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Limitations

Question 1

Maximum Operating Altitude

Answer 1

43,100

Limitations

Question 2

Maximum Takeoff and Landing Tailwind Component

Answer 2

10 knots, or as permitted by Company Pages

Limitations

Question 3

The turbulent air penetration speed (in severe turbulence) is defined as:

Answer 3

270 KIAS below 25,000 feet
280 KIAS/.82 Mach (whichever is lower) at and above 25,000 feet.
Maintain a minimum speed of 15 knots above the minimum maneuvering speed (amber band) at all altitudes when below 0.82 Mach.

Limitations

Question 4

The Delta 777 crosswind limit for takeoff and landing, including gusts.

Answer 4

40 knots

Note: The crosswind component may be further limited by low visibility
approaches, autolands, or contamination, or takeoff weights less than
550,000 pounds.

Note: If Takeoff Gross Weight is less than 550,000 pounds or the runway is
contaminated (not DRY), refer to SP.16, Guidelines for Takeoff on
Contaminated Runways or Landing with Braking Action Less than Good.

Limitations

Question 5

The autopilot must not be engaged below a minimum engage altitude of ? AGL after takeoff.

Answer 5

200 feet

Limitations

Question 6

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations (e.g. CAT II autoland, CAT III):

Answer 6

Headwind	25 knots
Crosswind	25 knots *
Tailwind	10 knots

* The Boeing AFM low visibility autoland crosswind limitation is 25 knots. To both initiate and land, Delta Ops Specs further restricts CAT II and CAT III low visibility operations to a 15 knot crosswind limit. For CAT I or higher visibility, apply the normal crosswind limit.

Limitations

Question 7

Flight control limitations

Answer 7

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA.

Memory Items

Question 8

Aborted Engine Start L, R

Answer 8

1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF

Memory Items

Question 9

Airspeed Unreliable

Answer 9

1 Autopilot disengage switch . . . . . . . . . . . . .Push
2 A/T ARM switches (both) . . . . . . . . . . . . . . .OFF
3 F/D switches (both) . . . . . . . . . . . . . . . . .OFF
4 If necessary to stabilize the aircraft, set the
following gear up pitch attitude and thrust:
       Flaps extended . . . . . . .  10 degrees and 85% N1
       Flaps up . . . . . . . . . . . 4 degrees and 70% N1

Memory Items

Question 10

[] CABIN ALTITUDE

Answer 10

1 Don the oxygen masks.
2 Establish crew communications.

Memory Items

Question 11

Dual Eng Fail/Stall

Answer 11

1 FUEL CONTROL switches
(both) . . . . . . . . . . . . . . . . . .CUTOFF, then RUN
2 RAM AIR TURBINE switch. . . . . . . . . . . Push and
                                     hold for 1 second

Memory Items

Question 12

[] ENG AUTOSTART L, R

Answer 12

1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF

Memory Items

Question 13

Eng Lim/Surge/Stall L, R

Answer 13

1 A/T ARM switch
(affected side) . . . . .Confirm . . . . . . . . . . . OFF
2 Thrust lever
(affected side) . . . . .Confirm . . . . . Retard until
                                     engine indications
                                  stay within limits or
                            the thrust lever is at idle

Memory Items

Question 14

Eng Svr Damage/Sep L, R

Answer 14

1 A/T ARM switch
(affected side) . . . . . Confirm . . . . . . . . . . . OFF
2 Thrust lever
(affected side) . . . . . Confirm . . . . . . . . . . . Idle

Memory Items

Question 15

[] FIRE ENG L, R

Answer 15

1 A/T ARM switch
(affected side) . . . . . Confirm . . . . . . . . . . . OFF
2 Thrust lever
(affected side) . . . . . Confirm . . . . . . . . . . . Idle

Memory Items

Question 16

[] STABILIZER

Answer 16

1 STAB cutout switches (both) . . . . . . . . . CUTOUT
2 Do not exceed the current airspeed.

Memory Items

Question 17

Emergency Evacuation Flow/Philosophy

Answer 17

STOP
CONFIGURE
SHUTDOWN
EVACUATE

Maneuvers

Question 18

V1 Cut

Answer 18

Initial target 10 to 12 degrees
V2 to V2 + 15
400'

Verify VNAV
Select or verify roll mode
call tower

1000'

Retract flaps on schedule.

Flaps Up

Verify CON thrust
Non-Normal checklist
After Takeoff checklist

Maneuvers

Question 19

Go Around

Answer 19

Pilot Flying	Pilot Monitoring
"GO AROUND, FLAPS 20"
	"TOGA VERIFIED"
	"POSITIVE RATE"
"GEAR UP"
400 feet RA:
Verify or call for roll mode.	Select or verify roll mode.
At acceleration height (normally 1,000 AFE):
Call for maneuvering speed for planned flaps.
"FLAPS __"
"AFTER TAKEOFF CHECKLIST"

Maneuvers

Question 20

All-Attitude Upset Recovery Strategy (AAURS)

Answer 20

Push
Roll
Power
Stabilize

Differences

Question 21

Warmup

Answer 21

ER- 5 min (3 min if the engines have been shutdown less than 1.5 hours)
LR - 3 min

Warning:

777 Flash Cards

Question:

Answer:

Info about the app

Info about the questions

Limitations

Question 1

Answer 1

Limitations

Question 2

Answer 2

Limitations

Question 3

Answer 3

Limitations

Question 4

Answer 4

Limitations

Question 5

Answer 5

Limitations

Question 6

Answer 6

Limitations

Question 7

Answer 7

Memory Items

Question 8

Answer 8

Memory Items

Question 9

Answer 9

Memory Items

Question 10

Answer 10

Memory Items

Question 11

Answer 11

Memory Items

Question 12

Answer 12

Memory Items

Question 13

Answer 13

Memory Items

Question 14

Answer 14

Memory Items

Question 15

Answer 15

Memory Items

Question 16

Answer 16

Memory Items

Question 17

Answer 17

Maneuvers

Question 18

Answer 18

Maneuvers

Question 19

Answer 19

Maneuvers

Question 20

Answer 20

Differences

Question 21

Answer 21

Differences

Question 22

Answer 22

Differences

Question 23

Answer 23