Master Question File (Pilot, FEB 2021) Flashcards by Mike B

General
1. Pilots shall not exchange seats during flight if only two pilots are aboard the airplane.

A. True B. False

Ans: A

Ref: T.O. 1C-135(K)R(II)-1, Page 4-2, Warning

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General
2. Verbal coordination between applicable crewmembers will be required when:

A. Control of the airplane is transferred between pilot and copilot or when an autopilot mode or axis is engaged or disengaged

B. Repositioning fuel panel valves and switches or when an electrical power source is changed

C. A crewmember leaves position or leaves interphone or goes on or off oxygen

D. Anyoftheabove

Ans: D

Ref: T.O. 1C-135(K)R(II)-1, Page 4-2

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General
3. Normal left and right hydraulic system pressure range is _____ to ____ psi.

A. 1000; 3000

B. 2400;3050

C. 1500;2800

D. 1971; 2469

Ans: B

Ref: T.O. 1C-135(K)R(II)-1, Page 5-6A

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General
4. Maximum EGT during engine start is _____ °C.

A. 870
B. 905
C. 725
D. 930

Ans: C
Ref: T.O. 1C-135(K)R(II)-1, Page 5-3

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General
5. EGT between _____ is limited to 5 minutes duration.
EGT between________ – Retard the throttle to bring EGT within limits. Operation is allowed until the next landing. If EGT exceeds _______– shut engine down using the ENGINE FIRE/FAILURE DURING FLIGHT checklist.

A. 725°C - 870°C; 871°C - 905°C; 906°C

B. 870°C - 905°C; 906°C - 930°C; 930°C

C. 725°C-870°C;906°C-930°C;930°C

D. The green arc

Ans: B
Ref: T.O. 1C-135(K)R(II)-1, Page 5-8

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General
6. Normal oil pressure limits are ___ psi. Oil pressure fluctuations of not more than ___ psi total are allowable, as long as fluctuations remain within normal limits.

A. 5–100;5

B. 11–92;10

C. 20–85;15

D. 30–60;20

Ans: B
Ref: T.O. 1C-135(K)R(II)-1, Page 5-3

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General
7. Moderate to severe airplane buffeting can occur with simultaneous use of speed brakes and flaps. This buffeting can result in damage or loss of airplane surfaces.

A. True
B. False

Ans: A

Ref: T.O. 1C-135(K)R(II)-1, Page 5-13

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General
8. Because of possible damage due to sonic airflow at certain angles of attack, do not extend flaps above___ feet pressure altitude.

A. 20,000

B. 15,000

C. 10,000

D. 5,000

Ans: A
Ref: T.O. 1C-135(K)R(II)-1, Page 5-13

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General
9. The takeoff and emergency procedures portion will be reviewed either just prior to_____ .

A. Stepping to Aircraft

B. Engine Start

C. Takeoff

D. B or C

Ans: D
Ref: T.O. 1C-135(K)R(II)-1, Page 2-2

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General
10. Based on ______ single pilot preflight operations where one pilot proceeds to the aircraft with the boom operator to perform the exterior safety check and begin the interior preflight checks, while the other pilot accomplishes additional duties (obtaining weather brief, etc.).

A. Operational Need

B. Mission Requirements

C. Personal Preference

D. A or B

Ans: D
Ref: T.O. 1C-135(K)R(II)-1, Page 2-2

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General
11. All crewmembers will inform the pilot when checking off and/or on interphone and will be on interphone during:

A. All ground operations (including engine starts) except when accomplishing crew duties that preclude use of interphone

B. Formation flying, rendezvous and air refueling

C. Flight under weather conditions and all takeoffs and landings

D. All of the above

Ans: D
Ref: T.O. 1C-135(K)R(II)-1, Page 4-3

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General
12. Because of the magnitude of interrelated aerodynamic effects, flying two airplanes in close vertical proximity is ______.

A. Routine

B. Safe

C. Not safe

D. Not recommended

Ans: C
Ref: T.O. 1C-135(K)R(II)-1, Page 5-18, Warning

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General
13. Speed brakes are NOT used during approach and landing flare.

A. True
B. False

Ans: A
Ref: T.O. 1C-135(K)R(II)-1, Page 6-18

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General
14. All snow and ice accumulations of any significant degree must be removed from the airplane surfaces prior to takeoff.

A. True
B. False

Ans: A
Ref: T.O. 1C-135(K)R(II)-1, Page 7-14

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Ground Operations
15. If the ____ is not down and in the detent, ensure that the _____ is installed. Notify the aircraft commander and maintenance personnel immediately. No further preflight actions will be accomplished until maintenance personnel correct the situation and confirm that the aircraft is in preflight configuration.

