The FAA
Flight Engineer
test bank contains questions pertaining to
Performance
. The following list contains only a relatively small percentage of the pertinent
questions. Our software, which you are free to download now at no cost, will
generally contain a much more complete set of questions associated with this
test bank. This list is intended only to familiarize you in a general way with
the questions of the
Flight Engineer
test bank.
GroundSchool:
Flight Engineer
FAA Written Test Prep Software
for
MS-Windows |
|
|
That said, while the following questions are intended
as a general familiarization tool, this list may not be up-to-date nor accurate.
We do not update this website as often as we update our software, which will
contain at any moment all questions that we have for a given test / topic. Therefore,
if you need to actually study for your test, instead of using the list below,
we strongly, strongly encourage you to download our GroundSchool
Flight Engineer
written test prep software. Not only is it more complete and more up to date,
but it also includes answers and explanation and has many features to make your
study fast and efficient.
Sample Questions
from the FAA
Flight Engineer
Test Bank |
- For an airplane with a given gross weight and constant cruise speed, what is the relationship between fuel flow, temperature, and altitude? Fuel flow is higher when
- How does high humidity affect engine performance on takeoff without water injection?
-
(Refer to figure 2.)
Compute the V speeds for the following conditions.
Gross weight 180,000 lb
Pressure altitude 1,028 ft
OAT +94 �F
Flaps 25�
Tailwind 8 kts
Airport BOS RWY 35
- An airplane has been cruising for 2 hours and 15 minutes at a speed of Mach .82. Total fuel consumed during this period has been 27,250 pounds. If Mach 1.0 is 595 knots, what has been the NM per 1,000 pounds of fuel?
-
(Refer to figure 30.)
How much fuel remains after dumping under operating conditions No. 1?
-
(Refer to figure 2.)
Compute the V speeds for the following conditions.
Gross weight 250,000 lb
Pressure altitude 428 ft
OAT +80 �F
Flaps 25�
Tailwind 5 kts
Airport SEA RWY 34
- While flying in a steady wind of 25 knots, the airplane is turned from a direct headwind to a direct tailwind. The indicated airspeed will
- An airplane is descending at Mach .6. The true airspeed will
-
(Refer to figure 6.)
The maximum temperature limitation for takeoff is ISA +35 �C. Which is the highest temperature that will allow a takeoff from a 6,000-foot pressure altitude airport?
The
list above contains 1/4 or less of the actual number of questions
and may not be up to date! Download the software today to get
access to all available questions. |
For
more information about the
Flight Engineer
test bank, click here.
Copyright,
Content, and Accuracy Notice: the questions presented here and the organization
thereof include both elements whose copyright status is consistent with that
of many US government publications and elements whose copyright status is vested
in Dauntless Software, a private concern. Dauntless Software grants visitors
permission to use the contents of this page for personal use - commercial or
public use, including collecting (or harvesting) of any data or material on
this page is strictly prohibited. This material is presented for informational
purposes only and may be in error. Dauntless Software works hard to maintain
our FAA written test question banks. If you see an error on this web page, it
is likely NOT an error that is repeated in our software, as our software (unlike
this web page) is connected to our editorial mechanism whose mission is to quickly
identify and correct errors. If you see what you believe to be an error, please
download and try our software to see if the error is repeated there. If you
believe it is, you can use the issue-reporting mechanisms within the software
to contact our editors about any concern you may have and we will be happy to
look into it promptly.
|