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zz emb-120 braz > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum Takeoff Weight (MTOW)

A

11,990 Kgs

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2
Q

Maximum Landing Weight (MLW)

A

11,700 Kgs

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3
Q

Maximum Zero Fuel Weight (MZFW)

A

10,900 Kgs

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4
Q

Maximum Ramp

Weight (MRW)

A

12,070 Kgs

Company use 12,040 Kgs

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5
Q

Maximum Turbulent Air Penetration Speed

A

175 KIAS

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6
Q

Restriction on Power Levers-Ground Operations

A

At or Below FLT Idle, brief excursions (Up TO 5sec) for maneuver

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7
Q

VMO

A

Below A080 250 KIAS
Between A080 and FL130 272 KIAS
Above FL130 M 0.52

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8
Q

MMO

A

0.52 M

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9
Q

Condition Levers must be in _________ position during all ground operations except when cleared for takeoff or landing roll

A

MIN RPM POSITION

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10
Q

APU maximum operating temperature (OAT)?

A

ISA+ 38C

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11
Q

Aviation Gasoline may be used in emergency for up to a limit of _______ hours between overhauls

A

150 hours

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12
Q

APU max allowable EGT during steady state operation?

A

680 C ( 680 - 732 permitted for up to 5 mins)

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13
Q

Maximum Tire Speed

A

165 KIAS

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14
Q

Maximum Operating Altitude, EEC ON

-engine bleed open/closed

A

Bleed Open 32,000

Bleed Closed 25,000

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15
Q

Maximum Operating Altitude, EEC OFF

-engine bleed open, closed

A

Bleed Open 25,000

Bleed Closed 20,000

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16
Q

With Engine Bleeds CLOSED and the only source of bleed air is the APU the maximum operating altitude is? (2)

A

Dual packs FL200

Single pack 10,000

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17
Q

Maximum demonstrated imbalance between L and R wings fuel tanks is? (lbs)

A

600lbs

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18
Q

Maximum takeoff and landing pressure altitude?

A

10,000 Press Alt, above 8000 PA EEC must be OFF

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19
Q

Runway Slope limit?

A

+/- 2% runway length

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20
Q

Cabin Pressurization Absolute Max Differential and Max Normal Differential?

A

Absolute Max 7.2 psid

Normal Max 7.0 psid

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21
Q

Main Gen Max Load

A

Below FL270 400 amps .
Above FL270 OR 380 amps
hotter than ISA + 27 on GRD

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22
Q

Maximum Load per Auxiliary Generator?

A

Below FL180 150 amps

Above FL180 140 amps

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23
Q

APU Generator max loads?

A

Below FL160 400 amps

Above FL160 290 amps

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24
Q

If the main ejector boost pump is inoperative you add ____ to the unusable fuel in the corresponding wing?

A

79.6 lbs /

46 ltr

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25
Q

Maximum Battery Temp?

A

70 C

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26
Q

Oxygen System duration with 30 passengers

A

00:50 min

Initial Px 1850 psi

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27
Q

Maneuvering Load Limits?

A
  • 1.0 to +2.8 Flaps Retracted

0. 0 to +2.0 Flaps Extended

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28
Q

V-wiper

A

160 KIAS

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29
Q

Minimum NH for operation of pneumatic deice system?

A

80% NH

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30
Q

Flight in Icing Conditions

Speed-Clean?

A

165 KIAS, All engines

160 for alarm

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31
Q

VA

A

200KIAS

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32
Q

Do we need all wing inspection lights operative to fly into icing conditions at night?

A

YES

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33
Q

Do one or both stall warning systems need to be operative prior to flight into icing conditions?

A

Both

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34
Q

APU Max starting EGT?

Garret Model

A

974 C

(732-974 C for 10 seconds max)

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35
Q

VFE 15

A

200KIAS

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36
Q

VFE 25

A

150 KIAS

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37
Q

VFE 45

A

135 KIAS

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38
Q

VLE / VLO

A

200 KIAS

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39
Q

VMCG

A

94KIAS

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40
Q

VMCA

A

97KIAS

41
Q

Maximum Tailwind

A

10 kts

42
Q

Max Reverse is NOT approved for?

A

Wet runway with areas of Standing water, due possible water ingestion

43
Q

Maximum Usable Fuel Quantity in EACH wing?

A

2866 lbs / 1628 ltr

44
Q

Unusable Fuel Quantity EACH wing?

A

24 lbs / 14 ltr

45
Q

Start T6

A

950 C
816-850 C (20 Secs)
850-950 C (5 Secs)

46
Q

Max Takeoff T6

A

Up to 816 C for 5 Mins

47
Q

Max Continuous T6

A

800 C

48
Q

Transient T6

A

850 C (Up to 850 C for 20 Secs)

49
Q

Max Continuous / Takeoff Torque

A

100% / up to 110% for 5 Mins

50
Q

Max Climb/Cruise Torque

A

84%

51
Q

Transient Torque

A

120% ( 20 Secs )

52
Q

Takeoff Np

A

100.0 - 101.0 %

53
Q

Max Climb/Cruise Np

A

100.0 - 101.0 %

54
Q

Max Reverse Np

A

80.5%

55
Q

Transient Np

A

110.0% ( 20 Secs)

