A320-2 Need To Know Flashcards
Required Knowledge to safely and efficiently operate the aircraft
OEI - DRIFTDOWN
- 3 Strategies for OEI drift-down
- Describe the strategy
- Where is the information found
- What is the procedure approaching level off
- What speed is flown at level off
- Where are performance tables found if EO CLR is accidentally selected on the MCDU
- Standard Strategy M.78/300
REC MAX EO cruise altitude
LRC with Anti Ice OFF,
MCDU PROG page, or
QRH Gross Ceiling at LRC with Anti Ice Off
When V/S reduces to 500 ft/min select V/S 500 ft/ min until level off
Fly at LRC (MCDU and QRH) - Obstacle Strategy
Used for clearing obstacles
Use G/DOT and altitude on MCDU PERF page
At level off continue with driftdown as to fly an ascending profile as fuel is burnt off
After clear of obstacles accelerate to LRC and
Continue driftdown, at level off engage A/THR - Fixed Strategy
Used for ETOPS when established before dispatch
FMS
- How to re-enter a FLT PLN after FMS deletes it
- DIR TO any waypoint then LAT DEV and enter new destination
PROCEDURES - PREFLIGHT
ALTIMETERS
- ADR 1 to ADR 2 Altimeter tolerance
- ISIS to any ADR tolerance
- QNH airport elevation to any ADR, RVSM (Ops Manual)
- AIP IFR Tollerences
OXYGEN
- Aprox minimum 2 crew:
- Aprox minimum 3 crew:
- Aprox minimum 4 crew:
BATTERY TEST
- What is the test
FLT RCDR
- How is the test conducted on the JQG/L/X:
ADIRS
- Full Alignment
First flight of the day after 1600z
Crew change
GPS not available and
navaid coverage is poor or
flight time >3hrs
- Fast Alignment
Whenever FMGC position >5nm
- When is a Tech Log Entry Required
ALTIMETERS
- ADR 1 to ADR 2: 20 ft
- ISIS to any ADR: 100 ft
- Ops Manual RVSM ground check: 75 ft
- AIP 60 ft, and one may be up to 75 ft or one flight
OXYGEN
- 2 crew: 800 psi
- 3 crew: 1000 psi
- 4 crew: 1300 psi
BATTERY TEST
- 10 Sec after cycling ON check charging less than 60A
FLT RCDR
- All A320’s are the same
ADIRS
- Full Alignment
First flight of the day after 1600z
Crew change
GPS not available Vavaid coverage is poor or flight time >3hrs
- Fast Alignment
When FMGC position >5nm
- Tech Log Entry if min >5 nm (see SOP PARKING)
APPROACH SLOPE GUIDANCE
- Destination
Preflight
After departure
- Is it required at Alternate
- Is it required at Adequate
- Displaced Threshold
- Destination - Preflight
Up to 7 days with approval from GM
Weather forecast above Circling Minima
- Destination - After Departure
PIC decision
- Is it required at Alternate: No
- Is it required at Adequate: No
- May only use Approach Slope Guidance, if unable to clear the displaced threshold by 20'ILS & AUTOLAND
- What is the significance if LAND GREEN mode:
- When is it active
1
AERODROME LIGHTING
CLASS G AERODROME
- At night, when must a responsible person be in attendance for
Destination
Alternate
Adequate
Emergency
1
Ref:
RVSM
- What is the altitude overshoot tolerance
- What is the altitude keeping tolerance
- What are the cruise altimeter tolerances
- If advised in real time that aircraft identified as having a total vertical error of …. what is the next step>300 ft deviation
- Why is 1 FWC required
- 150 ft
- ?
