P-8A NEW PILOT NATOPS QUESTION
BANK
Maximum start EGT is ______ Degrees C
A. 725
B. 750
C. 925
D. 950
A1-P8AAA-NFM-000 4-6 - ANSWER A
The maximum runway slope allowed for P-8A operation is
A. +-1%
B. +-2%
C. +-3%
D. +-4%
A1-P8AAA-NFM-000 4-2 - ANSWER B
Maximum takeoff and landing tailwind component is
A. 15 knots
B. 5 knots
C. 20 knots
D. 10 knots
A1-P8AAA-NFM-000 4-2 - ANSWER A
Maximum operating altitude is
A. 35,000 ft
B. 37,000 ft
C. 40,000 ft
D. 41,000 ft
,A1-P8AAA-NFM-000 4-2 - ANSWER D
Maximum takeoff and landing altitude is
A. 8400 ft
B. 7400 ft
C. 8200 ft
D. 9400 ft
A1-P8AAA-NFM-000 4-2 - ANSWER A
For RVSM operations when field elevation is between sea level and
5,000 ft, the maximum allowable difference between PFD altitude
display is _______ ft and the maximum difference between altitude
display and field elevation is ______ ft
A. 75, 100
B. 50, 75
C. 100, 200
D. 75, 75
A1-P8AAA-NFM-000 4-4 - ANSWER B
Maximum allowable taxi gross weight (MTW) is
A. 189200 lbs
B. 189700 lbs
C. 188200 lbs
D. 157000 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER B
Maximum allowable takeoff gross weight (MTOW) is
A. 189200 lbs
B. 189700 lbs
C. 188200 lbs
,D. 157000 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER A
Maximum allowable landing gross weight (MLW) is
A. 187000 lbs
B. 141800 lbs
C. 159800 lbs
D. 149800 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER D
Maximum allowable zero fuel weight (MZFW) is
A. 187000 lbs
B. 141800 lbs
C. 159800 lbs
D. 149800 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER B
Except when required during the Smoke or Fumes Removal emergency
procedure, with engine bleed air switches ON, do not operate the air
conditioning packs in HIGH for
A. Approach
B. Takeoff
C. Landing
D. All of the Above
A1-P8AAA-NFM-000 4-16 - ANSWER D
Engine Anti-ice must be ON during all flight operations when icing
conditions exist or are anticipated, except during climb and cruise when
temperature is below
A. -40 C SAT
, B. -35 C SAT
C. -35 C TAT
D. -40 C TAT
A1-P8AAA-NFM-000 17-13 - ANSWER A
To protect engine acceleration capablility, a minimum airspeed of
_______ KIAS is recommended above ______ feet when one BLEED
air switch is OFF and wing anti-ice is ON.
A. 200; 10000
B. 230; 15000
C. 250; 15000
D. 250; 10000
A1-P8AAA-NFM-000 17-15 - ANSWER B
Use of aileron trim with the autopilot engaged is
A. limited to 2 seconds or 5 clicks.
B. allowed only above 250 KIAS
C. not restricted
D. prohibited
A1-P8AAA-NFM-000 4-17 - ANSWER D
Do not engage the autopilot for takeoff below ______ AGL.
A. 400
B. 200
C. 100
D. 600
A1-P8AAA-NFM-000 4-17 - ANSWER A
Engine maximum and minimum limits are
A. marked by a red line on the DU
BANK
Maximum start EGT is ______ Degrees C
A. 725
B. 750
C. 925
D. 950
A1-P8AAA-NFM-000 4-6 - ANSWER A
The maximum runway slope allowed for P-8A operation is
A. +-1%
B. +-2%
C. +-3%
D. +-4%
A1-P8AAA-NFM-000 4-2 - ANSWER B
Maximum takeoff and landing tailwind component is
A. 15 knots
B. 5 knots
C. 20 knots
D. 10 knots
A1-P8AAA-NFM-000 4-2 - ANSWER A
Maximum operating altitude is
A. 35,000 ft
B. 37,000 ft
C. 40,000 ft
D. 41,000 ft
,A1-P8AAA-NFM-000 4-2 - ANSWER D
Maximum takeoff and landing altitude is
A. 8400 ft
B. 7400 ft
C. 8200 ft
D. 9400 ft
A1-P8AAA-NFM-000 4-2 - ANSWER A
For RVSM operations when field elevation is between sea level and
5,000 ft, the maximum allowable difference between PFD altitude
display is _______ ft and the maximum difference between altitude
display and field elevation is ______ ft
A. 75, 100
B. 50, 75
C. 100, 200
D. 75, 75
A1-P8AAA-NFM-000 4-4 - ANSWER B
Maximum allowable taxi gross weight (MTW) is
A. 189200 lbs
B. 189700 lbs
C. 188200 lbs
D. 157000 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER B
Maximum allowable takeoff gross weight (MTOW) is
A. 189200 lbs
B. 189700 lbs
C. 188200 lbs
,D. 157000 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER A
Maximum allowable landing gross weight (MLW) is
A. 187000 lbs
B. 141800 lbs
C. 159800 lbs
D. 149800 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER D
Maximum allowable zero fuel weight (MZFW) is
A. 187000 lbs
B. 141800 lbs
C. 159800 lbs
D. 149800 lbs
A1-P8AAA-NFM-000 4-11 - ANSWER B
Except when required during the Smoke or Fumes Removal emergency
procedure, with engine bleed air switches ON, do not operate the air
conditioning packs in HIGH for
A. Approach
B. Takeoff
C. Landing
D. All of the Above
A1-P8AAA-NFM-000 4-16 - ANSWER D
Engine Anti-ice must be ON during all flight operations when icing
conditions exist or are anticipated, except during climb and cruise when
temperature is below
A. -40 C SAT
, B. -35 C SAT
C. -35 C TAT
D. -40 C TAT
A1-P8AAA-NFM-000 17-13 - ANSWER A
To protect engine acceleration capablility, a minimum airspeed of
_______ KIAS is recommended above ______ feet when one BLEED
air switch is OFF and wing anti-ice is ON.
A. 200; 10000
B. 230; 15000
C. 250; 15000
D. 250; 10000
A1-P8AAA-NFM-000 17-15 - ANSWER B
Use of aileron trim with the autopilot engaged is
A. limited to 2 seconds or 5 clicks.
B. allowed only above 250 KIAS
C. not restricted
D. prohibited
A1-P8AAA-NFM-000 4-17 - ANSWER D
Do not engage the autopilot for takeoff below ______ AGL.
A. 400
B. 200
C. 100
D. 600
A1-P8AAA-NFM-000 4-17 - ANSWER A
Engine maximum and minimum limits are
A. marked by a red line on the DU
