OM-B NORMAL Flashcards
Checklist trigger point
Preflight
Pre takeoff data received
Checklist trigger point
Start
W&B completed, Doors closed, and if possible, clearance/ traffic received
Checklist trigger point
After start
Both pilots flow complete
Checklist trigger point
Before Takeoff
Cabin Secure received and takeoff imminent
Checklist trigger point
Climb
Passing transition altitude*
*Short flights, ex. JEG-JAV, complete climb and approach checklist at an appropriate time
Checklist trigger point
Approach
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.
Checklist trigger point
Landing
Prop full increase or 1050
Checklist trigger point
Anti-collision lights - on
Upon entering the runway environment
Checklist trigger point
Landing lights - on, taxi lights - off
Cleared for takeoff or just prior to takeoff run
Checklist trigger point
Taxi light on
Cleared for landing / no traffic on the runway reported
PF phase of flight responsibilities (general)
Taxiing (normally performed by LP)
Flight path and airspeed control
Airplane configuration
Navigation
PM phase of flight responsibilities (general)
Checklist Reading
Communications
Task asked for by the PF
Monitoring taxiing, flight path, airspeed, airplane configuration, and navigation
Terms regarding power settings
Full power
Firewall power
Terms regarding power settings
Max power
Max. Certified power (5 min limit)
TORQUE: In-flight (107,5%)
Terms regarding power settings
Max Takeoff (MTOP) power
Max. Certified power (5 min. Limit)
TORQUE: (Static 109,5%) (In-flight 107,5%)
Terms regarding power settings
Normal Takeoff (NTOP) power
TORQUE: (Static 99,5%) (In-flight 97,5%)
Terms regarding power settings
Max Continuous power (MCP)
According to torque power chart
TORQUE: (In-flight 97,5%)
Terms regarding power settings
Max Cruise power
According to torque power chart
TORQUE: (In-flight 114,2%)
Terms regarding power settings
“Power set”
Confirmation that requested power is set, and engine instruments checked for normal indications
Terms regarding power settings
“Set power…(TQ)..”
Calculated power given in terms of torque
Automation callouts
Level 2 - Selecting modes
PF “Select <mode>”
PM “<mode> selected”
PF “Checked”</mode></mode>
Automation callouts
Level 2 - Selecting armed modes
PF “Arm <mode>”
PM “<mode> armed”
PF “Checked”</mode></mode>
Automation callouts
Level 2 - Armed mode automatically engages
PF “<mode> capture” or “<radial> capture” or “LNAV”
PM “Checked”</radial></mode>
Automation callouts
Level 2 - Changing parameters
PF “Set Heading/IAS/VS xxx”
PM “Heading/IAS/VS xxx set”
Automation callouts
Engagement of Autopilot
PF “Engage autopilot”
PM “Autopilot engage, <mode>”</mode>
Automation callouts
Level 3 or 4 - Selecting modes
PF “<mode> selected”
PM “Checked”</mode>
Automation callouts
Level 3 or 4 - Selecting armed modes
PF “<mode> armed”
PM “Checked”</mode>
Automation callouts
Level 3 or 4 - Changing parameters
PF “Heading/IAS/VS xxx Set”
PM “Checked”
Automation callouts
Level 3 or 4 - Armed mode automatically engages
PF “<mode> capture” or “<radial> capture” or “LNAV”
PM “Checked”</radial></mode>
Automation callouts
Setting course direct to a waypoint
PF “Direct <waypoint> set”
PM “Checked”</waypoint>
Calls for Altitude Changes and Transitions
Altitude changes
PF “<FL/ ALTITUDE> set - ALT SEL armed”
PM “Checked”
Calls for Altitude Changes and Transitions
1000 feet before selected altitude/ FL
PM “Pre level”
PF “ALT SEL armed, QNH xxxx”
PM “Checked”
Calls for Altitude Changes and Transitions
Approaching selected altitude
PF “Altitude capture”
PM “Checked”
Calls for Altitude Changes and Transitions
Transition Altitude
PM “Transition Altitude”
PF “1013 FL…”
