TOLD Flashcards

1
Q

Takeoff Speed

A

The speed at which the main gear lifts off the runway

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2
Q

Single-Engine Takeoff Speed (SETOS)

A

The speed at which the aircraft is able to climb, once clear of ground effect, at a minimum of 100 ft/min with gear down and flaps 60%

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3
Q

Each extra knot above SETOS does what for your climb rate?

A

Gives you an extra 8-50 ft/min

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4
Q

Takeoff Distance

A

The distance from brake release to main gear liftoff

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5
Q

Normal Acceleration Check Speed (NACS)

A

The speed an average T-38C should reach at a specified check point during the takeoff roll

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6
Q

Minimum Acceleration Check Speed

A

The minimum acceptable speed at the check distance at which takeoff should be continued

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7
Q

Refusal Speed (RS)

A

The maximum speed to which the aircraft is able to accelerate to with both engines in MAX and then either:

  • abort with both engines operating (BEO)
  • abort with an engine failure (EF)
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8
Q

Decision Speed (DS)

A

The minimum speed at which an aircraft is able to experience an engine failure and still accelerate to SETOS and takeoff (approx 700 ft from the start of rotation at SETOS) within the remaining runway

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9
Q

Critical Engine Failure Speed (CEFS)

AND

Critical Field Length (CFL)

A

The minimum speed at which an aircraft can accelerate with both engines, lose an engine, and either:

  • accelerate to SETOS and takeoff
  • abort and decelerate to a stop within the same distance (Critical Field Length)
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10
Q

Landing Distance (LD)

A

The distance required from main gear touchdown to slow the aircraft from landing speed to a safe taxi speed

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11
Q

What do we do if there is no barrier available?

A

Use RS-BEO instead of RS-EF

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12
Q

How do you calculate MACS from NACS?

A

Subtract 3 knots for every 1000’ of difference between CFL and RWY length, up to a maximum of 10 knots

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13
Q

Assumptions of normal takeoff

A
  • MAX thrust
  • Aft stick applied at rotation speed and maintaining 7.5* NH
  • NW liftoff at 155
  • MW liftoff at 165
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14
Q

Assumptions with takeoff distance

A
  • normal Acceleration

- effects of rcr are negligible

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15
Q

Assumptions with refusal speed?

A
T-Three second reaction time
O-Optimum braking below 100, cautious between 100-130
M-Maintain 7.5* if rotated, until 120
B-BEO (Both max, both idle)
O-One engine (one idle, one windmilling)
N-Normal Acceleration up to abort
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16
Q

Assumptions with SETOS

A

1-100 FPNM climb out of ground effect
T-three point attitude while accelerating
O-one engine max, other windmilling
N-normal Acceleration/configuration

17
Q

Assumptions with decision speed

A

T-three point attitude while accelerating
O-one engine max, other windmilling
N-normal Acceleration/configuration

18
Q

Assumptions with CEFS STOP

A
T-three second reaction time
M-maintain 7.5* if rotated until 120
O-optimum braking below 100, cautious between    100-130
O-one engine (one idle, one windmilling)
N-normal Acceleration/config
19
Q

Assumptions with CEFS GO

A

T-three point attitude while accelerating
O-One engine max, other windmilling
N-normal acceleration/config

20
Q

Assumptions with NACS

A
  • normal acceleration

- must be less than go/no go Speed

21
Q

Assumptions with MACS

A

Allows for less than normal acceleration due to: formation takeoff, engine variations, pilot technique