OMA Flashcards

1
Q

Contingency Fuel

A
  1. Contingency fuel
    The fuel required to compensate for unforeseen factors which could have an
    influence on the fuel consumption to the destination aerodrome such as deviations
    of an individual aeroplane from the expected fuel consumption data, deviations from
    forecast meteorological conditions and deviations from planned routings and/or
    cruising levels/altitudes.
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2
Q
  1. Final reserve fuel
A

An amount of fuel, required to fly for 30 minutes at holding speed and at 1500 ft.
MSL/ISA conditions, calculated with regard to the expected landing mass at the
alternate airport (or at destination - if no alternate is required).

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3
Q

121.Obstacle clearance altitude (OCA) or obstacle clearance height (OCH)

A

the lowest altitude or the lowest height above the elevation of the relevant runway
threshold or the aerodrome elevation as applicable, used in establishing compliance
with appropriate obstacle clearance criteria.
Note 1.� Obstacle clearance altitude is referenced to mean sea level and obstacle
clearance height is referenced to the threshold elevation or in the case of non-precision
approaches to the aerodrome elevation or the threshold elevation if that is more than
2 m (7 ft) below the aerodrome elevation. An obstacle clearance height for a circling
approach is referenced to the aerodrome elevation.
Note 2.� For convenience when both expressions are used they may be written in the
form �obstacle clearance altitude/height� and abbreviated �OCA/H�.

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4
Q

146.Runway visual range

A

The range over which the pilot of an aircraft on the centre line of a runway can see
the runway surface markings or the lights delineating the runway or identifying its
centreline.

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5
Q

Technical Instructions

A

The latest effective edition of the Technical Instructions for the Safe Transport of
Dangerous Goods by Air (Doc 9284), including the Supplement and any Addendum,
approved and published by decision of the Council of the International Civil Aviation
Organization. (Oman Air uses IATA DGR latest yearly release.)

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6
Q

UN Number

A

The four-digit number assigned by the United Nations Committee of Experts on the
Transport of Dangerous Goods, to identify a substance, or a particular group of
substances.

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7
Q

Contaminated runway

A

A runway is considered to be contaminated, when more than 25% of the runway
surface area (whether in isolated areas or not), within the required length and width
being used, is covered by the following:
(a) Surface water with a dept. of 3 mm or more, or by slush, or loose snow,
equivalent to a water depth of 3 mm or more;
(b) Snow, which has been compressed into a solid mass which resists further
compression and will hold together, or break into lumps if picked up (compacted
snow); or
(c) Ice, including wet ice.

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8
Q

2.5.1 Power to Inspect

A

Any person authorised by the AUTHORITY is permitted at any time to board and fly
in any aeroplane operated in accordance with the AOC issued by AUTHORITY and to
enter and remain on the flight deck provided that the commander may refuse access
to the flight deck if, in his opinion, the safety of the aeroplane would thereby be
endangered.
�h The certification or inspection on the operation of flights may be carried out
during flight by a Flight Operations Inspector of the AUTHORITY on official duty
and in possession of a valid PACA Inspector Identification card.

�h The inspection may be carried out without prior notice to the crew. However
whenever possible, the AUTHORITY will notify Flight Operations at least 24 hours
in advance to avoid last minute changes of previous jump seat allocations.
�h A commercial seat shall be reserved and in case the aeroplane is already fully
booked, a cabin attendant seat shall be made available.
Conduct of Inspection
Full co-operation on the ground as well as on board will be given to the inspector on
duty. Any abuse or misconduct of the inspector will be reported on the CVR signed at
least by the Commander, another pilot on duty and the Purser. An ASR will be
submitted if the misconduct impairs safety of the flight or its occupants. In an extreme
case of violence, the inspector will be treated in accordance to refer OM-A-10.1.7.
Note: The Commander remains in charge of the Aeroplane at all times but will
consider the inspector as an additional crew member and will include him in all flight
briefings.
A normal passenger ticket is required.
If, for safety reasons, the Commander decides to refuse access of the Flight Deck to
an Inspector or to ask the inspector to leave the Flight Deck in flight, he will justify his
decision to that inspector and will forward a detailed CVR to the relevant Manager
Fleet, copy to SMLO and will call the Manager Fleet or his designee by phone
immediately upon arrival. If the flight terminates at main base, the Commander will
ensure that his report (in the flight envelope) is forwarded immediately. If the flight
terminates elsewhere, or during an overnight, the Commander will request the
Station Manager to fax immediately a copy of his report to the SMLO and will insert
the original copy into the Flight envelope.
While on the ground at outstations, other State Aviation Authorities inspectors, in
possession of valid identification, and on duty, are permitted access to the aircraft for
the purpose of conducting safety inspections. Such access is granted under
international Law, and shall be facilitated by all crew members.

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9
Q

4.1.2.3 Cabin Crew Composition

A

((a) Regulatory Minimum Cabin Crew Composition
The minimum number of cabin crew required for a specific aircraft is based on
CAR-OPS 1.990 and under no circumstances aircraft can depart with cabin crew
less than this minimum. Any reduction below this regulatory minimum shall
require specific authorisation from AUTHORITY.

