SDH EC130B4 Limitations Flashcards

SDH EC130B4 checkride study (39 cards)

1
Q

THE FOLLOWING ARE FORBIDDEN

A
  • Leaving the controls while the rotor is turning
  • Aerobatic maneuvers
  • Flight under falling snow (deleted because of Intec Filter)
  • Flight in freezing rain or icing conditions
  • In flight engine power reduction using twist grip control except for engine failure training
  • In flight, intentional VEMD complete shut-off
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2
Q

WHAT IS THE GROSS WEIGHT?

A

5350 lbs

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3
Q

WHAT IS THE MINIMUM PERMISSIBLE WEIGHT FOR FLIGHT?

A

3307 lbs

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4
Q

WHAT ARE THE FORWARD AND REARWARD CG LIMITS AT GROSS WEIGHT?

A

Forward = 124

Rearward = 140

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5
Q

AIRSPEED LIMITATIONS

A
  • 155 Knots - Power On
  • 125 Knots - Power Off
  • 70 Knots - Doors Off
  • 70 Knots - Sliding Door Open
  • -3 kias per 1000 Hp

(See chart in section 2 for airspeed/door open combinations)

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6
Q

ALTITUDE LIMITATIONS

A

RFM

23,000 feet

With Crash Resistant Fuel Tank

17,000 feet

If equiped with Airframe Fuel Filter

15,000 feet

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7
Q

TEMPERATURE LIMITATIONS

A
  • -20°c for start
  • 0°c before power application
  • ISA + 35°c (50°c)
    • 2°c per 1000’ DA Max
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8
Q

SLOPE LIMITATIONS

A
  • 6° UP
  • 6° DOWN
  • 8° SIDE TO SIDE
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9
Q

MANEUVER LIMITATIONS

A

Do not exceed load factor causing the limit caution light to illuminate

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10
Q

MAIN ROTOR RPM LIMITATIONS

A
  • 320 rpm Minimum for power-off
  • 320 to 375 rpm Caution range
  • 375 to 405 Normal operating range
  • 405 to 430 rpm Caution range
  • 430 rpm Maximum power-off
  • 170 rpm Rotor Brake operation HIGH WIND
  • 140 rpm Rotor Brake operation NORMAL
  • 100 rpm Rotor Brake Company

(Five minutes between rotor brake operation)

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11
Q

EXPLAIN THE NUMBERS ON THE FLI

A
  • 9.6 = Maximum Continuous
  • 9.6 to 10.0 = Takeoff Rating
  • 10 = Maximum Takeoff Rating
  • 10.4 = Maximum Transient Rating (5 Seconds)
  • (Company Cruise 9.0)
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12
Q

TORQUE LIMITATIONS

A

FLI 9

92.7 = Maximum Continuous

92.7 - 100 = Takeoff Rating below 40 knots

100% Maximum Takeoff Rating Torque

104% Maximum Transient Rating (5 Seconds)

Delta NG = -4 Maximum Continuous Rating

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13
Q

NF LIMITATIONS

A

349 Minimum rpm

349 - 418 Normal rpm

418 Maximum Continuous rpm

450 Maximum Transient rpm (5 Seconds)

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14
Q

NG LIMITATIONS

A

FLI 9

67% = Minimum

(Delta NG -4) 97.1% = Maximum Continuous Rating

100% = Takeoff Rating

(Delta NG 0) 101.1% = Maximum Takeoff Rating

1% Maximum Transient Rating (5 Seconds)

(Delta NG +1) (102.3% = Maximum Transient Rating)

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15
Q

T4 LIMITATIONS

A

STARTING

  • 750c Maximum Continuous
  • 865c Maximum Transient (10 Seconds)

FLIGHT

  • 849c Maximum Continuous Rating
  • 849c - 915c Takeoff Rating Range (no time limit)
  • 915c Maximum Takeoff Range
  • 941c Transient (20 Sec)
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16
Q

