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?

22
Q

Max groundspeed for emergency landing

23
Q

Max groundspeed taxi?

24
Q

Max groundspeed for brake application?

25
Vmini
50 kts
26
Max airspeed windshield wipers?
100 kias
27
Max airspeed for sideward flight / or crosswind hover?
35 kts
28
Max airspeed for rearward flight / or tailwind hover?
35 kts
29
Hvilke limitations for coupled operations?
+ 120 kts : 200 ft AGL | ---------------
30
Max takeoff and landing mass?
26500 lbs
31
Min operating mass?
16200 lbs
32
Max pressure fuel quantity?
5175 lbs
33
Rotor speed limits: Normal Precautionary range
104-106% | -------------------
34
OEI rotor speed: Normal: Precautionary: Transient minimum: Transient touchdown:
Normal: 100-106% Precautionary: 95-100% Transient minimum: 90% Transient touchdown: 80%
35
Power off rotor speed Max: Min (low rotor): Transient min:
Max: 110% Min: 95% Transient: 80%
36
Recommended rotor speed for normal and emergency rotor brake:
40%
37
Baggage loading limits
1000 300 + 700 NEW: 890
38
Low visibility take off brief
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
Innhold i en mayday
``` Mayday mayday mayday Station called Call sign Name of distress Pos/alt/hdg Intentions ```
40
Hva kvalifiserer til mayday i oma
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
Statement of intent:
Landing Continuing / Ditching Landing / Going around Landing
42
Minima offshore shuttle flight (less than 10nm) Day Night
Day: 300ft 2km -cloud base Night: 500ft 5km
43
ARA visibility and height req. Day Night
Day: 600ft 4000m Night: 1200ft 5000m ----------- Day: deck+50ft / 200ft 800m Night: deck+50ft / 300ft 1200m
44
Flare stack height
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
Special VFR
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
Performance class 2
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
Requirements for performance class 2
- No night operations o Sea state 5 or less o Rescue services must be available within an acceptable timeframe
48
Deck edge clearance
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