(b) Below Regulatory Minimum Cabin Crew
Due to last minute unforeseen circumstances if there is a requirement to
operate less than the stipulated regulatory minimum, the procedures in the
deployment of cabin crew shall be based on the following.
(1) Operations with below regulatory minimum cabin crew is not allowed for
flight from base (Muscat);
(2) Prior approval of AUTHORITY mandatory;
(3) Prior to the commencement of the flight, the commander shall receive
approval from the Post Holder Flight Operations;
(4) The number of passengers has been reduced in accordance with
procedures specified in OM-E. At least one cabin crew member is required
for every 50, or fraction of 50, passengers present in the aircraft;
(5) Re-seating of passengers with due regard to exits and other applicable
aeroplane limitations;
(6) Re-location of a cabin crew;
(7) Upon completion of the flight, the commander shall complete a
Mandatory OccE-F705-11E9-B9

Aircraft Type Regulatory Minimum
(AUTHORITY) @
A330-300 8
A330-200 8
B787-8/9 8
B737-800/900ER 4
B737-8 4
ERJ 170-200 2

Schedule minimum number of cabin crew with at least 3 months experience as
below:
Aircraft Type Minimum Cabin Crew with at least 3
months experience as cabin crew member
A330-300/200 4
B787-8/9 4
B737-800/900ER 2
B737-8 2
ERJ 170-200 1YP

The following minimum crew complement must be on board
(a) Prior to commencement of passenger boarding, except when operating with
below regulatory minimum crew.
(b) During transit when passengers are on board, except when operating with
below regulatory minimum crew.
(c) During re-fuelling / de-fuelling with passengers embarking, on board or
disembarking.
Aircraft Flight Deck Cabin Crew
A330-300/200
One Pilot
8
B787-8/9 8
B737-800/900ER 4
B737-8 4
ERJ 170-200 2

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10
Q

4.1.7 Restriction After Initial Line Clearance

A

(a) Commanders: For the first 100 hours on type as Pilot In Command
�h Airline Minima should be increased as given in OMA 8.1.3.23; and
�h No takeoffs and landings to be given to Co-pilots.
(b) Co-pilots: For the first 100 hours on type as Co-pilot
�h To be scheduled with Commanders having more than 100 hours on type
command experience; or
�h To be scheduled with Commanders having more than 500 hours of Command
experience.
(c) Cover Pilot: For a pilot to be scheduled as a cover pilot the requirement is 100
hours on type.

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11
Q

4.1.8 Co-pilot as Pilot Flying

A

A line Commander may allow a Co-pilot to carry out a Take-Off and/ or Landing
provided:
(a) The runway is not contaminated;
(b) The braking action is at least good;
(c) The cross wind component does not exceed 15 knots;
(d) For take-off the visibility is 1000 m or more; and
(e) For landing, the applicable minima for approaches.
The Commander is required to assume the duties of PF irrespective of prior
allocations:
�h at any time he considers it is necessary for the safety; or
�h at any time he considers Oman Air Standards are being compromised of the above
conditions.
Note: Training Commanders may allow Co-pilots to perform take-off and landing with
weather conditions below those indicated with the exception of the landing minima.exception of th

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12
Q

6.1.9 Deep Diving (SCUBA)

A

Flying in pressurized aircraft after deep sea diving can result in decompression
sickness (Bends). Therefore crew members should not participate in deep diving
within 48 hours before a flight.w

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13
Q

6.1.10 Blood Donation

A

After a blood donation the volume of blood lost is made up in a matter of hours but
the cellular content can take some weeks to return to the previous level. Therefore
crew members should not donate blood within 24 hours before a flight assignment
and should not volunteer as blood donors whilst in active flying.

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14
Q

7.1.3 Flight Crew � Flight Time

A

(1) 1000 hours in any period of 365 consecutive days; and
(2) 100 hours in any period of 28 consecutive days.

Reporting Time Between Maximum Uninterrupted Block
Time
0700 � 1359 11 hours
1400 � 1759 10 hours
1800 � 0459 9 hours
0500 � 0659 10 hours
TABLE 01: Maximum uninterrupted block times � flight crew of two

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15
Q

7.1.3.2 Duty periods - Flight Crew

A

Oman Air shall ensure that the total duty periods to which a flight crew
member is assigned shall not exceed:
(1) 1800 hours in any period of 365 consecutive days;
(2) 190 hours in any period of 28 consecutive days; and
(3) 55 hours (*) in any 7 consecutive days.

However this figure (*) can be increased to 58 hours when a rostered duty
consisting of series of duty periods has commenced and is subject to
unforeseen operational delays. A crew member may not start any duty
period knowing 55 hours will be exceeded in any consecutive 7 days.

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16
Q

7.1.3.3 Flight duty periods (FDP)w

A

Reporting Time (Local Time)
Number of landings as operating flight crew member
1-2 3 4 5 6 7 8
0700 - 1159 1400 1315 1230 1145 1100 1015 0930
1200 - 1359 1330 1245 1200 1115 1030 0945 0900
1400 - 1559 1300 1215 1130 1045 1000 0915 0900
1600 - 1759 1230 1145 1100 1015 0930 0900 0900
1800 - 0359 1200 1115 1030 0945 0900 0900 0900
0400 - 0459 1230 1145 1100 1015 0930 0900 0900
0500 - 0559 1300 1215 1130 1045 1000 0915 0900
0600 - 0659 1330 1245 1200 1115 1030 0945 0900
Table 02: Allowable Flight Duty Periods � Multi Pilot Operations

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17
Q

7.1.3.4 Augmented Flight Crew

A

Oman Air shall ensure:
(a) Irrespective of the reporting time, if a flight crew comprising at least 2 pilots is
augmented by the addition of at least one fully qualified flight crew member,
in order to increase the flight duty period derived from Table 02 of this section,
(1) where the additional flight crew member occupies a flight deck observer
seat during take-offs and landing, the flight duty time may be extended to
15 consecutive hours provided:
(i) The sharing of time away from controls between those flight crew
members leaving their posts is kept in balance.
(ii) The subsequent minimum rest period is increased by at least 2
hours.
(2) where a flight relief facility seat is provided, the flight duty time may be
extended to 17 consecutive hours, in which case the maximum flight deck
duty time for any flight crew member shall be 12 hours;
(3) where a flight relief facility bunk is provided, the flight duty time may be
extended to 20 consecutive hours, in which case the maximum flight deck
duty time for any flight crew member shall be 14 hours, provided:
(i) The sharing of time away from controls between those flight crew
members leaving their posts is kept in balance;
(ii) The subsequent minimum rest period is at least equal to the
length of the preceding flight duty time; and
(iii) The augmented flight crew is scheduled to carry out no more than
2 landings within a flight duty period or, with the approval of the
AUTHORITY, 3 landings, provided the block time for one sector is
2 hours or less.SUCH D

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18
Q

7.1.4.1 Duty Periods-Cabin Crew

A

Oman air shall ensure that the total duty periods to which a cabin crew
member is assigned do not exceed
(1) 1800 hrs in any period of 365 consecutive days;
(2) 190 hrs in any Period of 28 Consecutive days; and
(3) 60 hrs in any 7 consecutive days. However this figure can be increased to
63 hours when a rostered duty consisting of a series of duty periods has
commenced and is subject to unforeseen operational delays. A crew
member may not start any duty period knowing 60 hours will be exceeded
in any consecutive 7 days.

