Mission Fam Flashcards

1
Q
  1. Who directs frequency changes?
A

The flight lead

AFMAN11-247 8.4.2

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2
Q
  1. When does the formation switch to

departure frequency?

A

The formation will not switch to departure frequency until both aircraft airborne.
3 FTS OI Attachment 4 Formation Standards

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3
Q
  1. What is the standard speed for cruise,

climbs, and descents?

A

Lead will normally climb, descend, and maneuver at 220 KIAS. Lead will normally cruise at 240KIAS.
3 FTS OI Attachment 4 Formation Standards

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4
Q
  1. When can Lead use idle and speed brakes simultaneously?
A

When Wing has been notified

3 FTS OI Attachment 4 Formation Standards

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5
Q
  1. What will Lead and Wing squawk during

actual lost wingman?

A

Lead: Assigned Squawk. Wing: Emergency or 0100 in the local area.
3 FTS OI Attachment 4 Formation Standards

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6
Q
  1. During cell what is the standard set-up for

the A/P and A/A TACAN?

A

Lead and wing will fly with autopilot engaged and A/A TACAN on.
3 FTS OI Attachment 4 Formation Standards

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7
Q
  1. If Wing calls “blind,” what will Lead do?
A

Lead will acknowledge the call, maintain a predicable flightpath, and be directive to ensure altitude separation.
AFMAN11-247 8.2.3.2 & 8.13.2(cell)

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8
Q
  1. What if the wingman goes blind in

actual IMC conditions?

A

The wingman will perform the appropriate lost wingman procedures.
AFMAN11-247 8.2.4.1 & 8.13.2(cell)

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9
Q
  1. When are you not supposed to give your

wingman a frequency change?

A
Lead should never give a frequency change when the wingman is saturated with trying to fly
the aircraft (for example, during a breakout). If a frequency change must take place at an inopportune
time, lead will give the wingman time to make the change and respond. Lead should minimize maneuvering until the formation has checked in on the same frequency.
AFMAN11-247 8.4.4
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10
Q
  1. Can you use visual signals in the T-1A?
A

Not normally. Any visual signals to be used will be briefed by flight lead. Crewmembers should be familiar with AFI 11-205, Aircraft Cockpit and Formation Flight Signals, for formation visual signals that could be used in the case of an emergency.
AFMAN11-247 8.5

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11
Q
  1. What is the minimum runway width for
    both aircraft to take the runway during a
    formation departure?
A

150 feet.

AFMAN11-247 8.9.4

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12
Q
  1. Explain the differences between a fifteen second interval and a one-minute interval takeoff.
A

Fifteen-Second Interval: Once the flight is positioned on the runway and cleared for takeoff, lead will call for the runup (“Pain flight, run ‘em up”) to 80 percent N1 for the engine
checks. When number two calls, “Pain 2 is ready,” lead will release brakes and advance power.
When lead releases the brakes, the wingman will hack the clock and continue holding the brakes.
At 15 seconds the wingman will release the brakes and advance power.
One-Minute Interval: Once the flight is positioned on the runway and cleared for takeoff, lead will call for the runup (“Pain flight, run ‘em up”) to 80 percent N1 for the engine checks. When number two calls, “Pain 2 is ready,” lead will release brakes and advance power. When lead releases the brakes, the wingman will hack the clock and reduce the power to idle. At approximately 45 seconds, the wingman will advance power to 80 percent N1, check engines, and release brakes at one minute.
Both aircraft must maintain their side of the runway.
AFMAN11-247 8.10

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13
Q
  1. What are the parameters of the visual position?
A

The basic visual formation position for the wingman is approximately 600 to 700 feet behind and 200 to 300 feet to the right, out of lead’s jet wash. To maintain the proper position use the following visual references, the wingman should:
• Be close enough to easily read the letters on the tail, but just barely make out the tail numbers.
• Superimpose the right engine intake on lead’s emergency exit hatch. The stinger light should be seen in the tail cone of the left engine. The bottom of the left engine should rest tangent on the left wing.
• As a backup, use approximately .2 DME.
Lead may direct the wingman to be on the left side as required. The wingman will maintain the side assigned by lead.
AFMAN11-247 8.12.1