- 130 ft between PFD 1 and 2 (FCOM Limitation)
or, 200 ft in OM1 - 300 ft, advise ATC of inability to meet RVSM requirements
- for the Altitude Alerting System
- 2 primary altimeters, Autopilot, transponder
GO AROUND
- What is the minimum altitude to commence thrust reduction to CLB
- May this be done prior to LVR MCT
- When does the flight phase transition to CLB on a normal takeoff
- When does SRS mode disengage during a Go Around
- What occurs differently at the Acceleration Altitude when OEI for both TO and GA
- When does the Go Around phase end during a go around (3 ways)
- What is the SRS target speed
- What about OEI
- What are these speeds for TO
- What speed does Go Around phase target after the disengagement of SRS
- Minimum 800’ AGL for CLB THR
- Yes, can reduce any time before LVR CLB
- Normal TO, Climb phase at
Acceleration Altitude
Any change to vertical mode
- ALT*, V/S-0, OP CLB (May be result of Selected Speed) - SRS mode disengages as per points above during a Go Around
- SRS remains engaged and aircraft does not accelerate until another vertical mode is selected
- During a go around Go Around phase ends
Activating Approach Phase
Enabling Alternate
Lateral Deviation from a waypoint and selecting a new destination - What is the SRS target: Current speed up to VLS +25
- What about OEI: Current speed up to VLS +15
- TO; targets VLS+10, OEI current up to VLS+15
- GA phase targets smaller of G/DOT or speed restriction
FUEL EMERGENCY
- What does “Minimum Fuel” mean
- When would Mayday Fuel be declared:
- What are the post flight requirements:
- What does “Minimum Fuel” mean
- When would Mayday Fuel be declared:
- What are the post flight requirements:
Ref:
PHASE OF FLIGHT
CLB
- When does TO phase become CLB phase: At Aa, or change in vertical mode (inc. OP CLB from pulling speed)
- what is the target speed of CLB phase: ECON or any restriction such as 250<10000
GO AROUND
- Describe the 4 ways that the GA phase can be exited:
- Activating Approach phase
- ENANLE ALTN preferably from the TO waypoint
- Entering NEW DEST in the LAT DEV page at the TO waypoint
- Activating SEC F-PLN if prepared (usually used for diversion from cruise)
- If ENABLE ALTN what is the default CRZ altitude: FL220 or FL330
CLB
- CLB phase activates at Aa, or change in vertical mode (inc. OP CLB from pulling speed)
- Speed target is ECON or any restriction such as 250<10000
GO AROUND
- Exiting GA phase
- Activating Approach phase
- ENANLE ALTN preferably from the TO waypoint
- Entering NEW DEST in the LAT DEV page at the TO waypoint
- Activating SEC F-PLN if prepared (usually used for diversion from cruise)
- ENABLE ALTN, CRZ altitude is FL220 or FL330
PERFORMANCE - Runway Surface
- How shall the runway be treated when DAMP, for
Takeoff
Landing
Takeoff: Dry
Landing: Wet
OEI - TAKEOFF
- What is the maximum AoB during an EO procedure
- what is the gross 2nd segment climb performance
- What is the net 2nd segment climb performance
- What is the JQ minimum Aa for TO after an engine failure
- What is this limited by
- Where does the 2nd segment commence and finish
- 15 degrees
- 2.4%
- 1.6%
- From Gear UP until Aa
- 1500’ HAA
- 10 minutes at TO THR
PROCEDURES - PREFLIGHT, COLD WEATHER
- How much ice can be on the aircraft
- Operating engine
Oil temp
Oil pressure
Fan icing
1.
PROCEDURES - AFTER LANDING
- When would the Flaps & Slats be left extended after landing
- Anti Ice usage
- When would the Slats be left extended and for how long
- Engine ground runs
- Brake temps
When can the fans come on
What are the tolerances
1
FMS - SEC F-PLN
- How is it activated
- What are the conditions for the prompt to be available
1
COMPANY RESTRICTION
- Rates of descent
- Below 20,000'
Height above terrain
5000 ft/min until 5000 ft
3000 ft/min until 3000 ft
2000 ft/min until 2000 ft
1000 ft/min below 1000 ftAPPROACH - CIRCLING
CIRCLING APPROACH
- Configuration
- When is the Go Around altitude set
- Timing at 45 deg onto downwind
- Timing outbound at 1,000’
- Size of circling area
- Speed restrictions of circling
1
APPROACH - VISUAL CIRCUIT
- Cloud and visibility requirements
Class C
Class D
Class G
- Configuration entering the circuit
- Timing for 90 deg crosswind
- Timing for 45 deg crosswind
- Ideal spacing
- Timing outbound
- Go Around
Setting on FCU
Requirement
1.