PM “Set and crosschecked”
Calls for Altitude Changes and Transitions
Transition Level
PM “Transition Level”
PF “QNH…..FT”
PM “Set and crosschecked”
Deviation Calls, Different Phases of Flight
Approaching torque limit for current configuration
PM “Torque”
PF “Correcting”
Deviation Calls, Different Phases of Flight
Bank angle exceed 30 degrees
PM “Bank”
PF “Correcting”
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
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
Deviation Calls, Different Phases of Flight
1 dot localizer or 5˚ VOR/NDB/ deviation
PM “Track”
PF “Correcting”
Deviation Calls, Different Phases of Flight
1 dot glide slope deviation
PM “Above/ Below glide slope”
PF “Correcting”
Deviation Calls, Different Phases of Flight
Altitude deviations +/- 100 ft
PM “Altitude Above/ Below”
PF “Correcting”
Deviation Calls, Different Phases of Flight
Speed deviation +/- 10 kts
PM “Speed high/ low”
PF “Correcting”
Deviation Calls, Different Phases of Flight
Briefed Vref -0 / Vtrgt +10 kts
PM “Speed high/ low”
PF “Correcting”
Deviation Calls, Different Phases of Flight
Fast/ slow indicator deviating +/- 0.1
PM “Speed high/ low”
PF “Correcting”
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”
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”
Deviation Calls, Different Phases of Flight
Circling
PM - Call any deviation from speed/ altitude
PF “Correcting”
Landing Pitch Deviation Call Out
Pitch attitude 8˚ or more during landing
PM “Pitch….” - State actual pitch attitude
PF “Correcting”
Four basic methods of flying the DHC-8
Level 1
BASIC
Where the pilot manually flies the a/c without using the FD
Four basic methods of flying the DHC-8
Level 2
GUIDED
Where the pilot manually flies the V-bar of the FD
Four basic methods of flying the DHC-8
Level 3
DIRECTED
Where the AP flies the commands of the FD
Four basic methods of flying the DHC-8
Level 4
MANAGED
Using LNAV/ VNAV commands from the FMS
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
Walk-Around
Entering flight deck
Engage all pulled circuit breakers
Hydraulic pump handle stowed
Smoke goggles, Crew oxygen masks and oxygen quantity
Emergency equipment
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
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
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
When parking brake set
Minimum pressure indicated?
Min 1500 psi
Hydraulic Qty. Check
Min #1 og #2?
1 1,5 US Quarts
#2 3,0 US Quarts
TAKE-OFF ELEVATOR TRIM VS CG
Forward CG:
Aft CG:
Forward CG: AFT END (15% MAC)
Aft CG: FWD END (38% MAC)
USE OF HEADSET
On the ground
1:
2:
1: When receiving the ATC departure clearance via voice communication
2: When engines are running
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
When should the DEPARTURE BRIEFING be conducted?
By the PF between the preflight og start checklist
PF shall before departure briefing:
Have selected departure routing from the FPL/MENU/DEPART if applicable
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
Oil pressure below 75% NH during NORM ENG START is allowed between:
40 and 55 PSI
Altimeter checking
The altimeter shall not be used is the difference btwn true alt and indicated is:
More than 60 ft apart
Altimeter checking
Two altimeters Max difference
90 ft
Most exact altimeter should be used
Maximum speed during taxi
Depending on surface conditions
15 kts, except 30 kts during backtracking on rwy
Quiet Taxi mode, the RPM is limited to:
785 RPM
Flight control unluck and check should only be performed in:
Headwind
Nose When Steering
Steering range:
High-speed: 5˚ (Rudder pedals)
Low-speed: 60˚ (Steering control handle)
Unpowered (caster) mode: 120˚
The Autopilot shall not be engaged below?