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14
Q
  1. What are the parameters of offset position?
A

The offset position for the wingman is 600 to 4,000 feet (approximately .2 to.8 DME) of spacing. This allows the wingman to use visual references to determine the inner limit of the offset position. The wingman may fly on either side of lead, from the in-trail position up to line abreast. The offset position is fluid in nature, but the optimum position is in a 30- to 45-degree cone on either side of lead. The wingman may maneuver from side to side or farther back to optimize clearing. The wingman’s position is chosen to optimize clearing, avoid terrain and obstacles, and/or position for the next turn or a prebriefed threat.
AFMAN11-247 8.12.2

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15
Q
  1. Discuss a Position Change.
A

Lead will normally direct the change over the interplane radio frequency, “PAIN Flight, position change.” When the wingman acknowledges the position change radio call, he or she will normally turn right (away) momentarily, using 30 degrees AOB. The wingman will then return to the base heading while advancing power.
• The position change will be complete when the old wingman passes abeam the old lead. The old lead will transmit, “PAIN XX, you have the lead on the right (left).” The new lead will respond, “Roger, I have the lead on the right (left).” The new lead (the old Wingman) will turn the IFF to ON. The new wingman (the old lead) will turn the IFF to STBY and rejoin as directed by the new lead (the old wingman). It is acceptable for the new wingman (the old lead) to squawk STBY after the first TCAS hit.
• The wingman will assume lead responsibilities once passing abeam the old lead and appropriate radio calls have been made. The new wingman (the old lead) will decelerate to expedite the position change, returning to the prebriefed airspeed as the old wingman (the new lead) approaches the proper position. When the wingman acknowledges the lead change call, he or she will pick up the IFF and monitor the new wingman. It is imperative to monitor the old lead (the new wingman) and direct the new wingman to assume either the visual, offset, or cell formation position.
AFMAN11-247 8.15

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16
Q
  1. When are you required to do a breakout?
A

-Directed by the lead.
-Crossing under or in front of the lead.
-His or her presence constitutes a hazard to the formation.
-Unable to maintain sight of lead.
AFMAN11-247 8.16

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17
Q
  1. On a formation Tactical Overhead pattern, when will the wingman go into the break?
A

The wingman will break approximately 8 to 10 seconds after lead and roll out slightly outside
lead’s downwind ground track. The wingman must adjust the break point to build a 6,000-foot threshold spacing from lead.
AFMAN11-247, 8.17.3.1

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18
Q
  1. What is “Standard Formation?”
A

1 NM horizontally and 100 feet vertically from the lead aircraft. In the T-1A, the Visual and Offset positions are considered standard formation positions.
AFI 11-202v3, Appendix 1

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19
Q
  1. What is “Nonstandard Formation?”
A

Non-Standard Formation—Operations under any of the following conditions:
a. When the flight leader has requested and ATC has approved other than standard
formation dimensions (≤1 NM lateral separation or ≤ 100 ft. vertical separation).
b. When operating within an authorized altitude reservation (ALTRV) or under the
provisions of a letter of agreement.
c. When operations are conducted in airspace specifically designed for a special activity. In the T-1A, the Cell formation position is considered a non-standard formation position.\
11-2T-1v3 A8.3.2.7: NOTE: Clearance to maneuver enroute assumes non-standard formation. Wingmen will maintain within 2 NM and 2,000’ vertically of lead.
AFI 11-202v3, Appendix 1

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20
Q
3.  If you are recovering to Vance in
formation and cleared maneuvering, what
type of nonstandard formation are you
automatically cleared to fly? How long can
you maintain this nonstandard formation
before returning to standard?
A

NOTE: Clearance to maneuver enroute assumes non-standard formation. Formation members
will maintain within 2 NM and 2000 ft of each other. Terminate maneuvering and resume
standard formation NLT 20 DME from Vance.
AFI 11-2T-1v3, Vance Sup, A8.5.2

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21
Q
  1. What weather do you need to do practice lost wingman?
A

Day VMC above 1,000 feet AGL.