A. Flap Handle; Override Crank

B. Crew Entry Chute Grill; Crew Entry Ladder

C. Landing Gear Lever; nose gear ground downlock and release handle

D. Speed Brake Lever; Flight Control Snubbers

Ans: C
Ref: T.O. 1C-135(K)R(II)-1, Page 2-7, Caution

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Ground Operations
16. The pilot will ensure that no personnel are standing near _____ when pressurizing the left hydraulic system. Sudden closing of these doors could cause serious injury to personnel who may be in the path of the doors.

A. Cargo Door

B. Wheel Well Doors

C. Main Entry Door

D. APU Exhaust Doors

Ans: B
Ref: T.O. 1C-135(K)R(II)-1, Page 2-15, Warning

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Ground Operations
17. The copilot ANN DIM switch on the Copilot Overhead Light Panel must be out of the DIM (full ccw) position for _____ the to operate. Ensure that the copilot ANN DIM switch is out of the DIM (full ccw) position prior to closing the crew entry/cargo door. Once the crew entry/cargo doors are closed the DIM switch can be adjusted as required.

A. Co-Pilot’s Annunciator Panel

B. Side Panel Lighting

C. Engine Fire Lights

D. FDR

Ans: D
Ref: T.O. 1C-135(K)R(II)-1, Page 2-16, Note

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Ground Operations
18. Possible causes of a ______ are engaging the pilot’s interphone (on the yoke or the tiller), pressing the pilot’s FD ANN TEST button, a cold hydraulic system, the low- flow capability of the auxiliary hydraulic pump, and/or the use of other hydraulically- actuated systems during the EFAS test; in this case, the EFAS self-test is ______
indicating a system failure.

A. Failed EFAS test; correctly

B. Failed EFAS test; incorrectly

C. Failed SYD test; not applicable and

D. Failed SYD test; correctly

Ans: B
Ref: T.O. 1C-135(K)R(II)-1, Page 2-22, Note

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Ground Operations
19. Speed Brake Warning horn sounds when lever is pulled back more than _______ degrees out of the full forward position.

A. 5

B. 6

C. 2

D. 4

Ans: C
Ref: T.O. 1C-135(K)R(II)-1, Page 2-30B

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Ground Operations
20. Proper adjustment of the _____ is especially critical for takeoff, approach, and landing where full deflection of control surfaces may be required for safe operation of the airplane. To prevent inadvertent movement of the seat, ensure that the ______ is in the down and latched position.

A. Seat Belts and Shoulder Harnesses; seat vertical adjustment lever

B. Seat and Rudder Pedals; seat vertical adjustment lever

C. Seat and Rudder Pedals; seat horizontal adjustment lever

D. Seat Belts and Shoulder Harnesses; seat horizontal adjustment lever

Ans: C
Ref: T.O. 1C-135(K)R(II)-1, Page 2-42, Warning

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Ground Operations
21. If an APU with an operable generator is not available, and external power is not used, the start can be made on battery power only. During this procedure, all engine _____ gauges are inoperative until a generator is on the line and 28V AC power is available.

A. Oil Pressure and Fuel Flow

B. N1 and N2

C. Oil Low Pressure Lights and EGT

D. Instrument

Ans: A
Ref: T.O. 1C-135(K)R(II)-1, Page 2-62, Notes

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Ground Operations
22. Copilot checks for initial fuel flow peak of ___ pph (before ignition) and approximately _____ pph after ignition. If fuel flow exceeds ____ pph before lightoff, a hot start can occur.

A. 100; 1000; 100

B. 300-680; 900; 680

C. 725; 870; 930

D. Within the Green Arc

Ans: B
Ref: T.O. 1C-135(K)R(II)-1, Page 2-63, Caution

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Ground Operations
23. For temperatures ____ , failure to set the engine start switch to IGNITION may result in engine flameout when the throttles are retarded during taxi operations.

A. Colder than normal

B. At and below 10°C (50°F)

C. At and below 4°C (40°F)

D. At and below 0°C (32°F)

Ans: D
Ref: T.O. 1C-135(K)R(II)-1, Page 2-64, Note

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Ground Operations
24. Items 18. thru 29. of the Starting Engines and Before Taxi checklist may be accomplished while waiting for the ground crew report.

