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UH 72 > BWS / Review of P1 & P2 > Flashcards

BWS / Review of P1 & P2 Flashcards

1
Q

Name the types of VMC takeoffs

A
  1. Normal
  2. Constant angle
  3. Vertical
  4. Level acceleration
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2
Q

Describe normal takeoff

A
  • Off ground: 0.5 FLI, 3 degrees nose down
  • 50 KIAS until 50 feet
  • Above 50 feet = aircraft in trim
  • Accelerate to 65 KIAS
  • Adjust to desired rate of climb
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3
Q

Describe constant angle/vertical takeoff

A

Can very from vertical to almost flat.
When performing vertical takoff, it’s altitude over airspeed and will require OGE power.

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4
Q

Describe level acceleration takeoff

A

(Would be used when hover power is max power available)
- Achive ETL
- Prevent blowback
- Resume normal takeoff

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5
Q

What is max recommended nose low for acceleration during takeoffs?

A

5º

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6
Q

The decision to do a go around (when power limited) should be done when?

A

Prior to deccelerating below ETL

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7
Q

What the procedure for planning a VFR flight?

A
  1. Obtain WX (can VFR flight be preformed?)
  2. NOTAMS, Charts ect.
  3. Select course and altitude
  4. Determine; MAG HDG + GS + ETE (each leg)
  5. Computate: distance, time, fuel
  6. Verify aircraft CG & weight
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8
Q

What’s the descent profile of a normal approach ?

A

7 - 12 degrees starting at 300-500’ AGL

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9
Q

When will the aircraft go through ETL ?

A

16-24 kts

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10
Q

What does loss of ETL mean for us as a pilot on approach ?

A

Increase collective to maintain approach angle
the increase of collective tends to make nose rise requiring forward cyclic to maintain rate of closure
Left pedal to counteract TQ

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11
Q

What’s the descent profile of a steep approach ?

Cautions?

A

Approach angle greater than 12º

**Setteling with power:** 20-100% power applied, airspeed < 10 kts, descent > 300 FPM

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12
Q

In a steep approach, loss of ETL occurs ____ then during a normal approach

What does this require ?

A

Loss of ETL occurs higher

Requires collective increase to prevent settling with power

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13
Q

How could wind in confined areas affect a steep approach ?

A

Wind effects could be lost when descending below the confined area barrier, causing the aircraft to settle more quickly

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14
Q

What’s the descent profile of a shallow approach ?

A

Approach angle less than 7º
Usually 3-5º

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15
Q

When would we use a shallow approach and run on landing?

A

High density altitude
High gross weight condition
Emergency procedure

Due to the insufficient power to hover

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16
Q

Why does the lack of power to hover make us use shallow approach with run on landing ?

A

to make use of translational lift until surface contact is made

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17
Q

At what speed should the aircraft arrive at the touchdown point during a run on landing ?

A

At or slightly above ETL

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18
Q

What’s allowable drift during slope landings

A

± 1 foot

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19
Q

during slope landings, maintain heading ± ____ degrees

A

± 5º

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20
Q

What must you note before initiating the slope landing ?

A

Hover attitude, to determine if you are within limits during the landing

21
Q

When performing a run on landing, adjust cyclic to arrive at ____ kts at ____ ft

A

40 kts at 50’

22
Q

What’s max rate of descent during touchdown when performing run on landing ?

A

300 FPM

23
Q

When experiencing ENG FAIL and transitioning to OEI flight, maintain ____ kts until ____ ft AGL, afterwards ____ should be obtained.

A

When experiencing ENG FAIL and transitioning to OEI flight, maintain 45 kts until 200 ft AGL, afterwards 65 kts (Vy) should be obtained.

24
Q

What’s max rate of descent during an OEI approach ?

A

500 FPM

25
Q

When performing a run on landing OEI, reduce airspeed not to exceed ____ FLI with training device and ____ without training device

simulated OEI conditions?

A

12 FLI with training device
11 FLI without training device

AEO power for simulated OEI conditions

26
Q

simulated eng failure at low altitude/low airspeed w. flyaway

What are the initial immediate actions when detecting ENG FAIL at low altitude ?