AFI 11-2T-1V3, 3.11.2.1

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22
Q
  1. What is the minimum altitude for a

formation position change?

A

1,000 feet AGL.

AFI 11-2T-1V3, 3.11.2.5

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23
Q
  1. What separation should you look for
    during a formation drag to ensure proper
    spacing on landing?
A

T-1 Drag (VMC Only). Notify RAPCON if you plan to drag when requesting recovery
from the area, or on initial contact with Approach, if returning to the local area. The wingman
will maintain visual contact with lead and 1-1.5 miles of spacing.
AFI 11-2T-1v3, Vance Sup, A8.5.2.3.

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24
Q
  1. Walk through a lost wingman procedure?

Straight-ahead, Left turn, Right Turn

A

Lead Responsibilities. The flight lead should acknowledge the lost wingman’s radio call.
Lead should also transmit attitude, heading, altitude, airspeed, or any other significant information to
help the wingman maintain safe operations.
Turning as lead – When executing a turning lost wingman (practice or actual) as lead on the inside of the turn do not roll out until after stating your parameters and safe separation has been attained. If you choose to roll out state, “Callsign, lead is rolling wings level, new base heading is xxx.”
Wingman Responsibilities. The procedures to be used depend on the flight position at the
time sight is lost. Obtain a separate clearance if a rejoin is not possible.
Wings Level. Turn 45 degrees away for 10 seconds and then turn back to the original
heading. Use 30 degrees of bank during the turn and start timing after established on a heading 45 degrees away from lead (Figure 8.1.).
Turns. When outside of the turn, roll wings level, inform lead, and continue straight
ahead to ensure separation. If you are on the inside of the turn, maintain the turn and instruct lead to roll out. Lead may resume the turn only after adequate separation is assured. If the flight is either climbing or descending in a turn, level off to achieve additional separation.
AFMAN11-247 8.7 & 3 FTS OI Form Stds

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25
Q
  1. Explain lost wingman while climbing or

descending.

A

When wings level or turning, level off with a minimum of 1,000 feet separation, inform lead of your present condition, and resume course.
AFMAN11-247 8.7.2.2

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26
Q
  1. Explain lost wingman while in cell.
A

In level flight (wings level or turning), climb 1,000 feet above lead’s altitude. If the flight is descending, level off and maintain a position at least 1,000 feet above lead’s altitude. If the flight is climbing, level off and maintain a position at least 1,000 feet below lead’s altitude. Regardless of the situation, inform lead of the lost wingman condition. CAUTION: Maintain prebriefed airspeed to prevent overrunning lead.
AFMAN11-247 8.7.3

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27
Q
  1. How many channels separate

corresponding A/A TACANs?

A

63.

AFMAN11-247 8.8

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28
Q
  1. Explain the difference between Terminate

and Knock-it-Off.

A

Knock-It-Off: (NOTE: Refer to AFI 11-214, Air Operations Rules and Procedures, for
additional information.)