A. True

B. False

Ans: A
Ref: T.O. 1C-135(K)R(II)-1, Page 2-65, Note

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Taxi 25. Minimum taxiway width is _______ feet. A. 147 B. 74 C. 75 D. 100

Ans: B Ref: AFMAN 11-2KC-135 Vol 3, Paragraph 5.9.1

Taxi 26. Do not taxi or tow an aircraft within ____ feet of obstructions without wing walkers monitoring the clearance between the aircraft and the obstruction. Do not taxi aircraft closer than ____ feet to any obstruction. A. 10, 25 B. 25, 10 C. 10, 10 D. 25, 25

Ans: B Ref: AFMAN 11-218, Paragraph 3.7

Taxi 27. Do not operate aircraft within 25 horizontal feet of any obstruction without ______. A. Wing walkers B. Observing airfield markings C. Tower instructions D. “Follow me” vehicle

Ans: A Ref: AFMAN 11-218, Paragraph 3.7

Taxi 28. Available crew members should assist in clearing during: A. Taxi operations B. Receiver AAR C. Anytime the aircraft is below 10,000 feet AGL D. All of the Above

Ans: D Ref: AFMAN 11-2KC-135 Vol 3, Paragraph 5.6

Taxi 29. When operating in non-standard formation, flight leaders: A. Are required to advise ARTCC on intial contact of separation being used B. Ensure wingman echo separation on check in calls with ARTCC C. Should indicate non-std formation in remarks section of the flight plan D. A and C

Ans: D Ref: AFMAN 11-2KC-135 Vol 3, Paragraph 18.6

Taxi 30. Marshallers are required to use ______ during night or low visibility conditions. A. Whistle B. Wands C. Illuminated Wands D. Fluorescent Wands

Ans: C Ref: AFMAN 11-218, Paragraph 2.3.3

Taxi 31. Air Force pilots may passively participate in LAHSO (land or take-off when another aircraft has been given a LAHSO clearance). PIC is the final authority whether to takeoff, land or continue a touch-and-go when a merging aircraft has received a LAHSO clearance. A. True B. False

Ans: A Ref: AFMAN 11-202 Vol 3, Paragraph 18.2

Taxi 32. When must aircraft anti-collision lights be displayed? A. At the pilot's discretion B. From sunset to sunrise C. From just prior to engine start until after engine shutdown D. At all times when electrical power is available to operate anti-collision lights

Ans: C Ref: AFMAN 11-218, Paragraph 3.10

Taxi 33. You are approaching another aircraft on the ground head-on. What should you do? A. Keep moving in the direction intended. You have the right-of-way and the other aircraft will move B. Alter course to the left to remain well clear, or stop C. Alter course to the right to remain well clear, or stop D. Execute a 180 degree turn and return to parking

Ans: C Ref: AFMAN 11-218, Paragraph 3.5.1

Taxi 34. An AC or IP will make all heavyweight landings greater than _______ and landings during emergencies, unless conditions prevent compliance. A. 200,000 pounds B. 235,000 pounds C. 220,000 pounds D. None of the above

Ans: B Ref: AFMAN11-2KC-135Vol3,Paragraph5.4.1

Takeoff 35. In those situations where runway/taxi conditions or performance considerations are such that safety could be compromised, A. A static takeoff should be made B. A rolling or static/rolling takeoff should be made C. Extreme care should be given to calculating takeoff data D. B and C

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Caution

Takeoff 36. For a takeoff, approach or landing with fuel in any main tank below ____ pounds, open all tank to engine manifold valves. Open the line valve for all takeoffs when gross weight is greater than ____ pounds. Ensure line valve is closed for all takeoffs when gross weight is at or below ____ pounds. A. Full; 322,500; 5,900 B. 5,000; 180,000; 8,800 C. 10,500; 200,000; 200,000 D. 10,500; 180,000; 235,000

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-75, Step 3 and Warning

Takeoff 37. Exercise caution during throttle application to prevent asymmetrical thrust. Engine thrust should be stabilized at a minimum of ____ prior to advancing throttles to the takeoff thrust setting. A. 20% N1 B. 40%N1 C. 50%N1 D. Ground Idle

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Caution

Takeoff 38. Uncommanded stabilizer trim input is a safety-of-flight issue. Terminate the mission (and in flight, land as soon as practicable) any time uncommanded stabilizer trim input is encountered. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Warning

Takeoff 39. If any engine does not reach the charted N1 setting ____ , the engine is not providing the required rated thrust, and the takeoff shall be aborted. A. Upon initial takeoff power setting B. Prior to 90 knots C. Before S1 D. Between 40 and 80 knots

