Memory Items - Limits

Question 1

Severe Turbulence Speed

Answer 1

200 KIAS

Question 2

Maneuvering Speed (VA)

Answer 2

200 KIAS

Question 3

Max Flaps Speed 5º (VFE)

Answer 3

195 KIAS

Question 4

Max Flaps Speed 10º (VFE)

Answer 4

175 KIAS

Question 5

Max Flaps Speed 15º (VFE)

Answer 5

165 KIAS

Question 6

Max Flaps Speed 35º (VFE)

Answer 6

155 KIAS

Question 7

Landing Gear Operating Speed (VLO)

Answer 7

200 KIAS

Question 8

Landing Gear Extended Speed (VLE) doors closed

Answer 8

215 KIAS

Question 9

Ambient Temp Max (engine)

Answer 9

+50ºC or ISA +35ºC, whichever is lower

Question 10

Engine Starter Cranking Limits

Answer 10

Start: 1, Max Time on: 70 Seconds, Followed by: 2 minutes off

Question 11

On the ground (taxi and takeoff roll to the point of lift-off):
_____________ or below when precipitation in any form is present, or fog with visibility of
one mile or less; also when operating on ramps, taxiways, or runways where surface
snow, ice, slush, or standing water may be ingested by the engines or freeze on engines,
nacelles, or engine sensor probes.

Answer 11

OAT is 10ºC

Question 12

In flight (after lift-off to landing):
_____________ or below and _____________ is present in any form. Ice accretion on
aerodynamic surfaces is not considered to exist at temperatures of -40°C or below.

Answer 12

SAT is 5ºC, visible moisture

Question 13

Engine intake bypass doors shall be ________ for engine operations in icing conditions

Answer 13

Open

Question 14

Maximum crosswind component approved for takeoff and landing on a hard, dry, or wet
runway is ______.

Answer 14

32 knots

Question 15

Maximum fuel imbalance between contents of main fuel tanks is ______ (This is an in-flight
limitation only.)

Answer 15

600 lb

Question 16

Standby battery, Auxiliary battery and Main battery maximum loadmeter reading for
takeoff is

Answer 16

0.1

Question 17

Minimum battery temperature for takeoff is

Answer 17

-20ºC

Question 18

Maximum altitude with the landing gear and/or flap extended is

Answer 18

15,000 ft

Question 19

Setting takeoff power prior to brake release, with the nose of the airplane more than ____ out
of wind, is prohibited for wind speeds greater than ____ knots.

Answer 19

45°, eight

Question 20

Tank 1 and tank 2 auxiliary pumps must be ____ for takeoff and landing.

Answer 20

on

Question 21

Maximum operating altitude

Answer 21

25,000 ft ASL

Question 22

Maximum operating altitude for takeoff

Answer 22

10,000 ft ASL

Question 23

Airplane maximum operating ambient temperature limit

Answer 23

+50°C or ISA +35°C, whichever is lower

Question 24

Airplane minimum operating ambient temperature limit is _____.

Answer 24

-54°C

Question 25

Ambient temperature conditions on the ground shall be derived by reference to reported _____. Ambient temperature conditions in flight shall be derived by reference to indicated _____.

Answer 25

OAT, SAT

Question 26

Inflight operation of the _____aft of the _____ gate is _____.

Answer 26

Power Levers, FLIGHT IDLE, prohibited

Question 27

Maximum cabin pressure differential limit

Answer 27

5.95 psi

Question 28

Maximum cabin pressure differential limit during takeoff and landing

Answer 28

0.5 psi

Question 29

Bleed air must be _____ for takeoff whenever: • Tailwind component exceeds _____ knots • Takeoff is conducted with _____ power selected • _____ is suspected

Answer 29

off, ten, MTOP, Windshear

Question 30

For landing, bleed air must be _____ whenever: • Tailwind component exceeds _____ knots • Reported _____ exceeds _____ • _____is suspected

Answer 30

off, ten, OAT, 39°C (100°F), Windshear

Question 31

Takeoff in ______ mode is prohibited (AHRS)

Answer 31

BASIC, DG

Question 32

Baggage Compartment Fire Extinguishing: Unless the _____ baggage compartments are empty, the airplane shall not be operated farther than _____ hour flying time from a suitable airport for landing.

Answer 32

forward and aft, one

Question 33

_____ select switches on the Captain and First Officer ARCDU shall be _____ and the _____ switch on the observer's Audio Control Panel shall be _____, when using the flightdeck _____.

Answer 33

HOT MIC, OFF, INT/RAD, centered, speakers

Question 34

APU is approved for _____ OPERATION ONLY.

