Memory Items, Limitations

Question 1

(757) Maximum Operating Altitude

Answer 1

42,000 feet pressure altitude

Question 2

(767) Maximum Operating Altitude

Answer 2

43,000 feet pressure altitude

Question 3

Maximum Takeoff and Landing Tailwind

Component

Answer 3

10 knots, or as permitted by

Company Pages

Question 4

Turbulent air penetration speed.

Answer 4

290 KIAS /.78Mach, whichever is lower.

Question 5

757/767-300 crosswind limit

Answer 5

40 knots for takeoff and landing, including gusts

Note: The crosswind component may be further limited by low visibility
approaches, autolands, or contamination.

Note: Refer to 5.16.3, Guidelines for Takeoff on Contaminated Runways or
Landing with Braking Action Less than Good.

Question 6

Autopilot/Flight Director System

Answer 6

After takeoff, the autopilot must not be engaged below 200 feet AGL.

Use of aileron trim with the autopilot engaged is prohibited.

Question 7

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

Answer 7

Maximum Allowable Wind Speeds

• 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,
  the autoland crosswind limit is 40 knots

Question 8

Maximum altitude for flap extension

Answer 8

20,000 feet.

Question 9

Weather Radar

Answer 9

Avoid weather radar operation in a hangar

Question 10

(757)

– Aborted Engine Start –

Answer 10

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

(See Tab 7, Engines, APU)

Question 11

(757)

– Airspeed Unreliable –

Answer 11

1.) Autopilot disengage switch . . . . . . . . . . . . .Push
2.) A/T ARM switch . . . . . . . . . . . . . . . . . . . . . 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° and 75% N1
-Flaps up . . . . . . . . . . . . . . .
4° and 75% N1

(See Tab 10, Flight Instruments, Displays)

Question 12

(757)

– Dual Engine Failure –

Answer 12

1.) ENG START selectors (both). . . . . . . . . . . . . .FLT
2.) Thrust levers (both) . . . . . . . . . . . . . . . . . . Idle
3.) FUEL CONTROL
switches (both) . . . . . . . . . . . CUTOFF, then RUN

(See Tab 7, Engines, APU)

Question 13

(757)
– ENGINE FIRE
or Engine Severe Damage or Separation –

Answer 13

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

(See Tab 8, Fire Protection)

Question 14

(757)

– Engine Limit or Surge or Stall –

Answer 14

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

(See Tab 7, Engines, APU)

Question 15

(757)
– CABIN ALTITUDE
or
Rapid Depressurization –

Answer 15

1. ) Don the oxygen masks.
2. ) Establish crew communications.

(See Tab 2, Air Systems)

Question 16

Which memory items is different for the 767?

Answer 16

Airspeed unreliable

Question 17

(767)

– Airspeed Unreliable –

Answer 17

1.) Autopilot disengage switch . . . . . . . . . . . . .Push
2.) A/T ARM switch . . . . . . . . . . . . . . . . . . . . . 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° and 80% N1
-Flaps up . . . . . . . . . . . . . . .
4° and 75% N1

(See Tab 10, Flight Instruments, Displays)

Question 18

Emergency Evacuation Flow/Philosophy

Answer 18

STOP 
 - Set parking brake
CONFIGURE
 - Cab Alt mode: MAN
 - Cab Alt ctrl: Hold in CLB
 - Emer Lights: ON
SHUTDOWN
 - Fuel Control: Both Cutoff
EVACUATE