OIL TEMPERATURE LIMITATIONS

A

-10°c to 0°c = Caution Range

115°c = Maximum Oil Temperature

17
Q

OIL PRESSURE LIMITATIONS

A

1.1 bar minimum at 70% NG

1.1 to 2 bar = Caution Range

2 to 6 bar = Normal Range

6 to 9.8 bar = Caution Range

9.8 bar Maximum Pressure

18
Q

ELECTRICAL CURRENT LIMITATION

A

31.5v = Maximum Voltage

26 to 29v = Rated Voltage

150 Amps = Maximum Current

19
Q

FUEL LIMITATIONS

A
  • JET A
  • JP4
  • JP5
  • JP8
  • KEROSENE

OAT range for using fuel is: -40ºc to +50ºc

Below -20ºc, anti ice additive (Prist) is mandatory for fuels which do not contain it.

With Robertson crash resistant fuel tanks prist must be added at 0°c

20
Q

FUEL REPLACEMENTS

A

Below 25ºc and below 5000’ Hp

WIDECUT (JP4)

WIDECUT (JET B)

Below 40ºc and below 15000’ Hp

KEROSENE TS 1

KEROSENE RT

21
Q

MAIN GEAR BOX LUBRICANT

22
Q

MAXIMUM BAGGAGE IN RH BAGGAGE COMPARTMENT?

23
Q

MAXIMUM BAGGAGE IN LH BAGGAGE COMPARTMENT?

24
Q

MAXIMUM BAGGAGE IN REAR CARGO COMPARTMENT?

25
WHAT IS REQUIRED FOR USE OF AUDIO HORN SYSTEM?
Pilot headset to monitor warning sounds
26
MANDATORY EQUIPMENT REQUIRED FOR FLIGHT
TWO adequate radio/audio headsets. One worn by pilot, second in standby. Second headset need not be plugged in. Baggage door must be locked unless three latch system installed
27
WHAT TYPE OF OPERATION IS THIS AIRCRAFT APPROVED FOR?
DAY AND NIGHT VFR
28
CAN THIS AIRCRAFT BE FLOWN IN FALLING SNOW?
CHECK VISIBILITY REQUIREMENTS IN SUPPLEMENTAL SECTION IF FILTER INDICATES CLOGGING FOLLOW EP **LAND AS SOON AS POSSIBLE**
29
CAN P2 BLEED AIR BE USED WHEN ABOVE ENGINE MAXIMUM CONTINUOUS RATING?
NO (Shut off heater and de-mist)
30
YELLOW ZONE ON FUEL GAUGE
15.8 Gallons Remaining 15 Minutes Flight Time at MCP With Crash Resistant Fuel Tank Approx 18 Gallons 18 Minutes Flight Time at MCP
31
DOES THE FUEL GAUGE YELLOW ZONE INCLUDE NON-USABLE FUEL?
NO
32
FUEL CELL CAPACITY and (Usable Amount)
143 Gallons (142.7 Usable) With Crash Resistant Fuel Tank 144 Gallons (141.2 Usable)
33
CAN ANYTHING BE STORED UNDER THE SEATS?
NO
34
LIST DIFFERENT WARNING SOUNDS
GONG - When a red warning appears on panel CONTINUOUS HORN - When NR is below 360 rpm, When maximum takeoff limits are exceeded for more than 1.5 seconds INTERMITTENT HORN - NR above 410 rpm
35
MAXIMUM WIND FOR STARTING AND STOPPING ROTOR
40 knots from any direction 50 knots for direct headwind
36
CAN PILOT PERFORM AN EBCAU CHECK DURING FLIGHT OR ON THE GROUND?
NO
37
IS OUR GARMIN ACCEPTABLE FOR IFR FLIGHT?
NO, VFR only
38
TURBOMECA ARRIEL 2B1 Power Rating
847 SHP (through reduction derated to) 747 SHP (MTOP) 728 SHP (MCP)
39
MAXIMUM TEMP FOR HOT AIR DE-ICE
80c