• Any formation crewmember may call “knock-it-off” to cease maneuvering when safety of flight is a factor or where doubt or confusion exists. Initiation of a knock-it-off call will start with the flight call sign; for example, “PAIN Flight, knock-it-off.” Then both flight members will transmit their position number, in order, in the following format: “PAIN 1, knock-it-off,” “PAIN 2, knock-it-off.” If any flight member fails to respond correctly, the sequence should be initiated again.
• Upon hearing a knock-it-off call, all participating aircraft will clear their flightpath, cease maneuvering, climb or descend to a prebriefed safe altitude, and acknowledge with their call sign. Lead will maintain a predictable flightpath and will be directive before resuming maneuvering. He or she will direct a rejoin once safety of flight is ensured. The wingman will maintain positive aircraft separation and visual contact with lead while waiting for lead’s direction.
Terminate: (NOTE: Refer to AFI 11-214 for additional information.)
• Any formation crewmember may call “terminate” to cease maneuvering when safety of flight is not a factor or when desired learning objectives have been achieved. Terminate procedures should be used when the wingman is too far out of position, which would result in ineffective training.
• Initiation of a terminate call will start with the flight call sign; for example, “PAIN Flight, terminate.” Flight members transmitting their position number, in order, in the following format: “PAIN 1, Terminate,” “PAIN 2, Terminate.” If any flight member fails to respond correctly, the sequence should be initiated again.
• Upon hearing a terminate call, participating aircraft will clear their flightpath, cease maneuvering, and acknowledge with their call sign. Lead will maintain a predictable flightpath
AFMAN11-247 8.12.10 & 8.12.11

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29
Q
  1. What is windshear?
A

Windshear is a change of wind speed and or direction over a short distance along the flight path.
TO 1T-1A-1 (7-4)

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30
Q
  1. How is severe windshear defined?
A

Severe windshear is that which produces airspeed changes greater than 15 knots or vertical speed changes greater than 500 feet per minute.
TO 1T-1A-1 (7-4)

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31
Q
  1. What are some conditions that might indicate windshear?
A

If severe windshear is indicated, delay
takeoff or do not continue an approach. Conditions which may indicate windshear are:
• thunderstorm activity and associated gust front (may be indicated by blowing debris or dust)
• virga (rain that evaporates before reaching the ground)
• frontal passage (may be indicated by large amounts of blowing debris or dust)
• large temperature inversions
• pireps
• low level windshear alerting system LLWAS) warnings
TO 1T-1A-1 (7-5)

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32
Q

4.What is gain shear?

A

If actual groundspeed exceeds reference groundspeed, the pilot can expect a decreasing tailwind condition or gain shear during the approach.
TO 1T-1A-1 (7-5)

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33
Q
  1. What is loss shear?
A

If actual groundspeed is less than reference groundspeed, the pilot can expect a decreasing headwind condition or loss shear during the approach.
TO 1T-1A-1 (7-5)

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34
Q
  1. What should you do if you must takeoff into windshear conditions?
A

Use the longest suitable runway that avoids suspected areas of windshear. The choice of runway should include consideration of after takeoff obstacle clearance, crosswind and tailwind limitations, and runway surface conditions. Use 10
degrees flaps for takeoff. Determine takeoff speeds for actual takeoff conditions. If performance data allows, increase the rotation speed up to 10 knots, but do not reset the airspeed bugs. Rotate to normal initial climb attitude at the increased VROT and maintain that attitude.

(W) If acceptable takeoff performance can only be
achieved by selecting 0 degrees flaps and/or
ACM off, takeoff in the presence of potential
windshear is not recommended. Windshear conditions will quickly negate these minor performance enhancements.
TO 1T-1A-1 (7-5)

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35
Q
  1. What is reference groundspeed?
A

Reference groundspeed is the expected groundspeed on final at approach speed in a no-shear condition.
TO 1T-1A-1 (7-5)

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36
Q
  1. How is reference groundspeed computed?
A

Reference groundspeed is computed by subtracting the surface headwind component (adding tailwind component) from approach true airspeed. When actual groundspeed differs from reference groundspeed, wind change or shear will occur during approach.
TO 1T-1A-1 (7-5)

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37
Q
  1. During an approach in loss shear conditions should you attempt to maintain Vref or reference groundspeed?
A

EXAMPLE 1: Decreasing Headwind (Loss Shear)
FMS Wind………………………………………………290/35
Surface Wind ………………………………………….290/15
Landing RWY ………………………………………………29
Procedure:
Approach Speed ……………………………….. 125 KIAS
Reference Groundspeed ………………………115 knots
Hypothetical approach TAS (130) minus surface headwind component (15) equals reference groundspeed (115).
Actual Groundspeed …………………………….. 95 knots
Accelerate to 145 KIAS initially to maintain 115 knots groundspeed. Maintaining the reference groundspeed provides the necessary energy to penetrate the shear safely or go-around.
TO 1T-1A-1 (7-5)

