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1
Q

Static rollover Dynamic rollover 3 requirements

A

-42* -15* -rolling moment, pivot point, thrust greater than weight

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2
Q

Blade stall: -indication -recovery steps

A

-vibration, nose pitchup, roll to left -lower collective, aft cyclic

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3
Q

Effective transitional lift is?

A

16-24knts helicopter will want to climb vortices are washed out causing rapid increase in lift

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4
Q

When does transverse flow effect occur?

A

14-20knts

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5
Q

Vibration Frequencies: -low -medium -high

A

-main rotor -engine -tail rotor

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6
Q

Airspeeds: -minimal drag -max range

A

-53 -83

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7
Q

Manifold pressure marks: -upper red -yellow

A

-24.1 -19.6 to 24.1

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8
Q

Engine ratings: -Max Continuous -5Minute takeoff -Derated

A

-124 bhp -131 bhp -145 bhp

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9
Q

Engine rpm?

A

2652 rpm

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10
Q

Engine Tach Markings: -upper red -green -lower red -bottom yellow

A

-104 to 110 -101 to 104 -90 to 101 -60 to 70

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11
Q

Airspeed indication markings: -green arc -upper red

A

-50 to 102 -102vne

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12
Q

Engine make and model?

A

Lycomming o-360-j2a(beta2)

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13
Q

Rotor tach markings: -upper red -upper yellow -green -lower yellow -lower red -bottom yellow

A

-110 -104 to 110 -101 to 104 -90 to 101 -90 -60 to 70

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14
Q

5 Compass errors?

A

-magnectic variation -magnetic deviation -magnetic dip -acceleration error(ands=accel north decel south) -turning error(unos=unshoot north overshoot south)

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15
Q

What is the standard lapse rate for temp and press?

A

-temp=-2c(-3.5f) per 1000 ft elevation increase -pressure=-1hg per 1000 ft elevation increase

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16
Q

What elements onboard interfere with the compass?

A

-metal components -engine -radios -electric accessories

17
Q

IMSAFE

A

I-illness M-medication S-stress A-alcohol .04 and 8hrs F-fatigue E-eating

18
Q

Main rotor: -diameter -chord -twist -tip speed

A

-25ft 2in -7.2 –8 degrees -672 fps

19
Q

Tail rotor: -diameter -chord -twist -precone angle -tip speed

A

-3ft 6in -4in -0degrees -1 degree 11 minutes -599 fps

20
Q

Powerplant type

A

4 cylinder, horizontally opposed, direct drive, air cooled, carbureted, normally aspirated.

21
Q

never exceed speed is ___kias up to 3000 feet density altitude

A

102

22
Q

-Max gross weight -minimum gross weight -max per seat -max baggage

A

-1370 -920 -240 -50

23
Q

Max temp for cylinder head

A

500f

24
Q

Max oil temp

A

245f

25
Q

Oil pressures: -minimum during idle -minimum during flight -maximum during flight -maximum during startup

A

-25 -55 -95 -115

26
Q

3 conditions for settling with power?

A

-less than etl -at least 20% power -greater than 300fpm descent

27
Q

OODA loop stands for

A

observation orientation decision action

28
Q

DECIDE stands for

A

Detect-detect a change has occurred Estimate-estimate need to react Choose-which is more favorable Identify-identify theres change Do-do something Evaluate-evaluate the effect of what you did

29
Q

PAVE stands for

A

pilot-physical and emotionl readiness aircraft-capable of task, within weight, enough fuel enViroment- how will weather affect DA external pressures-dont override good judgment, dont feel pressured

30
Q

Lost procedures

A

-climb -conserve -communicate -confess -comply

31
Q

For flights away from departure airport you must review what specific info.

A

-weather -fuel requirements -alternates I case flight can’t be finished -any traffic delays known by atc -runway lengths intended -takeoff/landing distance

32
Q

What is SRM

A

Single pilot Resource Management Managing information for safe flight such as weather briefing, weight and balance, aircraft operating limitations, runway lengths, alternate routes, etc.

33
Q

5 dangerous attitudes to have as a PIC

A

-antiauthority:follow rules -invulnerability:it could happen to you -resignation:I’m not helpless -macho:taking chances is foolish -impulsivity:think first, not so fast

34
Q

What is dissymmetry of lift

A

One blade producing more or less lift than the other and do to forward momentum of air striking one blade one will always produce more than the other countering this by blade flapping

35
Q

3 types of LTE

A

-main rotor disc interference -tail rotor vortex ring state -weathercocking

36
Q

Low G conditions can cause what 3 things

A

-mast bumping -roll -cutoff tail boom