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19
Q

7.1.4.3 Extension of allowable Flight duty periods Cabin Crew

A

Oman air shall ensure that if extending the allowable flight duty periods for cabin
crew, irrespective of the reporting time, the flight duty period shall not exceed 18
hours, provided that no more than 2 landings are carried out within a flight duty
period, or, with the approval of AUTHORITY, 3 landings.
(a) When allocating flight duty periods above 16 hours for cabin crew members,
Oman air shall ensure that the following conditions are met.
(1) Each cabin crew member is free of all duties for a period of time equal to
one third of the period calculated by subtracting one hour for each landing
from the total block time in the flight duty period; and
(2) For at least one third of the number of cabin crew members, bunks for the
resting cabin crew members, separated and screened from the flight deck
and the passengers, are available.
(b) When allocating flight duty periods above 14 hours, but not exceeding 16
hours, for cabin crew members, Oman air shall ensure that the following
conditions are met.
(1) Each cabin crew member is free of duties for a period of time equal to one
quarter of the period calculated by subtracting one hour for each landing
from the total block time in the flight duty period; and
(2) For at least one quarter of the number of cabin crew members,
comfortable reclining seats for the resting cabin crew members,
separated from the flight deck and screened from the passengers, are
available.
(c) In exceptional circumstances, when allocating flight duty periods for cabin
crew members, who are above the maximum flight duty periods prescribed in
OM-A 7.1.3.3 Table 02, but not exceeding 14 hours, Oman air shall ensure that
each cabin crew member is free of duty for one hour during the flight.
(d) The periods free of duty should preferably be consecutive

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20
Q

7.2 Exceedances of Flight and Duty Time Limitation and/or
Reduction of Rest Periods

A

The allowable flight duty period may not be increased by more than 2
hours unless:
(i) The flight crew has been augmented, in which case the allowable
flight duty period may be increased by not more than 3 hours; or
(ii) For cabin crew, the allowable flight duty period has been extended
in accordance with OM-A 7.1.4.3, in which case the allowable
flight duty period may be extended by not more than 3 hours;

(1) The commander is required to submit a report to SMLO whenever a flight
duty period is increased or when a rest period is reduced in actual flight
operation; and
(2) Where the increase of a flight duty period or reduction of a rest period
exceeds one hour, a copy of the report, to which SMLO must add his
comments, is sent to AUTHORITY through the EVP-COO no later than 28
days after the event.an 3 hours;

Before arriving at a decision, the commander is required to consult every crew
member for their acceptance to the modifications to the FDTL.
During the consultation process the commander must ascertain from each crew
regarding their fitness to continue the duty and this will entail in differentiating
between tiredness (a normal feeling after or during work) and fatigue (extreme
tiredness caused by exertion or cumulative lack of rest).YP

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21
Q

8.1.0.3 Performance Considerations

A

Regardless of the AFM/FCOM/AOM performance data, a take-off or landing
shall not be made on runways with a reported braking action �POOR� (or a
braking coefficient less than 0.25), unless justified by an emergency situation

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22
Q

8.1.0.7 Routes and Area of Operation

A

Routes and Area of Operation
The Air Operator Certificate authorizes Oman Air to conduct worldwide
commercial air transport with the exception that scheduled flights may not be
conducted into Israel.
Except in accordance with an ETOPS approval and OM-A 8.5, two engined
aeroplanes shall not be operated over a route which contains a point further
from an adequate aerodrome than the threshold distance as per the following
table.
Aeroplane Type Threshold Distance
A330-200/300 430 NM (Based on IAS 330 Knots)
B787-8 443 NM (Based on IAS 320 Knots)
B787-9 443 NM (Based on IAS 340 Knots)
B737-800/900ER 395 NM (Based on IAS 310 Knots)
B737-8 415 NM (Based on IAS 320 Knots)
ERJ 170-200 349 NM (Based on IAS 290 Knots)
Table-Threshold Distance

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23
Q

8.1.1 Minimum Flight Altitudes

A

Engine Failure (CAR-OPS 1.500)
The mass of the aeroplane at the pre-flight or in-flight re-planning stage shall be
such that:
- the one engine inoperative net flight path has a positive gradient at 1500 ft
above the aerodrome where the landing is assumed to be made after engine
failure; and
- the gradient of the one engine inoperative net flight path must be positive at
least 1000 ft above all terrain and obstructions along the route within 5 nm on
either side of the intended track.
- The one engine inoperative net flight path must permit the aeroplane to
continue flight from the cruising altitude to an aerodrome where a landing can
be made while clearing vertically, by at least 2000 ft, all terrain and
obstructions along the route within 5 nm on either side of the intended track.

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24
Q

8.1.3 Methods for the Determination of Aerodrome Operating Minima

A

For Oman Air, the AUTHORITY has approved the use of the �new� appendix 1
to EU OPS 1.430 (same as appendix 1 to CAR OPS 1.430) as the method for
establishing Aerodrome Operating minima as determined by Jeppesen.
As per Oman Air policy, circling approaches are not permitted.
Surveillance Radar ApproaIn ches (SRA) are not permitted.

In case the State Minima is higher than the Jeppesen Minima, the higher
minima should be used.