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38
Q
  1. Should you use the autopilot during an approach in windshear conditions?
A

(N) Use of the autopilot during the approach should be considered as it will provide more time to
monitor and recognize deviations. Use the flight
director to the maximum extent possible.
TO 1T-1A-1 (7-6)

39
Q
  1. What flap settings should you use to land in windshear conditions?
A

Select 10 degrees flap approach and landing if stopping distance is not critical.
TO 1T-1A-1 (7-6)

40
Q
  1. When is the potential for icing on aircraft surfaces highest?
A

Icing occurs because of supercooled water vapor such as fog, clouds, or rain. The most severe icing occurs on aircraft surfaces in visible moisture or precipitation with a true outside temperature between 0 °C and minus 10 °C; however dangerous icing conditions may be encountered at temperatures below minus 10 °C. The probability of encountering icing is greater when flying through visible moisture. Visible moisture is defined as clouds, rain, snow, or fog. This probability is significantly increased when flying below 20,000 feet.
TO 1T-1A-1 (7-8)

41
Q
  1. What are the three types of hydroplaning?
A

DYNAMIC HYDROPLANING.
Dynamic hydroplaning occurs gradually as a wedge of water builds up pressure between the tires and pavement. As the tires lose contact with the runway, the coefficient of friction is reduced to zero making wheel braking, tire cornering, and steering totally ineffective. Once total dynamic hydroplaning begins, it may continue after the aircraft speed decreases below the total dynamic hydroplaning
initiation speed. Dynamic hydroplaning is the most
frequently encountered type of hydroplaning.
VISCOUS HYDROPLANING.
Viscous hydroplaning occurs at lower speeds than dynamic hydroplaning on surfaces with smooth texture or made smooth by rubber deposits or paint. This type of hydroplaning may perpetuate itself if the thin water layer is not broken by a rough surface. Even dew can create the viscous film
which acts as the lubricant for viscous hydroplaning.
REVERTED RUBBER HYDROPLANING.
Reverted rubber hydroplaning is caused by a skid which heats rubber to revert it to its natural latex state. The tire rides on a boundary layer of steam trapped between the tire and the pavement. This type of hydroplaning results in near zero braking coefficients and has been known to continue
almost to the point of zero groundspeed. A locked wheel may aggravate or initiate this condition.
9*(square root of the tire pressure) is the speed at which the aircraft will start to hydroplane.
TO 1T-1A-1 (7-15)

42
Q
  1. Does the radar do a good job of detecting volcanic dust?
A

(N) The weather radar system may not detect the
volcanic dust.
TO 1T-1A-1 (7-14)

43
Q
  1. How does desert operation affect your brakes?
A

To avoid overheating the brakes, use available runway for landing roll out. (W) After a minimum roll landing or excessive braking, personnel should stay clear of the main landing gear until the brakes have cooled.
TO 1T-1A-1 (7-13)

44
Q
  1. How do you find moment?
A

Weight x Arm = Moment

T-1A Aerodynamics, AE-03

45
Q
  1. Where do Arm measurements begin?
A

From a common reference point know as the Reference Datum. The reference datum in the T-1A is the nose of the aircraft, but this is not standardized among different types of aircraft. The arm is often referred to as a fuselage station (F.S.).
T-1A Aerodynamics, AE-03

46
Q
  1. What does it mean to say that a piece of equipment is located at Fuselage Station 120.0?
A

It means that the equipment’s center of mass is located 120.0 inches aft of the aircraft’s Reference Datum.
T-1A Aerodynamics, AE-03

47
Q
  1. Define Wing Chord.
A
The distance (imaginary line) between the leading edge and the trailing edge of a wing expressed in inches.
T-1A Aerodynamics, AE-03
48
Q
  1. Define Mean Aerodynamic Chord (MAC).
A