1000 ft
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
Takeoff in icing condition
Overall concept?
MAKE IT CLEAN AND KEEP IT CLEAN
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
Climb procedure
Type 1
210 KIAS Up to FL100, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS
Climb procedure
Type 2
170 KIAS Up to FL180, reduce by 5 KIAS each 1000’, final climb speed 130 KIAS
Climb procedure
Type 3
130 KIAS
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
If final level is FL190 or lower, propeller RPM may be reduced to:
900 RPM
Climb to cruise transition
PF will Call “?” And PM will ?
PF “Setting Cruise Power” - adjust pwr and condition levers
PM: Monitor torque gauges
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
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
Cruise torque setting
Approx. Minimum cost?
75% Torque
After cruise torque has been set….
Adjust the friction knob
Assigned FL or altitude shall be within an indicated tolerance of:
+/- 50 ft
Performance calculations
Should not be calculated earlier than?
30 min. Prior estimated time of landing
Standard target descent rate V/S
1800 ft/min
Non-turbulent conditions normal descent profile
Maximum speed
Vmo -10kt or 220 KIAS which ever is lover
Using no more than 42-45% torque
To take advantage of higher TAS at high altitude
Planned TVS and torque?
2200 Ft/min and 20-25% Torque
OFP Fuel and time calculations are basen on ____ during descent
AFM Type 1 descent profile
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
Recommended holding airspeed
150 KIAS with flaps up
To avoid cycling of the outboard Roll spoilers, do not hold at precisely ____ KIAS
140 KIAS
Approximate fuel consumption in holding and conditions
PWR as required
900 RPM
400 Kgs/Hr @FL100, ISA, 125 KIAS
Minimum holding speed in icing conditions
160 KIAS
More than light icing, its recommended to set condition levers fully forward
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”
Stabilized approach parameters
Speed @1000 ft AAL
Lower limit: Vref -5
Upper limit: Vtrgt +20
Stabilized approach parameters
Speed @300 ft AAL
Lower limit: Vref -5
Upper limit: Vtrgt +10
Stabilized approach parameters
ROD @1000 ft AAL
Precision and non-precision: Max 1500 ft/min
Visual and circling: Max 2000 ft/min
Stabilized approach parameters
ROD @300 ft AAL
Precision and non-precision: Max 1000 ft/min
Visual and circling: Max 1000 ft/min
Stabilized approach parameters
Configuration
Flaps for landing, gear down
Stabilized approach parameters
Precision approach
1 dot LOC/GP
Stabilized approach parameters
Non-Precision approach
1 dot/ 5˚NDB
Stabilized approach parameters
Visual and circling
Wings level
Max ft/min during steep approach
1450 ft/min
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”
Unstabilized approach callouts
Rate of descent in excess of stabilized approach parameters
PM: “Descent rate”
PF: “Go-Around” or “Correcting”
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
Minimum descent altitude during a visual app
500 ft AAL
DH setting shall be set no later than
2500 ft AAL
DH setting for visual approach
0 ft
DH setting for precision approach
200 ft AAL (or applicable minima if higher)
DH setting for non-precision
300 ft
During proceedures with procedure turn
VNAV shall not be armed until
The a/c is established on the final approach track
RNAV/ GNSS approach must be discontinued
When one of the following occurs
- SATTELITE POS ALARM (Indicated on FMS)
- GPS accuracy downgraded INTEG annunciation
Normal minimum torque setting during approach
15% torque
Max pitch during flare
6˚ to 8˚ nose up
Landing with 1050 NP may only be performed
To runway longer then 1000 meters
Prior setting T/O power on wet and contaminated runway
Confirm AUTO IGNITION prior setting T/O power
Prior T/O in ice conditions or where icing is likely
Minimum oil temp
45˚
Propeller de-icing may be enhanced by periodically selecting condition levers….
To maximum (1200 RPM)
Torque setting for approximate minimum cost
75% torque
