Flight Characteristics Flashcards

1
Q

VRS limitations: when does the high sink rate warning system come on?

A

<60KCAS ; >800fpm sink

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2
Q

What is pitch-up with side slip and what are factors that can cause it?

A

Pitch-up with side slip refers to the pitch-up tendency when the empennage and horizontal tail are directly downwind of a proprotor.

Factors that influence the onset and severity of this condition:
- Relative winds 30-60 deg off the nose that are greater than 20kts (downwash impingement on the tail causes the aircraft to pitch-up)
- Nacelle angle: higher nacelle angle reduce forward stick control margin, decreasing the ability to correct for inadvertent pitch up
- Longitudinal CG: Witch aft CG, any pitch-up tendency of the aircraft will be more difficult to arrest since control margins are already reduced in this axis

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3
Q

Wind tolerance for rotor start-up and shutdown

A

Up to 45kts

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4
Q

VTOL nacelle setting:

A

85-96 deg nacelles

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5
Q

CONV nacelle setting:

A

1-84 deg nacelles

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6
Q

APLN nacelle setting:

A

0 deg nacelle

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7
Q

Describe the stages of VRS:

A

Stage I
- characterized by increased vibration levels, pitch bucking, or sluggishness of aircraft response to control inputs
- corrective action - increase TCL; trim nacelles forward to max rate for 2sec (~15deg forward); fly out with forward stick

Stage II
- aural cues (rumbling onset), markedly increased descent rate, or improper roll control response as VRS gets worse
- corrective actions - trim the nacelles forward at max rate for two seconds (~15 deg forward); simultaneous and immediate forward stick to fly out of condition
*Increasing TCL in late stages of VRS may aggravate the condition and cause a roll-off

Stage III
- characterized by rapid uncommanded roll and corresponding large pitch; each rotor operating at very different aerodynamic conditions (known as “roll-off”)
- correction: nacelles should be rotated forward at max rate for 2 secs (~15 deg forward) and unusual attitude recovery procedures should be performed

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8
Q

75 STO

A
  • Nacelle 75
  • TCL full forward 6 seconds
  • Liftoff at Vlof
  • Approx 2 deg nose up
  • 70-80 KCAS climb
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9
Q

60 RTO

A
  • Nacelle 60
  • Release brakes ACFT begins to roll
  • QM approx. 50% then pause 4-5sec
  • Smoothly apply max TCL
  • Nose level to slightly high
  • Desired climb speed
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10
Q

60 STO Level Attitude

A
  • Nacelle 60
  • TCL full fwd 6 sec
  • Liftoff at Vlof
  • Approx. 2 deg nose up
  • 80-90 KCAS climb
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11
Q

60 STO Attitude Capture

A
  • Nacelle 60
  • TCL full fwd 6 sec
  • Rotate at Vrot
  • 10deg nose high in 2 sec
  • Accelerate to 80-90 KCAS
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12
Q

Eighty (80) TTO

A
  • Set hover nacelle
  • depart vertically
  • continue to climb at max power
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