OEI - CRUISE
- What altitude is displayed on MCDU PROG:
- If Double FMS failure where else can this altitude be found:
- At a Gross Ceiling of 20,000’ at ISA+10 what approximate weight would the aircraft be at
for LRC:
for G/DOT:
- MCDU PROG: REC MAX EO Cruise altitude equates to LRC with Anti-Icing OFF
- If Double FM failure: use QRH EO gross ceiling at LRC
- Gross Ceiling of 20,000’ at ISA+10
LRC = 63 ton
G/DOT = 70 ton
LIMITATIONS - STALL SPEEDS
Stalling Speed at MTOW (SL)
- Config 0
- Config 1
- Config 2,3,F
- Config 0: 165 kts
Config 1: 140 kt
Config 2,3,F: 122 kts
LIMITATIONS - Air-conditioning, Pressurisation, Ventilation
Differential Pressure for Ram Air Inlet OPEN
Limitation of using CONDITIONED AIR from LP ground unit
Limitation of using HP PNEUMATIC ground unit
Ram Air Inlet OPEN:
LIMITATIONS - AUTOFLIGHT
AUTOPILOT Min height for engagement on T/O Straight in Non-Precision App Circling Approach Go-Around All Other Phases
RNP-AR - JSS REQUIREMENTS
- A/P may remain in FINAL mode of a RNP down to what altitude
- Conditions to meet this requirement include being ‘Visual’, in FINAL APP Mode, MAP is at runway threshold, and?
NON PRECISION APPROACHES
- What are the navigation requirements to use FINAL APP mode
- Can they be flown via the AP with the OEI
AUTOLAND
- Minimum Decision Height (RA)
CAT II
CAT III passive (single)
CAT III Fail Operational (Dual)
- What is the minimum vis required for CAT 3 DUAL without a DH
- OEI, approved for fail
- If OEI procedures are completed by
OEI, what configurations is it approved for
AUTOPILOT Min height for engagement on T/O: 100' or 5 sec Straight in Non-Precision App: Minima Circling Approach: Minima -100 feet Go-Around: 100 feet All Other Phases: 500 feet
RNP-AR - JSS REQUIREMENTS
- A/P may remain in FINAL mode of a RNP down to what altitude: 250 feet
- Conditions to meet this requirement include being ‘Visual’, in FINAL APP, MAP is at runway threshold, and?: Final Approach Segment is aligned with the runway
NON PRECISION APPROACHES
- What are the navigation requirements to use FINAL APP mode: GPS Primary, or/ NAV Accuracy High and NAVAID raw data monitored
- Can they be flown via the AP with the OEI: Yes
AUTOLAND
- Minimum Decision Height (RA)
CAT II : 100 feet
CAT III passive (single): 50 feet
CAT III Fail Operational (Dual): 25 feet
- What is the minimum vis required for CAT 3 DUAL without a DH: 75m
- OEI, approved for fail: Passive only (Cat IIIA)
- If OEI procedures are completed by: 1000 feet
OEI, what configurations is it approved for: FULL only
LIMITATIONS - Environmental & Airport Ops
PASSENGER DOOR - Operation - Must be closed before Cargo Door - Operation - Must be closed before wind exceeding
PASSENGER DOOR
- Operation: 65 kts
- No limitation
CARGO DOOR
- Operation: 40 kts, 50 kts if A/C nose int wind or door on lee side
- Must be closed before wind exceeding: 65 kts
LIMITATIONS - Electrical
Max Continuous load per:
- Generator
TR
Max Continuous load per:
- Generator: 90 KVA (100%)
TR: 200 A
LIMITATIONS - Autoflight / NPA
NON PRECISION APPROACHES
