Memory Items / # Limitations

Question 1

Aborted Engine Start

Answer 1

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

Question 2

Dual Engine Failure

Answer 2

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

Question 3

Engine Fire or Engine Severe Damage or Seperation

Answer 3

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

Question 4

• Engine indications are abnormal
• Engine indications are rapidly approaching or exceeding limits
• Abnormal engine noises are heard, possibly with airframe vibration
• There is no response to thrust lever movement or the response is abnormal
• Flames in the engine inlet or exhaust are reported

Answer 4

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

Question 5

•A cabin altitude exceedance occurs

Answer 5

1. ) Don the oxygen masks

2. ) Establish crew communications

Question 6

The airspeed or Mach indications are suspected to be unreliable:

Answer 6

1.) Check the pitch attitude and thrust
2.) IF pitch attitude or thrust is NOT normal for phase of flight: •Autopilot disengage switch…………Push
•Autothrottle disconnect switch……Push
•F/D switches (both)……………………….OFF
•Establish normal pitch attitude and thrust setting for
phase of flight

Question 7

Where is the quickest available reference for evacuation procedures?

Answer 7

Back cover of the QRH

Question 8

(757) Maximum Operating Altitude

Answer 8

42,000 feet pressure altitude

Question 9

(767-300) Maximum Operating Altitude

Answer 9

43,000 feet pressure altitude

Question 10

Maximum Takeoff and Landing Tailwind Component

Answer 10

10 knots, or as permitted by Delta Special Pages (green pages)

Question 11

Turbulent air penetration speed

Answer 11

290 KIAS / .78 Mach, whichever is lower

Question 12

The Delta 757 / 767-300 crosswind limit for takeoff and landing

Answer 12

40 knots (including gusts)

Question 13

After takeoff, the autopilot must not be engaged below

Answer 13

200 feet AGL

Question 14

Use of which secondary flight control is prohibited with the autopilot engaged?

Answer 14

Aileron trim

Question 15

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

Answer 15

25 knots

Question 16

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

Answer 16

25 knots*

Note: 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 17

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

Answer 17

10 knots

Question 18

Maximum altitude for flap extension

Answer 18

20,000 feet