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25
8.1.3.6 General Guidelines on application on Aerodrome Operating Minima
An aircraft shall not descend below MDH/ MDA, unless: (1) the aircraft is in a position at that height from which a normal approach to the runway of intended landing can be made; and (2) the �required visual reference� (see note 1) has been established with regard to approach threshold of that runway or approach lights or other marking identifiable with the approach end of the runway. The approach may be continued below DA/H or MDA/H and the landing may be completed provided that the required visual reference is established at the DA/H or MDA/H and is maintained. Note 1:.The �required visual reference� means that section of the visual aids or the approach area which should have been in view for sufficient time for the pilot to have made an assessment of the aircraft position and rate of change of position, in relation to the desired flight path. (Visual references for different types of approaches are specified in this section). Notes: If MDA or DA is not specified, the authorised MDA or DA is the sum of the Obstacle Clearance Limit/Obstacle Clearance Height and Touch Down Zone elevation rounded up to the nearest 10 feet. If the touchdown zone elevation is not available, airport elevation shall be used. In no case this method of calculation permits lower minima than those outlined in this section. Whenever both RVR/ Visibility are available, RVR will be the criteria for landing.
26
8.1.3.6.2 Application of Ceiling and RVR
Ceiling must be taken into account when the only approaches available are non-precision. Vertical visibility if provided will replace ceiling. These values are given above the ground level. Note: Clouds reported broken or more will be considered for ceiling.g�� Take Off CAT I When touchdown and midpoint RVR values are available, BOTH shall be at or above the applicable Take-Off minima. Landing CAT I When touchdown and midpoint RVR values are available, the following criteria will be applied: �h Touch Down RVR at or above the landing minima �h Mid RVR equal to or greater than 350 meters ��unless a higher value is stated��. Approach and landing operations are NOT authorised when the prevailing visibility is below 800 meters or the Converted Meteorological Visibility (CMV) is below 800 RVR unless RVR reporting is available for the runway of intended use.a�
27
8.1.3.8 Take-off alternate aerodrome � Selection
Take-off alternate aerodrome � Selection Requirement: A take-off alternate must be selected and specified in the operational flight plan if it would not be possible to return to the aerodrome of departure for meteorological (weather conditions below CAT I minima, or applicable landing minima if ILS approach is not available), performance or operational reasons. The take-off alternate shall be located within: (1) For two-engined aeroplanes, either: One hour flight time at a one-engine-inoperative cruising speed in still air conditions based on the actual take-off mass; or When a take-off alternate is not available within one hour flight time as per (i) above, the approved ETOPS diversion time of 120 minutes, subject to any MEL restriction, at the one-engine inoperative cruising speed in still air standard conditions based on the actual takeoff mass for aeroplanes and crews authorised for ETOPS.
28
8.1.3.9 Takeoff Minima
(1) Before commencing take-off, a commander must satisfy himself that the RVR or visibility in the take-off direction of the aeroplane is equal to better than the applicable minima. The commander shall not commence take-off unless the weather conditions at the aerodrome of departure are equal to or better than CAT I minima or if ILS approach is not available applicable minima for landing at that aerodrome unless a suitable take-off alternate aerodrome is available. When the reported meteorological visibility is below that required for take-off and RVR is not reported, a take-off may only be commenced if the commander can determine that the RVR/visibility along the take -off runway is equal to or better than the required minimum. When no reported meteorological visibility or RVR is available, a take-off may only be commenced by the commander if he can determine that the RVR/visibility along the take-off runway is equal to or better than the required. Pilot assessment of visibility vs. RVR. Pilot�s assessment of visibility is acceptable ONLY when RVR is not reported. Pilots are NOT to use visibility assessment when RVR is reported. Use of terms RVR & Visibility. (A) RVR: Assessment of conditions by instruments. (B) Visibility: Assessment of conditions by manual observations.lined in this
29
Take - off Minima (RVR/Visibility)me � Selection
Nil (day only) 500 m Reported RVR/Visibility of only initial part of the takeoff run can be replaced by pilot assessment. (Applicable only when RVR is not reported) i) Day: Runway edge lighting and/or centerline marking ii) Night: Runway edge & runway end lights are required 400 m Reported RVR/Visibility of only initial part of the takeoff run can be replaced by Pilot Assessment (Applicable only when RVR is not reported)est).YP
30
8.1.3.11 Selection of Alternate Aerodromes (Weather Conditions)�
As per Oman Air Policy, for all flights at least one destination alternate is required. Oman Air does not operate flights without a destination alternate Takeoff Alternate It would not be possible to return to the aerodrome of departure due to: �h Weather conditions below the CAT I minima or applicable landing minima if ILS approach is not available at the aerodrome of departure; or �h For performance or operational reasons.s. Destination Alternate At least One alternate Weather reports or forecasts or any combination thereof, for the destination aerodrome indicate, that the weather conditions will be at or above the applicable destination landing minima. (Aerodrome Operating Minima) Two alternates �h Weather reports or forecasts or any combination thereof, for the destination aerodrome indicate, that the weather conditions are below the applicable destination landing minima. (Aerodrome Operating Minima); or �h No meteorological information is available.]P
31
8.1.3.12 Planning Minima for IFR flight
take-off alternate aerodrome when the appropriate weather reports or forecasts or any combination thereof indicate that, during a period commencing 1 hour before and ending 1 hour after the estimated time of arrival at the aerodrome, the weather conditions will be at or above the CAT I minima, or the applicable landing minima specified for the aerodrome if ILS approach is not available. (1) The ceiling must be taken into account when the only approaches available are non-precision approaches. (2) Any limitations related to one engine inoperative conditions must be taken into account. Planning minima for a destination aerodrome The destination aerodrome shall only be selected when: (1) the appropriate weather reports or forecasts or any combination thereof, indicate that, during a period commencing 1 hour before and ending 1 hour after the estimated time of arrival at the aerodrome, the weather conditions will be at or above the applicable planning minima (AOM as per Jeppesen) as follows: RVR/Visibility specified for the planned instrument approach at the aerodrome; and For a non-precision approach, the ceiling at or above MDH; or (2) Two destination alternate aerodromes are selected. Planning minima for a: (1) destination alternate aerodrome, or (2) 3% ERA aerodrome, or (3) en-route alternate aerodrome required at the planning stage Oman air shall only select an aerodrome for one those purposes when the appropriate weather reports or forecast, or any combination thereof, indicate that, during a period commencing one hour before and ending one hours after the estimate time of arrival at the aerodrome, the weather conditions will be at or above the planning minima in Table 4 below. Cat II and III (Pilots must be qualified for Cat II/III) Cat I (Note 1) Cat I Non-precision (Notes 1 & 2) Non-precision Non-precision (Notes 1 & 2) plus 200 ft/1000 mces.
