End of course questions ATP – CTP
questions and answers 100% guaranteed
success.
Place 3the 3following 3steps 3from 3the 3stall 3recovery 3template 3in 3the 3correct
3order:
A) retract 3speed 3brakes 3and 3spoilers
B) apply 3nose 3down 3pitch 3control 3until 3impending 3stall 3indications 3are
3eliminated
C) adjust 3bank 3angle 3to 3wings 3level
D) disconnect 3autopilot 3and 3auto-throttle 3/ 3auto 3thrust
E) return 3to 3the 3desired 3flight 3path
F) apply 3thrust 3as 3needed 3- CORRECT 3ANSWER. 3 D) 3disconnect 3autopilot
3and 3auto 3throttle
B) apply 3nose 3down 3pitch 3control
C) adjust 3bank 3angle 3to 3wings 3level
F) 3apply 3thrust 3as 3needed
A) 3retract 3speed 3brakes 3and 3spoilers
E) 3return 3to 3desired 3flight 3path
The 3objective 3in 3maneuvering 3the 3airplane 3is 3to 3manage 3energy 3so 3that?
A) Kinetic 3energy 3stays 3between 3limits.
B) Potential 3energy 3stays 3between 3limits.
C) chemical 3energy 3stays 3between 3limits.
D) All 3of 3the 3above. 3- 3 3 CORRECT 3ANSWER. 3 D) 3All 3of 3the 3above.
What 3is 3the 3effect 3on 3total 3drag 3if 3airspeed 3slows 3below 3L/D 3max?
,A) drag 3increases 3because 3of 3increase 3in 3parasitic 3drag.
B) drag 3decreases 3because 3of 3lower 3induced 3drag.
C) drag 3increases 3because 3of 3increased 3induced 3drag. 3- 3 CORRECT
3ANSWER . 3 C) 3drag 3increases 3because 3of 3increased 3induced 3drag.
A 3jet 3pilot 3flying 3at 3L/D 3max 3will 3obtain 3best:
A) Range
B) endurance
C) ride 3quality 3- CORRECT 3ANSWER. 3 A) 3Range
When 3a 3jet 3aircraft 3is 3flown 3at 3the 3appropriate 3airspeed 3for 3maximum
3range, 3which 3type 3of 3drag 3predominates?
A) parasite
B) induced 3drag
C) each 3type 3of 3drag 3contributes 3equally 3- CORRECT 3ANSWER. 3 A) 3parasite
While 3already 3at 3high 3speed 3what 3happens 3if 3mach 3is 3allowed 3to 3increase?
A) airflow 3over 3parts 3of 3the 3airplane 3begins 3to 3exceed 3the 3speed 3of 3sounds.
B) shock 3waves 3can 3cause 3local 3airflow 3separation.
C) characteristics 3such 3as 3pitch-up, 3pitch-down, 3or 3buffeting 3may 3occur.
D) All 3of 3the 3above. 3- 3 3 CORRECT 3ANSWER. 3 D) 3all 3of 3the 3above
What 3is 3the 3result 3of 3a 3shock 3induced 3separation 3of 3airflow 3occurring
3symmetrically 3near 3the 3wing 3root 3of 3a 3swept 3wing 3aircraft?
A) high 3speed 3stall 3and 3sudden 3pitch 3up
B) severe 3porpoising
C) A 3severe 3moment 3or 3"Mach 3Tuck" 3- CORRECT 3ANSWER. 3 C) 3a 3severe
3moment 3or 3"Mach 3Tuck"
The 3speed 3of 3sound 3generally 3decreases 3with 3increasing
3altitude. 3This 3occurs 3because:
A) the 3air 3temperature 3decreases
B) the 3air 3pressure 3decreases
C) the 3composition 3of 3the 3air 3changes 3- CORRECT 3ANSWER. 3 A) 3the
3air 3temperature 3decreases
critical 3mach 3number 3can 3be 3defined 3as:
A) the 3speed 3at 3which 3an 3aircraft 3is 3traveling 3faster 3than 3sound
B) the 3maximum 3Mach 3number 3at 3which 3an 3aircraft 3may 3be 3safely 3operated
, C) speed 3of 3an 3aircraft 3in 3which 3air 3flow
3over 3any 3part 3of 3the 3aircraft 3or 3structure 3first 3reaches 3but 3does 3not 3exceed
3mach 31 3- CORRECT 3ANSWER. 3 C)speed 3of 3an 3aircraft
3in 3which 3air 3flow 3over 3any 3part 3of 3the 3aircraft 3or 3structure 3first 3reaches 3but
3does 3not 3exceed 3mach 31
stability 3and 3the 3vertical 3axis 3tends 3to 3drive 3the 3side 3slip 3angle 3towards
3zero.
the 3most 3dynamic 3stability 3about 3the 3vertical 3axis 3on 3Modern 3jet 3transports
3is 3from?
