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CHIEF ADVANCEMENT QUESTIONS > CHIEF QUESTIONS #1 > Flashcards

CHIEF QUESTIONS #1 Flashcards

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1
Q

WHAT ARE THE AUTOMATIC SHUTDOWN CONDITIONS OF A A/S 37A-3 ?

A
  1. ENGINE EXCEEDS 2,400 RPMS
  2. OIL PRESSURE DROPS BELOW 10 PSI.
  3. ENGINE TEMPERATURE RISES TO 220 DEGREES FAHRENHEIT
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2
Q

WHAT MANUAL COVERS THE SHIPBOARD MOBILE ELECTRIC PLANT (MEPP) A/S 37A-3?

A

NAVAIR 19-45-26

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3
Q

DECK EDGE ELEVATOR DOORS ARE DESIGNED TO OPEN OR CLOSE IN HOW MANY SECONDS?

A

60 SECONDS

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4
Q

HANGAR DIVISION DOORS ARE DESIGNED TO OPEN AND CLOSE IN HOW MANY SECONDS?

A

28 SECONDS

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5
Q

A/S 32A-32 SPOTTING DOLLY IS CONTROLLED BY THE USE OF WHAT?

A

JOYSTICK

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6
Q

A/S 32A-30A HAS A SECONDARY MISSION OF WHAT?

A

TOWING SMALL AIRCRAFT

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7
Q

HOW PHASES ARE THERE IN THE GSE LICENSING PROGRAM?

A

2 PHASES

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8
Q

WHO HANDLES THE SECOND PHASE OF THE GSE LICENSING PROGRAM?

A

DIVISION

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9
Q

PHASE 2 OF THE GSE LICENSING PROGRAM CONSIST OF WHAT?

A

ON THE JOB TRAINING

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10
Q

WHAT MATERIAL IS THE NWC-4 MADE OF ?

A

POLYURETHANE (SELF EXTINGUISHING)

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11
Q

WHAT IS THE DIFFERENCE BETWEEN STANDARD AND AMPHIBIOUS TD-1BS?

A

LENGTH

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12
Q

FOR INFORMATION CONCERNING HIGH POWER TIE-DOWN ASSEMBLY FOR EACH TYPE OF AIRCRAFT, YOU WOULD REFER TO WHAT MANUAL?

A

NAVAIR 17-1-537

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13
Q

NWC-4 ADJUSTABLE END FACES?

A

AFT

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14
Q

TD-1B IS TIGHTENED BY THE USE OF?

A

TENSIONER ASSEMBLY

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15
Q

THE ALBAR 24 IS DESIGNED SPECIFICALLY FOR WHAT AIRCRAFT ?

A

SH-60 HELO

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16
Q

WHEN THE ELEVATOR IS LOADED TO CAPACITY, WITH ALL PUMPS IN USE, WHAT IS THE DUTY CYCLE TIME?

A

60 SECONDS

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17
Q

HORIZONTAL LOCKING BARS OF THE AIRCRAFT ELEVATORS ARE POWERED HOW?

A

PNEUMATICALLY

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18
Q

AIRCRAFT ELEVATOR STANCHIONS SHOULD NOT BE OPERATED IN WHAT MODE ?

A

AUTOMATIC

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19
Q

“A” DIVISION IS RESPONSIBLE FOR WHAT PART OF AIRCRAFT ELEVATOR OPERATION ?

A

MACHINERY ROOM.

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20
Q

THERE ARE HOW MANY DIFFERENT COMPOSITIONS OF NONSKID ?

A

THERE ARE TWO
(TYPE G AND TYPE L)

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21
Q

NON SKID COATINGS KITS ARE SUPPLIED IN HOW MANY COMPONENTS

A

2 COMPONENTS

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22
Q

WHAT IS DFT ?

A

DRY FILM THICKNESS

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23
Q

WHAT IS WFT ?

A

WET FILM THICKNESS

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24
Q

DFT IS MEASURE ONCE THE COAT IS ?