A
  • Trim rotorspeed to max
  • Obtain 45 KIAS
  • Announce
  • Adjust collective to maintain rotor limits
27
Q

simulated eng failure at low altitude/low airspeed w. flyaway

When performing “flyaway” what should collective be adjusted to ?

A

To maximum power available
- 12 FLI, 2.5 min power when OEI
- Not to exceed 12 FLI with training device
- simulated ENG FAIL AEO maintain AEO limits

When reaching 200' adjust to 65 KIAS and climb to altitude that allows you to reach suitable landing area

28
Q

simulated eng failure at low altitude/low airspeed FORCED LANDING

What’s the initial actions when detecting an ENG FAIL at low altitude with a suitable landing area beneath you ?

A

Simoustanly:
1. Trim rotorspeed to max
2. Obtain 45 KIAS
3. Announce
4. Adjust collective to maintain rotor limits

Then:
Adjust cyclic to arrive at 40 KIAS at 50’ AGL
Adjust airspeed as appropriate not to exceed AEO limits for simulated conditions

29
Q

Autorotation

State entry parameters for autorotation

A

700’ AGL
90 KIAS

30
Q

Autorotation

Why should we apply collective to reach >5%TQ ?

A

To enter an autorotational descent and not a steep approach

(Ensures that the rotor is decoupled from the engines)

31
Q

Autorotation

When should we ensure that a steady state autorotation is attained ?

If it is not?

A

Before reaching 300’AGL

Abort and perform go around

32
Q

Autorotation

What indicates a steady state autorotation ?

A
  1. Rotor RPM is within limits (96-104)
  2. Aircraft is at correct airspeed (60-90 KIAS)
  3. Aircraft in trim (± half a ball width)
  4. Aircraft in a position to terminate at the intended landing area
33
Q

Autorotation

How is it terminated ?

A

“Go around” : apply collective to arrest descent and establish climb
or
“terminate with power” : apply collective to arrst descent at an altitude that will ensure the tail stinger doesn’t touch the ground

34
Q

Autorotation

When should aft cyclic be applied to initiate a smooth, progressive deceleration?

How much flare attitude ?

A

100’ AGL = initiate deceleration

15-20º flare attitude

35
Q

Autorotation

At approximately ____ to ____ feet AGL, apply sufficient colletive to control descent rate and reduce flare attitude to approcimately ____ degrees

A

10 - 15 feet AGL
7º flare attitude

36
Q

Autorotation

When is the autorotation maneuver complete?

A

When the aircraft is HIGE at approximately 5 feet AGL

37
Q

Autorotation

What could happen when lowering the collective to initiate the autorotation ?

When would it possibly automatically shut down the engines ?

A

Nr- overspeed

Nr > 123.1 %

38
Q

What is important while flying “manual throttle”

A

To anticipate power and control requirements and seperate maneuvers. So don’t initiate decent and decceleration at the same time

39
Q

When flying manual throttle, maintain FLI +____ / - ____

A

+1/-2

40
Q

WARNING

What should the P on the controls be aware of when adjusting for a nr. 2 engine underspeed ?

A

That the limiting stop for the nr. 2 throttle doesn’t fall inadvertently into position when in the EMER area

41
Q

CAUTION

What should the P on the controls be aware of when adjusting for nr. 1 engine underspeed ?

A

That the safety latch is extemely difficult to release and additional time will be required

42
Q

What should you be aware of in regards to manual throttle and the N2 trim switch ? ( simulator training )

A

During manual throttle the trim switch movement will be simulated

43
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

What is airspeed limits when established on final ?

A

40 KIAS +10/-5

44
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

____ crosswind component is advantageous during approach and landing.

A

Left crosswind

45
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

What should be done, if nose yaws right on approach ?

Application of collective will accelerate ____ yaw

A

Apply forward cyclic

right

46
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

What is minimum airspeed until final ?

A

70 KIAS

47
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

On final, continue approach until ____ with ____ and then announce intentions to land or go around

A

40 KIAS with no more than 300 fpm rate of descent

48
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

What should the pilot do if at 5 feet the nose is still left ?

A

keep decreasing speed, maintaining altitude

49
Q

Anti-torque malfunction (Tail rotor failure/fixed pitch)

What should the pilot do if the nose yaws right past the centerline of the intended landing area ?

A

apply forward cyclic

Collective application will accelerate the right yaw

UH 72 (42 decks)

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