In flight, do not transmit on surveillance radar within _____ horizontally or _____ vertically from another aircraft.
Ref: T.O. 1E-3A-43-1-1 Pg: 1-3
A. 900 feet; 450 feet
B. 1300 feet; 650 feet
C. 2000 feet; 1000 feet
D. 1 mile; 1000 feetB. 1300 feet; 650 feet
If surveillance radar is operating on ground, observe following safety distance limits from rotodome: _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 1-3
A. 1,300 feet for personnel not inside the airplane
B. 1,300 feet for refueling and defueling operations
C. 3,000 feet for personnel not inside the airplane
D. a and b
D. a and b
Power to the frequency converter is controlled by a circuit breaker on the ______ panel.
Ref: T.O. 1E-3A-43-1-1 Pg: 1-8
A. P5
B. P66
C. P67-3
D. P67-2D. P67-2
The Electronic Support Measures (ESM) system is a passive detection system used to enhance E-3 surveillance capabilities. The purpose of the ESM System (ESMS) or ESM Group (ESMG) is to detect, identify and locate _____ RF emitters operating in a specific frequency range.
Ref: T.O. 1E-3A-43-1-1 Pg: 1-303
A. non communication
B. passive
C. only hostile
D. only airborneA. non communication
Selected UHF radios are capable of relaying _______ as needed.
Ref: T.O. 1E-3A-43-1-1 Pg: 1-380 A. CV (clear voice) B. NBSV (narrow band secure voice) C. WBSV (wide band secure voice) D. All of the above
D. All of the above
Interlock circuitry prevents the following:
Ref: T.O. 1E-3A-43-1-1 Pg: 1-415
A. Simultaneous transmission on clear and secure
direct access radio nets with priority given to
secure transmission demands.
B. Direct access transmissions from a position
originating a PA message
C. Listening on any secure net, when transmitting on
any clear direct access net.
D. all of the above
D. all of the above
The UHF equipment consists of the following:
Ref: T.O. 1E-3A-43-1-1 Pg: 1-454 A. Twenty (20) transceivers B. Two (2) high power amplifiers C. Thirteen (13) antennas D. all of the above
D. all of the above
Joint Tactical Information Distribution System (JTIDS) (LINK 16) _. terminal operates in the frequency range of _____ thru _____ MHz
Ref: T.O. 1E-3A-43-1-1 Pg: 1-624 A. 225.000; 399.975 B. 350.000; 399.975 C. 1030; 1090 D. 960; 1215
D. 960; 1215
The communications equipment receives its cooling from the _____ …
Ref: T.O. 1E-3A-43-1-1 Pg: 1-632 A. draw through B. forward forced air C. aft forced air D. All of the above
D. All of the above
Where two or more crewmembers are needed to perform a procedure, the steps are coded using crewmember symbols enclosed within _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 2-3 A. parentheses B. a circle C. a box D. none of the above
A. parentheses
Steps requiring coordination between mission crewmembers and flight crewmembers are indicated by _____ the checklist item number….
Ref: T.O. 1E-3A-43-1-1 Pg: 2-3
A. an arrow pointing to
B. a plus next to
C. a circle around
D. an asterisk next toC. a circle around
If the crew launching is not the crew which cocked the airplane, MCC, ART, CDMT, CSO, and CT will _____ before engine start.
Ref: T.O. 1E-3A-43-1-1 Pg: 2-4
A. review AFTO Form 781, Sections A & K
B. complete oxygen and ADS panel preflight
C. verify correct template
D. monitor UHF for command post information
A. review AFTO Form 781, Sections A & K
During OUTBOUND PROCEDURES, the flight engineer will clear the mission crew to power up mission systems once the following are complete:
Ref: T.O. 1E-3A-43-1-1 Pg: 2-13
A. rotodome turning at 6 rpm
B. TAT is 15 degrees C (59 degrees F) or less and not
rising
C. six generators on in parallel
D. all of the aboveD. all of the above
During PREPARATION FOR CONTACT (BEFORE 1/2 NM) (MCC) checklist, the ART informs MCC waveguide switch is _____, IFF is _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 2-15
A. in LOAD; in standby LESS NGIFF and manual
control
B. in standby; OFF
C. OFF; in TEST MAINTENANCE
D. under DPAG CONTROL; OFFA. in LOAD; in standby LESS NGIFF and manual control
Emergency procedures should be _____ so that the crew will be familiar with the procedures.
Ref: T.O. 1E-3A-43-1-1 Pg: 3-3
A. rigid
B. unique and accomplished only for flight
evaluations
C. the highest priority of the mission
D. practiced often
D. practiced often
MCC shall ensure _____ is aware that personnel are in _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 3-4 A. flight; aft lower compartment only B. flight crew; forward lower compartment only C. flight crew; lower compartments D. flight and mission crew; lavatory
C. flight crew; lower compartments
Crewmembers primarily involved with emergency will coordinate on _____. All other crewmembers will be on _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 3-4
A. maintenance net; maintenance net
B. net 1; nets 2 and 3
C. maintenance net; mission nets 2 and 3
D. net 1; maintenance net
C. maintenance net; mission nets 2 and 3
The mission crew has three designated fire fighters: _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-14
A. CT, CDMT and ART
B. CSO, CT and CDMT
C. CSO, CT and ART
D. AWO, AST and ARTA. CT, CDMT and ART
At least one member of refill team will maintain communications on _____.
Ref: T.O. 1E-3A-43-1-1 Pg: 3-18
A. Net 1
B. Net 2
C. Net 3
D. maintenance netD. maintenance net
During inflight refueling, from 1/2 mile before air refueling contact until _____ of refueling, or as directed by flight crew, the surveillance radar and the identification system will be put in standby.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-2 Chap:
A. end
B. five minutes after end
C. thirty minutes after end
D. normal orbit altitude is established after end
B. five minutes after end
The ROTODOME speed limits for proper AOCP operation is _____ RPM.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-9 A. 5 plus or minus 0.33 B. 5 plus or minus 0.25 C. 6 plus or minus 0.33 D. 6 plus or minus 0.25
C. 6 plus or minus 0.33
If the rotodome RPM is out of tolerance by a substantial amount, approximately 3 RPM, _____ is displayed on the consoles.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-9
A. mode control message
B. a single strobe
C. a wedge of targets
D. INVLD RPMC. a wedge of targets
Do not operate system M SEU for more than _____ without draw through cooling system in operation.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-9 A. five seconds B. five minutes C. 10 seconds D. 10 minutes
B. five minutes
The Iridium Communication System operates up to a cabin altitude of 25,000 feet and at temperatures from ____ F to ____ F.
Ref: T.O. 1E-3A-43-1-1 Pg: 5-14
A. 32 degrees; 100 degrees
B. 0 degrees; 120 degrees
C. 32 degrees; 122 degrees
D. 0 degrees; 100 degreesC. 32 degrees; 122 degrees