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H130T2 > Limitations > Flashcards

Limitations Flashcards

1
Q

Power Plant

A

Turbomeca Arriel 2D - MTOP 937 shp MCP 856 shp

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2
Q

5 Modules

A

axial compressor, gas generator, power turbine, reduction g/b, accessory GB/Trans Shaft

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3
Q

Main Rotor Starflex System

A

clockwise rotation, no lube, 3 glass resin blades, flapping thru star arms, lead lag & pitch thru elastomeric components

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4
Q

Tail Rotor Fenestron

A

10 blades shrouded, clockwise rotation viewed from LH

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5
Q

Chip detectors

A

1 eng, 1 trans gb, t/r gb,

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6
Q

Overall Length

A

41.47’

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7
Q

VEMD Prohibited flight

A

flt with VEMD completely shut off

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8
Q

Max Internal GW

A

5512 lbs

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9
Q

Min Internal GW

A

3307 lbs

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10
Q

Max Rear Cabin Floor

A

1091 lbs @ 62.5 psf

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11
Q

Max Load Rear Hold

A

176 lbs @ 30 psf

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12
Q

Max Altitude

A

23,000 Hp

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13
Q

Min ops temp

A

-40 °C ISA

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14
Q

Slopes (Landing & m/r stop limits)Nose UpNose DownSideways

A

6 °6 °8 °

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15
Q

VNE Power On (doors closed)

A

155 Kts @ 0 Hp - 3 kts/1000’

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16
Q

VNE All Doors Removed (√ config AFM)

A

100 kts or VNE all doors closed (lowest value)

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17
Q

VNE Doors Removed (√ config AFM) sliding doors

A

70-110 kts or VNE all doors closed (lowest value)

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18
Q

FLt with doors off/open

A

secure loose objects &belts/remove seat cushions

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19
Q

0 Fuel/Gross/Long C of G in Reduced VNE

A

area of Long C of G,

red VNE power on limit effective for entire flight

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20
Q

VNE Power Off Autorotation Max

A

125 Kts @ 0 Hp -3kt/1000’

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21
Q

Glide Distance in Autorotation

A

.54 nm/1000 ft @ 65 kts &Nr 410 rpm

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22
Q

Best Rate of Climb Speed (Vy) above 100 ft

A

70 kts at SL -1 kt/1000’

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23
Q

Fast Cruise Speed

A

airspeed of first limit (start of FLI amber area)(Tq,N1,TOT)(underlined value)

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24
Q

Best Approach Speed

A

65 kts -70 kts -1 kt/1000’

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25
Q

M/R Nominal Rotor Speed

A

386 rpm

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26
Q

T/R Nominal Rotor Speed

A

3568 rpm

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27
Q

M/R Power On Caution Ranges

A

320-375 rpm

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28
Q

M/R Power Off - Autorotation Min/Max

A

320-430 rpm

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29
Q

High Aural Rotor Horn 310 Hz - Intermittent

A

Nr Above 410 rpm
increase collective to mtn Nr in green
check engine parameters

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30
Q

Rotor Brake Max - high wind rotor speed Rotor Brake

A

170 rpm with engine shut down

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31
Q

FLI Max Cont Rating

A

8.2

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32
Q

TQ Max Cont

A

81.3% Tq

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33
Q

N1 Min Stabilized

A

67%

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34
Q

TOT Max Cont Start

A

750 °C

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35
Q

N2 Min

A

367 rpm

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36
Q

FUEL Capacity

A

100%/540 L/941 lbs

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37
Q

FUEL Types Normal (-40 to +50 C)

A

Jet A, A1, JP5, JP8

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38
Q

Hdy System - RH circuit

A

RH belt driven by engine power drive shaft close to the MGB power input

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39
Q

Engine Oil Max temp

A

117°C

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40
Q

C of G Longitudinal Datum

A

133.8” fwd of m/r head centerline

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41
Q

Electrical Voltage Range

A

26-29 V sys 2

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42
Q

GEN Amp

A

150 Amp Cont/200 Amp continuous

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43
Q

Take Off Profile

A

5’ HIGE CofG Check to 10’ @ 40 kts to 20’ @ 50 kts,

then >100’ @ 65 kts

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44
Q

Winds > 30 kts

A

park into wind/brake on with 1 blade to front, use tiedowns

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45
Q

Noise Level

A

81.1 dB @ .9 Vh (129 kts TAS)

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46
Q

Sand Filter must be OFF

A

in visible moisture and temp

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47
Q

Altitudes and Airspeeds

A

Hp and IAS Land

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48
Q

Flight Forbidden(3) weather related(1) twist grip related(1) vemd related(1) flight related

A

no start with snow/ice in or around engine air intake
no flight in falling snow without sand filter installed
no flight in freezing rain or icing conditions
no inflight engine power reduction using twist grip except for eng fail trg, emerg procedures requiring it, or maint check procedures
no flight with VEMD shut offno aerobatics

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49
Q

Limitation Exceedance

A

Each time an operating limitation is exceeded, an appropriate entry shall be made in the logbook (helicopter, engine, etc.). The entry shall state which limit was exceeded, the duration, the extreme valueattained, and any additional information essential in determining the maintenance action required.

