Limitations Flashcards

(50 cards)

1
Q

If a limit is exceed, the appropriate entry shall be made on DA FORM _ -_ -

Entry shall state what limits were _, _, and _ _ _

A

2408-13-01

Exceeded, range, time beyond limits

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2
Q

Avoid ranges 20-40% 60-90% NP except during _ and _

A

Start up and shutdown

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3
Q

Red and yellow striped tapes and red readouts indicate _ _ above or below, _ _ _ is likely to cause damage or _ _ _

A

The limit, which continued operation, shorten component life

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4
Q

Yellow tapes and readouts indicate the range _ _ _ should be given _ _ _ the instrument represents

A

When special attention, to the parameters

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5
Q

Green tapes and readouts indicate _ _ _ of the _ the instrument represents

A

Normal operating range, parameter

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6
Q

Rotor/Power displays. The NR and NP tapes are marked with a red lower limit line _%. A yellow minimum continuous limit line _%, and a red upper limit line _%NR and _%Np

A

91%.

95%.

110%Nr and 105%Np

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7
Q

Max weight that may be suspended from a rescue hoist is _

A

600 lbs

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8
Q

CAUTION: performing repetitive hoist lifts of _ or more, a _ rest period is required

A

300lbs

30sec

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9
Q

LWC stands for

A

Liquid water content

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10
Q

Trace LWC = _ to _ g/m3

A

0 to .25

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11
Q

Light LWC =

A

.25 to .5

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12
Q

Moderate LWC

A

.5 to 1

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13
Q

Heavy LWC

A

Greater than 1

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14
Q

The ice detection system is calibrated at _ knots

When flying at airspeeds above _ the ice rate meter will indicate _ LWC than normal

A

100

100 kts, higher

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15
Q

START LIMITS
At _ _ of _ degrees and below, _ consecutive starts may be made followed by a _ min rest period, followed by _ additional start cycles.

From _ to _ , _ consecutive starts may cycles may be made, A _ rest cycle is then required

A

Ambient temperature / 15
2, 3min, 2, 30min

15 / 52 degrees
2, 30 min

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16
Q

Max airspeed 1 engine inop

A

130

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17
Q

Max auto-rotational airspeed gross weight at 16,825 or less

A

150

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18
Q

Max auto-rotational airspeed more than 16,825

A

130

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19
Q

Sideward/ rearward flight. Hovering in winds greater than _ or _ its with ESSS from the sides or rear is prohibited.

A

45 / 35

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20
Q

Sideward/ rearward flight into the wind when combined with _ shall not exceed _ / _ with ESSS

A

Windspeed

45/35

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21
Q

1 SAS inop

22
Q

2 SAS inop

23
Q

Two SAS inop IMC

24
Q

1 hyd system inop

25
2 hyd system inop
150
26
2 hyd system inop IMC
140
27
Landing light
130-180
28
Searchlight
100-180
29
Cabin doors fully open up to
145
30
When the automatic stabilator control system has failed and Manuel control is available The Stabilator will be set full down at speeds below
40
31
When the automatic stabilator control system has failed, The Stabilator will be set to zero above
40
32
Vne becomes _ to indicate the airspeed limit applicable for the current _ _ except in no case shall the autorotation limit exceed _
Variable Stabilator position 120
33
Your stabilator has failed and Manuel control is available. You enter an autorotation. What is your max airspeed at all gross weights
120
34
Maneuvering limitations NOTE: maneuvers entered from a low power setting may result in _ of _ %Nr or greater
Transient droop 5
35
High speed maneuver limitations above _. avoid _ _ _ _to prevent excess tail rotor system _
80 Abrupt full pedal inputs Loading
36
Slope landing limitations The main gearbox may be operated up to _ at a time with _ _ when the helicopter is known to be at a _ _ _ (slopes or hover with extreme aft CG)
30min Pressure fluctuations Nose - up attitude
37
Cargo floor max capacity is _
300 lbs per square foot
38
Engine starter limits: An interval of at least _ between the completion of one start cycle and the beginning of the next cycle is required
60 seconds
39
A start cycle is defined as the _ from start initiation and acceleration of the compressor from _ to _
Interval From 0 RPM starter drop out
40
Vne is defined as a _ of _, , temperature, and _ _
Function Altitude Gross weight
41
Max air speed with external cargo hook loads up to 8,000 lbs
140
42
Max auto airspeed with volcano installed
100
43
Max airspeeds with skis installed
155
44
If you are required to open the cabin doors in flight you must be below _ KTS. and crewmembers must be secured to the _ prior to opening
80 Aircraft
45
46
Gunner or bam windows may be open up to
170
47
Do not open or close BAM windows above
120
48
Maneuvers entered from a low power setting …
May result in transient droop of 5% or greater
49
Eng inlet anti ice limitations Avoid operations under conditions of extreme _ _ requirements such as high rates of descent _ fpm or greater
Low power 1900
50
What two things must happen before opening cargo doors in flight
Aircraft must at 80 Kia’s or below Crew member opening the cabin door must be secured to the helicopter