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-76A, Warning

Takeoff 40. Illumination of the amber EGT caution light near or after S1 indicates that EGT may be approaching the takeoff limit. This indication is for crew awareness and does not indicate an engine operating limit has been exceeded. Continue normal operation and monitor EGT to prevent exceeding the takeoff EGT limit. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-76A, Note

Takeoff 41. When ____ throttle is advanced near OPEN, the warning horn sounds if the speed brake lever is more than 2 degrees out of the full forward position, if the flap lever is at or near the 0, 40, or 50 degree detent, or the leading edge flaps are not fully extended. A. No.1 B. No.2 C. No.3 D. No.4

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-77

Takeoff 42. Sudden reversal of rudder direction at high rudder deflections, due to improper rudder application or abrupt release, can result in _____. A. Failure of the rudder PCU B. Failure of the rudder pressure controller C. Over-G of the aircraft D. Over-stressing the vertical fin

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 3-198

Takeoff 43. If stabilizer trim has moved from setting selected during the TAXI checklist, _____. A. Abort the mission B. Reset to original setting C. Call maintenance D. Immediately place the stabilizer trim switch to the CUT-OFF position and manually trim throughout departure

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-74, Step 2

Takeoff 44. When experiencing a loss shear on takeoff, anticipate a loss in indicated airspeed and altitude. This situation is potentially dangerous if the airplane is close to the ground. If this loss is expected to be ____ knots or more, the takeoff shall be delayed, if possible, until more favorable conditions exist. A. 10 B. 15 C. 20 D. 25

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 7-7

Departure 45. When the airplane is definitely airborne and a positive rate of climb is established (vertical velocity pointer above zero), retract the landing gear. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-84

Departure 46. Follow Dash One procedures until reaching ______________, obstacle clearance height, or the altitude associated with a departure procedure required climb, whichever is higher. A. [BLK 40] 800 feet above the runway B. [BLK45] 2000 feet above the runway C. Level off altitude D. A and B

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Pages 2-84 and 2-85

Departure 47. Leave ignition on if engine anti-ice is on. If anti-ice is not required, turn starter switches off ____. A. once climb thrust is established B. upon reaching 2000 feet C. Both A and B D. 5 minutes after established at cruise altitude

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-89, Step 14

Departure 48. Do not climb at a speed more than the recommended three engine climbout speed. A. True B. False

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-85, Warning

Departure 49. Maneuvering at speeds below three engine climbout speed plus ____ knots is not recommended. A bank angle of 30 degrees at climbout speed with flaps down could reduce climb capability by as much as ____ fpm. A. 10, 200 B. 25, 300 C. 35, 300 D. 50, 400

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-85, Warning

Departure 50. [Without TCTO 1823] If airplane is to remain in closed traffic after takeoff, thrust will be adjusted to climb out at the same speed to be used on the downwind leg, and a rate of climb of approximately ____ feet per minute. A. 500 B. 1000 C. 1500 D. 2500

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-85

Departure 51. If an engine failure occurs during climbout, continue to follow the command bars. With inoperative command bars, if an engine failure occurs during or immediately after take- off, _____ ; if an engine failure occurs after attaining three engine climbout speed, do not reduce airspeed but continue to climb at the speed attained at the point of engine failure. A. Increase thrust to accelerate to enroute climb speed B. Climb at Vco+10 C. Climb at recommended three-engine climbout speed D. Land immediately

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-86, Warning

Departure 52. Flap retraction in a turn is not recommended. Retracting flaps from 20 degrees to 0 reduces available lateral (outboard ailerons) control and increases initial buffet speed considerably and rapidly as the trailing edge and leading edge flaps retract. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-87

Departure 53. After setting climb thrust, no further throttle adjustment should be necessary during climb if the power management control (PMC) system is NOT operating. A. True B. False

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-87

Departure 54. A departure alternate is required if weather is below landing minimums for the lowest suitable approach (at departure aerodrome). To qualify as a departure alternate, the airfield must be: A. Within 30 minutes flying time, the existing weather is equal to or better than the published approach minimums and forecast to remain so until 1 hour after takeoff B. Within one hour flying time, better than published mins for the lowest suitable approach (to include a circling approach) until end AAR time C. Within two hours flying time, the existing weather is at least 500-1 above the lowest compatible published approach minimums, but not less than 600-2 (precision) or 800-2 (non-precision) and forecast to remain so for 1 hour after ETA at the alternate D. A or C

Ans: D Ref: AFI 11-202 Vol 3 AMC Supplement, Paragraph 5.1.1.2.2

Departure 55. Manual damping of dutch roll is to be accomplished only with _______. A. Manual trim B. Rudder C. Lateral (aileron) control D. Elevator

