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EMB 120 > Limitations > Flashcards

Limitations Flashcards

1
Q

General

Minimum External Temperature

A

-54°C

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2
Q

General

Maximum External Temperature

A

+38°C

With air condition functioning

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3
Q

General

Maximum Operating Altitude

Bleeds OPEN

A

EEC ON: 32,000 ft
EEC OFF: 25,000 ft

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4
Q

General

Maximum Operating Altitude

Bleeds COSED

A

EEC ON: 25,000 ft
EEC OFF: 20,000 ft

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5
Q

General

Above what altitude EEC must be OFF for takeoff and landing

A

8,000 FT

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6
Q

Genaral

What is the maximum takeoff and landing altitude

A

10,000 ft

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7
Q

Genaral

What is the maximum runway slope

A

+/- 2°

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8
Q

Genaral

Maximum Ramp Weight

MRW

A

26,609 lb

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9
Q

Genaral

Maximum Takeoff Weight

MRW

A

26,433 lb

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10
Q

Genaral

Maximum Landing Weight

MLW

A

25,794 lb

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11
Q

Genaral

Maximum Zero Fuel Weight

MZFW

A

24,030 lb

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12
Q

Speed

Maximum DV window seeped

A

140 KIAS

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13
Q

Autopilot

Minimum speed with autopilot ON

One Engine

A

120 KIAS

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14
Q

Speed

Maximum turbulence penetration seeped

Vb

A

175 KIAS

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15
Q

Speed

Maximum tire speed

A

165 KIAS

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16
Q

Electrical

Starter duty cycle

A

30s ON: 3min OFF
30s ON: 3min OFF
30s ON: 30min OFF

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17
Q

Pressurization

Maximum Differential Pressure

A

7.2 PIS

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18
Q

Pressurization

Normal Differential Pressure

A

7 PSI

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19
Q

Fuel

Total Fuel

A

5,732 lb

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20
Q

Fuel

Maximum Usable Fuel per wing

A

2,886 lb

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21
Q

Fuel

Unusable Fuel in each wing

A

24 lb

Add 76.9 lb when main ejectror pump inop

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22
Q

Fuel

Maximum demonstrated fuel imbalance

A

600 lb

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23
Q

ICE

When can leading edge deicers be activated during takeoff

A

At final segament speed

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24
Q

ICE

Atmospheric icing condition exists when

A

Indicated OAT during ground operations or TAT in flight is 10°C or below and visible moisture in any form is present

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25
Q

ICE

Ground icing condition exists when

A

Indicated OAT during ground operations is 10°C or below and visible moisture, standing water, slush, ice, snow, is present on ramps, taxiways, or runways

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26
Q

ICE

In icing condition use of flaps is restricted to what flight conditions

A

Takeoff, approach and landing only

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27
Q

ICE

When flaps have been extended they may not be retracted unless

In flight icing condition

A

The uppers surface of the wing aft of the protected area is clear of ice, or unless flap retraction is essential for go-arounds

28
Q

ICE

All wing inspection lights must be operational prior to flight in

A

Known icing at night

29
Q

ICE

Both stall warning systems must be operative prior to

A

Flight into known icing

30
Q

ICE

When ice protection is detecting ice and/or the deice boots are activated what indication is unreliable