Answer 34

GROUND

Question 35

APU shall be _____ prior to takeoff

Answer 35

shutdown

Question 36

APU shall not be operated _____ with _____ on board

Answer 36

unattended, passengers

Question 37

APU shall not be operated during _____ refueling.

Answer 37

gravity (overwing)

Question 38

To maintain steady electrical state, the APU _____ be started during _____.

Answer 38

shall not, refueling

Question 39

APU ambient temperature limitations (max)

Answer 39

+50ºC or ISA +35ºC, whichever is lower

Question 40

APU ambient temperature limitations (min)

Answer 40

-54ºC

Question 41

When the APU has been shut down in _____ below _____ for greater than _____ hour, it must be preheated prior to start in accordance with applicable maintenance procedures.

Answer 41

outside air temperature, -35ºC, one

Question 42

The APU Bleed Air shall be selected _____ when the aircraft is being _____.

Answer 42

off, deiced/anti-iced

Question 43

APU starter cranking limits (Start 1)

Answer 43

Max Time on: 60 seconds, Followed By: 5 minutes off

Question 44

APU starter cranking limits (Start 2)

Answer 44

Max Time on: 60 seconds, Followed By: Maintenance action required

Question 45

(APU) Including the time taken for maintenance action following the second start attempt, a minimum of _____ minutes must elapse prior to the next start attempt.

Answer 45

30

Question 46

During autopilot operation, the pilot shall be seated at the _____ with _____ secured.

Answer 46

controls, harness

Question 47

Autopilot (coupled) and Flight Director (manual) approaches are approved from a nominal glideslope angle of _____ to maximum of _____.

Answer 47

2.5°, 4°

Question 48

AFCS is approved for autopilot coupled approaches to _____ limits only.

Answer 48

CAT I

Question 49

______ approaches are approved for _____ flap configurations.

Answer 49

Autopilot coupled, all

Question 50

Use of Flaps _____, autopilot coupled is prohibited with _____

Answer 50

35°, one engine inoperative

Question 51

Autopilot coupled approaches have been demonstrated in crosswind components up to _____ knots. _____.

Answer 51

18, This is not considered limiting

Question 52

After takeoff or go-around, the minimum height for autopilot engagement is _____.

Answer 52

1,000 feet AFE

Question 53

Autopilot shall be disengaged at or above _____ for: - HGS approaches flown in _____ mode - Approaches flown with an _____ - Approaches flown with Flap _____

Answer 53

1,000 feet AFE, AIII, inoperative engine, 0°

Question 54

For coupled approaches, the autopilot shall be disengaged at or above _____.

Answer 54

200 feet AFE

Question 55

Autopilot shall be disengaged in _____ icing.

Answer 55

severe

Question 56

Autopilot shall be disengaged in _____ atmospheric turbulence

Answer 56

severe or extreme

Question 57

Max Flaps Speed 0º (VFE)

Answer 57

Vmo-10kts

Question 58

Maximum Tire Speed

Answer 58

182 KIAS

Question 59

Maximum Alternate Gear Extension Speed

Answer 59

185 KIAS

Question 60

Min Flaps Speed 5º (Vmin)

Answer 60

160 KIAS

Question 61

Min Flaps Speed 0º (Vmin)

Answer 61

180 KIAS

Question 62

Min Flaps Speed 15º (Vmin)

Answer 62

145 KIAS

Question 63

Min Flaps Speed 10º (Vmin)

Answer 63

150 KIAS

Question 64

Abort engine start if

Answer 64

- Engine ITT approaches or exceeds 920ºC - NH is not in the green arch within 70 seconds of selecting Condition Lever to START & FEATHER - Engine Oil Pressure fails to reach 44 psi by start SELECT switch reset

Question 65

Takeoff Abort required when

Answer 65

- Takeoff warning horn - Failure of the A/F ARM message to illuminate on ED - Engine fire or failure - MASTER WARNING - Takeoff torque not obtained on either engine - Exceeding engine limitations - Windshear encounter - HGS failure, "TO WARN," or loss of HGS symbology during takeoff below 500 RVR when the runway centerline is not in sight

Question 66

O2 required when either pilot detects a situation

Answer 66

- Which could introduce smoke or fumes in the flightdeck, shall state. "Smoke - Don mask," - Results in loss of cabin pressure above 10,000 MSL, shall state, "Oxygen - Don mask."

Question 67

Max ramp weight

Answer 67

65, 400 lbs

Question 68

Maximum takeoff weight

Answer 68

65,200 lbs

Question 69

Maximum landing weight

Answer 69

62,000 lbs

Question 70

Maximum zero fuel weight

Answer 70

58,000 lbs

Question 71

Minimum structural design weight

Answer 71

31,753 lbs