EP’s And Limits Flashcards

1
Q

Max TOT starting

A

8.5 FLI
785 TOT

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2
Q

TOT starting transient

A

8.5-11 FLI
5 seconds
865 TOT

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3
Q

AEO takeoff Power range

A

8.5 - 10 FLI
5 minutes
%tq 71-88

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4
Q

AEO take off power Max

A

10 FLI
5 minutes
88% TQ

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5
Q

OEI MCP Max

A

11 FLI
91 % TQ

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6
Q

OEI 2.5 minute power

A

12 FLI
2.5 min
125 % TQ

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7
Q

AEO transient Max

A

10.5 FLI
12 seconds
97 % tq

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8
Q

OEI transient Max

A

14 FLI
12 seconds
140% TQ

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9
Q

Max gross mass for flight

A

7905 lbs

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10
Q

Airspeed limits

A

Vne OEI: 110 Kias
Vne Steady auto : 90 Kias
Min a/s auto: 60 Kias
Target a/s auto: 75 Kias

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11
Q

Slope limits

A

Slope left: 11°
Slope right: 6°
Slope nose up or down: 8°

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12
Q

Prohibited flight maneuvers

A

Aerobatic maneuvers
Full auto
Flight into icy cond.

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13
Q

Rotor rpm

A

95% steady light/ low beep tone
106% flash light gong
110% flash light high tone

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14
Q

Eng 1 or 2 fail

A

OEI flight cond. : Establish
Affected engine: identify
Sees: perform
Practicable

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15
Q

Fire 1 or 2

A

OEI flight condition; establish
Airspeed: reduce if IAS exceeding 100 Kias
Fire switch (affected engine): raise Guard, press
Bot 1/2 pb : Press; bot 1 activate - ext Ind come on
Clock - start after bot I legend and ext Ind go off
Affected engine - identify
Sees : perform
Land as soon as possible
If Fire still on:
Bot 1/2: Press ext Ind go on
Land immediately

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16
Q

XSMN oil Press

A

Power: reduce
Land as soon as Practicable
If both Ind. Below 1.0 bar
Land immediately

17
Q

SEF HOGE

A

Collective lever - adjust to maintain rotor rpm
Airspeed - increase if possible
- forced landing
Landing attitude - establish
Collective - raise as necessary to stop descent or cushion landing
Affected engine - I’d
Sees - perform
- transition to OEI flight
Collective - adjust to Oe limits or below
Rotor speed -trim to max
Airspeed - gain 65 knots
- after reaching safe altitude
Collective - reduce to OEI MCP or below
Affected engine-id
Sees-perform

18
Q

SEF - flight

A

OEI flight condition - establish
Rotor speed _. trim to max
Affected engine-id
Sees - perform

19
Q

Single engine emergency shutdown (sees)

A

Twist grip (affected engine) - rotate slowly to idle (check indications)
Rotor speed - trim to max

20
Q

Engine over speed (governor failure)

A

OE1 flight condition - establish
Var NAR - check Man
N2 trim sw - trim to 101% with matched TQ
- if step 3 not possible-
Affected engine - id
Twist grip - rotate to idle until N2 and NRO stabilize

21
Q

Engine underspeed ( Gov failure )

A

OE1 flight cond.- establish
Bleed air consumers- off
Var NAR - check man
Affected engine- id
N2 trim sw - compensate n2/nro drop and match TQ
-If match tq not possible-
Twist grip (affected engine ) - release stop plate rotate towards flight until n2 match
Sees - perform

22
Q

Double engine emergency shut down

A

Both twist grips - off
Both fuel pumps prime - off
Bat master sw- Off
-In flight -
Both twist grips - off
Both emer off sw- press

23
Q

Autorotation

A

Collective - reduce to maintain NRO within limits
Airspeed - 75 knots
Double engine emergency shutdown - perform
-
-
-
Bat master sw - off

24
Q

Tail rotor Drive/ fixed pitch

A

Collective - reduce to obtain minimum side slip
Airspeed - 70 knots or higher
Shallow approach nose left- perform
Airspeed - reduce close to ground until nose aligned with flight path
Landing - perform
- can’t land -
Airspeed - increase
Approach - abort climb to sufficient altitude to perform auto
Auto-perform