8 Flashcards

1
Q

ETOPS planning minima 8.21.5

From anticipated time of landing until 1 hour after latest time of landing:

A

Precision App:
DA + 200 ft RVR + 800 m

Non-precision App:
DA + 400 ft RVR + 1500 m

Crosswinds unaffected by engine status.
Can apply relevant correction to Cat II / III minima.

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2
Q

8.22.1 Low Visibility Operations

Strictly speaking, the term Low Visibility Operations (LVO) applies only to takeoff operations conducted in less than ??? RVR, or approach and landing operations in less than ??? RVR

A

Take-off 400m

Landing 550m

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3
Q

For takeoff operations with any RVR element – TDZ, mid-point or stop-end – below 200 m

A

All 3 RVRs are required to be at or above the appropriate minimum value.

8.22.1a

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4
Q

LVP Ops - Commencement & continuation of approach.

On landing – whether the stop-end is relevant?

If it is what is required stop end RVR?

8.22.6a

A

‘Relevant’ in this context means that part of the runway used during the high-speed phase of the landing down to a speed of approximately 60 kt.

If the crew deems the stop-end to be relevant, it is controlling and the required RVR is always 75 m.

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5
Q

8.22.6a

What RVRs are required for LVP approach to continue below 1000ft Above the Aerodrome?

A

The touchdown zone RVR shall always be controlling. If reported and relevant, the midpoint and stopend RVR shall also be controlling. The minimum RVR value for the midpoint shall be 125 m or the RVR required for the touchdown zone if less, and 75 m for the stopend. For aircraft equipped with a rollout guidance or control system, the minimum RVR value for the midpoint shall be 75 m.

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6
Q

8.22.3d
Take-off – Take-off Ban
Take-off is not permitted if any of the following is below the relevant minimum:

Note:
Pilot assessment of TDZ RVR when practical always overrides the reported TDZ RVR or Met visibility (either to increase or decrease the reported RVR). Pilot assessment may not be practical where runways are humped or the RVR limit is high.

A

1) The reported Touchdown Zone (TDZ) RVR or Met Visibility
2) The Mid-point RVR, when reported.
3) The Stop-end (Rollout) RVR, for operations below 200 m RVR.
4) The cloud-ceiling (if specified in the AOM) or:
5) The runway is indistinguishable from its surroundings.

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7
Q

What is the minimum required runway lights for take off / landing at night?

8.22.3e

A

Night: at least:
runway edge lights and runway end lights;
or
runway centreline lights and runway end lights

8.22.9 Night Operations
Runway edge and runway end lights must be on for all night operations, threshold lights must be on for landing by night.

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8
Q

8.22.5.c Authorisation of Non-precision Approaches Flown Without Using the CDFA Technique.

EASA Ops requires authorisation from the CAA to fly any Non-precision Approach other than by using the CDFA technique. The following approaches are authorised?

A

KJFK VOR or GPS Rwy 13 L/R (The ‘Canarsie approach’)

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9
Q

8.22.8

A conversion of meteorological visibility to RVR (CMV) is not to be used:

A

1) When reported RVR is available; or
2) For calculating any takeoff minima; or
3) to establish any required approach and landing RVR minimum less than 800 metres.

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10
Q

Effect on Landing Minima of Temporarily Failed or Downgraded Ground Equipment.
RVR Assessment System:
1) CAT III B No DH
2) CAT III B / CAT III A / CAT II

8.22.11

A

1) At least one RVR value to be available on the aerodrome.

2) On runways equipped with two or more RVR assessment units, one may be inoperative.

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11
Q

8.28.5d
Severe windshear is considered to be uncontrollable changes from normal steady flight conditions below 1000 AGL, in excess of the following:

A

1) 15 kts indicated airspeed.
2) 500 fpm vertical speed.
3) 5° pitch attitude
4) 1 dot displacement from the glideslope/glidepath.
5) Unusual thrust levels for a significant period of time.

Reduced thrust may be used if any windshear expected during or after take-off is caused by strong winds not associated with CBs or frontal activity.

Windshear Go-around
On aircraft fitted with aural windshear warning systems, if a GPWS “Windshear” warning is received, a windshear Go-Around must be carried out.

Exceptionally, in conditions of extreme turbulence associated with strong winds and not Cb or frontal activity, a warning may be treated as advisory provided that this warning has been anticipated, briefed for in the Approach Briefing and appropriate allowance made.

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12
Q

8.0.5 Crew Operating out of Uniform
Authorisation to operate out of uniform must be obtained from the DFCM or DOM, as appropriate.

How many crew many crew in uniform required?

A

At least the minimum legal Cabin Crew complement must be in uniform to operate with passengers on board.

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13
Q

Aircraft Emergency Alternate (E)

8.2.3 Airfield Classification Policy

A

These airfields are colour-coded RED and have at least:

1) one suitable runway, LDA sufficient at MLW wet zero wind
2) basic RFF cover (at least RFF 4).

Some ground handling facilities may be available but this has not been checked and therefore cannot be assured. Flight crew should only elect to land at an Aircraft Emergency Alternate if there is an Aircraft Emergency and no other suitable alternate is available.

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14
Q
Secondary Alternate (S)
8.2.3 Airfield Classification Policy
A

These airfields are colour-coded YELLOW and have suitable runways, taxiways, aprons and basic RFF cover (at least 4).

Only basic ground handling facilities may be available and passenger handling is not assured.

