Airframe Flashcards

1
Q

How many sections in the airframe?

Describe their divisions

A

3
Forward: Cabin nose to Bulkhead aft if passenger compartment
Intermediate: Bulkhead aft of passenger compartment to Tailboom
Tailboom: start of Tailboom and aft

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2
Q

Main materials in the Forward section.

A

Aluminum honeycomb and carbon graphite structures

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3
Q

Purpose, location and size of the tapered fairings in the Forward section.

A

Reduce aerodynamic drag
Forward door hinge to the bulkhead
3.5 inches per side

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4
Q

Materials that make up the nose

A

Fiberglass composite

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5
Q

Materials that make up the internal structure

A

Aluminum

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6
Q

Materials that make up the doors and door frames

A

Carbon-fiber composites

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7
Q

Describe door emergency egress function

A

Doors are jettisonable via a secondary release handle that disconnects the attachment pins from the door hinges

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8
Q

Litter Door CAS

A

Litter door not securely latched

Land as soon as practical

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9
Q

What are the seats made of?

A

Flame resistant leather fabric

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10
Q

Describe the materials that go into the windows

A

Windscreen: Polycarbonate shatter resistent windscreens
Chin bubbles: tinted acrylic plastic
Roof: Dark tinted acrylic plastic
Crew/Pax: Light gray tinted acrylic plastic

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11
Q

Main materials in the Intermediate section

A

Semi-monocoque structure with four longerons and carbon fiber composite side skins

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12
Q

Engine pan serves what 2 purposes?

A

As both a drip pan and a firewall made of titanium

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13
Q

What is in the equipment compartment?

A

Below the engine, behind the parcel shelf, above the baggage compartment.

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14
Q

Whats in the equipment compartment?

A

avionics/electrical equipment, fuel signal conditioner, space for optional equipment

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15
Q

Baggage compartment max weight

A

250 lbs

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16
Q

Baggage compartment max volume

A

16 cubic feet

17
Q

How many tied downs in the baggage compartment?

18
Q

Baggage Door CAS

A

Baggage door is not securely latched
Land as soon as Practical

  • shore power door on same CAS message
19
Q

Main materials in Tailboom section

A

Full monocoque design, obtaining its strength through skin and internal bracing

20
Q

How is the tailboom attached?

21
Q

What supports the tail rotor drive shaft?

A

The hanger bearings which are mounted via brackets. Six in total.

22
Q

Describe the horizontal stabilizer (mounting, material, purpose)

A

The horizontal stabilizer is a one-piece aluminum honeycomb inverted airfoil mounted through the tailboom. The inverted airfoil provides downward lift to maintain the cabin in a nearly level attitude through all cruise speeds.

23
Q

What is on the leading edge of the horizontal stabilizer and whats its purpose?

A

A leading edge slat

Improves pitch stability during climbs

24
Q

What is on the trailing edge of the horizontal stabilizer and what is its purpose?

A

Gurney flap

Reduces mast stress at high speeds

25
What is mounted on the end of the horizontal stabilizer and what is the purpose?
``` End auxiliary fins offset 5 degrees from the centerline Improves dihedral (roll) stability in forward flight ```
26
Describe the vertical stabilizer (fin) | Purpose and construction
Provides directional (yaw) stability Canted outboard 9 degrees to reduce required amount of tail rotor thrust during forward flight at cruise speeds Composed primarily of aluminum honeycomb
27
Purpose and limits of the stinger
Installed to prevent tail rotor making contact with the ground 400 lbs of force
28
Describe the cowls, positions, and what they are made of
1. Forward - hydraulics, carbon-fiber composite 2. Transmission - fiberglass composite 3. Air induction - aluminum 4. Engine - carbon-fiber composite 5. Aft - oil cooler, blower assembly, engine oil tank, carbon-fiber composite 6. Tailcone - covers tail rotor driveshaft, fiberlass composite
29
MR tie down max load
60 lbs
30
MR tie down max deflection
50 inches