A

CURED

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25
WHAT IS THE TERM USED FOR A MISSED SPOT DURING COATING APPLICATION ?
HOLIDAY
26
SHIPS FRAME NUMBERS ARE MARKED IN INTERVALS OF WHAT?
10 FRAMES
27
WHO IS RESPONSIBLE FOR THE PROPER HOOK UP OF THE AIRCRAFT TO CATAPULT UPON LAUNCHING ?
TOP SIDE SAFETY PETTY OFFICER (TSPO, V-2)
28
WHO IS RESPONSIBLE FOR THE SAFE LAUNCHING OF AIRCRAFT AND PROPER CATAPULT LAUNCH PROCEDURES?
LAUNCH OFFICERS (YELLOW SHIRT/ GREEN CRANIAL, V-2)
29
WHAT HAND SIGNAL IS USED MORE FREQUENTLY ABOARD AIRCRAFT CARRIERS THAN ON SHORE STATIONS ?
!!!EMERGENCY STOP!!!
30
WHO WEARS A BLUE CRANIAL , BLUE JERSEY ?
AIRCRAFT HANDLING CREW AND CHOCK MEN
31
COMNAVAIRFORINST 3100.5
AIR DEPARTMENT STANDARD OPERATING PROCEDURES
32
WHAT IS THE STANDARD POSITION FROR A DIRECTOR IN RELATION TO THE AIRCRAFT ?
SLIGHTLY AHEAD AND IN THE LINE WITH THE LEFT WING TIP.
33
WHOM INFORMS THE DIRECTOR WHEN TO BRING THE AIRCRAFT TO THE CATAPULT PRIOR TO FIRST LAUNCH?
CATAPULT OFFICER
34
AIRCRAFT MUST NOT HAVE THE LAUNCH BAR OVER THE SHUTTLE SPREADER UNTIL?
THE AIRCRAFT IS ARMED AND PROPERLY CONFIGURED FOR FLIGHT.
35
AFTER TENSIONING, THE PILOT MUST NOT BE PLACE THE LAUNCH BAR SELECTOR SWITCH IN THE OFF, ABORT, OR RETRACTED POSITIONS UNTIL?
THE PILOT RECEIVES THE RAISE LAUNCH BAR SIGN FROM THE DIRECTOR.
36
WHEN THE AIRCRAFT IS READY FOR TENSIONING AND UPON SIGNAL FROM THE TSPO, THE DIRECTOR GIVES WHAT SIGNAL?
TENSION AIRCRAFT
37
WHO IS THE TENSION AIRCRAFT SIGNAL GIVEN TO ?
PILOT, DECK EDGE CONTROL PANEL OPERATOR AND/ OR ICCS OPERATOR.
38
WHEN THE DIRECTOR IS SATISFIED THAT THE AIRCRAFT IS READY FOR LAUNCH AND THE CATAPULT AREA IS CLEAR, THE DIRECTOR THEN DOES WHAT?
PASSES CONTROL TO THE CATAPULT OFFICER BY GIVING THE PASS CONTROL SIGNAL.
39
UPON SEEING THE DIRECTORS TENSION SIGNAL, THE PILOT?
INCREASES ENGINE THRUST TO THE LEVEL AUTHORIZED BY THE APPLICABLE NATOPS MANUAL.
40
NAVAIR 51-25-19
MK 2 NOSE GEAR LAUNCH EQUIPMENT
41
WHO IS RESPONSIBLE FOR PORTABLE DECK RAMPS?
V-1 DIVISION
42
A BLAST FROM A WHISTLE IS EQUIVALENT TO WHAT SIGNAL?
STOP TAXI
43
IN NAVAL AVIATION , APPROXIMATELY HOW MANY PERSONS ARE REQUIRED TO KEEP EACH AIRCRAFT IN FLYABLE CONDITION?
10 PERSONS
44
DURING HEAVY WEATHER, CHOCKS SHOULD BE SECURED WITH?
21 THREAD OR GREATER MANILLA LINE
45
WHO COORDINATE THE FORMAL TRAINING OF THE INTEGRITY WATCH STANDERS?
AIR WING WATCH COORDINATOR
46
MULTI ENGINE AIRCRAFT ARE TIED DOWN AT HOW MANY POINTS?
SIX 3) LANDING GEAR 2) WINGS 1) TAIL
47
DOD 5200.33-R
DEFENSE COURIER SERVICE REGULATION
48
OPNAVINST 5530.14
PHYSICAL SECURITY AND LOSS PREVENTION MANUAL
49
SECNAVINST 4355.18
REPORTING OF SUPPLY DISCREPANCIES
50
AFI41-301
WORLDWIDE AEROMEDICAL EVACUATION
51
ON THE FLIGHT DECK, ALL OFFICERS, CHIEF PETTY OFFICER, AND LEADING PETTY OFFICERS ARE IDENTIFIED BY?
