Formation Stage Maneuvers Flashcards

1
Q

Minimum Qm for lead during descents

A

20%

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2
Q

Lead climb rate and airspeed

A

180 KCAS, 2000 fpm unless otherwise briefed

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3
Q

Vertical separation

A

CONV: 25 foot step upAPLN: 25 foot step down

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4
Q

TACAN A/A

A

provides range information to another aircraft if the TACAN channels are separated by 63 channels

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5
Q

Visual

A

Sighting of a friendly aircraft or ground position

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6
Q

Blind

A

No visual contact with a friendly aircraft or ground position

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7
Q

Tally

A

Sighting of a target, bandit, bogey, or enemy position

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8
Q

No Joy

A

Aircrew does not have visual contact of a target, bandit, bogey, or enemy position

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9
Q

Contact

A

Acknowledges sighting of a specified reference point or zone

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10
Q

How to perform time sync

A
  1. CDU MENU 2 - GPS TIME UPDATE2. COMM MENU 2 - TIME SYNC ALL
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11
Q

When should you perform a time sync

A

prior to HQ or SINCGARS Communications

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12
Q

When performing Radio Check in procedures, what does the term CLEAR mean

A

Unsecure communications

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13
Q

When performing Radio Check in procedures, what does the term ACTIVE mean

A

HAVEQUICK or SINCGARS transmissions

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14
Q

Alpha Check

A

Request for, and confirmation of bearing and range to described point.

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15
Q

Formation taxi distance

A

1 to 1.5 blade span separation nose to tail distance

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16
Q

During formation takeoff when do you configure to NVG lighting

A

Once all aircraft are established on the runway

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17
Q

Lead should not pass ___ nacelle with the gear down

A

60 degree

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18
Q

Formation Takeoff Procedure

A
  1. Lead position on downwind side of the runway and wing on upwind side2. Lead sets 60 nacelle and once all aircraft are at appropriate nacelle setting, lead releases brakes3. Wing releases brakes 3 seconds after lead 4. lead will stabilize at 60 nacelle and conduct rendezvous
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19
Q

Aborted takeoff

A

If lead aborts wing remains on deck, or if airborne wing will stay in their lane or gain lateral separation and continue takeoffIf wing aborts, lead will continue takeoff, return to the runway and re-evaluate the situation

20
Q

Aborted takeoff should be announced over what frequency

A

Tower

21
Q

Formation transition to APLN

A
  1. Lead signals to transition by raising the gear2. Lead will use half rate to 45 degrees then full rate to downstops3. Wing will rotate nacelles and add power to maintain step up4. As nacelles pass 30 degrees, wing should descend to stepped down APLN mode formation
22
Q

Carrier Rendezvous

A
  1. Lead establishes constant altitude and 15 degrees bank turn at pre-briefed airspeed2. Wingman uses 45 degree rendezvous bearing on lead to cut inside of leads turning radius. 3. Wing can either join on inside of lead or execute crossunder and join on outside of leads turn
23
Q

Wingman loses sight of lead

A
  1. Increase step up or down2. Turn away from lead3. Transmit “blind” call
24
Q

What should be done if an excessive closure rate develops

A

CONV/VTOL: Overrun (stepped up)APLN: Under-run (stepped down)If below 220 KCAS wing can autobeep

25
Q

Over-run procedure when lead is turning in CONV

A

POWER LEVEL AFT1. Increase power to increase step up to 50 ft2. Level the wings and aim aft of leads tail3. Nacelles aft4. Pass above and behind lead and rejoin on the outside of lead

26
Q

Under-run procedure when lead is turning in APLN

A

LOWER LEVEL IDLE1. Lower the nose to increase step down to 50ft2. Level the wings and aim aft of leads tail3. Power toward idle4. Pass below and behind and rejoin on the outside of lead

27
Q

Over-run procedure when lead is straight and level in CONV

A

POWER LEVEL AFT1. Increase power to increase step up to 50 ft2. Level the wings and aim aft of leads tail3. Nacelles aft4. Pass above and behind lead and rejoin on the outside of lead

28
Q

Under-run procedure when lead is straight and level in APLN

A

LOWER LEVEL IDLE1. Lower the nose to increase step down to 50ft2. Level the wings and aim aft of leads tail3. Power toward idle4. Pass below and behind and rejoin on the outside of lead

