Memory Items Flashcards
ABORTED ENGINE START
- FUEL CONTROL switch (affected side) - CUTOFF
IAS DISAGREE
or
Airspeed Unreliable
- Autopilot disengage switch - Push
- A/T ARM switch - OFF
- F/D switches (both) - OFF
- If necessary to stabilize the aircraft, set the following gear up pitch attitude and thrust:
Flaps extended - 10 degrees and 75% N1 [80% N1 for all 767s]
Flaps up - 4 degrees and 75% N1
CABIN ALTITUDE
or
Rapid Depressurization
- Don the oxygen masks.
- Establish crew communications.
Dual Engine Failure
- ENG START selectors (both) - FLT
- Thrust levers (both) - Idle
- FUEL CONTROL switches (both) - CUTOFF, then RUN
Engine Limit or Surge or Stall
- A/T ARM switch - OFF
- Thrust lever (affected side) - Confirm - Retard until engine indications stay within limits or the thrust lever is at idle
ENGINE FIRE
or
Engine Severe Damage or Separation
- A/T ARM switch - OFF
- Thrust lever (affected side) - Confirm - Idle
Airplane General
Operational Limitations
- 757 & 767-300 Max Operating Altitudes
- 757 & 767-300 Max T/O and Landing Tailwind Component
757: 42,000’ pressure altitude
767-300: 43,000’ pressure altitude
10 knots, or as permitted by the Company Pages
Airplane General
Non-AFM Operational Info
Turbulent Air Penetration Speed
Delta 757 / 767-300 / 767-400 crosswind limitations (e.g. all aircraft variants)
290 KIAS / .78 Mach, whichever is lower
40 knots for T/O & 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 T/O on contaminated runways or Landing with braking action < GOOD.
Autoflight
Autopilot / Flight Director System Limitations
(All aircraft variants)
After T/O the autopilot must not be engaged below 200 feet AGL.
Use of aileron trim with the autopilot engaged is prohibited.
Autoflight
Automatic Landing
Maximum allowable wind speeds when landing weather minima are predicated on autoland operations (e.g. CAT II autoland, CAT III)
(All aircraft variants)
Maximum Allowable Wind Speeds
Headwind - 25 knots
Crosswind - 25 knots*
Tailwind - 10 knots
- The Boeing AFM low vis autoland crosswind limit is 25 knots. To both initiate and land, Delta Ops Specs further restricts CAT II & III to a 15 knots crosswind. For CAT I or higher, autoland crosswind limit is 40 knots.
Flight Controls
Max altitude with flap extension
(All aircraft variants)
20,000 feet
Aircraft General
Operational Limitations
767-400 Max Operating Altitude
767-400 Max T/O Tailwind Component
767-400 Max Landing Tailwind Component
43,100’ pressure altitude
Max TW for T/O = 15 knots
Max TW for Landing = 10 knots
Emergency Evacuation Flow / Philosophy
*Check DOORS on overhead panel - pax not auto-evacuating!
STOP: set brake; “EASY VICTOR” x 3
CONFIGURE: CABIN ALT CTRL - MAN; CLIMB - FULL OPEN; EMER LIGHTS - ON
SHUTDOWN: FUEL CONTROL switches (both) - CUTOFF
EVACUATE: Notify FA’s and ATC/Tower. PA: “This is the Captain. Evacuate, Evacuate.” Engine & APU Fire switches (all) - override and pull