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15
Q
Primary Alternate (P)
8.2.3 Airfield Classification Policy
A

These airfields are colour-coded as GREEN and have suitable runways, taxiways and aprons. A full range of ground handling facilities including some level of engineering cover and full RFF cover (2 below a/c cat). These airfields are the primary alternates in all circumstances including medical diversions.

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16
Q
BA Destination (D)
8.2.3 Airfield classification policy.
A

These airfields are colour-coded BLUE and have the same characteristics as Primary Alternates but are also BA Destinations.

17
Q

8.2.5.f Take-off Alternate

Requirement:

A

A take-off alternate shall be specified and annotated on the flight plan if it would not be possible to return to the aerodrome of departure for meteorological or performance reasons based on weather conditions at the time of departure.

Normal operating minima apply, engine failure limitations must be considered. From the definition above, the Take-off alternate (to which Planning minima, see OM A 8.2.5.m Application of Forecast Conditions, and time windows apply) is not the aerodrome of departure.

Cirrus will check the requirement for a Take-off alternate and select a take-off alternate when necessary. The selected take-off alternate will be one of approved destination alternates for the departure airfield and aircraft type. The requirements of sub para (b) below are not included automatically in the Cirrus calculation but will be checked manually by FTD.

ii.
The take-off alternate shall be located:

a.
For two-engined aeroplanes: within 60 minutes flying time in still air standard conditions at the one-engine-inoperative cruising speed based on the actual takeoff mass.

b.
For three and four-engined aeroplanes: within 120 minutes flying time in still air standard conditions at the one-engine-inoperative cruising speed based on the actual takeoff mass.

c.
For ETOPs approved aeroplanes and crews, additionally, for all states except USA and Saudi Arabia: within 120 minutes flying time in still air standard conditions, or the approved ETOPS diversion time if this is less, at the one-engine-inoperative cruising speed based on the actual takeoff mass.

18
Q

8.2.5.n Planning Minima for Specific Aerodromes

A) 8.2.5.o Take-off Alternates
(All States except USA, Canada and Saudi Arabia.)

B) 8.2.5.p Destination Aerodrome (except Isolated Destination Aerodrome)

C) 8.2.5.q Isolated Destination Aerodromes, Destination Alternates or Required En-route Alternates

A

A) Normal operating minima apply, engine failure limitations must be considered. The ceiling must be taken into account when the only approaches available are non-precision and/or circling approaches.

B) Normal operating RVR.

 For non-precision or circling approaches, cloud ceiling at or above         
 the minimum specified on the Instrument Approach Charts.

C) Step down minima.

19
Q

8.2.9 MSA & SSA on flight documents.
8.2.9.b CIRRUS Plans
The bandwidth used for calculating MSAs for flight plan tracks is ???nm on each side of track.

The MSAs shown on CIRRUS plan are subject to a minimum of 2000 ft.

Between the aerodrome and the first fix, on take-off, and between the last fix and the aerodrome, on landing, the MSA relates to the direct track between the points. When transferring from CIRRUS to aerodrome documentation, care must be taken to ensure that any relevant MSAs are not infringed

A

20 nm each side of track.

20
Q

8.2.9 MSA & SSA on flight documents
8.2.9.d Aerodrome Related Charts
MSA represents the safe altitude around a navigation station or aerodrome reference point. If no other information is present, the radius is ?? nm and may be valid for a specific sector or approach runway. In case of an RNAV approach, MSA may be replaced by a Terminal Arrival Altitude (TAA) based on one of the procedure fixes. The borders of each sector are defined by bearings in regard to the originating point of the arc, MSAs and TAAs are used for airport navigation and provide a ????? Ft/M obstacle clearance down to the intermediate approach segment. MSA and TAA sectors and values are officially published by State authorities.

A

1) 25 nm

2) 1000 ft (300m)

21
Q

8.3.4 Fuel System Handling

When selections are required on the fuel system panel in flight?

A

1) Both pilots must be involved.
2) If both engines are to be fed from one wing tank (twin-engined aircraft only) the estimated time of completion of balancing must be recorded on CIRRUS plan, or by suitable use of FMS waypoints and systems display.
3) Fuel balancing should only be performed by reference to the appropriate FCOM/QRH procedure.

22
Q

8.3.15 Aircraft Lights

Type-specific lights shall be switched on when operating below FL100. What about high Aerodromes?

A

When operating to aerodromes at elevations above 2000 ft these lights shall be on during operations below 10,000 ft AAL.

23
Q

8.4.1.a Maximum Numbers of Persons with Reduced Mobility

What is the limit:

A

There is no limit to the number of PRMs who may travel on an aircraft, however, passengers who are non-self-reliant must provide an able bodied attendant/escort who will accompany them on the flight.

In circumstances where the number of PRMs forms a significant proportion of the total number of passengers on board the aircraft, the number of PRMs should NOT exceed the number of able-bodied persons capable of assisting with emergency evacuations.

Note:
Immobile passengers may be self-reliant if they have upper body strength and are able to self-lift. The relevant questions should be asked to determine the passenger’s specific needs and booking codes.

Exceptionally, when it is not possible to secure a severely-disabled passenger (e.g. a double leg amputee) in a normal passenger seat, a ‘cradle’ or other restraint device may be used instead, providing the disabled passenger and device are properly secured.

Up to 2 severely disabled passengers may be accommodated by these means per flight