We can improve vulnerability by _____________

placing fuel tanks on the engine

avoiding fuel tanks near to the engine

placing fuel tanks on the engine

placing fuel tanks inside the engine

placing fuel tanks at any location

FMEA will consider _____________

which battle damage can affect individual aircraft components?

Failure mass and effect analysis

Failure modes and effect analysis

Failure mass and effect analysis

Failure mass and effective analogy

Failure modes and effect analogy

Vulnerability of an aircraft is ability of the aircraft ______________

to sustain damage, continue flying and return to base

Explore topic-wise MCQs in Aircraft Design.

This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Design knowledge and support exam preparation. Choose a topic below to get started.

1.	If an aircraft has three components which can be considered as vulnerable components then, evaluate total vulnerable area. Given area of component 1, 2 and 3 are 5ft², 4ft² and 80ft² respectively with Pk as 1, 0.5 and 0.3 for component 1, 2 and 3 respectively.
A.	31ft<sup>2</sup>
B.	50ft<sup>2</sup>
C.	10ft<sup>2</sup>
D.	4ft
Answer» B. 50ft<sup>2</sup>

Discussion

2.	An aircraft component has presented area 6 ft² with Pk as 1.0. Find vulnerable area.
A.	6ft<sup>2</sup>
B.	82ft<sup>2</sup>
C.	7ft<sup>2</sup>
D.	72ft<sup>2</sup>
Answer» B. 82ft<sup>2</sup>

Discussion

3.	In order to improve vulnerability consideration, we can use _________
A.	redundant components
B.	high lift device
C.	vortex generator
D.	we cannot improve it
Answer» B. high lift device

Discussion

4.	A firewall should be provided for vulnerability consideration.
A.	True
B.	False
Answer» B. False

Discussion

5.	We can improve vulnerability by _____________
A.	avoiding fuel tanks near to the engine
B.	placing fuel tanks on the engine
C.	placing fuel tanks inside the engine
D.	placing fuel tanks at any location
Answer» B. placing fuel tanks on the engine

Discussion

6.	FMEA will consider _____________
A.	which battle damage can affect individual aircraft components?
B.	lift
C.	weight by an aircraft
D.	rcs
Answer» B. lift

Discussion

7.	FMEA stands for?
A.	Failure modes and effect analysis
B.	Failure mass and effect analysis
C.	Failure mass and effective analogy
D.	Failure modes and effect analogy
Answer» B. Failure mass and effect analysis

Discussion

8.	Vulnerable area will be same for each and every aircraft.
A.	True
B.	False
Answer» B. False

Discussion

9.	__________ is key parameter for vulnerability.
A.	Vulnerable area
B.	RCS
C.	IR
D.	Visual area
Answer» B. RCS

Discussion

10.	Vulnerability of an aircraft is ability of the aircraft ______________
A.	to sustain damage, continue flying and return to base
B.	to get damaged and failed
C.	to the radar detection
D.	to an IR detection
Answer» B. to get damaged and failed

Discussion

Explore topic-wise MCQs in Aircraft Design.

If an aircraft has three components which can be considered as vulnerable components then, evaluate total vulnerable area. Given area of component 1, 2 and 3 are 5ft2, 4ft2 and 80ft2 respectively with Pk as 1, 0.5 and 0.3 for component 1, 2 and 3 respectively.

An aircraft component has presented area 6 ft2 with Pk as 1.0. Find vulnerable area.

In order to improve vulnerability consideration, we can use _________

A firewall should be provided for vulnerability consideration.

We can improve vulnerability by _____________

FMEA will consider _____________

FMEA stands for?

Vulnerable area will be same for each and every aircraft.

__________ is key parameter for vulnerability.

Vulnerability of an aircraft is ability of the aircraft ______________

If an aircraft has three components which can be considered as vulnerable components then, evaluate total vulnerable area. Given area of component 1, 2 and 3 are 5ft², 4ft² and 80ft² respectively with Pk as 1, 0.5 and 0.3 for component 1, 2 and 3 respectively.

An aircraft component has presented area 6 ft² with Pk as 1.0. Find vulnerable area.