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Helicopter types > A109SP General > Flashcards

A109SP General Flashcards

1
Q

Type of engines?

A

PWC207C

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2
Q

Max. gross weight for TO and LDG’s

A

3175 Kg.

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3
Q

Ambient air temperature limitations

A

-25 degrees C

+50 degrees C

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4
Q

VNE with any door removed or open to lock position?

A

75 KIAS

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5
Q

Slope limitation?

A

Nose down: 2 degrees
Nose up: 10 degrees
Sideward: 10 degrees

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6
Q

Weight of 1l Kerosin?

A

0.8 Kg

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7
Q

Autopilot?

A

AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) The Automatic Flight Control System (AFCS) mainly consists of a four-axis dual-duplex HAC3000-109 autopilot system. The system comprises: – One Flight Control Computer (FCC) – One AutoPilot Mode Selector (APMS) control panel – Three pairs of linear actuators – Four trim actuators (or magnetic brakes) – Four angular position transducers. The FCC, installed in the electro-avionic compartment, has two inde- pendent channels (Channel 1 and Channel 2). Each channel, pow- ered by an independent power supply unit, has two sections (Section A and Section B). Each section includes a CPU-board and an I/O-board. The two channels communicate with each other via dedi- cated internal and external data links.

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8
Q

Dimensionen

A

Länge: Ca. 13m

Durchmesser: Ca. 11m

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9
Q

What has to be noted concerning the hydraulic pressure if parking?

A

Hydraulic pressure decreases over time

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10
Q

How do we activate the autopilot in the cockpit?

A

Autopilot Mode Selector

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11
Q

Where do we select the heading?

A

Remote Bug Panel (RBP) => rechts und links (Cockpit)

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12
Q

What system provides flight environmental data?

A

Air Data Units ( ADU 1 und ADU 2)

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13
Q

What is the name of the standby horizon?

A

ESIS => Electronic Standby Indicator Sytem

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14
Q

How is the transponder activated?

A

WOW => Weight on wheel micro-switch

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15
Q

What means MFD?

A

Multi Function Display

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16
Q

What means EDU?

A

Electronic Display Unit

Rechts: EDU 1
Links: EDU 2

Achtung: Restliche Instruments: Rechts: 2, links: 1

17
Q

What means AHRS?

A

Attitude and Heading Reference System

18
Q

Autopilot => Function of NAV?

A

Lateral guidance (VOR etc.)

19
Q

Disconnect autopilot parameters => Which switch?

A

Collective => ATT (see Info on Display)

20
Q

Magenta Colour?

A

What the aircraft is achieving

21
Q

Annunciation: What means OS?

A

Over station mode

22
Q

Fuel capacity? Difference to regular capacity without additional tanks?

A

633 Kg.

Regular: 460Kg.

23
Q

Fuel consumation?

A

Ca. 210 Kg/h

24
Q

Low fuel warning?

A

66 Kg (33 Kg / Tank)

25
Q

VTOSS?

A

TO safety speed: 35 KIAS

26
Q

VY?

A

80 KIAS up to 10’000ft

2kts reduction /1000ft

60 KIAS at 20’0000

27
Q

Values for CAT A ground level heliport TO

A

35ft, VTOSS (35KIAS) up to 200ft, VY up to 1000ft.

28
Q

What is an ADI?

A

An attitude indicator (AI), also known as gyro horizon or artificial horizon or attitude director indicator (ADI, when it has a Flight Director), is an instrument used in an aircraft to inform the pilot of the orientation of the aircraft relative to Earth’s horizon. It indicates pitch (fore and aft tilt) and bank (side to side tilt) and is a primary instrument for flight in instrument meteorological conditions.

29
Q

What is an HSI?

A

Horizontal Situation Indicator (HSI) The HSI is a direction indicator that uses the output from a flux valve to drive the dial, which acts as the compass card. This instrument, shown in Figure 5-38, combines the magnetic compass with navigation signals and a glideslope. This gives the pilot an indication of the location of the aircraft with relationship to the chosen course.

INSTRUMENT FLYING HANDBOOK FAA

30
Q

What is an ESIS?

A

Electronic Standby Instrument System

31
Q

What means NLOC

A

NavLOC => Localizer based on GPS information

Remark: VLOC => VOR-Localizer

32
Q

Number and function of flux valves?

A

Magnetic sensor which brings information to the AHRU (Attitude and Heading Reference Unit) => AHRS (Attitude and Reference System)

RFM 7-246

Helicopter types (12 decks)

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