- What are the navigation requirements to use FINAL APP mode
Can they be flown via the AP with the OEI
- What are the navigation requirements to use FINAL APP mode: GPS Primary, or/ NAV Accuracy High and NAVAID raw data monitored
Can they be flown via the AP with the OEI: Yes
LIMITATIONS - Fuel
IMBALANCE
- Maximum imbalance between INNER Tanks (outer tanks balanced) with one tank full:
ALL
Sharklet Prior to T/O
- Maximum imbalance between OUTER tanks (inner tanks balanced):
ALL
Sharklet prior to T/O
FUEL TEMPERATURE
- Maximum Jet A
- Maximum Jet A
- Minimum Jet A1
- Minimum Jet A
GENERAL
- Minimum QTY for T/O
- T/O with ECAM, WING TK LO LVL Warning
- Tanks must be emptied in the following order
- T/O on which Tank is prohibited
IMBALANCE
- Maximum imbalance between INNER Tanks (outer tanks balanced) with one tank full:
ALL: 1500 kg
Sharklet Prior to T/O: 500 kg
- Maximum imbalance between OUTER tanks (inner tanks balanced):
ALL: 690 kg
Sharklet prior to T/O: 370 kg
FUEL TEMPERATURE
- Maximum Jet A: 54 DegC
- Maximum Jet A: 54 degC
- Minimum Jet A1: -43 degC
- Minimum Jet A: -36 degC
GENERAL
- Minimum QTY for T/O: 1500 kg
- T/O with ECAM, WING TK LO LVL Warning: Must not T/O
- Tanks must be emptied in the following order: Centre Tanks, Wing Tanks
- T/O on which Tank is prohibited: Centre Tank
LIMITATIONS - Oxygen
Approximate minimum Bottle Pressure at 30 deg reference temperature:
- 2 Crew
- 2 Crew +1 Obs
2 Crew +2 Obs
- 2 Crew: 800 psi
- 2 Crew +1 Obs: 1000 psi
2 Crew +2 Obs: 1300 psi
LIMITATIONS - Hydraulic
Normal operating pressure, +/-
3000 psi +/- 200
LIMITATIONS - Power Plant
EGT
- TOGA
- How long can TOGA thrust be used
- MCT
- Starting
OIL - Min starting temp - Min temp prior to exceeding idle - Min temp prior to T/O - Min pressure Max continuous temp - Minimum QTY
RPM
- N1
- N2
STARTER
- Max time
- Or, how many cycles
- Max N2 for starter engagement
On ground
In flight
- Capable of starting in crosswinds up to
REVERSE THRUST
- Max reverse should not be used below what speed
- Idle revers is approved down to what speed
FLEX
- Max derate is
Or
EGT
- TOGA: 650 degC
- How long can TOGA thrust be used: 5 min, 10 min OEI
- MCT: 610 degC
- Starting: 635 degC
OIL
- Min starting temp: -40 deg C
- Min temp prior to exceeding idle: -10 degC
- Min temp prior to T/O: 50 degC
- Min pressure: 60 psi
Max continuous temp: 155 degC (up to 165 for max 15 min)
- Minimum QTY: 11 qts + 0.3 /hour
RPM
- N1: 100%
- N2: 100%
STARTER
- Max time: 4 mins
- Or, how many cycles: 3 cycles, 2 x2min and 1 x1min with 15 sec in-between
- Max N2 for starter engagement
On ground: 10%
In flight: 18%
- Capable of starting in crosswinds up to: 35 kts
REVERSE THRUST
- Max reverse should not be used below what speed: 70 kts
- Idle revers OK to stop
FLEX
- Max derate is: 25%
Or: ISA + 55 degC
LIMITATIONS - Landing Gear
Max temp for T/O with brake fans off Disengage A/BRK; 2 methods: - 1. - 2. - 1 tyre per gear (i.e max 3 tyres) - 2 tyres on same gear Nose Wheel Steering Angle limit: - Tiller Towing
Max temp for T/O with brake fans off: 300 degC
