omB Flashcards

1
Q

The following equipment must be operational:

A

1: APU
2: 2x DCU
3: 4 MFD’s configured:
4: PFD mode on both outboard display
EICAS on one inboard display
5: 2x Primary AC Generators
6: All standby instruments

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2
Q

Prohibited:
Freezing drizzle
Freezing rain
Super cooled large droplets

A

.

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3
Q

Maximum bank angle with one primary flight servo inop

A

30 degrees

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4
Q

High winds is above

A

30 kts for High wind rotor start and Shutdown procedure

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5
Q

Airspeed

Vne power on

A

165 kias

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6
Q

Airspeed

Ldg down or in transit

A

165 kias

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7
Q

Airspeed

APU operating

A

150 kias

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8
Q

Airspeed

Vne power off

A

120 kias

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9
Q

Airspeed

  • one engine inop
  • one or both SAS inop
  • one primary flight control servo inop
  • hydrolic boost inop
A

120 kias

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10
Q

Airspeed

inadvertent float deployment

A

Climb: 50 kias
Level: 55 kias
descent/auto: 60 kias

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11
Q

Groundspeed norm landing / takeoff

A

50 knots

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12
Q

Groundspeed emergency landing

A

65 knots

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13
Q
  • Groundspeed taxi

- Brake operations

A

35 knots

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14
Q

Max airspeed

  • sideward flight
  • rearward flight
  • crosswind hover
  • tailwind hover
A

35 knots

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15
Q

Flight in limited icing is

A

approved

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16
Q

Flight into limited icing condition

A

a positive air temperature band must exist at an altitude of at least 500ft above the surface to deice

17
Q

RIPS degradation

A

Aircraft may transition as long as power req to maintain level flight less than 81% and no more than 10% above the value cruise performance chart

If need more than 81% / 10% heli must descent to deice prior to continue

18
Q

Limitations limited icing conditions

A

1: Engine inlet anti-ice
2: Pitot heat
3: Windshield anti-ice
4: Ice rate system
5: OAT system

19
Q

Ambient temperature limits

A

-40 to ISA +35 C

20
Q

Pre-heat below

21
Q

Nr avoid range

A

36% - 49% (tail rotor drive shaft)

55% - 67% (engine power turbine critical range)

22
Q

Engine oil pressure MAX

A

5min: 100-120 psi

Must be below 100psi before run up

23
Q

Max wind for rotor engagement (any direction)

24
Q

Rotor brake recommended speed

A

40 % Nr

emergency brake 105% Nr

25
Coupled flight limits
above 120 kts: 200 feet agl below 120 kts: 50 feel agl Coupled below 200feet agl must monitor controls in case of excessive rate of descent. Coupled flight below 100 feet will be in VMC
26
Altimeters must read of each other
50 feet
27
Engine anti-ice on ground
60 seconds EXCEPT when OAT less than 5C AND visible moisture is present
28
Rotor brake max pressure
200psi. Normal: 150-200psi
29
Short runway takeoff. Runway below
800 meters