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15 Cards in this Set
- Front
- Back
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106. ______ Due to the lack of surge protection features, reverse refueling is prohibited.
A. [ARR E] B. [ARR B] C. [ARR C] D. [ARR G] |
A. [ARR E]
Ref: T.O. 1C-135(K)R(II)-1, Page 2-189, Warning |
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107. The ________ valve will be CLOSED before operating the A/R fuel pumps because fuel pressure surges
could cause rupture of the ARR manifold in the cockpit area. A. manifold flight B. single point refueling C. main ARR (IFR) D. line |
C. main ARR (IFR)
Ref: T.O. 1C-135(K)R(II)-1, Page 3-80, Warning |
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108. When transferring fuel, only ____ A/R pump(s) shall be operated at a time. This precludes the possibility of over-pressurizing a fuel tank if a fuel level control valve fails in the open position.
A. 4 B. 3 C. 2 D. 1 |
D. 1
Ref: T.O. 1C-135(K)R(II)-1, Page 3-80, Warning |
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109. Monitor the fuel quantity gauges to avoid exceeding airplane _______ limits. Maintain symmetrical fuel
quantities in the wing tanks to prevent lateral unbalance. A. CG B. Structural C. Maneuvering D. Fuel Tank |
A. CG
Ref: T.O. 1C-135(K)R(II)-1, Page 3-80, Warning |
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110. [Manual Boom Latching] The receiver pilot must initiate all disconnects before _____________________.
A. fatigue sets in B. over pressurizing the ARR manifold C. exceeding any of the limits D. called by the boom operator |
C. exceeding any of the limits
Ref: T.O. 1C-135(K)R(II)-1, Page 3-80B, Caution |
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111. The ____________ valve will be CLOSED before operation of the air refueling pumps because fuel pressure
surges could cause rupture of the ___ manifold in the cockpit area. A. tank to engine manifold; tank to engine manifold B. single point refueling; single point refueling C. main ARR/IFR; ARR D. tank to engine manifold; main IFR |
C. main ARR/IFR; ARR
Ref: T.O. 1C-135(K)R(II)-1, Page 8-6, Warning |
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112. A controlled tension brute force disconnect will be accomplished only __________.
A. by a qualified instructor boom B. as a last resort, after all other normal and emergency methods of disconnect have failed C. when agreed upon by both the receiver and tanker D. on [ARR E] configured jets |
B. as a last resort, after all other normal and emergency methods of disconnect have failed
Ref: T.O. 1C-135(K)R(II)-1, Page 3-42, Caution |
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113. The receiver pilot should use caution not to overrun the tanker. If overrunning does occur, under no conditions
should a turn, either right or left, be made until __________. A. a breakaway has been completed B. speed brakes are deployed C. the tanker is visual D. throttles are advanced |
A. a breakaway has been completed
Ref: T.O. 1C-135(K)R(II)-1, Page 3-18A, Warning |
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114. Approaching boom limits at relatively high velocity can cause _________ due to binding action of the boom
nozzle. A. operating limits to be exceeded prior to disconnect B. negative contact indication C. structural damage as a result of an inability to disconnect D. a pressure disconnect |
C. structural damage as a result of an inability to disconnect
Ref: T.O. 1C-135(K)R(II)-1, Page 8-4, Caution |
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115. The receiver will stabilize in the astern position with a _____ rate of closure. If the receiver fails to attain a
stabilized position, or it becomes apparent that a closure overrun will occur, a breakaway will be initiated. Failure to initiate a breakaway under closure overrun conditions can result in a mid-air collision. A. slight B. zero C. negative D. slow |
B. zero
Ref: T.O. 1C-135(K)R(II)-1, Page 8-3, Warning |
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116. If the receiver director lights fail to illuminate when contact is established, the _______ will inform the
_______ if refueling operations are to be continued. If refueling is continued, verbal corrections from the boom operator may be requested. A. receiver copilot; tanker copilot B. receiver pilot; tanker pilot C. receiver pilot; boom operator D. boom operator; receiver pilot |
C. receiver pilot; boom operator
Ref: T.O. 1C-135(K)R(II)-1, Page 8-3, Caution |
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117. One of the greatest potential hazards during air refueling is ___________. On becoming fatigued or if for any
reason large oscillations develop which require increasing amounts of control displacement, break contact and __________________ the airplane in the astern position for a few minutes. A. Explosive vapors, ventilate B. Fatigue, let the other pilot fly C. flameout of engines, look around D. rupture of the ARR manifold in the cockpit area, |
B. Fatigue, let the other pilot fly
Ref: T.O. 1C-135(K)R(II)-1, Page 8-4 |
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118. Attempts to effect a contact during loss of any air refueling lighting that results in less than desired
illumination will be at the discretion of the ____________. A. receiver pilot B. tanker pilot C. boom operator D. instructor pilot |
C. boom operator
Ref: T.O. 1C-135(K)R(II)-1, Page 8-3, Caution |
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119. The boom operator is unable to release the boom toggles during manual boom latching.
A. TRUE B. FALSE |
A. TRUE
Ref: T.O. 1C-135(K)R(II)-1, Page 3-80B, Caution |
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120. If the receiver is more than ___ in trail with the tanker, airspeed may be increased to ___ KIAS for closure.
The normal speed schedule will be resumed at 3 NM in trail. A. 3NM; 350 B. 3NM; 330 C. 4NM; 350 D. 4NM; 330 |
D. 4NM; 330
Ref: T.O. 1C-135(K)R(II)-1, Page 8-2, Note |