32
8.1.3.22 Visual Approach
If NO circling minima is specified, the cloud ceiling must be at or above the appropriate Minimum Safe Altitude and the reported visibility at least 5000 meters.t/1000 mces. A side-step maneuver may be performed in Day VMC conditions, provided the criteria for stabilized approach is met. Once the aeroplane is established and descending on final approach to the runway of intended landing, 360� turns and other manoeuvres for descent profile adjustment are NOT PERMITTED. Minimum Flight Altitude shall be observed. If a full circuit pattern is flown, the circuit altitude shall be 1500 feet above aerodrome elevation.ast 5000 meters.t/1000 mces.
33
8.1.3.23 Airport Operating Minima for newly released PIC � on type
PIC up to 100 hours on type Plus 100 feet Plus 400 meters\_T�|ġ�
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8.1.3.24 Meteorological Conditionflightselection
For all flights a commander shall not (1) Commence take-off; nor (2) Continue beyond the point from which a revised flight plan applies in the event of in-flight re-planning, unless information is available indicating that the expected weather conditions at the destination and/or required alternate aerodrome(s) are at or above the planning minima prescribed in OM-A 8.1.3.12 (b) for destination aerodrome and OM-A 8.1.3.12 (c) (Table 4) for destination alternate and en-route alternate. Note: For destination expected weather conditions shall be above the applicable landing minima; and for required alternates the expected weather conditions shall be above the planning minima given in OM-A 8.1.3.12 (c) (Table 4). For all flights, a commander shall not continue beyond (1) Decision point when using the decision point procedure; or (2) Pre-determined point when using the predetermined procedure, unless information is available indicating that the expected weather conditions at the destination and/or required alternate aerodrome(s) are at or above the applicable aerodrome operating minima. For all flights, a commander shall not continue towards the planned destination unless latest information available indicates that, at the expected time of arrival, the weather conditions at the destination, OR at least one destination alternate aerodrome, are, at or above the applicable aerodrome operating minima.]P
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8.1.3.28 Commencement and Continuation of Approach
(a) The commander or the pilot to whom conduct of the flight has been delegated may commence an instrument approach regardless of the reported RVR/Visibility but the approach shall not be continued beyond the outer marker, or equivalent position, if the reported RVR/visibility is less than the applicable minima. (b) When RVR is not available, RVR values may be derived by converting the reported visibility in accordance with the OM-A 8.1.5.5. (c) If, after passing the outer marker or equivalent position (note 1 below) in accordance with (a) above, the reported RVR / visibility falls below the applicable minimum, the approach may be continued to DA/H or MDA/H. (d) When no outer marker or equivalent position (note 1 below) exists, the commander or the pilot to whom conduct of the flight has been delegated shall make the decision to continue or abandon the approach before descending below 1000 feet above the aerodrome on the final approach segment. (e) If the MDA/H is at or above 1000 feet above the aerodrome, the approach may be continued to MDA/H. below which the approach shall not be continued if the RVR/Visibility is less than the applicable minima. (f) The approach may be continued below DA/H or MDA/H and the landing may be completed provided that the required visual reference is established at the DA/H or MDA/H and is maintained. (g) The touchdown zone RVR is always controlling. If reported and relevant (see note 2), the midpoint and stop end are also controlling. Note 1: The �equivalent position� mentioned above can be established by means of a DME distance, a suitably located NDB or VOR, SRE or PAR fix or any other suitable fix that independently establishes the position of the aeroplane. Note 2: �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 knots.
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8.1.7.5 In-flight fuel Checks / Management - Requirements
The commander shall continually ensure that the amount of usable fuel remaining in flight is not less than the fuel required to proceed to an aerodrome where a safe landing can be made, with final reserve fuel remaining. In flight Fuel Check A commander must ensure that the fuel checks are carried out in flight at regular intervals. The remaining fuel must be recorded and evaluated to: (1) Compare actual consumption with planned consumption; (2) Check that the remaining fuel is sufficient to complete the flight; and (3) Determine the expected fuel remaining on arrival at the destination. (4) The relevant fuel data must be recorded. In flight Fuel Management (1) If, as a result of an in-flight check, the expected fuel remaining on arrival at the destination is less than the required alternate fuel PLUS final reserve fuel, the commander must take into account the traffic and the operational conditions prevailing at the destination aerodrome, along the diversion route to an alternate aerodrome and at the destination alternate aerodrome, when deciding to proceed to the destination. (2) In arriving at this decision and when within 1 hour of the destination, the commander may continue so as to land at the destination with not less than final reserve fuel if: The actual and forecast weather conditions at the destination will permit a visual approach; There are no known ATC delays for the period of ETA to ETA plus one hour; and There are at least two suitable geographically located separate (See note 1 below) runways available for landing. Note 1: Separate Runways: Runways on the same aerodrome are considered to be separate runways when: (A) They are separate landing surfaces which may overlay or cross such that if one of the runways is blocked, it will not prevent the planned type of operations on the other runway; (Mumbai airport does not fulfil this requirement) and (B) Each of the landing surfaces has a separate approach procedure based on a separate aid. (3) The commander shall request delay information from ATC when unanticipated circumstances may result in landing at the destination aerodrome with less than the final reserve fuel plus any fuel required to proceed to an alternate