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49 Cards in this Set

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Airplane/Powerplant maximum operating ambient temperature

+50C or ISA +35C (whichever is lower)

Airplane/Powerplant minimum operating temperature

-54C

APU maximum operating ambient temperature

+50C or ISA +35C (whichever is lower)

APU minimum operating ambient temperature

-54C

Maximum operating altitude

25,000 ASL

Maximum operating altitude for takeoff

10,000 ASL

Maximum crosswind component for takeoff and landing (conditions: hard, wet, or dry runway)

32 kts

Maximum ramp weight (MRW)

65,400 lbs

Maximum takeoff weight (MGTOW)

65,200 lbs

Maximum landing weight (MLW)

62,000 lbs

Severe turbulence airspeed

210 kts

Maneuvering speed (Va)

204 kts

Maximum gear operating speed (VLE)

215 kts

Maximum gear operating speed (VLO)

195 kts

Structural landing gear operating speed

200 kts

Define "icing conditions" (on ground)

Static air temperature (SAT) is 10C 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.

Define "icing conditions" (in flight)

Static air temperature (SAT) is 5C or below and visible moisture is present in any form. Ice accretion on aerodynamic surfaces is not considered to exist at temperature of -40C or below.

Flap VMIN, VMAX, and structural speeds for Flaps 0

VMIN - 180 kts


VMAX - VMO


Structural - Not Applicable

Flap VMIN, VMAX, and structural speeds for Flaps 5

VMIN - 160 kts


VMAX - 195 kts


Structural - 200 kts

Flap VMIN, VMAX, and structural speeds for Flaps 10

VMIN - 150 kts


VMAX - 175 kts


Structural - 181 kts

Flap VMIN, VMAX, and structural speeds for Flaps 15

VMIN - Solid or Open Bug


VMAX - 165 kts


Structural - 172 kts

Flap VMIN, VMAX, and structural speeds for Flaps 35

VMIN - Solid or Open Bug


VMAX - 155 kts


Structural - 158 kts

Maximum Fuel Capacity

11,724 lbs

Maximum Fuel Imbalance - Inflight Only

600 lbs

Tank 1 and Tank 2 Auxiliary Pumps

On for Takeoff and Landing

Engine starter cranking limit

70 seconds ON, followed by 2 min OFF

APU starter cranking limit

60 seconds ON, followed by 5 min OFF


2nd attempt - 60 seconds ON, followed by MX Req'd.


*30 minute minimum from 2nd start attempt before 3rd start attempt (after mx action)

Battery load prior to takeoff (main, aux, standby)

0.1

Min battery temperature prior to takeoff

-20C

Maximum altitude for gear and flaps extended

15,000 ASL

Miscellaneous Engine Operation Limitations (see hint, if needed)
1. Setting power for takeoff prior to brake release with winds over 8 kts more than 45 deg off the nose is prohibited
2. Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited
3. Engine intake bypass doors must be open for operation in icing conditions
Three items.
1. What wind condition prohibits takeoff prior to break release?
2. Inflight operation aft of flight idle gate is allowed (T or F).
3. Bypass doors must be ___ for operation in icing conditions.

Air Conditioning


Maximum Cabin Differential

5.95 psi (in-flight)


0.5 psi (takeoff and landing)

When must bleed air be off for takeoff and landing?

1. Windshear is suspected


2. Tailwind exceeds 10 kts


3. For takeoff - when conducted with MTOP selected


4. For landing only - when OAT exceeds 39C (100F)

Four conditions. Two wind related, one power setting related, on temperature related.

What AHRS modes are prohibited for takeoff?

BASIC mode and DG mode

Baggage compartment fire extinguishing operational requirement

Unless the forward and aft baggage compartments are empty, the airplane shall not be operated farther than one hour flying time from a suitable airport for landing.

What are the flight compartment communication settings when using the flight deck speakers?

HOT MIC select switches on the Captain and First Officer ARCDU shall be OFF and the INT/RAD switch on the observer's Audio Control Panel shall be centered.

APU Operating Requirements and Procedures
1. APU is only approved for ground operation
2. APU shall be shutdown prior to takeoff
3. APU shall not be operated unattended with passengers on board
4. APU shall not be operated during gravity refueling
5. APU shall not be operated during refueling to maintain steady electrical state (QX SOP only)

During autopilot operation the pilot will be. . . .

. . . seated at the controls with harness secured

Coupled autopilot and hand-flown FD approaches are approved for what glide slope angles?

2.5 deg to 4 deg

When must the autopilot be disengaged?

1. Severe icing


2. Severe or extreme atmospheric turbulence

What is the minimum height for autopilot engagement?

1,000 AFE

Autopilot coupled approaches are approved to what minima?

CAT 1 limits only

What flaps configurations are approved for autopilot coupled approaches?

All flap configurations

At what flap setting(s) are autopilot coupled approaches prohibited with one engine inoperative?

Flaps 35

What is the demonstrated crosswind component for autopilot coupled approaches?

18 kts

Autopilot shall be disengaged at or above 1,000 AFE for:

1. HGS approaches flown in AIII mode


2. Approaches flown with an inoperative engine


3. Approaches flown with Flap 0

What is the minimum altitude before the autopilot must be disengaged on a coupled approach?
200 AFE

Use of VOR without associated DME is prohibited in what mode?

APP Mode

Reduced Np landings are prohibited when:

1. Landings are accomplished at Solid Bug


2. Performance requires Bleeds OFF


3. Tailwind exceeds 10 kts.


4. Windshear is reported or suspected


5. Runway is contaminated or braking action is less than good


6. Landing performance is derived from the E&A Checklist "Adjusted Landing Speed and Distance Tables"

Six items - mostly weather and performance related