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 3-37

Departure 56. For an unplanned thunderstorm penetration, use the lower of 280 KIAS or cruise Mach (0.77 to 0.80) and do NOT change the _______. A. Autopilot configuration B. Stabilizer Trim setting C. Route of flight D. Steering solutions

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 7-5, Step 1 and Caution

Air to Air Refueling 57. No HF transmissions are to be made from a tanker or receiver when a receiver is in contact or about to make contact and all HF equipment must be switched to STANDBY/MONITOR where possible. A. True B. False

Ans: A Ref: ATP-3.3.4.2 Chapter 2, Section V, Paragraph 2.55b

Air to Air Refueling 58. For all _____ AARs, do not transmit on the HF radio when the receiver is within 1⁄2 NM; this includes datalink. A. USAF B. USN C. USAF & USN D. foreign aircraft

Ans: D Ref: ATP-3.3.4.2 US SRD Appendix 8D, 8D-1, Page 8-9, Warning

Air to Air Refueling 59. Pilots must use extreme care in those cases when the speed brakes are required for deceleration. Ascertain that the receiver ____ prior to speed brake actuation. A. will be established on track B. is in the astern position C. is in the contact position D. will not overrun the tanker

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-176D, Warning

Air to Air Refueling 60. For airplanes equipped with standard speed booms, if airspeed must be increased above ____ KIAS/.85 Mach, the pilot will notify the boom operator to stow the boom. A. 325 B. 330 C. 335 D. 340

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-176E, Caution

Air to Air Refueling 61. During any air refueling which requires the indicated airspeed to be less than 220 KIAS, _____ for dry contacts to preclude fuel siphoning from the forward body tank, causing unexpected CG changes. A. place the A/R manifold to engine manifold valve to CLOSE B. minimize the number of requests C. keep the centerwing to forward body tank valve switches closed D. keep the A/R line valve closed

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-90R, Caution

Air to Air Refueling 62. When the receiver is in or near the contact position, the pilot _____ at the first indication of autopilot malfunction, including an inadvertent autopilot disconnect, if accompanied by out-of-trim control forces. A. will switch the autopilot attitude source from VG to INU-2 B. should initiate a breakaway C. should start a gentle climb D. will initiate a breakaway

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-176F, Warning

Air to Air Refueling 63. Air refueling for the receiver that required a controlled tension disconnect will be terminated except during fuel emergencies or when continuation of air refueling is dictated by operational necessity. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 3-42, Caution

Air to Air Refueling 64. Unless dictated otherwise by ATP-3.3.4.2 (Chapter 2, Section I, Warning) or by mission requirements, tankers will establish the applicable contact air refueling airspeed before the receiver reaches _____. If the tanker is off airspeed by more than _________ knots, the receiver pilot will be informed prior to tanker airspeed changes. A. 1NM, 5 B. 1NM, 10 C. Astern,5 D. Astern, 10

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-176D, Warning

Air to Air Refueling 65. Following an inadvertent brute force disconnect, air refueling __________. A. may be continued if the tanker and receiver air refueling systems function normally B. should be terminated C. will be terminated D. will be terminated except during fuel emergencies or when continuation of air refueling is dictated by operational necessity

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 3-42, Caution

Air to Air Refueling 66. The position approximately 50 ft behind and slightly below the tanker boom nozzle where the receiver stabilizes with zero rate of closure before being cleared to the contact position is called: A. Astern B. Pre-Contact (USAF receivers) C. Stabilized D. Either A or B

Ans: D Ref: ATP-3.3.4.2 Chapter 1, Section II, Paragraph 1.11 and US SRD Appendix 8D, Page 8-10, Note

Air to Air Refueling 67. Tanker responsibilities during a Rendezvous Delta is (are) to: A. Be at the base AAR altitude B. Enter the refueling holding orbit from anydirection C. Attempt to arrive at least 10 min before the ARCT and, normally, establish a left-hand holding pattern using the ARCP as an anchor point D. All of the above

Ans: D Ref: ATP-3.3.4.2 Chapter 2, Section I, Paragraph 2.16

Air to Air Refueling 68. When planning to conduct a Rendezvous G, a common track length equivalent to _____ minutes flying time should be planned to allow for tanker descent to RV FL/altitude/height, visual acquisition and timing corrections. A. 5 B. 10 C. 15 D. 20

