問題一覧
1
What position on the NVD mounting bracket is the on position
up
2
What position on the NVD mounting bracket is the off position
down
3
At what angle do you hold the NVG’s to attach them to the mounting bracket
30 degree angle
4
On the low profile battery pack for the NVG’s what position is the primary on position
right
5
On the low profile battery pack on the NVG’s which position is the back up on position
left
6
How long will the high resolution test using the ANV – 20/20 stay on
3 minutes
7
exposing the NVDA to a highlight level for more than ____ Can cause a projected image to burn into the image intensifier
10 minutes
8
The maximum acceptable current for the binocular assembly is
90 miliampere
9
The internal life on the ANV – 126A is approximately _______ On low intensity level
60 minutes
10
if ANV-126A is left on an inactive shut off will occur in eight hours(after 7 hrs 30 minutes in power save state
false
11
in battery mode the ANV – 126A, shut off will occur after inactivity for 15 minutes (after five minutes in power save mode)
true
12
Begins at the edge and moves inward. You cannot see an image through it
shading
13
Cosmetic blemishes in the image intensifier, dirt or debris between the lines
black spots
14
A cosmetic blemish characterized by a faint hexagon pattern throughout the viewing area that most often occurs at high light Levels or when viewing very bright lights
fixed pattern noise
15
And a regular pattern of dark thin lines in the field of view either throughout the image area or in parts of the image area
Chicken wire
16
A small non-uniform bright area that may flicker or appear constant
Bright spots
17
Steady or fluctuating pinpoint of bright light in the image area which does not go away when all light is blocked from the objective lens
Bright spots
18
Occurs when light outside the field of view strikes the objective lens and scatters instead of passing straight through the lens
veiling glare
19
Ensure the focus stop pin on the NVG is torqued to
14 in ounce
20
Purging of the AN/AVS-9 Can be accomplished at any time.
false
21
if nitrogen tank is below ___ of capacity of the tank, replace with a full one
10 %
22
Set both IPD knobs on the binocular assembly two _____ when purging
72 mm
23
watch The gauge on the purge control box to see that it indicates ____
3+-1/2 psi
24
Cycle between pumping the -20 inch mercury and 3+-1/2 psi nitrogen for a total of ___
3 cycles
25
The purge valve and performed packing must be replaced and tightened within ______ Or the nitrogen within the monocular may be
30 seconds
26
torque the purge valve on the NVG monocular to ____
8 in ounce
27
using the ___ hex key, carefully remove the focus stop pin by turning CCW
1/16
28
when replacing the monocular housing solder iron should be set to ____ And applied until the wires come loose
625+-5 degrees
29
retrained wrench gets torqued to ___
130 in ounce(8 in pounds)
30
hazard AFI
91-201
31
ideal conditions for packing parachutes are a temperature of ___ in a relative humidity of ____
75 degrees, 60 %
32
ensure that no more than___of suspension line is stowed inside the container
16 in
33
Double wrap a piece of ___ wide thermosetting tape around the full length of the reefinv line snap
.5 to 1 in
34
Cutters not to extend more than___above closed flaps
.5 in
35
strict adherence to the____extension of suspension line bight through aft locking loop as required to prevent potential snagging and lock up of suspension line during deployment
.75 to 1 in
36
Stow all but the last___of suspension lines in the container tunnels
18 to 22 in
37
blow out the inside if the pitot tubes with dry air or nitrogen not to exceed
15 Psi
38
Routine inspection shall be accomplished every___on parachutes installed in MK – H7
10-14 days
39
IPI checklist will be standardized, reviewed, and approved by the unit___
QA
40
Center of webbing Fraying beyond___or center black thread is discernible
3/4 in
41
if emergency oxygen cylinder is installed, inspect for proper installation and proper hose length in accordance with
15X1-4-2-12
42
Do you not use bourdon forge___ejection snaps on ejection seat aircraft
85
43
Full force required to release ejector snaps it should be ___
7+-2 pounds
44
Inspect oxygen regulator connector mounting bracket for proper installation in accordance with_
15 X 5–4 – 1–101
45
Static line cord pull force should be ____
10 to 15 Pounds
46
UWARS is an explosive item classified as
1.4s
47
parachute Inspection record shall be maintained in accordance with ___
00–2 5–241
48
At time of removal, stamp or stencil date on to components adjacent to date of manufacture
Month and year proceeded by the letter I
49
place locally manufactured _____ Shot bag onto pilot chute, if it compress the spring fully replace
17 pounds
50
Inspect security of attachment for Line jettison anchor loops on suspension lines
3 and 26
51
when inspecting the parachute tension canopy to ____
20 Pounds
52
release lanyard slack shall be ____
Minimum 1 inch, maximum 3 inch
53
torque connector links to___
8 to 10 Pounds
54
