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why am i saying what what way > Operating Suggestions > Flashcards

Operating Suggestions Flashcards

1
Q

-1 Prohibited Maneuvers

A

-Simultaneous movement of both PCLs to IDL or OFF in flight (PCL chop)
-Hovering turns > 30 deg per second
-Aerodynamic beaming with collective full down once main landing gear touchdown
-Rearward ground taxi
-Practice touchdown autorotation
-Flight beyond 90 deg angle and 45 deg nose up or down

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2
Q

-1 Section V
Non-prohibited but prohibited Maneuvers

A

-Taxiing with engine inlet(s) removed
•Engine overspeed check in flight
-Operating an engine against the gust lock
-Hovering in winds > 45kts from the sides or rear
-Flight with cockpit doors removed
•Maneuvering flight which results in significant increase in 4 per
•Nose downslope with winds > 15kts
-Flight into heavy or sever icing
-Intentional flight into severe turbulence
-Intentional flight into thunderstorms

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3
Q

Q 10 Sec Transient
Dual Engine
>80 KIAS

A

100-144%

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4
Q

Q 10 Sec Transient
Dual Engine
< or equal 80 KIAS

A

120-144%

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5
Q

Q 10 Sec Transient
Single Engine

A

135-144%

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6
Q

Q Continuous
Dual Engine
>80 KIAS

A

0-100%

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7
Q

Q Continuous
Dual Engine
< or equal 80 KIAS

A

0-120%

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8
Q

Q Continuous
Single Engine

A

0-135%

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9
Q

Emergency Stop NR

A

76%

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10
Q

Routine Stops with Rotor Brake

A

NR < 40%
150-180 psi
12-18 seconds

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11
Q

Engine Start Minimum and Maximum psi

A

450 min
690 max

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12
Q

Time limit with rotor brake operations

A

None

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13
Q

Use of rotor brake with engine(s) operating restrictions

A

At IDLE only, single and dual engine starts authorized.

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14
Q

Starter Limits Temperature Range

A

<16
16-52

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15
Q

Starter Limits <16 degrees C

A

1 min
3 min
1 min
30 min

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16
Q

Starter Limits 16-52 degrees C

A

1 min
30 min

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17
Q

When can we do dual engine starts?

A

Inside the ENGINE START ENVELOPE chart PTO -1.

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18
Q

Maximum wind velocity for rotor start or stop

A

45 kts

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19
Q

Maximum airspeed one engine INOP

A

130 KIAS

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20
Q

Maximum airspeed autorotation

A

120 KIAS

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21
Q

Maximum hovering wind velocity from the sides or rear

A

45 kts

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22
Q

One SAS INOP

A

170 KIAS

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23
Q

Two SAS INOP

A

150 KIAS

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24
Q

Two SAS INOP IMC

A

140 KIAS

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25
Q

One hydraulic system malfunctioning

A

170 KIAS

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26
Q

Two hydraulic system malfunctioning

A

150 KIAS

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27
Q

Two hydraulic system malfunctioning IMC

A

140 KIAS

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28
Q

Landing light must be extended prior to

A

130 KIAS

29
Q

Searchlight (and rescue hoist searchlight) must be extended prior to

A

155 KIAS

30
Q

Cabin door fully open airspeed

A

145 KIAS

31
Q

Opening and closing cabin doors airspeed

A

120 KIAS

32
Q

Opening and closing cabin doors descents and ascents

A

descent - 1500 fpm
ascent - 500 fpm

33
Q

Maximum airspeed for gunner’s window

A

170 KIAS

34
Q

Manual operation of the stabilator in flight is prohibited except…

A
  1. Stabilator emergency training
  2. Functional check flight requirements
  3. Alternate stabilator control in case of AUTO mode malfunctions
35
Q

APU operating limits with engine and rotor operating

A

Ambient temperatures above 43 degrees C limited to 30 minutes

36
Q

When do maximum airspeed, pitch and bank limits applicable for the FRIES bar?

A

Only for the use of the SPIE rope and personnel attached to the D-Ring.

37
Q

Maximum touchdown sink rate on level terrain

A

300 fpm

38
Q

Maximum touchdown sink rate on slopes

A

180 fpm

39
Q

Maximum forward touchdown ground speed on level terrain

A

60 kts

40
Q

Nose upslope limit

A

6 degrees

41
Q

Right/left wheel upslope limit

A

12 degrees

42
Q

How does wind affect the landing limitations?