THREE ORANGE STRIPES ON THE CRANIAL
52
AFTER THE LAUNCH BAR HAS BEEN PROPERLY SEATED AND VERIFIED BY THE HOOKUP PETTY OFFICER, WHAT SIGNAL IS GIVEN TOT HE DIRECTOR?
GO (THUMBS UP)
53
RECOVERY STATIONS SHOULD BE MANNED HOW MANY MINUTES PRIOR?
30 MINUTES
54
FOR INFORMATION CONCERNING THE ATTACHMENT POINTS ON AN AIRCRAFT, REFER TO THE?
MIM
55
WHO MAY AUTHORIZED THE MOVEMENT OF AIRCRAFT IN PORT?
AIR DEPARTMENT DUTY OFFICER (ADDO)
56
80T-122
HELICOPTER OPERATING PROCEDURES FOR AIR CAPABLE SHIPS
57
HAND PUSHING SHOULD NOT BE ATTEMPTED IF THE SHIP’S PITCH AND ROLL EXCEEDS?
PITCH EXCEEDS 5 ROLL EXCEEDS 10
58
WHAT IS THE PREFERRED BRAKE METHOD WHILE TOWING MV-22 AIRCRAFT?
AUXILIARY BRAKE PUMP
59
IN HEAVY AND MODERATE WEATHER, ENGAGING OR DISENGAGING THE V-22 WITH THE SPOTTING DOLLY AT ANGLES OF HOW MANY DEGREES MAY CAUSE DAMAGE?
60 DEGREES OR GREATER
60
USE OF THE LHA PART-TIME ELEVATOR FOR V-22’S REQUIRES?
THE V-22 ARE DEFUELED TO 40,000 POUNDS MAXIMUM
61
AN AV-22 WITH FIXED IFR PROBE MAY NOT BE TRANSPORTED ON WHICH LHA ELEVATOR?
STERN ELEVATOR
62
WHAT MUST OCCUR PRIOR TO ENGAGING THE V-22 WITH AN SD-2?
NOSE GEAR MUST BE HIKED.
63
THE V-22 NOSE GEAR WILL EXTEND AN AVERAGE OF HOW MANY INCHES WHEN HIKED?
8 INCHES
64
A V-22 ON AN LHD ELEVATOR SHALL BE SPOTTED ?
PERPENDICULAR TO SHIP’S CENTERLINE (PORT TO STARBOARD)
65
POTENTIAL WASH DOWN HAZARD MAY EXTEND HOW MANY FEET FROM A H-53?
300 FEET
66
MAX AVERAGE VELOCITY FOR H-53 DOWN WASH OCCURS AT?
49 FEET ROTOR CENTER
67
MAX AVERAGE VELOCITY FOR H-53 DOWN WASH VARIES FROM ?
50 TO 95 KNOTS
68
WHEN WORKING WITH THE H-53 IN HOVER, WHAT EQUIPMENT IS REQUIRED?
STATIC DISCHARGE DEVICE AND INSULATED GLOVES WITH A MINIMUM OF 20,000 VOLTS
69
80T-111
V/STOL AND LANDING SIGNAL OFFICER NATOPS
70
NIGHT HELICOPTER LAUNCHES MAY ONLY BE PERFORMED FROM SPOTS OFFERING WHAT CONDITIONS?
SPOTS THAT AFFORD VISUAL REFERENCE TO THE DECK.
71
H-60 ROTOR BLADES CAN DIP AS LOW AS?
4 FEET FROM THE DECK
72
ALL PERSONNEL ENTERING AND EXITING ROTOR ARCHS SHALL DO SO FROM WHAT RELATIVE POSITIONS ?
3 O’CLOCK 9 O’CLOCK
73
MAXIMUM SAFE RELATIVE WIND CONDITIONS FOR FOLDING OR UNFOLDING PROPELLER ROTOR BLADES AND WING STOW/UNSTOW IS?
45 KNOTS FROM ANY QUADRANT
74
FOR DECK HEAT MITIGATION , A V-22 WITH AN OPERABLE COANDA EXHAUST DEFLECTOR SYSTEM SHOULD?
RETARD OVER-DECK ENGINE TOWARD IDLE (84% NR) WITHIN 10 MINUTES
75
FOR DECK HEAT MITIGATION , A V-22 WITHOUT AN OPERABLE COANDA EXHAUST DEFLECTOR SYSTEM ON THE OVER-DECK ENGINE SHOULD?
LAUNCH OR SHUT DOWN WITHIN 5 MINUTES.
76
FOR DECK HEAT MITIGATION, A V-22 WITHOUT AN OPERABLE COANDA EXHAUST DEFLECTOR SYSTEM ON THE OVER-WATER ENGINE SHOULD?
LAUNCH OR SHUTDOWN OVER-WATER ENGINE WITHIN 5 MINUTES, SHUT DOWN OVER-DECK ENGINE WITHIN 10.

CHIEF ADVANCEMENT QUESTIONS (1 decks)

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