Disengage A/BRK; 2 methods:
- 1. Pressing the pb of the armed mode, or
- 2. applying sufficient pressure to the brake pedals
Taxi with Deflated Tyres
- 1 tyre per gear (i.e max 3 tyres): max 7 kts
- 2 tyres on same gear: max 3 kts and steering angle max 30 deg
Nose Wheel Steering Angle limit:
- Tiller: 75 deg
Towing: 95 deg
LIMITATIONS - Autoflight / Autoland
- Configurations approved
- VAPP min and max wind correction
- Minimum Decision Height (RA)
CAT II
CAT III passive (single)
CAT III Fail Operational (Dual) - What is the minimum vis required for CAT 3 DUAL without a DH
- OEI, approved for fail
- If OEI procedures are completed by
- OEI, what configurations is it approved for
- Wind Limitations
Headwind
Crosswind
Tailwind - Sharklet Differences:
Crosswind, Automatic Rollout
Crosswind, Manual Rollout
Crosswind, 1 REV only
OEI or 1 THR REV inop
- Configurations approved: Config FULL & 3
- VAPP min and max wind correction: 5 to 15 kts
- Minimum Decision Height (RA)
CAT II : 100 feet
CAT III passive (single): 50 feet
CAT III Fail Operational (Dual): 25 feet - What is the minimum vis required for CAT 3 DUAL without a DH: 75m
- OEI, approved for fail: Passive only (Cat IIIA)
- If OEI procedures are completed by: 1000 feet
- OEI, what configurations is it approved for: FULL only
- Wind Limitations
Headwind: 30 kts
Crosswind: 20 kts
Tailwind: 10 kts - Sharklet Differences:
Crosswind, Automatic Rollout: 15 kts
Crosswind, Manual Rollout: 20 kts
Crosswind, 1 REV only: 15 kts
OEI or 1 THR REV inop: REV IDLE only
Wake Turbulence
Medium Following a Super
Medium following a Heavy
Additional time if conducting an Intermediate T/O
Minimum distance in to be considered Intermediate
Super: 3 min or 7 nm
Heavy: 2 min of 5 nm
Intermediate T/O: 1 min
150 metres
Ignition Start
When what 2 phenomena’s are expected is IGN START selected
- Heavy Rain
2. Severe Turbulence
ICING - EAI, WAI, AIRFRAME
EAI
Is used on all ground and in flight when encountering or anticipating icing conditions
- Except when in Climb or Cruise and SAT is
- EAI must be on during descent in citing conditions regardless of the (?) temperature
WAI
May be used to prevent or remove ice accumulations, should be ON whenever there is an indication that airframe icing exists on the:
- 1.
- 2.
What limitations exist in relation to the use of the WAI in regards to the Flaps/Slats
GENERAL
- If significant ice accretion on no heated structure minimum speed:
Config FULL
Config
EAI
Is used on all ground and in flight when encountering or anticipating icing conditions
- Except when in Climb or Cruise and SAT is: below -40 degC
- EAI must be on during descent in citing conditions regardless of the (?) temperature: SAT
WAI
May be used to prevent or remove ice accumulations, should be ON whenever there is an indication that airframe icing exists on the:
- 1. Visual Ice Indicator
- 2. Windscreen Wipers
What limitations exist in relation to the use of the WAI in regards to the Flaps/Slats: None, but extended flight in icing conditions with Slats extended should be avoided.