A

For upslope and right/left operations will be further reduced by 2 degrees for every 5 kts of wind.

43
Q

What is the ice detector calibrated to? What will happen outside these parameters?

A

100 KIAS
Airspeeds above 100 KIAS ice rate meter will indicate higher liquid water content than the actual conditions.

44
Q

What equipment is required to be installed, operational, and turned on to fy into trace or light icing?

A

Windshield anti-ice
pitot heat
engine anti-ice
engine inlet anti-ice modulating valve
insulated ambient air sensing tube

45
Q

What equipment is required to be installed, operational, and turned on to fly into moderate icing conditions?

A

Windshield anti-ice
pitot heat
engine anti-ice
engine inlet anti-ice modulating valve
insulated ambient air sensing tube
and
blade deice

46
Q

Windshield anti-ice temperature limitations

A

Shall not be used when OAT is over 27 degrees C

47
Q

Backup Hydraulic Pump Hot Weather Limits apply when the rotor is static or operating?

A

Static

48
Q

Backup Hydraulic Pump Temperatures

A

-54-32
33-38
39-52

49
Q

Backup Hydraulic Pump Temperatures with Operating Time and Cooldown Time

A

Temp
-54-32 is unlimited with zero cooldown time
33-38 is 24 minutes op time and 72 min cooldown
39-52 is 16 minutes op time and 48 min cooldown

50
Q

APU operating limits with engine and rotor operating

A

Ambient temperatures above 43 degrees C limited to 30 minutes

51
Q

APU operating limits engine and rotor NOT operating

A

Continuously up to 51 degrees C

52
Q

What is required if the APU OIL HOT caution illuminates?

A

30 minutes cooldown period is required before checking oil level

53
Q

What is required if the APU OIL HOT caution illuminates?

A

30 minutes cooldown period is required before checking oil level

54
Q

What configurations can fuel be dumped in? When is it not recommended and why?

A

All forward airspeeds, during climbs, descents.
It is not recommended while hovering in ground effect because the fuel could recirculate and create a hazard.

55
Q

Full anti-ice capability cannot be provide at what engine power levels?

A

10% Q per engine and below

56
Q

PTO -1
Do not power up the EO?IR in temperatures below

A

-40 degrees C

57
Q

PTO -1
When can we expect transmission oil pressure to drop?

A

During nose-up slop operations (because oil pumps are located forward)

58
Q

PTO -1
What are the slope landing limits based on/how will the angle be measured?

A

It’s based on the actual slope of the terrain not the angle indicated on the attitude indicator. (Attitude indicator may show greater slope due to compression of landing gear strut.

59
Q

PTO -1
When will abrupt, full pedal input be avoided?

A

Above 80 KIAS

60
Q

PTO -1
What are bank angles limited to with PRI SERVO 1 or 2 illuminated?

A

30 degrees

61
Q

PTO -1
Limits with rearward flight and downwind hovering
Why?

A

Prolonged operations are to be avoided to prevent accumulation of exhaust fumes in the helicopter and heat damage to windows on open cargo doors.

62
Q

PTO -1
Limits with simulating stabilator automatic mode failure

A

Stabilator shall only be slewed in the trailing edge up direction.

63
Q

PTO -1
How will a fully developed blade stall present itself?

A

heavy 4 per revolution vibration
increasing Q
loss of altitude

64
Q

PTO -1
Which turn direction (right vs left) will take more time to recover from?

A

Right

65
Q

PTO -1
Limitation with Stab auto mode failure

A

Do not exceed the airspeed indicator variable VNE red arc

66
Q

PTO -1
CAUTION With opening cabin doors

A

Crewmembers must have full control of the cabin door when opening or closing it.

67
Q

PTO -1
Power Off (autorotational) max rotor speed

A

120%

68
Q

PTO -1
CAUTION with Engine start limitation pressure altitude

A

Engine start attempts at or above a pressure altitude of 18,000’ could result in a hot start.

69
Q

PTO -1
When does the starter limitation rest period timing start?

A

When the first attempt is aborted for any reason (it applies regardless of the duration of the first attempt).

why am i saying what what way (19 decks)

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