It is the average distance from the leading edge to the training edge of a wing. For swept wing aircraft, designers must determine the average chord of an imaginary wing that has the same aerodynamic characteristics as the actual wing. In the T-1A it is 73 inches.
T-1A Aerodynamics, AE-03

49
Q
  1. Define Leading Edge of Mean Aerodynamic Chord (LEMAC).
A

The distance, expressed in inches between the Reference Datum and the leading edge of the MAC. In the T-1A it is 251 inches.
T-1A Aerodynamics, AE-03

50
Q
  1. Define Basic Aircraft Weight.
A

It is EMPTY WT plus unusable fuel, engine oil, ballast, and operating equipment minus any missing installed equipment. This weight is found in the Chart C and is use to start filling out the Form F.
T-1A Aerodynamics, AE-03

51
Q
  1. Define Operating Weight.
A

It is BASIC WT plus crew, crew baggage, emergency equipment, and other nonexpendable items not included in basic weight.
T-1A Aerodynamics, AE-03

52
Q
  1. Define Zero Fuel Weight.
A

It is OPERATING WT plus payload (cargo, passengers, and passenger baggage). Maximum zero fuel weight in the T-1A is 13,000lbs.
T-1A Aerodynamics, AE-03

53
Q
  1. What is the ARIP?
A

ARIP - Air Refueling Initial Point - A point located upstream from the ARCP at which the receiver aircraft initiates a rendezvous with the tanker. Descent to refueling altitude will be made between ARIP and ARCP.
FLIP AP/1B, 5-1

54
Q
  1. What is the ARCP?
A

ARCP - Air Refueling Control Point - The location where the tanker and receiver rendezvous is completed prior to refueling. Tankers orbit at this point.
FLIP AP/1B, 5-1

55
Q
  1. The ARCT is the planned point/time of what?
A

The ARCT is the receiver’s planned arrival time at the ARCP. AFMAN 11-247, 9.1.3

56
Q
  1. By what means will be the primary method of conducting a rendezvous?
A

The A/A TACAN will be the primary method of effecting the rendezvous. The tanker aircraft will use the higher channel, and the receiver will use the lower channel.
AFMAN 11-247, 9.1.1.2

57
Q
  1. What altitude will the receiver be compared the tanker before crossing the IP?
A

The receiver must be established 1,000 feet below the tanker prior to crossing the ARIP. AFMAN 11-247, 9.1.2.1

58
Q
  1. If the receiver can’t confirm 1,000’ of separation compared to the tankers altitude prior to crossing the IP, what must the receiver do?
A

The receiver will hold at the ARIP.

AFMAN 11-247, 9.1.2.1

59
Q
  1. The receiver will stay 1,000’ below the tanker until when?
A

Positive visual contact is established with the tanker.

AFMAN 11-247, 9.1.4

60
Q
  1. Who declares MARSA?
A

Only the tanker will declare MARSA.

AFMAN 11-247, 9.2

61
Q
  1. What conditions must be met before declaring MARSA?
A

Radio contact has been established with the receiver, positive altitude separation has been confirmed, and positive position identification of the receiver has been confirmed.
AFMAN 11-247, 9.2

62
Q
  1. When is the latest the radios and A/A TACAN must be set up?
A

15 minutes prior to the ARCT.

AFMAN 11-247, 9.5.1

63
Q
  1. The first radio contact between the tanker and receiver will happen no later than when?
A

Will be not later than 15 minutes prior to the ARCT.