aerodrome. (4) Notwithstanding (2) above, in terminal area, the commander may decide to use the alternate fuel to continue approach, or hold and land at the destination aerodrome when: In the judgement of the commander a safe landing, with not less than final reserve fuel remaining can be accomplished at the destination aerodrome; and An allocated Expected Approach Time or confirmation from ATC of maximum likely delay is available; and Landing is assured in the prevailing and immediate forecast conditions. Note: In such cases, a CVR must be submitted to the company. (5) The commander shall advise ATC of a minimum fuel state by declaring MINIMUM FUEL when, having committed to land at a specific aerodrome, the pilot calculates that any change to the existing clearance to that aerodrome may result in landing with less than planned final reserve fuel. (6) If MINIMUM FUEL is declared, a CVR must be submitted immediately to the company. Notes: The declaration of MINIMUM FUEL informs ATC that all planned aerodrome options have been reduced to a specific aerodrome of intended landing and any change to the existing clearance may result in landing with less than the planned final reserve fuel. This is not an emergency situation but an indication that an emergency situation is possible should additional delay occur. It should be noted that Pilots should not expect any form of priority handling as a result of a �MINIMUM FUEL� declaration. ATC will, however, advise the flight crew of any additional expected delays as well as coordinate when transferring control of the aeroplane to ensure other ATC units are aware of the flight�s fuel state.
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8.1.8.10 Last Minute Changes (LMC) Procedure`"
Tolerance Limit A-330 B787-8 B787-9 B737 ERJ 170-200 Traffic Load and Operational Loads Plus or Minus 500 kg Plus or Minus 1400 Kg Plus or Minus 1180 Kg Plus or Minus 400 kg Plus or Minus 220 kg Corresponding Index Plus or Minus 10 Plus or Minus 4 Plus or Minus 4 Plus or Minus 5 Plus or Minusuel state. Note A: After a LMC, actual ZFW, TOW and LAW must be amended. However LMC less than 100 kg do not require such amendments. If the LMC total exceeds the limits as indicated above (LMC Tolerance Limits) a new load sheet must be prepared.�
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8.1.9.5 Compliance with and Deviation from Flight PlanX"a�~Km�\�
Flight shall be conducted in accordance with the flight plan. Deliberate deviation from flight plan enroute when necessitated by a change in conditions affecting safety, quality etc. shall be first requested from the appropriate ATC authority unless the deviation is necessitated by sudden emergency, in which case ATC shall be informed at the earliest possible time. In each case the appropriate ATC procedure shall be employed. In the event of inadvertent departure from flight plan, if it should be: (1) Deviation from the track � the aircraft will be navigated to regain track as soon as possible, unless ATC is advised and approves, if necessary, the new track. (2) Variation of TAS by plus or minus 5%, ATC will be informed of the variation. (3) Change in Estimated Elapsed Time of over 3 minutes to next reporting point. ATC will be notified of the change.�\>T'
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8.1.10.2 Computer Flight Plan System-Failure`"
In case of system failure, whereby it is not possible to generate a CFP, it is in order to use historic flight plans, while ensuring that: Historic flight plan is for the same type of aircraft and engine; Performance adjustment as required is made; Additional fuel is catered for on the basis of estimated wind component, when it is higher than the flight plan; and Delta correction is applied for difference in Estimated Take-Off Weight.P
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8.2.1.3 Refuelling with One Engine Runningre`"
This is strictly an emergency procedure and is used when APU is unserviceable or at airports where ground power is not available. The procedure for refuelling with one engine running is given in FCOM/AOM.
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8.2.1.4 Refuelling and Defuelling (Fuelling) when Passengers are Embarking, On-board or Disembarking
Fuelling is NOT PERMITTED with passengers boarding, on board or disembarking with WIDE CUT GASOLINE TYPE FUEL (Jet B, JP4, JP8 or equivalent) or when a mixture with these types of fuel might occur. Fuelling with JP 1 or Jet A1, when passengers are embarking, onboard, or disembarking is ALLOWED. However, when passengers are involved, precautions must be taken to ensure that they can be evacuated in the unlikely event that fire does occur. These precautions involve the Ramp Agent/Turnaround Coordinator, the engineer (qualified ground crew member), the cabin crew and the pilot(s) working as a team. Crew, staff and passengers must be warned that refuelling/defuelling will take place. No stretcher patients or passengers with reduced mobility to be boarded. Note: It is not necessary to disembark stretcher patients or passengers with reduced mobility before refuelling/defuelling. Such passengers may remain on board during refuelling / defuelling. Cabin crew must follow appropriate procedures in the event of evacuation/deplaning.
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8.2.1.4.1 Evacuation/Deplaning
In the case of a fire resulting from fueling operations, or from a large fuel spillage, a precautionary deplaning or an emergency evacuation may be performed. In both cases, the same recommendations apply.
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8.2.1.5 Refuelling/De-fuelling with Wide-Cut Fuel-Precautions/|�
Wherever possible, the use of wide-cut fuel types should be avoided. But in exceptional circumstances other types of fuel such as Jet B, JP-4 or AVTAG may be supplied if Jet A1 is not available and this may be accepted unless prohibited by the AFM. In such situations it is necessary to be aware that mixtures of widecut fuels and kerosene turbine fuels can result in the air/fuel mixture in the tank being in the combustible range at ambient temperatures. NO PASSENGERS ON BOARD.
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8.2.2.6 Death of Passengers
In the event of a passenger�s death on board an aircraft, bearing in mind that only a Physician can certify death and pronounce passenger dead, the Commander shall, according to prevailing circumstances, decide whether to return to last airport of departure, make a landing en-route or continue to scheduled destination. (2) However, when death is not certified, the Pilot-in Command (P.I.C) must divert to the nearest suitable airport. In such a case, the Cabin Director must move the other passenger away from the apparently-dead passenger; cover the body and calm passengers in the best possible manner. (3) If passenger is certified dead, the Pilot-in Command (P.I.C) may continue to destination. (4) The Commander shall inform Airport Services Manager/Representative (or handling agent) at the station by VHF communication of the presence of a dead passenger on board and if possible, name and nationality.�
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8.2.3 Procedure for Refusal of Embarkationre`"