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50
Q

Mandatory Audio

A

2 headsets (1 for pilot & spare to monitor ICS System)

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51
Q

When starting selector switch on check (4)

A

Ng increasingTOT within limits

Rotor turning by 25%EOP increasing

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52
Q

Autorotation Trg Engine Power Loss Indications

A

RH yaw, red warnings, gong, Nr decay, HighNR continuous audio

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53
Q

FADEC FAIL Level 1 YELLOW GOV FLASHING

A

flashing yellow GOV at idle, start/stop seq, no effect on eng control, redunancy loss

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54
Q

Overall Height

A

11.84’

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55
Q

Main Rotor Diameter (3 Bladed Starflex)

A

35.07’

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56
Q

Tail Rotor Diameter (10 blade Fenestron)

A

3.28’

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57
Q

High Skid Width

A

7.57’

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58
Q

High Skid Length

A

10.48’

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59
Q

VEMD Red Line

A

safety limit or takeoff limitation

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60
Q

VEMD Green line

A

normal ops range

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61
Q

VEMD Red with white hatching

A

VNE power off

62
Q

VEMD Yellow line

A

caution or takeoff rating range

63
Q

VEMD White Triangle

A

equipment ops limit

64
Q

VEMD Red Triangle

A

Transient limit

65
Q

VEMD YELLOW underlined

A

parameter is in caution or MTOP range

66
Q

VEMD RED underlined and flashing

A

parameter at or above safety limit or MTOP range

67
Q

VEMD At N1 > 60%

A

VEMD upper screen switches to FLI display

68
Q

VEMD operating time

A

counted from Ng > 60% until Ng

69
Q

VEMD At end of flight check advisory messages

A

failure or overlimit detected

70
Q

Max Forward Cabin Floor

A

893 lbs @ 62.5 psf

71
Q

Max Left Cargo Hold

A

342 lbs @ 62.5 psf

72
Q

Max Right Cargo Hold

A

287 lbs @ 62.5 psf

73
Q

Max ops temp

A

+35 °C limited to +50 °C

74
Q

Economic Cruise Speed

A

set Tq to 10% less than MCP Tq

75
Q

Turbulence Airspeed

A

reduce IAS in turbulence

76
Q

M/R Power On Normal ops range

A

375-405 rpm

77
Q

M/R Power On Caution Ranges

A

405-430 rpm

78
Q

High Aural Rotor Horn 310 Hz - Continuous

A

Nr Below 360 rpm
decrease collective to mtn Nr in green
check engine parameters

79
Q

Low Aural Rotor Horn 285 Hz - Continuous

A

after 1.5 sec if power remains in transient range
immediately when transient power limits are exceeded
immediately when max transient rating is or will be exceeded during fast power increase

decrease collective to mtn pwr in limits
check engine parameters

80
Q

Rotor Brake - normal rotor speed

A

140 rpm with engine shut down

81
Q

Min time between R/B application

82
Q

FLI Takeoff Power Rating

83
Q

FLI Max Takeoff Rating

84
Q

FLI Max Transient (max 5 sec)

A

10.4 max 5 sec

85
Q

FLI Use of heat/demist authorized

A

up to max Take off power

86
Q

TQ Takeoff Power (Airspeed

A

81.3% - 100% Tq

87
Q

Takeoff Power (Airspeed

A

30 min continuous use max 60 min per flight

88
Q

Heating and demisting authorized

A

up to max TOP

89
Q

TQ Max Takeoff Rating

90
Q

TQ Transient

A

104% max 5 sec

91
Q

TQ SHP

A

598 kW @ 386 Nr

92
Q

Tq on power up

A

Tq indicates 89.5% for 2 sec then 0

93
Q

N1 Max Cont

A

∆N1 = -4%

94
Q

N1 Take Off Power Range

A

∆N1 = -4% to 0%

95
Q

N1 Max Take Off Power Rating

A

∆N1 = 0%

96
Q

N1 Max Transient (20 sec)

A

∆N1 = +1% max 20 sec

97
Q

100% N1 corresponding Ng rpm

98
Q

TOT Max Transient Start (10 sec)

A

840 °C / 10 sec

99
Q

TOT Max Cont Flight

100
Q

TOT Max Cont Take Off Power Range

A

905-949 °C

101
Q

TOT Max Take Off

102
Q

TOT Max Transient (20 sec)

A

981 °C max 20 sec

103
Q

N2 Normal ops

A

367-413 rpm

104
Q

N2 Max cont max

105
Q

N2 Transient max 20 sec

A

440 rpm max 20 sec

106
Q

Nr of 385.8 rpm corresponding N2 speed

107
Q

FUEL Useable (indicated by 10 on fuel guage)