GENERAL
- If significant ice accretion on no heated structure minimum speed:
Config FULL: VLS +5
Config
RAIN REPELLANT
Rain Repellant should only be used in what sort or rain intensity
Moderate to Heavy
AVIONICS
What is the procedure to protect the avionics from heavy rain when parked
After Landing
After T/O
- At what temperature is there no limit on leaving the above avionics cooling configuration
Otherwise what is the limit
After Landing: EXTRACT…..OVRD and both Packs ON
After T/O: EXTRACT…..AUTO
- At what temperature is there no limit on leaving the above avionics cooling configuration: 39 degC or below
Otherwise what is the limit: 3 hours
TOGA THRUST
Reduced Thrust operations are not permitted for:
- Items affecting performance cause an increase in crew workload
- More than one MEL with multiple performance penalties
- When the calculated flex temperature is lower than flat rated temp (ISA + 30 degC) or actual OAT
Name 4 other reasons
- Runway Contaminated
- Frontal or Thunderstorm activity likely
- Windshear is likely
- Wet runway not on regular schedule
FLIGHT MANAGEMENT - EARLY LEVEL OFF
- What FMA modes can be expected upon early level off below the Aa when capturing an FCU altitude
- What should crew be prepared for
- What occurs when ‘Push-to-level-off’ (or any other change in vertical mode) is used below the Aa and FCU altitude
What effect does Selected Speed have below the Aa
- ALT* engages which triggers the LVR CLB message
- Prepare for quicker than usual acceleration
- A change in vertical mode below the Aa will cause the CLB phase to activate and target the initial climb speed (usually 250 kts) or any other speed restriction
Selecting speed below the Aa will change the vertical mode to OP CLB and activate the CLB phase
CLIMB SPEEDS
- 2nd Segment Climb Speed:
Normal
E/O - Maximum Pitch for T/O
- During Windshear why may the pitch be higher that 22.5 deg
- Maximum Rate
Where can time and distance required to achieve a selected altitude at Max Gradient be found
- 2nd Segment Climb Speed:
Normal: V2+10 up to ?
E/O: V2 to V2+15 - Maximum Pitch for T/O: 18 deg (22.5 in W/S)
- During Windshear why may the pitch be higher that 22.5 deg: SRS may target pitch required to fly 120 fpm minimum
- Maximum Rate: Between ECON and G/DOT best Rule of Thumb is to use ‘turbulence’ speed
- Maximum Angle/Gradient: G/Dot
Where can time and distance required to achieve a selected altitude at Max Gradient be found: MCDU PERF CLB page
TAKE OFF - HEAVY WEIGHT
ARS - Automatic Retraction System
- What will it do to Flap 1+F
- When will it do it
- What speed will VFE not reflect
- When can the flap lever be selected to 0
ALPHA LOCK FUNCTION - What does it do - How do you know it's active - Is this normal during a heavy weight takeoff How should the crew respond
ARS - Automatic Retraction System
- What will it do to Flap 1+F: Retract flap to 0
- When will it do it: at 210 kts
- What speed will VFE not reflect: 230 kts
- When can the flap lever be selected to 0: Above ‘S’ speed
ALPHA LOCK FUNCTION
- What does it do: Prevents SLAT retraction at high AOA of low speed a the moment the flap lever is moved from Flaps 1 to 0
- How do you know it’s active: “A. LOCK” pulses above the E/WD Slat indication.
- Is this normal during a heavy weight takeoff: Yes
- How should the crew respond: Continue the acceleration, allowing further slats retraction
TAKEOFF
- Tail-Strike Attitude
L/G Compressed
Extended - At VR rotate at what rate and to what attitude
- What attitude if an engine has failed
- After lift-off what should be pitched for
- When do packs 1 & 2 get turned ON after T/O
What is the minimum time between turning Pack 1 & 2 ON
- Tail-Strike Attitude
L/G Compressed: 11.7 deg
Extended: 13.5 deg - At VR rotate at what rate and to what attitude: 3 deg/S to 15 deg
- What attitude if an engine has failed: 12.5 deg
- After lift-off what should be pitched for: SRS command bar
