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PH AIRBUS H130T2 > SDH H130T2 Limitations > Flashcards

SDH H130T2 Limitations Flashcards

Airbus H130T2, SDH, Study

1
Q

DISCLAIMER

A

This flash card study aide is provided to ease and assist in studying much more comprehensive material provided by Eurocopter / Airbus. The creator of this study aide accepts no responsibility for inaccuracies or abbreviation of procedures. This is intended to introduce the associated material and all persons using these cards should study and reference the officially distributed material from the manufacturer. It is recommended that after referencing each card, the student should independently verify the information on that card by looking it up and learning the comprehensive information from the direct source. If any inaccuracies, misleading or typo errors are found, please notify the administrator of the study deck.

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2
Q

WHAT IS THE

MINIMUM

PERMISSIBLE WEIGHT FOR FLIGHT?

A

3307 lbs

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3
Q

WHAT IS

THE

MAXIMUM

WEIGHT?

A

5512 lbs

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4
Q

WHAT ARE THE

FORWARD AND

REARWARD CG LIMITS AT

GROSS WEIGHT?

A

Forward = 125

Rearward = 136

(Datum is located 133.8” forward of mast)

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5
Q

ELECTRICAL

CURRENT

LIMITATION

A

31.5v = Maximum Voltage

26 to 29v = Rated Voltage

150 Amps = Maximum Current

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6
Q

MANEUVER

LIMITATIONS

A

Do not exceed load factor causing the limit caution light to come on

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7
Q

ENGINE

OIL

A

Mobile Jet 254

(Average Synthetic

MIL-23699)

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8
Q

SERVO

CONTROL

FLUID

A

Synthetic

MIL-H-83282

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9
Q

THE FOLLOWING ARE FORBIDDEN

A
  • Leaving the controls while the rotor is turning
  • Aerobatic maneuvers
  • Flight in falling snow without optional sand 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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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 operation COMPANY

(Five minutes between rotor brake operation)

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11
Q

MAXIMUM

BAGGAGE (weight) IN

RH BAGGAGE COMPARTMENT?

A

287 lbs

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12
Q

WHEN MUST

ANTI ICE ADDITIVE

BE ADDED

TO FUEL?

A

If the fuel does not contain a freezing inhibitor and if the OAT is below -20 °C, the use of an anti-icing additive is mandatory.

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13
Q

N2

LIMITATIONS

A
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14
Q

WHAT TYPE OF

OPERATION IS THIS AIRCRAFT

APPROVED FOR?

A

DAY AND

NIGHT VFR

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15
Q

FUEL

LIMITATIONS

A
  • JET A
  • JP5
  • JP8

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

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

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16
Q

TAKEOFF POWER

RATING

LIMITED TO:

A

MAX AIRPSEED 40 KIAS

30 MIN CONTINUOUS USE

60 MIN CUMULATED USE PER FLIGHT

USE OF HEATING DEMISTING IS AUTHORIZED UP TO MAX. TOP

17
Q

MANDATORY

EQUIPMENT

REQUIRED FOR FLIGHT

A

TWO adequate radio/audio headsets.

One worn by pilot, second in standby.

Second headset need not be plugged in.

18
Q

CABIN

LOAD

LIMITS

A

FORWARD FLOOR - 893 lbs

REAR FLOOR - 1091lbs

62.5 lbs per square ft

19
Q

SLOPE

LIMITATIONS

A
  • 6° UP
  • 6° DOWN
  • 8° SIDE TO SIDE
20
Q

HOVER

LIMITATION

A

If OAT Over 35ºc, Hover IGE & OGE With Relative RH Wind from 45º to 135º Is Limited To 5 Min for ANY Power Rating and ANY Windspeed Over 5 kt

21
Q

WHAT IS REQUIRED

FOR USE OF AUDIO

HORN SYSTEM?

A

Pilot headset to monitor warning sounds

22
Q

OIL

PRESSURE

LIMITATIONS

A

(Oil pressure has variable limits that depend on N1)

23
Q

TOT

FLIGHT

LIMITATIONS

A
24
Q

TORQUE

LIMITATIONS

A
25
Q

N1

LIMITATIONS

A
26
Q

ENGINE OIL

TEMPERATURE

LIMITATIONS

A

-10°c to 0°c = Caution Range

0ºc Before Power Application

MAX 117°

During the oil warm up period, the engine must be run with the collective pitch control in its full down position. The twist grip can be in “IDLE” or “FLIGHT” position.

27
Q

AIRSPEED

LIMITATIONS

A
  • 155 Knots - Power On
  • 125 Knots - Power Off
  • -3 Kt per 1000’ Hp
  • 100 Knots - All doors Off
  • 70 Knots - Sliding Door Open

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

28
Q

TEMPERATURE

LIMITATIONS

A
  • -40°c for start
  • ISA + 35°c (50°c)
    • 2°c per 1000’ Hp Max
29
Q

ALTITUDE

LIMITATIONS

A

23,000 feet

30
Q

MAXIMUM

BAGGAGE (weight)

IN LH BAGGAGE COMPARTMENT?

A

342 lbs

31
Q

CAN THIS

AIRCRAFT BE

FLOWN IN

FALLING SNOW?

A

YES

WITH SUPPLEMENTAL FILTER

CHECK VISIBILITY REQUIREMENTS IN SUPPLEMENTAL SECTION

32
Q

FUEL

REPLACEMENTS

A

Below 43ºc and below 10000’ Hp

WIDECUT (JP4)

WIDECUT (JET B)

Below 43ºc and below 15000’ Hp

KEROSENE TS 1

KEROSENE RT

33
Q

MAXIMUM

BAGGAGE (weight)

IN REAR CARGO COMPARTMENT?

A

176 lbs

34
Q

TOT

STARTING

LIMITATIONS

A
35
Q

MAIN

(and tail)

GEAR BOX

LUBRICANT

A

Mineral Oil

36
Q

CAN ANYTHING

BE STORED

UNDER THE SEATS?

A

NO

37
Q

EXPLAIN THE

NUMBERS

ON THE FLI

A

COMPANY CRUISE 7.5 FLI

PH AIRBUS H130T2 (3 decks)

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