AFMAN 11-247, 9.6.3.1

64
Q
  1. What information will the receiver transmit to the tanker during the 15 minute call?
A

ETA to ARIP (on time, minutes early, minutes late), TAS during rendezvous, altitude, and altimeter setting.
AFMAN 11-247, 9.6.3.3

65
Q
  1. Who is responsible for navigation while conducting air refueling?
A

Tanker, who also ensures the receiver is updated on any changes.
AFMAN 11-247, 9.3.1

66
Q
  1. If the tanker has to orbit at the ARCP what are the parameters of the holding pattern?
A

Left-hand orbit, 30-degree bank turns, 2-minute legs at 250 KIAS.
AFMAN 11-247, 9.6.1

67
Q
  1. If an overrun is imminent who will make the call? The receiver or tanker?
A

The first crew to recognize an overrun will make an advisory call, “Pain 11, initiate overrun procedures.”
AFMAN 11-247, 9.10.2

68
Q
  1. What is the precontact position? Parameters?
A

50 feet directly behind the tanker and 15 feet below. The receiver has 9 feet of tail-to-belly clearance on the tanker, which should place the tanker’s wingtips just filling your side of the windscreen.
AFMAN 11-247, 9.11.1

69
Q
  1. What is the contact position?
A

Distinct references include: 1) placing the bottom of the VHF antenna on the stripe painted on the bottom of the aircraft, and 2) being able to see the AOA vanes in front of the leading edge of the wing.
AFMAN 11-247, 9.13.3

70
Q
  1. Explain the “Breakaway” maneuver.
A

Any time the tanker or receiver determines aircraft separation is required immediately to avoid a collision or prevent a dangerous situation from developing. The tankers call sign will be used to initiate the breakaway. The radio call will be, “Pain 11, breakaway, breakaway, breakaway,” and it may be called by either aircraft.
AFMAN 11-247, 9.15.1

71
Q
  1. Can Air Refueling operations be

conducted under VFR rules per AP/1B?

A

Aerial refueling operations will be conducted under instrument flight rules on the Aerial Refueling Tracks/Anchors described in this section.
FLIP AP/1B, 5-1

72
Q
  1. What are the responsibilities of the tanker

after completion of the Air Refueling?

A

Requesting altitude clearance and routing (if different than flight plan routing) for the receiver and tanker aircraft beyond the AR exit point. Throughout the refueling operation, controller initiated heading assignments may not be given without the concurrence of the tanker.
FLIP AP/1B, 5-1

73
Q
  1. What will the receiver do if it is unable to get
    a clearance after completions of the air
    refueling?
A

Follow the tanker

FLIP AP/1B, 5-1

74
Q
  1. At the end of an air refueling track what is

to happen to air refueling operations?

A

NOTE: Aerial refueling operations are terminated at the end of the refueling point unless an extension of the aerial refueling track is received.
FLIP AP/1B, 5-1

75
Q
  1. How do you find where to schedule an air

refueling track?

A

SCHEDULING UNIT - The military unit responsible for scheduling refueling operations. It provides daily schedules covering requested altitudes/flight levels and times of use for proposed operations to the assigned ARTCC
.

FLIP AP/1B, 5-1

76
Q
  1. Explain an air refueling anchor point.
A

ANCHOR POINT - The geographical point upon which the anchor pattern is oriented.
FLIP AP/1B, 5-1

77
Q
  1. What are the dimensions of a standard

anchor pattern?

A

ANCHOR PATTERN - A left-hand race track pattern with legs separated by a minimum of 20 NM and a minimum leg length of 50 NM.
FLIP AP/1B, 5-1

78
Q
  1. A simulated airdrop maneuver is performed at a minimum of _______feet AGL (or _______feet above planned route altitude.)
A

The planned drop altitude will normally be 1,000 feet AGL (or 500 feet above the planned route altitude)
AFMAN 11-247, 10.23

79
Q
  1. On the route, the wingman will never fly
    below lead or_______ feet AGL, whichever is higher. Whenever a flight path conflict with lead exists, cross_______ in relation to lead.
A

500 feet. Above & Behind

AFMAN 11-247, 10.26

80
Q
  1. Airdrop configuration is _______degrees flap setting and _______KIAS minimum.
A

140 KIAS, 10-degree flaps

AFMAN 11-247, 10.23

81
Q
  1. Airdrop/Low-Level. Wing is automatically cleared _______upon route entry and will rejoin to the visual position NLT the slowdown point.
A

Offset

3 FTS OI, ATTACHEMENT 4

82
Q
  1. Brief the _______airdrop altitude during the formation briefing.
A

MSL airdrop

3 FTS OI, ATTACHEMENT 4

83
Q
  1. Once commencing slowdown, lead will

avoid exceeding_______ ° AOB.

