Limitations

Question 1

General

Minimum External Temperature

Answer 1

-54°C

Question 2

General

Maximum External Temperature

Answer 2

+38°C

With air condition functioning

Question 3

General

Maximum Operating Altitude

Bleeds OPEN

Answer 3

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

Question 4

General

Maximum Operating Altitude

Bleeds COSED

Answer 4

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

Question 5

General

Above what altitude EEC must be OFF for takeoff and landing

Answer 5

8,000 FT

Question 6

Genaral

What is the maximum takeoff and landing altitude

Answer 6

10,000 ft

Question 7

Genaral

What is the maximum runway slope

Answer 7

+/- 2°

Question 8

Genaral

Maximum Ramp Weight

MRW

Answer 8

26,609 lb

Question 9

Genaral

Maximum Takeoff Weight

MRW

Answer 9

26,433 lb

Question 10

Genaral

Maximum Landing Weight

MLW

Answer 10

25,794 lb

Question 11

Genaral

Maximum Zero Fuel Weight

MZFW

Answer 11

24,030 lb

Question 12

Speed

Maximum DV window seeped

Answer 12

140 KIAS

Question 13

Autopilot

Minimum speed with autopilot ON

One Engine

Answer 13

120 KIAS

Question 14

Speed

Maximum turbulence penetration seeped

Vb

Answer 14

175 KIAS

Question 15

Speed

Maximum tire speed

Answer 15

165 KIAS

Question 16

Electrical

Starter duty cycle

Answer 16

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

Question 17

Pressurization

Maximum Differential Pressure

Answer 17

7.2 PIS

Question 18

Pressurization

Normal Differential Pressure

Answer 18

7 PSI

Question 19

Fuel

Total Fuel

Answer 19

5,732 lb

Question 20

Fuel

Maximum Usable Fuel per wing

Answer 20

2,886 lb

Question 21

Fuel

Unusable Fuel in each wing

Answer 21

24 lb

Add 76.9 lb when main ejectror pump inop

Question 22

Fuel

Maximum demonstrated fuel imbalance

Answer 22

600 lb

Question 23

ICE

When can leading edge deicers be activated during takeoff

Answer 23

At final segament speed

Question 24

ICE

Atmospheric icing condition exists when

Answer 24

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

Question 25

# ICE Ground icing condition exists when

Answer 25

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

Question 26

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

Answer 26

Takeoff, approach and landing only

Question 27

# ICE When flaps have been extended they may not be retracted unless | In flight icing condition

Answer 27

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

Question 28

# ICE All wing inspection lights must be operational prior to flight in

Answer 28

Known icing at night

Question 29

# ICE Both stall warning systems must be operative prior to

Answer 29

Flight into known icing

Question 30

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

Answer 30

Fast/slow

Question 31

# AUTOPILOT The Autopilot and Yaw Damper must be off | All flight conditions

Answer 31

Takeoff and landing

Question 32

# AUTOPILOT Minimum Altitude for Autopilot/Yaw Damper on ILS coupled approaches

Answer 32

200 ft AGL

Question 33

# GENERAL Required Flight Crew

Answer 33

Pilot and Copilot

Question 34

# GENERAL Kinds of Opeartions

Answer 34

VFR, IFR, FIKI

Question 35

# GENERAL Maneuvering Load Factors Limits

Answer 35

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

Question 36

# GENERAL Condition lever position during all ground opeartions | Exept when cleard for takoff or during landing roll

Answer 36

MIN RPM

Question 37

# Genaral Power Levers must be in what position during all ground operations | Exept for breif excursions as needed to maneuver the airplane

Answer 37

GROUND IDLE

Question 38

# SPEED Maximum speed for windshield operations

Answer 38

160 KIAS

Question 39

# SPEED Vmo/Mmo

Answer 39

272 KIAS/0.52 MACH

Question 40

# SPEED Va

Answer 40

200 KIAS

Question 41

# SPEED Vle/Vlo

Answer 41

200 KAIS

Question 42

# SPEED Vfe

Answer 42

200 KAIS 150 KIAS 135 KIAS

Question 43

# GENERAL Max Demonstrated Crosswind

Answer 43

30 KIAS

Question 44

# GENERAL Maximum Tailwind Speed Takeoff and Landing | Gear and Flaps Up

Answer 44

10 KIAS

Question 45

# SPEED Minimum Speed in Icing Conditions | Gear up Flaps 15°

Answer 45

165 KIAS

Question 46

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

Answer 46

16,000 ft

Question 47

# APU APU maximum speed and altitude | For starting

Answer 47

200 KAIS 20,000 ft | Airspeed may vary with altitude

Question 48

# APU APU maximum operating temperature | APU limitation

Answer 48

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

Question 49

# APU APU maximum allowable EGT during start | During Start

Answer 49

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

Question 50

# ELECTRICAL Maximul Load per MAIN genrator

Answer 50

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

Question 51

# ELECTRICAL Maximum Laod per AUX generator

Answer 51

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

Question 52

# APU Maximum Load per APU generator

Answer 52

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

Question 53

# ELECTRICAL Maximum Battery temperature

Answer 53

70°C

Question 54

# FUEL Fuel Used

Answer 54

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

Question 55

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

Answer 55

150 hours between overhauls

Question 56

# 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

Answer 56

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

Question 57

# SPEED Bird impact speed

Answer 57

250 KIAS below 8,000 ft

Question 58

# GEMERAL PROP SYNC must be off | Flight condition

Answer 58

For Takeoff and Landing per airworthiness directive

Question 59

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

Answer 59

Zero

Question 60

# ICE Continuous ignition must be used during the following conditions

Answer 60

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

Question 61

# GENERAL Zone Weight Limits

Answer 61

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

Question 62

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

Answer 62

45°C

Question 63

# ICE Minimum Nh required for operations of the pneumatic deicing system

Answer 63

80%

Question 64

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

Answer 64

40 PSID

Question 65

# GENERAL Operation id oil pressure is below what PSID is not permitted

Answer 65

40 PSID