading/IAS/VS xxx Set” PM “Checked”
29
Automation callouts Level 3 or 4 - Armed mode automatically engages
PF “ capture” or “ capture” or “LNAV” PM “Checked”
30
Automation callouts Setting course direct to a waypoint
PF “Direct set” PM “Checked”
31
Calls for Altitude Changes and Transitions Altitude changes
PF “ set - ALT SEL armed” PM “Checked”
32
Calls for Altitude Changes and Transitions 1000 feet before selected altitude/ FL
PM “Pre level” PF “ALT SEL armed, QNH xxxx” PM “Checked”
33
Calls for Altitude Changes and Transitions Approaching selected altitude
PF “Altitude capture” PM “Checked”
34
Calls for Altitude Changes and Transitions Transition Altitude
PM “Transition Altitude” PF “1013 FL…” PM “Set and crosschecked”
35
Calls for Altitude Changes and Transitions Transition Level
PM “Transition Level” PF “QNH…..FT” PM “Set and crosschecked”
36
Deviation Calls, Different Phases of Flight Approaching torque limit for current configuration
PM “Torque” PF “Correcting”
37
Deviation Calls, Different Phases of Flight Bank angle exceed 30 degrees
PM “Bank” PF “Correcting”
38
Deviation Calls, Different Phases of Flight Any deviation from lateral or vertical flight path
PF - Explain why deviation is made PM - Verify and accept deviation
39
Deviation Calls, Different Phases of Flight Any improper FGC or FMS selection
PM - Bring attention of the improper selection mode PF - Correct the improper selection
40
Deviation Calls, Different Phases of Flight 1 dot localizer or 5˚ VOR/NDB/ deviation
PM “Track” PF “Correcting”
41
Deviation Calls, Different Phases of Flight 1 dot glide slope deviation
PM “Above/ Below glide slope” PF “Correcting”
42
Deviation Calls, Different Phases of Flight Altitude deviations +/- 100 ft
PM “Altitude Above/ Below” PF “Correcting”
43
Deviation Calls, Different Phases of Flight Speed deviation +/- 10 kts
PM “Speed high/ low” PF “Correcting”
44
Deviation Calls, Different Phases of Flight Briefed Vref -0 / Vtrgt +10 kts
PM “Speed high/ low” PF “Correcting”
45
Deviation Calls, Different Phases of Flight Fast/ slow indicator deviating +/- 0.1
PM “Speed high/ low” PF “Correcting”
46
Deviation Calls, Different Phases of Flight @300 ft AGL and below
If aircraft not within criteria for stabilized approach configuration PM “Go Around” PF “Go Around, Set power Flap 15”
47
Deviation Calls, Different Phases of Flight Passing runway threshold, for Short field; runway edge
If aircraft not within criteria for stabilized landing configuration PM “Go Around” PF “Go Around, Set power Flap 15”
48
Deviation Calls, Different Phases of Flight Circling
PM - Call any deviation from speed/ altitude PF “Correcting”
49
Landing Pitch Deviation Call Out Pitch attitude 8˚ or more during landing
PM “Pitch….” - State actual pitch attitude PF “Correcting”
50
Four basic methods of flying the DHC-8 Level 1
BASIC Where the pilot manually flies the a/c without using the FD
51
Four basic methods of flying the DHC-8 Level 2
GUIDED Where the pilot manually flies the V-bar of the FD
52
Four basic methods of flying the DHC-8 Level 3
DIRECTED Where the AP flies the commands of the FD
53
Four basic methods of flying the DHC-8 Level 4
MANAGED Using LNAV/ VNAV commands from the FMS
54
Summary of actions before a flight First Officer
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
Walk-Around Entering flight deck
Engage all pulled circuit breakers Hydraulic pump handle stowed Smoke goggles, Crew oxygen masks and oxygen quantity Emergency equipment
56
AC TEST XXX/XXX VOLTS: XXX LOAD X.XX After 2 seconds VOLTS: XXX+/-X LOAD X.XX+/-X
INVERTER / VARIABLE FRQUENCY VOLTS: 188 LOAD 1.88 After 2 seconds VOLTS: 150+/-3 LOAD 1.05+/-3
57
DC POWER NORM VOLT: XX-XX Volt MAX: XX,X Volt MIN: XX Volt
DC POWER NORM VOLT: 24-29 Volt MAX: 31,5 Volt MIN: 22 Volt
58
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
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
When parking brake set Minimum pressure indicated?
Min 1500 psi
60
Hydraulic Qty. Check Min #1 og #2?
#1 1,5 US Quarts #2 3,0 US Quarts
61
TAKE-OFF ELEVATOR TRIM VS CG Forward CG: Aft CG:
Forward CG: AFT END (15% MAC) Aft CG: FWD END (38% MAC)
62
USE OF HEADSET On the ground 1: 2:
1: When receiving the ATC departure clearance via voice communication 2: When engines are running
63
USE OF HEADSET In Fligth 1: 2: 3:
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
When should the DEPARTURE BRIEFING be conducted?