A) the 3vertical 3fin
B) the 3rudder
C) an 3active 3stability 3augmentation 3system/ 3yaw 3damper
D) pilot 3roll 3input 3- CORRECT 3ANSWER. 3 C) 3an 3active 3stability
3augmentation 3system/ 3yaw 3damper
swept 3wings 3cause 3a 3sufficient:
A)increase 3of 3effectiveness 3of 3flaps
B) decrease 3in 3effectiveness 3of 3flaps
C) flap 3actuation 3reliability 3issue 3- CORRECT 3ANSWER. 3 B) 3decreased
3 effectiveness 3of 3flaps
why 3is 3divergence 3of 3stall 3AOA 3and 3Mmo 3hazardous?
A) any 3decrease 3in 3airspeed 3will 3cause 3the 3aircraft 3to 3buffet 3and 3potentially
3stall
B) any 3increase 3in 3airspeed 3may 3cause 3the 3aircraft 3to 3buffet 3and
3potentially 3suffer 3mach 3tuck
C) airspeed 3changes 3may 3occur 3due 3to 3environmental 3factors 3without 3pilot
3input
D) all 3of 3the 3above 3- CORRECT 3ANSWER. 3 D) 3all 3of 3the 3above
to 3maintain 3altitude 3in 3a 3banked 3turn, 3the 3lift 3produced 3by 3the 3airplane
3must 3be:
A) greater 3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of 3bank
3angle.
B) greater 3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of
3altitude
C) equal 3to 3the 3weight 3of 3the 3airplane 3- 3 CORRECT 3ANSWER. 3 A) 3greater
3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of 3bank 3angle.
excessive 3bank 3angles 3at 3high 3altitudes 3can 3be 3hazardous 3because?
A)the 3extra 3drag 3produced 3by 3the 3turn 3can 3lead 3to 3an 3Excursion 3below 3L/D
3 max
B) aircraft 3engines 3at 3higher 3altitudes 3produce 3less 3thrust 3to 3overcome 3drag
C) the 3aircraft 3will 3be 3operating 3closer 3to 3the 3buffet 3boundaries
questions and answers 100% guaranteed
success.
Place 3the 3following 3steps 3from 3the 3stall 3recovery 3template 3in 3the 3correct
3order:
A) retract 3speed 3brakes 3and 3spoilers
B) apply 3nose 3down 3pitch 3control 3until 3impending 3stall 3indications 3are
3eliminated
C) adjust 3bank 3angle 3to 3wings 3level
D) disconnect 3autopilot 3and 3auto-throttle 3/ 3auto 3thrust
E) return 3to 3the 3desired 3flight 3path
F) apply 3thrust 3as 3needed 3- CORRECT 3ANSWER. 3 D) 3disconnect 3autopilot
3and 3auto 3throttle
B) apply 3nose 3down 3pitch 3control
C) adjust 3bank 3angle 3to 3wings 3level
F) 3apply 3thrust 3as 3needed
A) 3retract 3speed 3brakes 3and 3spoilers
E) 3return 3to 3desired 3flight 3path
The 3objective 3in 3maneuvering 3the 3airplane 3is 3to 3manage 3energy 3so 3that?
A) Kinetic 3energy 3stays 3between 3limits.
B) Potential 3energy 3stays 3between 3limits.
C) chemical 3energy 3stays 3between 3limits.
D) All 3of 3the 3above. 3- 3 3 CORRECT 3ANSWER. 3 D) 3All 3of 3the 3above.
What 3is 3the 3effect 3on 3total 3drag 3if 3airspeed 3slows 3below 3L/D 3max?
,A) drag 3increases 3because 3of 3increase 3in 3parasitic 3drag.
B) drag 3decreases 3because 3of 3lower 3induced 3drag.
C) drag 3increases 3because 3of 3increased 3induced 3drag. 3- 3 CORRECT
3ANSWER . 3 C) 3drag 3increases 3because 3of 3increased 3induced 3drag.
A 3jet 3pilot 3flying 3at 3L/D 3max 3will 3obtain 3best:
A) Range
B) endurance
C) ride 3quality 3- CORRECT 3ANSWER. 3 A) 3Range
When 3a 3jet 3aircraft 3is 3flown 3at 3the 3appropriate 3airspeed 3for 3maximum
3range, 3which 3type 3of 3drag 3predominates?
