Limitations Flashcards

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1
Q

Internal weight

A

5225 / no ELO w/ internal wgt > 4961

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2
Q

VNE POWER ON

A

155 -3kts per 1000’ PA (-10kts <30° C)

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3
Q

VNE POWER OFF

A

125kts -3kts per 1000’ PA (-20 <20° C)

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4
Q

Min & Max TEMPS

A

-40° C / +50° C

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5
Q

ROTOR SPEED POWER ON. ground flat pitch / in flight

A

380 +/- 5 on ground 375 - 405 in flight

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6
Q

ROTOR SPEED POWER OFF

A

320 -430

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7
Q

ROTOR WARNING HORN

A

360 Low 410 High

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8
Q

FLI MAX CONT

A

9.6

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9
Q

FLI MAX TRANSIENT

A

10.4 for 5 Sec.

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10
Q

FLI TAKEOFF

A

9.6 -10 for 5 minutes

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11
Q

Tq below 40kts continuous

A

100%

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12
Q

Tq below 40kts 5 second transient

A

104%

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13
Q

Tq above 40kts continuous

A

92.7%

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14
Q

T4 MAX FOR ENGINE START

A

750°C

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15
Q

T4 MAX TRANSIENT FOR ENGINE START

A

865°C for 10 sec

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16
Q

MAX T4 ON TAKE OFF

A

915°C

17
Q

MAX CONTINUOUS T4

A

849°C. (below 810 if Ng inop)

18
Q

Ng SPEED MAX TRANSIENT

A

102.3% for 5 Sec. delta +1

19
Q

Ng SPEED MAX TAKEOFF

A

101.1% for 5 min. delta +0

20
Q

Ng SPEED MAX CONT

A

97.1% delta -4

21
Q

Yaw servo control valve siezure (pedal drive) in flight

A

• Airspeed ……………………………..adjust (40-60kts) • Yaw servo hydraulic switch (colective)…..off • Land As Soon As Practical

22
Q

Nf SPEEDS MIN / MAX

A

349 -418

23
Q

ENG OIL PRESS MIN / NORM / MAX STARTING

A

1.1 bar (15.9 psi) min 2-6 bar (29-87 psi) norm 9.8 bar (142.1 psi)max start

24
Q

ENG OIL TEMP MIN/MAX

A

0°C - 115°C

25
Q

Electrical MIN VOLTS FOR START MAX VOLTS

A

15 V min. 31.5 V Max

26
Q

ROTOR BRAKE

A

170 RPM MAX 100 RPM REC 5MIN BETWEEN APPLICATION

27
Q

SLOPES

A

10° nose up. 8° side 6° nose down

28
Q

RUN ON LANDING MAX SPEED

A

40kts

29
Q

X WIND / HEAD WIND

A

40 kts x wind / 50 kts headwind

30
Q

AOH MIN FUEL

A

18 gal

31
Q

MAX NVG HOURS IN ONE DAY

A

4 hrs

32
Q

NVG PROFILES BELOW 500’

A

30° AOB MAX 10KTS MAX

33
Q

TAKEOFF MINS. DAY / NIGHT / NVG TRAINIG

A

1/2 mile clear of clouds DAY. Clear of clouds 500 and 2 NIGHT. 1000 & 3 NVG Training

34
Q

ENGINE FAILURE (CRUISE)

A

● AUTOROTATE…………………….AIRSPEED 65KTS

35
Q

ENGINE FIRE DURING START

A

• START SELECTOR………………off • Fuel shutoff………………close • Rotor brake….. (as necessary)…..engage • Fuel pump………………………….off • Crank switch……………………..engage 10 sec • Master switch ………………….off

36
Q

ENGINE FIRE (IN FLIGHT)

A

• Autorotate • Fuel shutoff……………..close • Generator…………………off • Master Switch…..(if there is a burning smell)……..off