Carriers may in the exercise of reasonable discretion refuse to carry or cancel the reserved space of and/or remove at a place en route when: Such action is necessary for safety reasons. Passengers who are not in conformity with the passport, visa, health or customs regulations of the countries of transit, destination and origin. Passengers who are not in possession of a valid ticket or having a counterfeit/altered ticket. Passengers whose transportation by air represents a danger or risk to themselves and/or their fellow travellers or property. Passengers, who show visible signs of disease and who, by their appearance, behaviour or kind of nursing required, are likely to cause discomfort to other passengers. Passengers requiring individual nursing and care during the flight and who are not accompanied by attendants. Persons obviously under the influence of alcohol, drugs or narcotics. Persons who fail to observe the instructions of the carrier. The passenger has refused to submit to a security check. In most cases, the decision whether a passenger falls within any of the above categories or not, and whether he should be accepted or not, would rest on the correct judgment of the Airport Services Manager and his correct interpretation of these rules. D50 Effective: 16-Feb-17tination, OR
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8.2.4.15 Checks Post De-icing / Anti-icing Check
Pre take off check The Commander shall continually monitor the weather conditions after the performed deicing / anti-icing treatment. Prior to takeoff he shall assess whether the applied holdover time is still appropriate and/or if untreated surfaces may have become contaminated. This check is normally done from inside the flight deck. Pre-Take-Off Contamination Check This is a check of critical surfaces for contamination. This check shall be performed when the condition of the critical surfaces of the aeroplane cannot be effectively assessed by a pre-take off check or when the applied holdover time has been exceeded. This check is normally performed from outside the aeroplane. The alternate means of compliance to a pre take off contamination check is a complete de-icing/anti-icing re-treatment of the aeroplane.
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8.2.4.19 Procedure in case of Hold Over Time is exceeded
The commander shall continually monitor the weather conditions after the performed de-icing/anti-icing treatment. Prior to take-off he shall assess whether the applied HOT is still appropriate and/or if untreated surfaces may have become contaminated. When holdover time tables are used as decision making criteria, take off after HOT has been exceeded CAN occur ONLY if pre take off contamination inspection is completed or the aircraft is de-iced / anti-iced again. If HOT is exceeded, the PIC shall contact the de-icing agency to De-ice the aircraft.
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Receiver autonomous integrity monitoring (RAIM):
A form of ABAS whereby a GNSS receiver processor determines the integrity of the GNSS navigation signals using only GPS signals or GPS signals augmented with altitude (baroaiding). This determination is achieved by a consistency check among redundant pseudo-range measurements. At least one additional satellite needs to be available with the correct geometry over and above that needed for the position estimation for the receiver to perform the RAIM function. RNAV operations: Aircraft operations using area navigation for RNAV applications. RNAV operations include the use of area navigation for operations which are not developed in accordance with PBN manual.
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8.3.2.11.5 ABAS Requirements
In the event of a predicted, continuous loss of appropriate level of fault detection of more than five minutes for any part of the RNP/RNAV operation where GPS is mandatory, the flight plan should be revised (e.g. delaying the departure or planning a different departure/arrival procedure).
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8.3.2.11.6 Flight crew proceduresitoring (RAIM):
Where only RNAV approaches are available at the destination, an alternate aerodrome is required that has an IAP based on conventional navigation aids. If an alternate is required, it must have an approved non�]GPS instrument approach procedure expected to be available at the estimated time of arrival.
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8.3.2.11.7 Electronic Database management(RAIM):
Verify the aircraft�s RNP/RNAV system is available, operating correctly, and the correct airport and runway data are loaded, prior to commencing take-off. Note that the Navigation databases are expected to be current for the duration of the flight. If the AIRAC cycle is due to change during flight, pilots should collect an additional Operational Flight Plan with the data of the next cycle, and use both plans on currently, until the ARINC cycle changes, at which point the OFP based on the expired ARINC cycle may be discarded. The electronic database must not be switched during flight. Not fly an RNP/RNAV SID or STAR unless it is retrievable by route name from the onboard navigation database and conforms to the charted route. However, the route may subsequently be modified through the insertion or deletion of specific waypoints in response to ATC clearances. The manual entry, or creation of new waypoints by a manual entry, of latitude and longitude or Place/Bearing/Distance values is not permitted. Additionally, pilots must not change any RNAV SID or STAR database waypoint type from a fly-by to a flyover or vice versa.9
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8.3.2.13.1 DiversionP
Minimum fuel for diversion The minimum fuel for a diversion includes fuel burn from the point of diversion to landing at the diversion aerodrome plus final reserve (fuel for 30 minutes holding at 1500 ft above diversion aerodrome at standard temperature).H 8.3.2.13.2 Diversions to Airports with Oman Air Representative If the alternate airport has Oman Air representative, he shall co-ordinate with the Commander and the Cabin Director and be responsible for handling the diversion in accordance with local procedure. 8.3.2.13.3 Diversions to Airports without Oman Air Representative If the alternate airport has No Oman Air Representative, the Commander shall be responsible for the correct co-ordination of all activities and to delegate the Cabin Director or other member of the crew for special duties. 8.3.2.13.4 Notification / Responsibilities En-route and destination station as well as the Operations Control Centre shall be informed of the actual time of arrival, expected time of delay and handling of passengers and load. Normally, the national carrier will act as an agent for Oman Air in areas where Oman Air has no representative. Handling Agent, as per Commander�s instructions will provide all the necessary requirements asked for by the Commander. The Cabin Director will be responsible for the welfare of the passengers. At least two of the cabin crew will have to accompany the passengers to the transit lounge. If it is decided that the passengers should go to the hotel, the commander with the agent will have to arrange for suitable accommodation for the passengers. The Cabin Director will ensure that there is always some cabin crew with the passengers.