29
Q

Welded Wing

A

Where wingman remains in a fixed bearing and distance from lead, but does not necessarily mean turning about lead’s axis

30
Q

Visual checkpoints for step up in CONV/VTOL

A

Lead’s proprotor hubs on same horizontal plane as the horizon

31
Q

Visual checkpoints for horizontal separation in CONV/VTOL or APLN

A

0.0 to 0.2 DME5 blade spans (0.1 DME)

32
Q

Crossover procedure

A
  1. Increase step up until lead’s vertical stabilizer is at the middle trailing edge of the wing (50-75ft step up)2. Adjust cyclic to initiate movement to the opposite side3. Adjust cyclic to achieve wings level 4. Approaching the appropriate visual checkpoints for the desired bearing, input cyclic into opposite direction to neutralize lateral motion.5. Decrease step up to 25 ft
33
Q

Crossovers in turns

A

Leads upper proprotor should be one rotor disk below the horizon

34
Q

APLN Cruise Formation Position

A

30 to 45 degree bearing with 25ft step down and 3 to 5 blade spans (0.0 to 0.2 DME) of separation

35
Q

Visual checkpoints for step down in APLN

A

Place lower tip of lead’s proprotor tip path plane 1/2 proprotor radius above the horizonFar nacelle just above the horizontal stabilizer

36
Q

Cruise, 30 degree Bearing Checkpoints in APLN (Near)

A

Align leads center flap split with the trailing edge of the cockpit window

37
Q

Cruise, 30 degree Bearing Checkpoints in APLN (Far)

A

Align lead’s far side nacelle half way between the vertical stabilizers

38
Q

Crossunder Procedure

A
  1. Increase step down until lead’s vertical stabilizer is level with the trailing edge of leads flaperon (50ft)2. Adjust cyclic to initiate movement to the opposite side3. Adjust cyclic to achieve wings level 4. Approaching the appropriate visual checkpoints for the desired bearing, input cyclic into opposite direction to neutralize lateral motion.5. Adjust pitch until lower tip of lead’s proprotor tip path plane returns to half proprotor radius above the horizon
39
Q

Airspeed for APLN Formation

A

200 KCAS

40
Q

Turn Pattern CONV

A
  1. Roll into 20 degree AOB turn for 90 degrees heading change2. Wingman uses welded wing to stay in position3. Roll into 20 degree AOB turn in opposite direction for 90 degrees heading change 4. Wingman uses welded wing to stay in position5. Roll into 30 degree AOB turn for 180 degrees heading change6. Wingman uses radius of turn to stay in position7. Roll into 30 degree AOB turn in opposite direction for 180 degrees heading change8. Wingman uses radius of turn to stay in position
41
Q

Turn Pattern APLN

A
  1. Roll into 30 degree AOB turn for 90 degrees heading change2. Wingman uses welded wing to stay in position3. Roll into 30 degree AOB turn in opposite direction for 90 degrees heading change 4. Wingman uses welded wing to stay in position5. Roll into 45 degree AOB turn for 180 degrees heading change6. Wingman uses radius of turn to stay in position7. Roll into 45 degree AOB turn in opposite direction for 180 degrees heading change8. Wingman uses radius of turn to stay in position
42
Q

Turns into and Turns away

A

turn about own axis for turns awayturn about leads axis for turns into

43
Q

Flight lead should be no faster than ___ KCAS and power no less than ___ during descents

A

240 KCAS20% Qm

44
Q

Formation Conversion to CONV

A
  1. Lead calls “Decel”2. Lead calls “Beeping” at 170 KCAS3. Use constant rate to convert to 60 degree nacelle4. Wingman should allow aircraft to climb to stepped up position between 30 and 45 nacelle
45
Q

IIMC Fan Breakup and Rendezvous

A
  1. Wing initiates with “Two has lost sight, POPEYE”2. Lead responds “Crossbow XX flight, fan break. Base Altitude X, Base Heading X”3. Wing turns 20 degrees for 30 seconds returns to base heading while climbing 200ft above base altitude4. Once visual is established, lead clears wing to descend to briefed altitude5. Prior to anchor point announce join up procedures6. At rendezvous anchor point lead begins 15 degree AOB turn to the left7. Once cleared to join, wing maneuvers inside of leads radius of turn to execute join 8. Approaching the normal cruise separation wing should execute a crossunder.