A

15° AOB.

3 FTS OI, ATTACHEMENT 4

84
Q
    1. T/F: Any formation crewmember may call “knock-it-off” to cease maneuvering when safety of flight is a factor or where doubt or confusion exists.
A

TRUE

AFMAN11-2T-1v3, A7.2

85
Q
  1. T/F: Any formation crewmember may call “terminate” to cease maneuvering when safety of flight is not a factor or when desired learning objective have been achieved.
A

TRUE

AFMAN11-2T-1v3, A7.4

86
Q
  1. T/F Wing should follow lead into IMC

conditions.

A

False

3 FTS OI, ATTACHEMENT 4

87
Q
  1. Lead will immediately announce base
    heading, then initiate a climb at ______
    KIAS to the _______.
A

220-250 KIAS to the ERAA.

3 FTS OI, ATTACHEMENT 4

88
Q
  1. T/F Lead will inform wing of his/her

climb airspeed.

A

True

3 FTS OI, ATTACHEMENT 4

89
Q
  1. Wing will simultaneously turn _____° from the base heading for 10 seconds then turn back to base heading while climbing approximately _______KIAS below lead’s climb airspeed at_______ KIAS to ERAA+_______ .
A

45°, 40, at 180-210 KIAS to ERAA + 1,000’.

3 FTS OI, ATTACHEMENT 4

90
Q
  1. T/F Formation may rejoin on top if
    conditions permit. Otherwise, proceed single
    ship.
A

True.

3 FTS OI, ATTACHEMENT 4

91
Q
  1. Orbit Procedures. In the event the
    weather prevents a VMC formation flight to
    the low-level entry point, the following
    procedure may be used to rejoin a formation
    prior to route entry
A

The flight lead will prebrief the orbit point, holding turn direction and expected altitude for
rejoin. The lead aircraft should plan to take off, as a minimum, 8 minutes earlier than normally
required to enter the route. This allows two standard holding patterns to complete the rejoin prior to
route entry time. The suggested minimum takeoff interval is 4 minutes. The lead aircraft will hold at
an orbit point no lower than 1,500 feet AGL. The wingman will enter the same holding pattern a minimum of 1,000 feet above the lead’s altitude until both aircraft are in VMC, a visual tally is confirmed by the wingman, and the flight lead declares MARSA. NOTE: MARSA requires a letter of agreement with the owning ARTCC facility.
• The wingman will maneuver as required to complete the rejoin. If a rejoin cannot be accomplished, the wingman will coordinate to obtain clearance to depart the orbit first.
• Following the low-level portion of the flight, lead may be required to separate the formation due to weather prior to RTB. This may be accomplished by holding in VMC while coordinating for separate clearances or, if weather allows, coordinating en route
AFMAN 11-247, 10.10

92
Q
  1. The flight lead will prebrief the orbit

point, holding turn_______ and expected _______for rejoin.

A

Direction, altitude

AFMAN 11-247, 10.10.1

93
Q
  1. The lead aircraft should plan to take off,

as a minimum, _______minutes earlier than normally required to enter the route.

A

The lead aircraft should plan to take off, as a minimum, 8 minutes earlier than normally
required to enter the route. This allows two standard holding patterns to complete the rejoin prior to
route entry time. The suggested minimum takeoff interval is 4 minutes.
AFMAN 11-247, 10.10.1

94
Q
  1. The lead aircraft will hold at an orbit

point no lower than _______feet AGL.

A

1,500 feet AGL.

AFMAN 11-247, 10.23