EA-18G NATOPS EXAM QUESTIONS WITH
100% VERIFIED ANSWERS
What is the military and afterburner thrust of the F414-GE-400 engine?
13,900; 20,700
To prevent an APU running engagement and exhaust torching, a
minimum of _________ must elapse between APU shutdown and
another APU start
2 minutes
Read More
Under less than optimal conditions, as few as _______ of emergency
oxygen may be available
3 minutes
What two things happen when the APU FIRE light is pressed?
-arms the fire extinguisher
-fuel to the APU is secured
t/f, the alpha tone is disabled in GAIN ORIDE with FLAPS HALF or FULL
True
t/f, as mechanize d,there's no hazard associated with multiple FCS
RESET attempts to regain an X'd out surface following a hydraulic circuit
failure
true
Hydraulic pump output pressures are _____ and ______ psi
3000;5000
The STOP position on the EXT TANKS transfer switch prevents a
transfer and refueling of controlled external tank(s) except with a ______
caution
FUEL LO
T/F, with an air to ground store or tank on a wing station (not HUNG),
maximum roll rate is automatically reduced.
true`
If the _______ handle isn't set during the right or first engine start, a
_____ caution light comes on, when the corresponding generator comes
online.
parking brake; GEN TIE
list the seven cockpit circuit breakers
, -launch bar
-fcs channels 1,2,3,4
-hook
-landing gear
failure of the power transmission shaft (PTS) results in the display of the
associated________ and both ______ circuit cautions `
GEN, DC FAIL, BOOST LO, AMAD PR; HYD
What are the cockpit indications of a single TR failure?
there are none
At what altitude will the cockpit begin to pressurize?
>8000 feet
In flight, cabin over-pressurization is defined as more than _____ feet
below the scheduled cabin pressure altitude. On deck, cabin over-
pressurization is defined as more than _____ feet or __ needle widths
below the cabin pressure altimeter needle position prior to engine start
2000;2000;2
What are the three approach lights on the nose-gear and what do they
indicate?
-Red (fast)
-amber (on-speed)
-green (slow)
What is the reason for putting the flap switch to full prior to engine
shutdown?
to test switching valve operation, b
t/f in the event of a FADEC channel control system failure, the fadec
automatically selects the channel with the better capability
true
What is the primary and backup source of overspeed cutout protection
for the ATS during start?
-Primary: corresponding generator
-back-up: frequency sensing relay (FSR)
The control augmentation system (CAS) operates in two basic modes
up / auto (UA), powered approach (PA)
T/F, during landing, full-time NWS (low) is automatically engaged when
the nose landing gear and at least one main landing gear have weight
on wheels.
true
100% VERIFIED ANSWERS
What is the military and afterburner thrust of the F414-GE-400 engine?
13,900; 20,700
To prevent an APU running engagement and exhaust torching, a
minimum of _________ must elapse between APU shutdown and
another APU start
2 minutes
Read More
Under less than optimal conditions, as few as _______ of emergency
oxygen may be available
3 minutes
What two things happen when the APU FIRE light is pressed?
-arms the fire extinguisher
-fuel to the APU is secured
t/f, the alpha tone is disabled in GAIN ORIDE with FLAPS HALF or FULL
True
t/f, as mechanize d,there's no hazard associated with multiple FCS
RESET attempts to regain an X'd out surface following a hydraulic circuit
failure
true
Hydraulic pump output pressures are _____ and ______ psi
3000;5000
The STOP position on the EXT TANKS transfer switch prevents a
transfer and refueling of controlled external tank(s) except with a ______
caution
FUEL LO
T/F, with an air to ground store or tank on a wing station (not HUNG),
maximum roll rate is automatically reduced.
true`
If the _______ handle isn't set during the right or first engine start, a
_____ caution light comes on, when the corresponding generator comes
online.
parking brake; GEN TIE
list the seven cockpit circuit breakers
, -launch bar
-fcs channels 1,2,3,4
-hook
-landing gear
failure of the power transmission shaft (PTS) results in the display of the
associated________ and both ______ circuit cautions `
GEN, DC FAIL, BOOST LO, AMAD PR; HYD
What are the cockpit indications of a single TR failure?
there are none
At what altitude will the cockpit begin to pressurize?
>8000 feet
In flight, cabin over-pressurization is defined as more than _____ feet
below the scheduled cabin pressure altitude. On deck, cabin over-
pressurization is defined as more than _____ feet or __ needle widths
below the cabin pressure altimeter needle position prior to engine start
2000;2000;2
What are the three approach lights on the nose-gear and what do they
indicate?
-Red (fast)
-amber (on-speed)
-green (slow)
What is the reason for putting the flap switch to full prior to engine
shutdown?
to test switching valve operation, b
t/f in the event of a FADEC channel control system failure, the fadec
automatically selects the channel with the better capability
true
What is the primary and backup source of overspeed cutout protection
for the ATS during start?
-Primary: corresponding generator
-back-up: frequency sensing relay (FSR)
The control augmentation system (CAS) operates in two basic modes
up / auto (UA), powered approach (PA)
T/F, during landing, full-time NWS (low) is automatically engaged when
the nose landing gear and at least one main landing gear have weight
on wheels.
true