A

Fast/slow

31
Q

AUTOPILOT

The Autopilot and Yaw Damper must be off

All flight conditions

A

Takeoff and landing

32
Q

AUTOPILOT

Minimum Altitude for Autopilot/Yaw Damper on ILS coupled approaches

A

200 ft AGL

33
Q

GENERAL

Required Flight Crew

A

Pilot and Copilot

34
Q

GENERAL

Kinds of Opeartions

A

VFR, IFR, FIKI

35
Q

GENERAL

Maneuvering Load Factors Limits

A

Flaps up: +2.8G/-1.0G
Flaps down: +2.0G/-0G

36
Q

GENERAL

Condition lever position during all ground opeartions

Exept when cleard for takoff or during landing roll

A

MIN RPM

37
Q

Genaral

Power Levers must be in what position during all ground operations

Exept for breif excursions as needed to maneuver the airplane

A

GROUND IDLE

38
Q

SPEED

Maximum speed for windshield operations

A

160 KIAS

39
Q

SPEED

Vmo/Mmo

A

272 KIAS/0.52 MACH

40
Q

SPEED

Va

A

200 KIAS

41
Q

SPEED

Vle/Vlo

A

200 KAIS

42
Q

SPEED

Vfe

A

200 KAIS
150 KIAS
135 KIAS

43
Q

GENERAL

Max Demonstrated Crosswind

A

30 KIAS

44
Q

GENERAL

Maximum Tailwind Speed Takeoff and Landing

Gear and Flaps Up

A

10 KIAS

45
Q

SPEED

Minimum Speed in Icing Conditions

Gear up Flaps 15°

A

165 KIAS

46
Q

APU

Operations above what altitude is permitted only with APU bleed extraction set to both air conditioning packs

APU limitation

A

16,000 ft

47
Q

APU

APU maximum speed and altitude

For starting

A

200 KAIS
20,000 ft

Airspeed may vary with altitude

48
Q

APU

APU maximum operating temperature

APU limitation

A

Up to 16,000 ft: +38°
Above 16,000 ft: +35°

49
Q

APU

APU maximum allowable EGT during start

During Start

A

732°C

EGT above 732°C to a max of 947°C are limited to 10 seconds only

50
Q

ELECTRICAL

Maximul Load per MAIN genrator

A

Up to 27,000 ft: 400 AMPS
Above 27,000 ft: 380 AMPS

51
Q

ELECTRICAL

Maximum Laod per AUX generator

A

Up to 18,000 ft: 150 AMPS
Above 18,000 ft: 140 AMPS

52
Q

APU

Maximum Load per APU generator

A

ISA below 35°C
Up to 16,000 ft: 400 AMPS
Above 16,000 ft: 290 AMPS
ISA above 35°C
Up to 16,000 ft: 400 AMPS
Above 16,000 ft: 280 AMPS

53
Q

ELECTRICAL

Maximum Battery temperature

A

70°C

54
Q

FUEL

Fuel Used

A

JET A, JET A-1,*JET B
QAV 1, *QAV 4
*JP 4, JP 5, JP 8

* Emergency only

55
Q

Aviation gasoline may be used in an emergency up to a limit of

A

150 hours between overhauls

56
Q

ICE

When ground or athmospheric icing condition exists or at the first sign of ice accretion enywhere on th airplane or ICE DETECTOR ilght is illuminated, turn ON the following ice protection swithces

A

AOA, TAT, Slip, Engine Air Inlet, Ignition, Propeller, Leading Edge Deicer, Windshield Heat

57
Q

SPEED

Bird impact speed

A

250 KIAS below 8,000 ft

58
Q

GEMERAL

PROP SYNC must be off

Flight condition

A

For Takeoff and Landing per airworthiness directive

59
Q

FUEL

When fuel quatity indicator reads what indication in level flight, any fuel ramining in the tank cant be used safetly in flight

A

Zero

60
Q

ICE

Continuous ignition must be used during the following conditions

A

Takeoff and landings on contaminated runways
Takeoffs with inoperative EEC
Flight trough moderate or greater rain
Flight trough known or forecasted icing

61
Q

GENERAL

Zone Weight Limits

A

Zone 1-3: 2,600 lb.
Zone 4: 1,213 lb.

62
Q

FUEL

Minimum oil pressure to ensure intake deicing and to prevent fuel icing

A

45°C

63
Q

ICE

Minimum Nh required for operations of the pneumatic deicing system

A

80%

64
Q

ICE

The propeller blades may be heated only when the oil pressure is above

A

40 PSID

65
Q

GENERAL

Operation id oil pressure is below what PSID is not permitted

A

40 PSID

EMB 120 (22 decks)

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