Shared Flashcard Set

Details

UPS 767 memory items
UPS B-767 non-normals and limitations
24
Aviation
Professional
02/01/2011

Additional Aviation Flashcards

 


 

Cards

Term
CABIN ALTITUDE or Rapid Depressurization
Definition

OXYGEN MASKS...........ON

CREW COMMUNICATIONS...........ESTABLISH

Term
Dual Engine Failure (767 GE)
Definition

ENGINE START SELECTORS (Both)..........FLT

THRUST LEVERS (Both)...........CLOSE

FUEL CONTROL SWITCHES (Both)..........CUT OFF, THEN RUN

 

If engine appears stalled or EGT approaches the Standby Engine Indicator placard limit: Repeat the above step on affected engine(s)

[Reduces EGT and improves airflow]

Term
Airspeed Unreliable
Definition

AUTOMATION..........DISENGAGE

 

[Disengage autopilot and autothrottles, and turn off flight directors.]

Establish normal pitch attitude and thrust setting for phase of flight.

Term
Maximum takeoff and landing pressure altitude:
Definition

8,400 feet

9,500 feet B767 tail numbers 335 and subsequent

14,000 feet B757 Tail numbers: 451 thru 470

Term
Maximum operating pressure altitude:
Definition

(757) - 42,000 feet

(767) - 43,100 feet

Term
Runway Slope Limits:
Definition
+/- 2%
Term
Maximum takeoff and landing tailwind component:
Definition
10 knots
Term
Turbulent air speed:
Definition
290 knots/ .78M, whichever is lower
Term
Maximum demonstrated crosswind Takeoff and Landing:
Definition
30 knots (not considered limiting on a dry runway with all engines operating)
Term
Flap extension, maximum altitude:
Definition
20,000 ft
Term
Maximum temperature for JET A:
Definition
49 degrees C
Term
Minimum fuel tank temperatures:
Definition

(757) Minus 45 degrees C or 3 degrees above the freezing point of the fuel being used (whichever is higher)

(767) 3 degrees C above the freezing point of the fuel being used

Term
(757) Maximum fuel imbalance between left and right main tanks for all operations:
Definition
1800 lbs
Term
(767) Maximum fuel imbalance between left and right main tanks for all operations:
Definition

2500 lbs (main tank fuel load 48,000lbs or less)

linear reduction to 1500 lbs (48,000 to 79,800 lbs)

1500 lbs (greater than 79,800 lbs)

Term
(757) The center tank fuel pumps must be OFF for takeoff if center tank fuel is less than ______ with the aircraft readied for initial taxi.
Definition
5000 pounds
Term
(757) Both Center Tank Fuel Pump switches must be selected OFF when center tank fuel quantity reaches approximately ________ during climb, cruise, or descent.
Definition
1000 pounds
Term
Limitation for use of AUTOMATIC FLIGHT
Definition
On takeoff, do not engage autopilot below 200 ft AGL.
Term
LIMITATION for non-precision approach
Definition
VOR approaches: One pilot must have raw data from the VOR associated with the approach displayed in the HSI VOR mode no later than the final approach fix.
Term
Maximum taxi weights (pounds):
Definition

(757) 251,000

(767) 409,000

404,000 aircraft with "light weight gear"

Term
Maximum landing weight (pounds):
Definition

(757) 210,000

(767) 326,000

Term
Maximum zero fuel weight (pounds):
Definition

(757) 200,000

(767) 309,000

Term
Ignition
Definition
Continuos ignition shall be on for flight in severe turbulence.
Term
Reverse Thrust:
Definition
Reverse thrust is restricted to ground use only.  Backing the airplane with use of reverse thrust is not permitted.
Term
Minimum turning radius (767)
Definition
A 180 degree turn on a 150 ft wide runway is not authorized.
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