All Weather Operations Flashcards

(42 cards)

1
Q

Min Landing RVR for CAT II

A

300m

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2
Q

Min altitude by which “DUAL FD” has to appear on both PFD’s has to appear to continue on CAT II

A

1.100 ft

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3
Q

Only flap setting for CAT II

A

15°

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4
Q

Is RDC NP allowed for simulated and real CAT II/III approaches?

A

No

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5
Q

CAT II glideslope angle limits

A

2.5° to 3.5°
(OM-B 1.3.1.2)

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6
Q

Min decision height CAT II above threshold

A

100 ft

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7
Q

Minimum Use Height (MUH) for CAT II (autopilot must be disengaged at the latest at)

A

80 ft

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8
Q

are CAT II/III approaches allowed with AFM supplement 94 (Ops with gear extended)

A

No

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9
Q

Min RVR for CAT III

A

200m

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10
Q

min RVR for LVTO without and with HGS

A

125m and 75m (if airport approved)

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11
Q

HGS CAT III minimum AP disengagement

A

1.000 ft AGL

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12
Q

Minimum DH manual CAT III

A

50 ft

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13
Q

if engine failure occurs below 1.000ft, we must …………. the approach

A

discontinue

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14
Q

CAT III HGS glideslope limits

A

2.5° to 3.0°

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15
Q

Allowed flap settings for CAT II/III

A

15°

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16
Q

Max runway slope (not glideslope) for CAT III

A

1%

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17
Q

From what RVR is a takeoff considered as LVTO

18
Q

Max flaps for HGS LVO takeoff

19
Q

Rolling takeoff allowed in Low Vis Guided T/O?

20
Q

Practice CAT II approach minima (ceiling + vis)

A

ceiling 400ft and visibility 2000m

21
Q

Visual approach approach minima

A

Circling minima (or 3 km if not published) and runway in sight

22
Q

Generic circling minima for CAT C aircraft (MDH+ vis)

A

MDH 600 ft and vis 2400m

23
Q

When is it commanders landing for ILS approaches (additives to DH and req vis)

A

DH + 100ft and Req visibility + 700m

24
Q

When is it commanders landing for Non-Precision approaches (additives to DH and req vis)

A

DH + 200ft and Req visibility + 1000m

25
Apart from clouds or visibility, when is it commander's landing?
* Close to maximum crosswind * Reported windshear on final * Performing a CAT II or III approach * Major deficiencies on the aircraft or ground installations * Landing on a category C aerodrome * Any other unfavorable condition * Close to minimum runway length for landing
26
Max Crosswind (T/O or LDG, normal ops with wet or dry RWY)
32 kts
27
Max Crosswind (AP CAT II)
18 kts
28
Max Crosswind (HGS CAT II/III)
15 kts
29
Max Crosswind (London City Steep Appr)
25 kts
30
Max Crosswind (London City Takeoff)
32 kts
31
Max Tailwind (T/O or LDG, normal ops with dry or wet RWY)
20 kts (with other limiations)
32
Max Headwind (AP CAT II)
24 kts
33
Max Tailwind (AP CAT II)
10 kts
34
Max Headwind (HGS CAT II/III)
24 kts
35
Max Tailwind (HGS CAT II/III)
10kts
36
Tailwind between 10 and 20 kts is allowed for T/O or LDG normal operations if
* Anti-skid brake control system must be operative. * Nose wheel steering system must be operative. * Flight spoilers must be operative. * No operation with landing gear extended (Supplement 94). * Runway must be dry or wet for takeoff and landing. * Takeoff with NTOP / MTOP (limited to 5 minutes) with Bleeds OFF only. * Takeoff must be made with flaps 10° or 15°. * No icing conditions below 1.000 ft AGL for takeoff. * No CAT II/III or steep approaches * Landing with MAX NP, Flaps 35° and Bleeds OFF only. * Commander landing only.
37
Max Tailwind London City for T/O and Landing
5 kts
38
Max depth of contamination
60 mm
39
Max WED (Water Equivalent Depth)
15 mm
40
max runway slope (up or down)
2%
41
Definition of a windshear
* 10 knots indicated airspeed * 500 feet per minute vertical speed * 5 degrees pitch attitude * 1 dot displacement from the glideslope * Unusual power lever angle for a significant period of time
42
Single engine taxi-in must not be conducted
* With reported surface wind speeds 20 knots or more (propeller ground operating limitations) * When 180° turns are required, e.g. LCY * During freezing precipitation * During low visibility operations * On contaminated runways or ramps * With inoperative anti-skid brake control system * With inoperative nosewheel steering system * With inoperative #2 DC GEN or #2 AC GEN * With any hydraulic system failure * After alternate landing gear extension