Limitations Flashcards

1
Q

Load Limit Is

A

Max load expected in services

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2
Q

Ultimate Load Limit

A

Failing of a structure 1.5 times to load limit

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3
Q

Load Limit for CS25

A

2.5G

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4
Q

Load Limit for CS23 commuter

A

3.8G

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5
Q

Load Limit for a CS23 utility

A

4.4G

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6
Q

Load Limit for CS23 aerobatics

A

6G

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7
Q

Manoeuvre Envelope

A

Referred to as the Vn diagram (load factor against EAS)

The set out envelope we fly within

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8
Q

Stall Boundary in the Vn graph is where

A

Left had side of the envelope below the va speed

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9
Q

Vd

A

Design speed - used by engineer to structural will be the speed at which ac structure fails if falls outside this

Vibration and flutter likely

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10
Q

Va

A

Design Manoeuvre speed

Highest speed at which sudden full up elevator can be made without exceeding limit load factor

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11
Q

Va - Design Manoeuvre speed varies with

A

Mass - higher mass gives us a greater va

Altitude - va increases with altitude

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12
Q

Vc is

A

The design cruise speed

Faster than vb to cope with inadvertent speed increases by turbulence

Must be 32% more than VB

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13
Q

Vb

A

Design speed for max gust intensity

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14
Q

Vmo

A

Maximum operating speed

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15
Q

MNO

A

Max operating speed at altitude when flying with a Mach number

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16
Q

VLE

A

Max landing gear extended speed

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17
Q

VLO

A

Max speed when extending landing gear

Speed lower than VLE

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18
Q

VFE

A

Maximum flaps extension speed

Reduces max load factor

19
Q

Vra

A

Turbulence penetration speed

Must be 35kt below vmo

20
Q

Vne

A

Small aeroplane never exceed speed
Set at 0.9 VD
Red radial line on ASI
Small margin

21
Q

VNO

A

Maximum structural cruise speed
Cannot be faster than VC
0.89 of Vne

22
Q

Gust Loads

A

Sudden extra load felt through turbulence vertically

23
Q

How do you cope with a gust load

A

Maintain altitude and allow ac to respond naturally to severe up/down droughts

24
Q

Gust loads what to do with speed and altitude

A

Fly close to Vb and descend if near aerodynamic ceiling

25
Altitude on gust load factor
Low altitude means higher gust load factor Higher altitude means lower gust factor
26
Mass on load factor
Higher the mass the lower the load factor Lower the mass the greater the load factor
27
Wing loading on load factor
Low wing loading has a higher load factor High wing load has a lower load factor
28
Airspeed on wing load
Higher airspeed has a higher load factor increase Lower airspeed has a lower load factor increase
29
Load factor is proportional to
Wing area AOA EAS
30
Wing load is inversely proportional to
Wing loading Mass Altitude
31
Where does the gust load factor envelope start for speed and load factor on the graph
LF - 1 VS - 0
32
Vb Gust load factor
+-66FPS
33
Vc gust load factor FPS
+-50fps
34
VD gust load factor fps
+-25FPS
35
Resonance
Mass/stiffness determine natural frequency of oscillations Flutter - mass balancing and putting mass in front of hinge line
36
What needs to be taken into account when determining Va?
The Limit Load factor
37
How do you calculate Va from VS1
Find limiting load factor (4.4/2.5g etc) Use three step method to calculate VA from limiting load factor a load factor at 1G
38
VNo must not be greater than what of VNE
0.89
39
Large transport ac VC to VD negative load factor limit
VC -1 VD 0
40
MMO VMO applies to
CS23/S25
41
VNO and VNE apples to
CS23
42
Load Limit of a CS25 AC with flaps extended
2.0g
43
Design speeds and design gust values are
EAS