Ans: C Ref: ATP-3.3.4.2 Chapter 2, Section I, Paragraph 2.19

Air to Air Refueling 69. Tankers will only refuel those aircraft listed in ATP-3.3.4.2 and the US SRD or specifically authorized by MAJCOM/A3V, Air Tasking Order, Operational Order (OPORD), Exercise Order, or on approved flying schedule. Receiver aircraft not previously certified for refueling operations (includes foreign variants of US-produced aircraft) must be certified for technical and operational compatibility in accordance with ATP-3.3.4.2 prior to refueling (N/A AFMC). A. True B. False

Ans: A Ref: AFMAN 11-2KC-135 Vol 3, Paragraph 15.6.1

Air to Air Refueling 70. Unless otherwise directed, an altimeter setting of ____ is to be used for AAR operations at or above transition altitude, or when over water and operating in accordance with ICAO procedures. Regardless of whether or not the aircraft are operating on standard pressure settings, tanker crews _______ to include the altimeter setting in the RV Initial Call. A. QFE, are required B. 29.92,are required C. 29.92,are not required D. QNH, are not required

Ans: B Ref: ATP-3.3.4.2 Chapter 2, Section 1, Paragraph 2.2

Air to Air Refueling 71. Tanker pilots should ensure the boom operator notifies receiver pilots when any axis of the autopilot is not used. If a tanker pilot or receiver pilot is required to fly autopilot- off for qualification training, the pilot flying the opposing aircraft will be qualified. A. True B. False

Ans: A Ref: AFMAN 11-2KC-135 Vol 3, Paragraph 15.2.3

Air to Air Refueling 72. The tanker will note the receiver’s distance when ____ through the turn back to the ARCP. This is the best time to determine if an overrun condition exists and the best time for visual sighting. Except for overtaking point parallel rendezvous, the distance to the receiver should be approximately 1/3 of the turn range when____through the turn. A. 1/3rd , halfway B. Halfway,1/3rd C. Halfway,halfway D. Beginning, beginning

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-176C

Air to Air Refueling 73. Tanker aircrew will advise ATC of tanker and receiver end aerial refueling altitude requests at least five (5) minutes prior to AREX. A. True B. False

Ans: A Ref: JO 7610.4V, Paragraph 10-1-6a.10

Air to Air Refueling 74. After experiencing two-way communications failure while conducting aerial refueling, tanker aircraft will discontinue AAR and continue flight by doing what? A. Squawk code 7600 for at least two (2) minutes prior to exiting track or anchor B. If altitude instructions beyond the exit point have not been received, exit the track or anchor at the highest altitude in the clearance for the refueling portion of the flight C. Proceed in accordance with “Procedures for Two-Way Radio Failure IFR-VFR” set forth in the DoD Flight Information Handbook D. All of the above

Ans: D Ref: DoD Flight Information Handbook (FIH), Two-Way Radio Failure, Page A-7

Air to Air Refueling 75. Normally, tanker orbit patterns are located within a rectangle, 60 NM long, 25 NM wide with left turns. While established in and awaiting their receivers, tanker aircraft: A. Are automatically cleared down to the IP, if needed for rendezvous B. Must receive clearance from the box to the IP, if airspace is desired C. Can change direction of turn, if they wish D. Must notify ATC if shortening leg lengths

Ans: B Ref: JO 7610.4V, Paragraph 10-2-5, Note

Air to Air Refueling 76. Closely monitor airplane CG during reverse air refueling, as the aft CG limit can be quickly exceeded when operating at ________ gross weights. A. Light B. Heavy C. Medium D. Maximum

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 3-44C, Warning

Oceanic and Coronet 77. Routing and altitudes(s) of aircraft established on an approved ALTRV must not be changed except in the interest of safety of flight or as outlined in Chapter 3 of JO 7610.4. A. True B. False

Ans: A Ref: JO 7610.4, Paragraph 3-3-8

Oceanic and Coronet 78. To avoid datalink initialization failure, the flight crew ensures that the flight-specific information entered into the aircraft system is the same as the corresponding details filed _______. A. On the Form F B. In the Aircrew Briefing Guide C. By the Copilot D. In the flight plan

Ans: D Ref: GOLD Manual, Paragraph 1.2.2.2.3

Oceanic and Coronet 79. The flight crew should monitor the forward estimate for oceanic entry, and if this changes by ______ minutes or more, unless providing position reports via ADS-C, pass a revised estimate to ATC. A. 1 B. 2 C. 3 D. 5

Ans: C Ref: North Atlantic Operations and Airspace Manual [NAT Doc 007 (EN)], Paragraph 5.1.7