By the PF between the preflight og start checklist
65
PF shall before departure briefing:
Have selected departure routing from the FPL/MENU/DEPART if applicable
66
During NORM ENG START F/O tasks:
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
Oil pressure below 75% NH during NORM ENG START is allowed between:
40 and 55 PSI
68
Altimeter checking The altimeter shall not be used is the difference btwn true alt and indicated is:
More than 60 ft apart
69
Altimeter checking Two altimeters Max difference
90 ft Most exact altimeter should be used
70
Maximum speed during taxi
Depending on surface conditions 15 kts, except 30 kts during backtracking on rwy
71
Quiet Taxi mode, the RPM is limited to:
785 RPM
72
Flight control unluck and check should only be performed in:
Headwind
73
Nose When Steering Steering range:
High-speed: 5˚ (Rudder pedals) Low-speed: 60˚ (Steering control handle) Unpowered (caster) mode: 120˚
74
The Autopilot shall not be engaged below?
1000 ft
75
Autopilot and FMS three-step:
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
Takeoff in icing condition Overall concept?
MAKE IT CLEAN AND KEEP IT CLEAN
77
Takeoff in icing conditions Before takeoff (3 items)
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
Climb procedure Type 1
210 KIAS Up to FL100, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS
79
Climb procedure Type 2
170 KIAS Up to FL180, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS
80
Climb procedure Type 3
130 KIAS
81
Climb procedure Company flight plan calculation is basen on which climb type?
Type 2 due to cost factors This should be used when conditions and terrain separation allow
82
If final level is FL190 or lower, propeller RPM may be reduced to:
900 RPM
83
Climb to cruise transition PF will Call “?” And PM will ?
PF “Setting Cruise Power” - adjust pwr and condition levers PM: Monitor torque gauges
84
Climb to cruise transition Use of synchrophaser
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
Passenger briefing should include? 7 items
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
Cruise torque setting Approx. Minimum cost?
75% Torque
87
After cruise torque has been set….
Adjust the friction knob
88
Assigned FL or altitude shall be within an indicated tolerance of:
+/- 50 ft
89
Performance calculations Should not be calculated earlier than?
30 min. Prior estimated time of landing
90
Standard target descent rate V/S
1800 ft/min
91
Non-turbulent conditions normal descent profile Maximum speed
Vmo -10kt or 220 KIAS which ever is lover Using no more than 42-45% torque
92
To take advantage of higher TAS at high altitude Planned TVS and torque?
2200 Ft/min and 20-25% Torque
93
OFP Fuel and time calculations are basen on ____ during descent
AFM Type 1 descent profile
94
Temperature corrections
-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
Recommended holding airspeed
150 KIAS with flaps up
96
To avoid cycling of the outboard Roll spoilers, do not hold at precisely ____ KIAS
140 KIAS
97
Approximate fuel consumption in holding and conditions
PWR as required 900 RPM 400 Kgs/Hr @FL100, ISA, 125 KIAS
98
Minimum holding speed in icing conditions
160 KIAS More than light icing, its recommended to set condition levers fully forward
99
Callouts during climb
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
Stabilized approach parameters Speed @1000 ft AAL
Lower limit: Vref -5 Upper limit: Vtrgt +20
101
Stabilized approach parameters Speed @300 ft AAL
Lower limit: Vref -5 Upper limit: Vtrgt +10
102
Stabilized approach parameters ROD @1000 ft AAL
Precision and non-precision: Max 1500 ft/min Visual and circling: Max 2000 ft/min
103
Stabilized approach parameters ROD @300 ft AAL
Precision and non-precision: Max 1000 ft/min Visual and circling: Max 1000 ft/min
104
Stabilized approach parameters Configuration
Flaps for landing, gear down
105
Stabilized approach parameters Precision approach
1 dot LOC/GP
106
Stabilized approach parameters Non-Precision approach
1 dot/ 5˚NDB
107
Stabilized approach parameters Visual and circling
Wings level
108
Max ft/min during steep approach
1450 ft/min
109
Unstabilized approach callouts Airspeed outside stabilized LIMITS from briefed Vtrgt or Airspeed -5 from flaps Max limit speed
PM: “Airspeed” PF: “Go-around” or “Correcting”
110
Unstabilized approach callouts Rate of descent in excess of stabilized approach parameters
PM: “Descent rate” PF: “Go-Around” or “Correcting”
111
With PROP’s not at MAX RPM What to look for?
An engine overtorque can occur if a sudden climb or go-around is performed
112
Minimum descent altitude during a visual app
500 ft AAL
113
DH setting shall be set no later than
2500 ft AAL
114
DH setting for visual approach
0 ft
115
DH setting for precision approach
200 ft AAL (or applicable minima if higher)
116
DH setting for non-precision
300 ft
117
During proceedures with procedure turn VNAV shall not be armed until
The a/c is established on the final approach track
118
RNAV/ GNSS approach must be discontinued When one of the following occurs
1. SATTELITE POS ALARM (Indicated on FMS) 2. GPS accuracy downgraded INTEG annunciation
119
Normal minimum torque setting during approach
15% torque
120
Max pitch during flare
6˚ to 8˚ nose up
121
Landing with 1050 NP may only be performed
To runway longer then 1000 meters
122
Prior setting T/O power on wet and contaminated runway
Confirm AUTO IGNITION prior setting T/O power
123
Prior T/O in ice conditions or where icing is likely Minimum oil temp
45˚
124
Propeller de-icing may be enhanced by periodically selecting condition levers….
To maximum (1200 RPM)
125
Torque setting for approximate minimum cost
75% torque

DHC8 (3 decks)

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