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daffisinUtsjekk > Gjennomgang til OPC > Flashcards

Gjennomgang til OPC Flashcards

1
Q

Length S92? d-value

A

20.88 m

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2
Q

Hva MÅ fungere for å fly?

A 
APU
2x DCU
4x MFD
2x AC gen
All stby instruments
PFD outboard, EICAS inboard
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3
Q

Minimum tid 360 hover turn?

A

12 sec

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4
Q

Hva er max PA for RIPS?

A

10 000 ft

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5
Q

Hva er max DA for enroute?

A

15000 ft

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6
Q

Hva er max crosswind for Cat A takeoff?

A

35 kts

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7
Q

Max bank angle with one primary flight control servo U/S

A

?

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8
Q

With low fuel light, avoid..

A

10´pitch up. 5´pitch down

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9
Q

Slope landing limits?

A

UP/DOWN: 10 degrees

Right/left: 13 degrees

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10
Q

Max airspeed for instruments approach above 90 KIAS?

A

4,0 degrees

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11
Q

VNE

A

165 KIAS

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12
Q

Max airspeed ldg gear down or in transit?

A

165 KIAS

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13
Q

Max airspeed with APU operating?

A

150 KIAS

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14
Q

VNE power off?

A

120 KIAS

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15
Q

Max airspeed one/both SAS inop?

A

120 KIAS

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16
Q

Max airspeed with one primary flight control servo inop?

A

120 KIAS

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17
Q

Max airspeed with hydraulic boost inop?

A

120 KIAS

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18
Q

Max airspeed for landing gear emergency blowdown?

A

90 KIAS

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19
Q

Max airspeed with floats armed?

A

80 KIAS

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20
Q

Max airspeed after inadvertent float deployment?
-Climb
-Cruise
_Descent

A

50 / 55 / 60 KIAS

21
Q

Max groundspeed for normal landing and take off?

A

50 kts

22
Q

Max groundspeed for emergency landing

A

65 kts

23
Q

Max groundspeed taxi?

A

35 kts

24
Q

Max groundspeed for brake application?

A

35kts

25
Q

Vmini

A

50 kts

26
Q

Max airspeed windshield wipers?

A

100 kias

27
Q

Max airspeed for sideward flight / or crosswind hover?

A

35 kts

28
Q

Max airspeed for rearward flight / or tailwind hover?

A

35 kts

29
Q

Hvilke limitations for coupled operations?

A

+ 120 kts : 200 ft AGL

—————

30
Q

Max takeoff and landing mass?

A

26500 lbs

31
Q

Min operating mass?

A

16200 lbs

32
Q

Max pressure fuel quantity?

A

5175 lbs

33
Q

Rotor speed limits:
Normal
Precautionary range

A

104-106%

——————-

34
Q

OEI rotor speed:

Normal:
Precautionary:
Transient minimum:
Transient touchdown:

A

Normal: 100-106%

Precautionary: 95-100%

Transient minimum: 90%

Transient touchdown: 80%

35
Q

Power off rotor speed

Max:
Min (low rotor):
Transient min:

A

Max: 110%

Min: 95%

Transient: 80%

36
Q

Recommended rotor speed for normal and emergency rotor brake:

A

40%

37
Q

Baggage loading limits

A

1000
300 + 700

NEW: 890

38
Q

Low visibility take off brief

A

This will be a low visibility takeoff at rwy __
dep to follow
TDP at 45 kts
At TDP I will call committed or delay depending on visual references and remaining runway lenght

major mal………….

39
Q

Innhold i en mayday

A 
Mayday mayday mayday
Station called
Call sign
Name of distress
Pos/alt/hdg
Intentions
40
Q

Hva kvalifiserer til mayday i oma

A

1: Dual eng failure
2: Engine fire
3: fire smoke
4: Helicopter control problems due to loss of vital system
5: pilot incapasitation
6: low fuel/less than final reserve
7: unruly pax
8: Failure of systems that may turn critical

41
Q

Statement of intent:

A

Landing
Continuing / Ditching
Landing / Going around
Landing

42
Q

Minima offshore shuttle flight (less than 10nm)

Day
Night

A

Day: 300ft 2km -cloud base

Night: 500ft 5km

43
Q

ARA visibility and height req.

Day
Night

A

Day: 600ft 4000m

Night: 1200ft 5000m

Day: deck+50ft / 200ft 800m

Night: deck+50ft / 300ft 1200m

44
Q

Flare stack height

A

radius 150 m from the flare tip.

Vertical extent from 100 ft below the top of the flare boom up to 1,500 ft.

45
Q

Special VFR

A

VFR departures/arrivals can be authorized by the appropriate ATS unit as Special VFR flights to operate within a Control Zone by day in meteorological conditions lower than ceiling 1500 feet and ground visibility less than 5000m.
A clearance for a Special VFR flight may be granted to helicopters when:
• The flight visibility is not less than 1500m when entering or leaving the CTR via an established or agreed route (otherwise 3km).
• The clouds - rags included – are not below 200ft.
• The VFR flight can be executed clear of clouds and in continuous sight of ground or water.

46
Q

Performance class 2

A

A helicopter with performance such that, in the event of critical power-unit failure, performance is available to enable the helicopter to safely continue the flight, except when the failure occurs early during the take-off manoeuvre or late in the landing manoeuvre, in which case a forced landing may be required.

47
Q

Requirements for performance class 2

A
  • No night operations
    o Sea state 5 or less
    o Rescue services must be available within an acceptable timeframe
48
Q

Deck edge clearance

A

helideck operations shall be planned upon a minimum horizontal deck edge clearance of 15 feet,

and vertical obstacle clearance of 35 feet, in case of OEI during take-off and landing

daffisinUtsjekk (4 decks)

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