Oceanic and Coronet 80. For oceanic crossings, aircrew will use _______. A. The in-flight guide B. Only the MAJCOM Stan/Eval MDS-specific checklist posted on the Aircrew Pubs Sharepoint. If an MDS-specific checklist is not posted, aircrew may use the Sample Oceanic Checklist, published via NAT OPS Bulletin C. Locally generated oceanic checklists D. AP1B

Ans: B Ref: AFI 11-202 Vol 3 AMC Supplement, Paragraph 13.5.1.4

Oceanic and Coronet 81. If operating on an ALTRV and mission is to be delayed beyond the AVANA time, rescheduling the ALTRV: A. Will normally be in 24-hour increments after the original schedule B. Is at the discretion of the mission commander C. Can be in less than the time specified above,subject to CARF discretion and after approval from the affected ARTCC/CERAP/HCF D. A or C

Ans: D Ref: JO 7610.4, Paragraph 3-4-4

Oceanic and Coronet 82. [Oceanic Plotting Chart] While flying the oceanic route, crews will maintain situational awareness to include positional awareness and accurate fuel readings. In order to assist with this, crews will: A. When under radar contact and at intervals of approximately once every hour, aircrews will annotate waypoint crossing time, flight level, and fuel remaining in the appropriate areas of the CFP for the given waypoint B. Approximately 10 minutes after passing each oceanic waypoint, or every 500 miles, whichever is shorter, record and plot the aircraft full Latitude/Longitude position, Flight Level/Altitude and UTC time on the chart, and ensure compliance with courses and ETA tolerances C. If a revised clearance is received, aircrew will record and plot the new course on the chart D. All of the above

Ans: D Ref: AFI 11-202 Vol 3 AMC Supplement, Paragraphs 13.5.9.1, 13.5.2.2 and 13.5.10

Oceanic and Coronet 83. [CPDLC] The lead aircraft will initiate a logon at the correct time. Once in formation, only the lead aircraft will make position reports. A. True B. False

Ans: A Ref: GOLD Manual, Paragraph 6.4.2

Oceanic and Coronet 84. If a logon request has been initiated with incorrect aircraft identification and aircraft registration, the logon process will fail. The flight crew will need to ____. A. Call Command Post to verify aircraft registration B. Transmit AFN logon, then re-transmit with correct identification C. Omit AFN logon from checklist D. Correct the information and reinitiate the logon request

Ans: D Ref: GOLD Manual, Paragraph 4.2.1.2, Note 1

Oceanic and Coronet 85. Approximately ____ minutes after exiting CPDLC and/or ADS-C service areas, the flight crew should ensure there are no active CPDLC or ADS-C connections. A. 15 B. 30 C. 40 D. 45

Ans: A Ref: GOLD Manual, Paragraph 4.2.5.1

Oceanic and Coronet 86. Experience has shown that many of the track-keeping errors in the NAT HLA occur as a result of crews programming the navigation system(s) with incorrect waypoint data. These are referred to as Waypoint Insertion Errors. They frequently originate from: A. Failure to observe the principles of checking waypoints to be inserted in the navigation systems, against the cleared route B. Failure to load waypoint information correctly C. Failure to cross-check on-board navigation systems D. Any combination of the above

Ans: D Ref: North Atlantic Operations and Airspace Manual, Paragraph 5.6.3

Descent and Approach 87. Steep idle thrust approaches, or all approach angles and rates of descent requiring large changes in pitch attitude during the landing flare, will be avoided. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-98, Warning

Descent and Approach 88. For approach purposes, the KC-135R is considered a Category _____ airplane. In those cases where the speed for a circling approach exceeds 166 knots, Category ____ will be applied. minima A. C, D B. D,E C. D,D D. C, C

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-94, Note

Descent and Approach 89. A speed brake lever position of less than _____ degrees is not recommended, due to a tendency to over-control at these settings. A. 20 B. 30 C. 40 D. 50

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-91, Note

Descent and Approach 90. For all FMS approaches, at 2 NM prior to the final approach fix ensure system is in the _____ mode (as indicated by the blinking ______________CDU annunciation), or discontinue the approach. A. Terminal, <> B. Enroute,<> C. Approach,<> D. Message, <>

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-94, Note

Descent and Approach 91. If multiple instrument approach patterns are flown in the clean configuration, maintain a minimum of ______ KIAS until crossing the initial approach fix or turning base leg if receiving radar vectors. A. VREF B. VREF+25 C. VREF + 50 D. VREF +70

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-94, Note

Descent and Approach 92. Unless fuel consumption is a factor, hold at ____ for all gross weights up to 170,000 pounds. At gross weights above 170,000 pounds, use ______ as holding speed. A. 220 KIAS, best endurance plus 10 knots B. 200 KIAS, 220 KIAS C. VREF +50, VREF +25 D. 220 KIAS, best range plus 10 knots