A) parasite
B) induced 3drag
C) each 3type 3of 3drag 3contributes 3equally 3- CORRECT 3ANSWER. 3 A) 3parasite
While 3already 3at 3high 3speed 3what 3happens 3if 3mach 3is 3allowed 3to 3increase?
A) airflow 3over 3parts 3of 3the 3airplane 3begins 3to 3exceed 3the 3speed 3of 3sounds.
B) shock 3waves 3can 3cause 3local 3airflow 3separation.
C) characteristics 3such 3as 3pitch-up, 3pitch-down, 3or 3buffeting 3may 3occur.
D) All 3of 3the 3above. 3- 3 3 CORRECT 3ANSWER. 3 D) 3all 3of 3the 3above
What 3is 3the 3result 3of 3a 3shock 3induced 3separation 3of 3airflow 3occurring
3symmetrically 3near 3the 3wing 3root 3of 3a 3swept 3wing 3aircraft?
A) high 3speed 3stall 3and 3sudden 3pitch 3up
B) severe 3porpoising
C) A 3severe 3moment 3or 3"Mach 3Tuck" 3- CORRECT 3ANSWER. 3 C) 3a 3severe
3moment 3or 3"Mach 3Tuck"
The 3speed 3of 3sound 3generally 3decreases 3with 3increasing
3altitude. 3This 3occurs 3because:
A) the 3air 3temperature 3decreases
B) the 3air 3pressure 3decreases
C) the 3composition 3of 3the 3air 3changes 3- CORRECT 3ANSWER. 3 A) 3the
3air 3temperature 3decreases
critical 3mach 3number 3can 3be 3defined 3as:
A) the 3speed 3at 3which 3an 3aircraft 3is 3traveling 3faster 3than 3sound
B) the 3maximum 3Mach 3number 3at 3which 3an 3aircraft 3may 3be 3safely 3operated
, C) speed 3of 3an 3aircraft 3in 3which 3air 3flow
3over 3any 3part 3of 3the 3aircraft 3or 3structure 3first 3reaches 3but 3does 3not 3exceed
3mach 31 3- CORRECT 3ANSWER. 3 C)speed 3of 3an 3aircraft
3in 3which 3air 3flow 3over 3any 3part 3of 3the 3aircraft 3or 3structure 3first 3reaches 3but
3does 3not 3exceed 3mach 31
stability 3and 3the 3vertical 3axis 3tends 3to 3drive 3the 3side 3slip 3angle 3towards
3zero.
the 3most 3dynamic 3stability 3about 3the 3vertical 3axis 3on 3Modern 3jet 3transports
3is 3from?
A) the 3vertical 3fin
B) the 3rudder
C) an 3active 3stability 3augmentation 3system/ 3yaw 3damper
D) pilot 3roll 3input 3- CORRECT 3ANSWER. 3 C) 3an 3active 3stability
3augmentation 3system/ 3yaw 3damper
swept 3wings 3cause 3a 3sufficient:
A)increase 3of 3effectiveness 3of 3flaps
B) decrease 3in 3effectiveness 3of 3flaps
C) flap 3actuation 3reliability 3issue 3- CORRECT 3ANSWER. 3 B) 3decreased
3 effectiveness 3of 3flaps
why 3is 3divergence 3of 3stall 3AOA 3and 3Mmo 3hazardous?
A) any 3decrease 3in 3airspeed 3will 3cause 3the 3aircraft 3to 3buffet 3and 3potentially
3stall
B) any 3increase 3in 3airspeed 3may 3cause 3the 3aircraft 3to 3buffet 3and
3potentially 3suffer 3mach 3tuck
C) airspeed 3changes 3may 3occur 3due 3to 3environmental 3factors 3without 3pilot
3input
D) all 3of 3the 3above 3- CORRECT 3ANSWER. 3 D) 3all 3of 3the 3above
to 3maintain 3altitude 3in 3a 3banked 3turn, 3the 3lift 3produced 3by 3the 3airplane
3must 3be:
A) greater 3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of 3bank
3angle.
B) greater 3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of
3altitude
C) equal 3to 3the 3weight 3of 3the 3airplane 3- 3 CORRECT 3ANSWER. 3 A) 3greater
3than 3the 3airplanes 3weight, 3and 3the 3amount 3is 3a 3function 3of 3bank 3angle.
excessive 3bank 3angles 3at 3high 3altitudes 3can 3be 3hazardous 3because?
A)the 3extra 3drag 3produced 3by 3the 3turn 3can 3lead 3to 3an 3Excursion 3below 3L/D
3 max
B) aircraft 3engines 3at 3higher 3altitudes 3produce 3less 3thrust 3to 3overcome 3drag
C) the 3aircraft 3will 3be 3operating 3closer 3to 3the 3buffet 3boundaries