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8.3.2.13.5 Passenger�s Travel Following Diversion for Medical Assistance
If the physician advises that further travel is undesirable, but does not threaten the person�s life, the person may be carried if he signs the following statement. �I acknowledge that the examining physician has recommended against my onward travel on Oman Air----- from------to------, but I elect to continue despite this advice�.
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8.3.2.17 Abnormal flight
The PF will be responsible for ATC communication during emergency or abnormal procedure, when PM is carrying out the Emergency or abnormal/check list.
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8.3.5 Ground Proximity Warning System Procedures
EGPWS warnings must always be regarded as �genuine� warnings. Action taken in response to a EGPWS hard warning i.e. �Terrain, Terrain� is to apply maximum power as aggressively as possible and rotate the aircraft to achieve the maximum possible angle of climb until the warning stops and minimum terrain clearance is attained. The above applies to any stage of height at night, in IMC or reduced visibility conditions. During daylight VMC conditions, if it can be positively confirmed by both the pilots to be a false warning, the commander may decide as the course of action to be taken. Any EGPWS activation must be reported in the ASR. When such activation indicates a technical malfunction of the system an appropriate entry should also be made in the Technical Log.
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8.3.18.24 System Malfunction � Reset of CB
After a system malfunction or trip, a circuit breaker may be reset if allowed by the applicable procedure in the aircraft QRH. The pilot who is doing the QRH procedure shall reset the circuit breaker, if directed by the QRH procedure. If the breaker trips again, the system or component should be considered inoperative and the breaker shall not be reset, unless a greater emergency exists, then only at the Commander's discretion. Weight.P
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8.3.18.25 Speed Control below 10,000ft AMSL
For climb, when above MSA and only with the approval or request of ATC, a higher speed may be maintained below 10,000 ft AMSL. During descent, with the approval or request of ATC, a higher speed may be maintained below 10,000 ft AMSL but the speed must be reduced to 250 knots or less, prior to descending below 5000 ft AAL.planing.
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8.3.18.28 Repeated Approach Attemptsft AMSL
A maximum of two approach attempts at the destination aerodrome are permitted. The following must be considered: �h Must have the required fuel to divert after the approach attempt. �h Before attempting a second approach, the PIC must be reasonably sure that the reason for Go around will not be encountered again and landing can be accomplished safely. �h Use of maximum possible automation and flying a higher category of approach, if available.atures.
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8.4.4.1 Precision Approach CAT IIptsft AMSL
Category II operation is a precision instrument approach and landing using ILS: o A Decision Height below 200 ft but not lower than 100 ft; and o RVR of not less than 300 m.
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8.4.4.2 Precision Approach CAT IIItsft AMSL
Category III operations are subdivided as follows: o Category III A operations: A precision instrument approach and landing using ILS with a decision height lower than 100 feet; and a runway visual range not less than 200 m. o Category III B operations: A precision instrument approach and landing using ILS with : �X A decision height lower than 100 ft, or no decision height; and �X A runway visual range lower than 200m but not less than 75m. Note: Where the decision height (DH) and runway visual range (RVR) do not fall within the same Category, the RVR will determine in which Category the operation is to be considered.
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8.4.20 Commencement and Continuation of an Approach
The Commander may commence an instrument approach regardless of the reported RVR/visibility but the approach shall not be continued beyond the Approach Ban point, if the reported RVR/visibility is less than the applicable minima. If, after passing the Approach Ban point, the reported RVR/visibility falls below the applicable minimum, the approach may be continued to DA/H. When no outer marker or equivalent position exists, the commander or the pilot to whom conduct of the flight has been delegated shall make the decision to continue or abandon the approach before descending below 1000 feet above the aerodrome on the final approach segment. The conversion of visibility to RVR is not applicable to CAT II/III approach. Continuation of approach below DH The approach may be continued below DA/H or MDA/H and the landing may be completed provided that the required visual reference is established at the DA/H or MDA/H and is maintained.1E9-B9
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8.4.28 Practice Low Visibility Approach/Autoland
When practicing CAT II / III procedures in weather conditions of CAT I or better, it will not be feasible to expect ATC to provide LVP protection. Commander should be alert to the possibilities of beam deflection by aircraft and vehicles on the ground and preceding traffic and notify ATC that they will be doing a practice approach.
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8.4.30 Loss of Visual References
Operations with DH - Before Touchdown If the decision to continue has been made and the visual references subsequently become insufficient (for the appropriate category), or the flight path deviates unacceptably, a go-around shall be initiated (a go around initiated below the MABH, whether auto or manual, may result in ground contact). Note: If the touchdown occurs after GA is engaged the AP remains engaged in that mode, and ATHR remains in Full Thrust. Ground spoilers and auto-brake are inhibited. Operations with DH - After Touchdown If the visual references are lost after touchdown, a go-around should not be attempted. (1) Fail Operational Aircraft: should continue the rollout with AP in ROLLOUT mode down to taxi speed. (2) Fail Passive Aircraft: Disconnect A/P after touchdown and maintain direction using localizer.�\>T'
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8.4.31 Failures and Associated Actionsh/Autoland
Downgrading during LVO approaches shall be conducted in accordance with FCOM procedures. If the required visual reference has already been obtained and a landing can be safely conducted, the approach may be continued at the Commander�s discretion. In general there are three possible responses to the failure of any system, instrument or element of the AFS during the approach, which causes capability reduction: REVERT to a higher minima and proceed to a new DH provided it has been included in the landing briefing. GO-AROUND and re-assess the capability, LAND if the required visual reference has been attained. The nature of the failure and the point of its occurrence will determine which response is appropriate.
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