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-91

Descent and Approach 93. Occupants of the pilot and copilot seats may remove the shoulder harness during cruise flight, but shall fasten them prior to ________. A. Air refueling rendezvous B. Descent for landing C. A and B D. None of the above

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-92, Note

Descent and Approach 94. [Descent] As a minimum, the pilot flying the approach will brief the crew on the transition level, planned descent rate, DH/MDA/VDP, missed approach procedures and assign crew responsibilities for backing up the pilot flying the airplane _____. A. During the full stop landing B. If wind shear is encountered along the final approach course C. While accomplishing a touch and go landing D. If an unplanned go-around occurs

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-92, Item 2

Descent and Approach 95. From 500’ AGL to the runway, the PF will execute a go-around/missed approach when which of the following parameters are exceeded. A. Airspeed: +10/-5 knots from target B. Bank Angle: +/-15degrees C. Rate of Descent: +/-300 FPM from target D. Any of the above

Ans: D Ref: AFI 11-202 Vol 3 AMC Supplement, Paragraphs 18.8.1 – 18.8.3

Descent and Approach 96. During the descent checklist, an accurate check of the electric and hydraulic systems consists of the pilot checking switches and pressure in the left, right, reserve brake and powered rudder systems while the copilot checks electrical power system indicators and hydraulic quantities. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-93

Landing 97. When landing with less than full flaps, avoid excessive flare with resultant floating in an attempt for a smooth landing. Make a normal flare and touchdown at _____. A. Threshold speed minus 10 knots B. Threshold speed minus 5 knots C. V_app for the applicable flap setting D. V_REF

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-99, Warning

Landing 98. Application of ____ brakes during landing ground roll may override the ____ antiskid brake system and lock the airplane brakes resulting in possible blown tires or reverted rubber hydroplaning. A. Pilot,Co-Pilot B. Pilot,Pilot C. Co-Pilot,Pilot D. Co-Pilot, Co-Pilot

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-99, Caution

Landing 99. Engine acceleration from ground idle to touch and go target thrust may require up to 20 seconds. Attempting a go-around after the engines have decelerated to ground idle results in an extended ground run. Consider aborting the takeoff if the engines go to ground idle. A. True B. False

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-107, Warning

Landing 100. Touchdown with a crab angle and with wings level may result in a rapid rising of the _______wing and may cause the ____ engine nacelles to drag on the runway. A. Upwind, Upwind B. Downwind,Downwind C. Downwind,Upwind D. Upwind, Downwind

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-99, Caution

Landing 101. Do not allow the bank angle at touchdown (4 to 6 degrees pitch attitude) to exceed ___ degrees due to possibility of dragging an outboard engine nacelle. A. 4 B. 6 C. 8 D. 9

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-99, Caution

Landing 102. During landing ground roll, do not allow airplane to bank beyond ___ degrees due to possibility of dragging an engine nacelle. A. 4 B. 6 C. 8 D. 9

Ans: A Ref: T.O. 1C-135(K)R(II)-1, Page 2-99, Caution

Landing 103. Prior to initiating turns, visually check for other traffic. The first turn should not be initiated until ______. A. Reaching minimum traffic pattern (maneuver) speed B. A safe altitude C. Passing the end of the runway D. All of the above

Ans: D Ref: T.O. 1C-135(K)R(II)-1, Page 2-100, Warning

Landing 104. Remove crab ____, maintaining a slight wing low attitude into the wind, as necessary to counteract drift. A. Over the threshold B. Prior to touchdown C. When pulling power D. Prior to the threshold

Ans: B Ref: T.O. 1C-135(K)R(II)-1, Page 2-99

Landing 105. N1 settings, pattern, approach, and reference speeds will be recomputed when: (1) Gross weight changes >/= ___ pounds (2) Temperature changes >/= ___ (5F) (3) Pressure altitude changes >/= ___ feet (4) Airplane configuration changes (5) Changes in wind conditions require an adjustment to the charted speeds A. 5,000; 5C; 500 feet B. 10,000; 3C; 250feet C. 10,000; 3C; 500feet D. 5,000; 2C; 500 feet

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-104, Note

Landing 106. [Go-Around] The minimum airspeed for retracting flaps to _____ degrees is flaps 50° VTH speed. A. 50 B. 40 C. 30 D. 20

Ans: C Ref: T.O. 1C-135(K)R(II)-1, Page 2-106, Step E