inspect pull down vent line for proper length by applying 25 pounds attention for 15 seconds. Replace any line under ___ and over____
22 feet, 23 feet
55
If canopy quick release opening force is less than___or more than___canopy quick release assembly shall be
6 pounds, 19 pounds
56
on the UWARS assembly, torque the four screws securing the cover to___
4+ -1 inch ounces
57
When inspecting the ripcord housing apply___to rip cord grip
7 pounds
58
Stamp a T on record grip at point where ripcord cable joins grip using a die stamp no larger than
.15 inches
59
When removing ripcord grip apply no more than__
20+ -5 pounds
60
removal of ripcord handle from pocket to require a force no more than_no Less than_
18 pounds, 12 pounds
61
ensure pack opening bands for the MK/H7 length fully stretch position should be no less than __ or no more than ___
12, 14 1/2
62
extraction force for automatic survival kit actuator shall be _____
25+-5
63
operational check for the hook blade knife consists of cutting through ____
550 parachute cord
64
Survival kit components shall be inspected in accordance with
14S1-3-51
65
When performing drop tests torso dummy wait Shall be
250 pounds
66
when performing drop test, drop altitude shall be _____, Pressure altitude shall not exceed 5000 feet
1500 feet
67
when performing drop test airspeed shall be ____
170 knots
68
for back automatic and torso harnes assemblies used on ejection seats the sling strap will be replaced every ____, not to exceed 10 years
7 years
69
for harnesses that are not used in ejection seats the service life is ___
13 years
70
combat edge is designed to provide the air crewmember with pressure breathing for positive acceleration protection at altitudes up to ____
50,000 feet
71
Serves as the central interface for breathing, gas hose, vest hose and emergency oxygen hose
ITB
72
Provides a man/aircraft interface separation point during ground egress or ejection and is categorized as man side equipment
ITB
73
Has a pressure relief valve which provides system over pressure protection
CRU-120
74
The rotation feature of the R2 (rotatable bayonet receiver) allows the receiver jar to rotate___ To either
15 degrees
75
tighten your cup screws using size ___ Allen wrench
.035
76
when using FAABS Velcro trap with ejection seats position the bulb ___ On the neighbors dropped her rent snagging during injection
Horizontally
77
when installing bayonet receivers, on the outside of the shell make a mark ___ From the helmet shell or edge roll edge
1/2 in
78
drill Bennett receiver holes using ___ drill bit
no 25
79
Essentially a three-way manifold block
cru-8
80
upon injection remove the mask as soon as the parachute deploy’s below ______ altitude
10,000 feet
81
Has the added ability to disconnect to swing 180° to allow straight pull during ejection sequence
cru-60
82
Insufficient for prolonged use above 30,000 feet altitude so that in the media to send to 30,000 feet altitude or below is mandatory if cabin pressure is lost using any of these adapters
cru-43/a and cru-44a/a
83
connector assemblies must be inspected every ____ days for rejection application and not to exceed ___ days for non-ejection
30+-10, 120
84
Force required to disconnect CRU should be between ____ pounds
12-20
85
when using the MQ–1/MQ–1A a tester for inspection on oxygen connectors turn tester to above _____ feet
45,000
86
repeatedly squeeze and release the end bulb of the MH – two tester until the pressure gauge indicates ___ of water
15 in
87
A two way, department of defense controlled, geosynchronous satellite communication system provided worldwide coverage between 70° north latitude and 70° south latitude
UHF SATCOM
88
the CSEL Use this constellation of satellites to provide the primary means of communication with a radio
UHF SATCOM
89
the CSEL System message architecture divides each hour into 230 minute periods each with ___ Timeslots or frame synchronize to universal time coordinated(UTC)
225 8 second
90
provides radio signals by hostile forces using a number of transmission techniques to significantly reduce user vulnerability to detection and interception
LPE
91
Provides two way, secure, line of site communication between the radio and rescue Forces
TAC
92
also known as Distance Measuring Equipment
TAG
93
is a transponder based radio navigation technology That measures distance by timing the propagation delay of radio signals
TAG
94
___ capable radios are designated as AN/PRQ-7A
TAG
95
Is a one-way dedicated search and rescue system operated by US, Russia, France and Canada provide in global coverage including polar areas
COSPAS-SARTAT
96
Uses satellites to locate emergency beacon carried by ships, aircrew or
COSPAS-SARSAT
97
The radio provides the ______ Beacon capability operating at 406 MHz
COSPAS-SARSAT
98
The ground station processes the CSEL signal and transmits the global positioning system(GPD) position from the radio to the Mission control center(MCC) Where it is joined with identification data and other information on the beacon
true
99
once the Mission control center (MCC) obtains the GPS they then send it to the AFRCC
true