A

99.6%/538 L/937 lbs

108
Q

FUEL Unusable (0 on guage)

A

0.4%/2 L/2.2 lbs

109
Q

FUEL Consumption

A

33%/Hr; 180 Lph

110
Q

Low Level Fuel Warning (yellow line)

A

11%/104 lbs/60 L

111
Q

Low Level Fuel Warning (yellow line) Time

A

15 min @ MCP at start of this range

112
Q

Anti-ice additive mandatory

A

freezing inhibitor required below -20 C

113
Q

Fuel Types Replacement (

A

Jet B, JP4

114
Q

Fuel Mixing

A

most restrictive limitation applies

115
Q

Hdy System - LH circuit

A

LH driven by MGB front accessory mechanical output

116
Q

Engine Oil Min oil temp for ops

A

0°C (oil 5 cSt) or -10 °C (oil 3.9 cSt)

117
Q

Engine Oil Warmup

A

eng run with coll full down, twist grip in idle or flight

118
Q

Engine Oil Cooldown

119
Q

C of G LateralDatum

A

in the plane of symmetry of the helicopter

120
Q

Electrical VoltageMax

121
Q

Electrical Voltage Max Current

A

150 Amp Cont (200 amp if OP-3821 installed)

122
Q

Electrical Voltage Min on Start

123
Q

Electrical Voltage Emerg Shed

A

all DC pwr off except NR/N2 ind, map/com lites, fadec start/stop switch, intercom, trspdr, radios, Inst lite

124
Q

Ground Power Unit

A

28 Vdc max 600A

125
Q

Winds > 40 kts

A

heli must be tied down

126
Q

In windy conditions on start

A

add little cyclic into windandwhen N1>67%, twist grip to FLIGHT position

127
Q

In windy conditions on shutdown

A

cool eng with twist grip in FLIGHT position

128
Q

WARNING

A

failure to follow procedure could cause injury or loss life

129
Q

CAUTION

A

failure to follow procedure could cause damage to heli

130
Q

NOTE

A

ops procedure essential to highlight

131
Q

SHALL

A

procedure is mandatory

132
Q

SHOULD

A

procedure is recommended

133
Q

MAYor NEED NOT

A

procedure is optional

134
Q

WILL

A

indicates future event or action (not mandatory)

135
Q

Land Immediately Land

A

Land Immediately

136
Q

LAND ASAP

A

Urgent - Land at the nearest landing siteat which a safe landing can be made

137
Q

Land ASAPL

A

Non-Urgent - proceed to the nearest airfield where assistance can be expected

138
Q

Continue Flight

A

continue flight

139
Q

Audio Intercom Fail Safe in case of ICS failure

A

pilots headset and mic defaults to COM 1 audio warnings available through pilot headset only

140
Q

Co Pilot Seat Belts

A

must be fastened at all times

141
Q

RH Inner Knob on ICS

A

RH Inner Knob in is pilot ics volume,

pull out for passenger ics volume

142
Q

At Ng > 60% VEMD upper screen

A

switches to FLI display

143
Q

Autorotation TrgTwist Grip idle to flight

A

idle to flight at any time for any Nr value

144
Q

Autorotation Trg shall be conducted within

A

gliding distance of a suitable running landing area

145
Q

Autorotation Trg Procedure
at 70 ft with Nr in the Green
at 20 ft

A

Reduce Collective,
Twist to Idle (gong & eng audio@ 68% N1 idle)
Twist grip to flight, mtn Nr in Green, flare
inc coll to reduce r of d and fwd speed
cyclic slight fwd in ldg attitude, pedal & Coll as req

146
Q

FADEC FAIL Level 2 STEADY RED

A

steady Red GOV, degraded eng controlor backup system out of neutral position,eng control & monitoring may be degraded

147
Q

FADEC FAIL Level 3 STEADY YELLOW

A

total FADEC FAIL,FADEC metering valve frozen at last computed value, backup system activated,auto start impossible

148
Q

FUEL GOV backup system STEADY RED &YELLOW

A

RED & YELLOW GOV
backup gov takes control of engine fuel flow
EBCAU controls N2 between 388 &400 rpm

149
Q

LAND AS SOON AS POSSIBLE

A

Emergency conditions are urgent and require landing at the nearest landing site at which a safe landing can be made.

150
Q

LAND AS SOON AS PRACTICABLE

A

Emergency conditions are less urgent and in the pilot’s judgment, he may proceed to the nearest airfield where he can expect appropriate assistance.

151
Q

CONTINUE FLIGHT

A

CONTINUE FLIGHT Continue flight as planned.Repair at the destination according to the maintenance manual.

152
Q

LAND IMMEDIATELY

A

LAND IMMEDIATELY Self explanatory.

H130T2 (4 decks)

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