- When do packs 1 & 2 get turned ON after T/O: CLB - THR (so not EGT increase) and FLAP retraction
What is the minimum time between turning Pack 1 & 2 ON: 10 seconds
AUTOTHRUST
GENERAL
- What effect does retarding the thrust levers below CLB with the A/THR active
- Arming the A/THR in flight with the thrust levers between CLB and IDLE inclusive will
ARMING / ACTIVATING
- 3 ways to arm the A/THR inflight:
- Once armed when is it activated
- And OEI
DISCONNECTING
- 2 Standard ways to disconnect A/THR
- 2 Non Standard ways to disconnect A/THR
ALPHA FLOOR
- What is Alpha Floor
- What causes the A/THR to enter Alpha Floor
- How is the A/THR taken out of Alpha Floor
EMERGENCY
- How is the A/THR locked out
does this disable all A/THR functions including ALPHA FLOOR
GENERAL
- What effect does retarding the thrust levers blow CLB with the A/THR active: limits thrust to thrust lever range
- Arming the A/THR in flight with the thrust levers between CLB and IDLE inclusive will: Activate the A/THR as it is within the active range
ARMING / ACTIVATING
- 3 ways to arm the A/THR inflight:
- by pressing the A/THR pb on the FCU,
- by moving the A/THR out of the active range with the A/THR active
- engaging Go-Around
- Once armed when is it activated: when the thrust levers are in range of CLB to IDLE inclusive
- And OEI: up to and including MCT
DISCONNECTING
- 2 Standard ways to disconnect A/THR
- instinctive disconnect pb on thrust levers
- setting both thrust levers to IDLE (landing)
- 2 Non Standard ways to disconnect A/THR
- Pushing the A/THR pb on FCU
- system looses an arming condition
ALPHA FLOOR
- What is Alpha Floor:
- What causes the A/THR to enter Alpha Floor:
- How is the A/THR taken out of Alpha Floor:
EMERGENCY
- How is the A/THR locked out: pb pressing and holding the intuitive disconnect pb on the thrust levers for more than 15 seconds
does this disable all A/THR functions including ALPHA FLOOR: Yes
THUNDERSTORMS
TAKEOFF
- Do not takeoff if active part of storm is within how many NM of takeoff and initial climb: 5NM in the pilots opinion
LANDING
- The circuit and approach shall be flown clear of storms by at least how many NM: 5 NM
CRUISE
- What are the minimum distance requirements for storm clearance during cruise:
CAVEAT
When may fly closer than 5 NM
TAKEOFF
5NM in the pilots opinion
LANDING
5 NM
CRUISE
20 NM above FL 250
10 NM when OAT (SAT)
FUEL - INFLIGHT
- Normal
- OEI; General, ETOPS, FLT Planned
- DP; General, ETOPS,FLT Planned
1
PITCH ATTITUDES
- AEO Rotation
Normal 15*
Max 18*
W/S no SRS: 22.5* or req for 120'/min CLB
- OEI Rotation: 12.5* initially
- Approach
Config FULL:
Config 3:
- Climb
32,000': 3* / 80%
1.
AUTOLAND & LOW VIS - WIND LIMITS
AUTOLAND
- HW
- XW
- TW
LOW VIS LANDING
- HW
- XW
- TW
LOW VIS TAKEOFF
- HW
- XW
- TW
1.
PHASE OF FLIGHT
CLIMB PHASE
- When is it activated
- What happens when SPEED is pulled with T/O phase active
APPROACH PHASE
- When is it activated, 2 ways
- How to get direct to CLB Phase bypassing Go Around Phase, (e.g. Diverting prior to conducting approach): Insert new CRZ Altitude
GO AROUND PHASE
- 3 ways to leave this phase
1.
OEI - ENGINE SECURE
- Engine Failure
- Engine Damage
- Engine Fire
- How to identify if damage:
1.
FUEL TANKERING
WHEN
PLANNING LIMITATIONS
WHERE ARE THESE FOUND
- ## LIMITATIONS
LOADING
NOTOC: When is one required
- When Dangerous Goods or Special Load is carried
- When cargo carried but no statement on the cargo manifest stating that there are no Dangerous Goods or Special Load
PERFORMANCE
Landing Distance Required Calculation
Pre Dispatch:
Inflight:
LAHSO:
Additives to inflight (QRH) calculation:
- Pre Dispatch: CAO 20.7.1B (OM6-4 / Coy Procedures).
- Inflight: QRH Inflight Landing Distance.
- LAHSO: use pre dispatch calculation.
- Additives to inflight (QRH) calculation: 15% for all normal and abnormal landings unless a “Pan” is declared.