56
Q

Ground Nh

A

62.0% MIN

57
Q

Takeoff/Continuous Nh/NL

A

102.0%

58
Q

Max Climb/Cruise Nh/NL

A

100.0%

59
Q

Start Oil Temp

A

-40 C MIN

60
Q

Max Climb/Cruise Oil Temp

A

115 C

61
Q

Min Medical Oxygen Pressure

A

1500 psi for Op’s above FL250

62
Q

Transient Oil Temp

A

115 C - 125 C (15 Mins MAX)

63
Q

Start Oil PX

A

70 psi MAX

64
Q

Ground Idle Oil PX time limitations

A

40 Min

OPS Between 40 - 55 Only if Nh is below 75%

65
Q

Takeoff/Max Continuous Oil PX

A

65 psi

66
Q

Transient Oil PX

A

40 psi - 70 psi

67
Q

MAX Operating Temp (OAT)

A

ISA +35 C Aircon working
ISA +20 C Aircon NOT working
(ALT Alert OFF / Radio mast ON)
ISA +15 C Aircon NOT working
(ALT Alert ON)
*May use ISA +20 for up to 30 mins Radio Mast ON
(except Start)
Aircon maybe turned OFF for up to 2 mins without limitation for T/Off and LDGing

68
Q

APU Air start speeds

A

Not Less than 135 Kts
Max 240 Kts @ 5000
decreasing to
Max 210 Kts @ FL200

69
Q

APU Air-start Altitudes

A

Min ALT 1000’

Max ALT FL200

70
Q

Starter Duty Cycle limits

A

1st Cycle 30 sec ON 3 min OFF
2nd Cycle 30 sec ON 3 min OFF
3rd Cycle 30 sec ON 30 min OFF

71
Q

MIN Operating Temp (OAT)

A

-54 C

72
Q

Flight Crew

A

2 Crew, Pilot and Co pilot

73
Q

Kinds of Operations

A

VFR / IFR / Icing Conditions / Category II

74
Q

Landing above “Quick turn around WGT”

A

Delay T/Off for at least 26 mins

75
Q

Flight in Icing Conditions

Speed- flaps 15 and gear up?

A

140 KIAS, All engines

76
Q

Maximum Allowable Cruise Power (1305 SHP)

A

100%Np - 72% Tq
90% Np - 80% Tq
85% Np - 84% Tq

77
Q

Minimum Oxygen PSI for dispatch

A

Main 4 Crew / 30 PAX 1470 psi
3 Crew / 30 PAX 1300 psi
Attendant Portable 1200 psi

78
Q

Maximum Negative cabin Pressure

A
  • 0.3 psid
79
Q

Air cond / Press Cabin Pressure

A

Sea Level - 16,800 Sea Level

16,800 - 32,000 - Cabin Alt up to 8000’

80
Q

Engine bleeds ______ on Take Off

A

Engine bleeds LOW, maybe closed if APU on / wet or gravel RWY

81
Q

Max Operating ALT with one pack

A

FL250

82
Q

Min ALT for Autopilot / Yaw dampener Engagement

after T/Off

A

500’ AGL

83
Q

Min airspeed for Autopilot / Yaw dampener

2 engines

A

110 KIAS

84
Q

Min airspeed for Autopilot / Yaw dampener

OEI - single engine

A

120 KIAS

85
Q

Min ALT for Autopilot / Yaw dampener

Coupled ILS approach

A

200’ AGL

86
Q

Min ALT for Autopilot / Yaw dampener

Non precision approach

A

50’ Below MDA

87
Q

Min ALT for Autopilot / Yaw dampener

All other approaches

A

500’ AGL

88
Q

Use of Flaps in known icing conditions

A

Restricted to T/Off, App & Landing. Must not be retracted unless upper wing clear of ice or required for Go Around

89
Q

Use of Leading edge deicers during Take Off into known icing conditions

A

Use of the leading edge deicers delayed until reaching Vfs (final segment speed)

90
Q

Atmospheric icing conditions exist when

A

OAT or TAT less than 10 C and visible moisture present

91
Q

Max Baggage Weight

A

Overall 550 Kg
Section 1 - 550 Kg
Section 2 - 258 Kg
*Together can’t exceed 550 Kg

92
Q

Loss Of LEFT Hydraulic System

A 
GREEN GROOMS LEFT
Gear doors
Rudder 1
Outboard Flaps
Outboard Brakes
Main Door
Steering (nosewheel)
93
Q

Loss Of RIGHT Hydraulic System

A 
BLUE FIRE RIGHT
F Inboard Flaps
I Inboard Brakes
Rudder 2
Emergency braking
94
Q

EMERGENCY MODE, requirements

A

Atleast one Main Generator switched on
Power source selected to BATTERY
Loss of BOTH MAIN GENERATORS

95
Q

EMERGENCY MODE, Causes Loss Of

A 
F - Fuel 
A - Autopilot
C - COMMS 2
E - Engine Instruments (except T6 & Tq)
F - Flaps
L - Landing Light
A - Anti-Skid
P - Pressurization
96
Q

Manoeuvring Speed

Clean

A

Min 160

Target 180

97
Q

Manoeuvring Speed

Flap 15

A

Min 140

Target 150

98
Q

Manoeuvring Speed

Flap 25

A

Min 130

Target 135-140

99
Q

Manoeuvring Speed

Flap 45

A

120

zz emb-120 braz (6 decks)

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