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74 Cards in this Set
- Front
- Back
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Runway Slope |
+/- 2% |
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Max Operating Altitude |
43,100 feet pressure altitude |
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Max Takeoff and Landing Altitude |
8,400 feet pressure altitude |
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N342AX through N378AX
Maximum Takeoff and Landing Tailwind Component |
10 knots |
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N225AX, N234AX, N387AX, N396AX
Maximum Takeoff and Landing Tailwind Component
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15 knots |
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Turbulent air penetration speed |
290 KIAS/.78 whichever is lower |
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The navigation and display system does not support operations at latitudes greater than? |
87 degrees north or south |
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Do not operate HF radios during? |
Refueling operations |
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Standby altimeters_____meet altimeter accuracy requirements of RVSM? |
Do not |
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The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation is? |
200 feet |
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Max allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM
Sea level: CA & FO |
40 feet |
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Max allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM
5000 feet: CA & FO |
45 feet |
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Max allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM
10,000 feet: CA & FO |
50 feet |
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Max allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM
All altitudes: CA or FO & Field Elevation |
75 feet |
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Do not operate weather radar when/where? |
In a hangar or within 50 feet of personnel, or a fuel spill.
Note: Hangar and personnel restrictions do not apply to radar test mode. |
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Operational check of the flight deck access system must be done when? |
Once each flight day, and MX performs the check during the service/transit checks. |
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Entry door evacuation slides must be armed, and the engagement of the girt bar must be verified when? |
Prior to taxi, takeoff, or landing whenever passengers are carried. |
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Do not operate cargo doors in winds more than? |
40 knots |
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Do not leave cargo doors open in winds more than? |
65 knots |
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Photo luminescent floor proximity escape path lighting must be? |
Charged in accordance to approved procedures |
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N351AX, N378AX, N396AX (767-300)
Max Taxi Weight |
413,000 lbs |
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N351AX, N378AX, N396AX (767-300)
Max Takeoff Weight |
412,000 lbs |
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N351AX, N378AX, N396AX (767-300)
Max Landing Weight |
320,000 lbs |
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N351AX, N378AX, N396AX (767-300)
Max Zero Fuel Weight |
295,000 lbs |
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N342AX, N387AX (767-300)
Max Taxi Weight
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409,000 lbs |
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N342AX, N387AX (767-300)
Max Takeoff Weight |
408,000 lbs |
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N342AX, N387AX (767-300)
Max Landing Weight |
320,000 lbs |
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N342AX, N387AX (767-300)
Max Zero Fuel Weight |
295,000 lbs |
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N225AX, N234AX (767-200)
Max Taxi Weight |
396,000 lbs |
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N225AX, N234AX (767-200)
Max Takeoff Weight |
395,000 lbs |
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N225AX, N234AX (767-200)
Max Landing Weight |
300,000 lbs |
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N225AX, N234AX (767-200)
Max Zero Fuel Weight |
260,000 lbs |
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After takeoff, the autopilot must not be engaged below? |
200 feet AGL |
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Use of aileron trim with autopilot engaged |
is prohibited |
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N342AX, N378AX
Max allowable wind speeds autoland |
Headwind: 25 knots Crosswind: 25 knots Tailwind: 10 knots |
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N225AX, N234AX, N387AX, N396AX
Max allowable wind speeds autoland |
Headwind: 25 knots Crosswind: 25 knots Tailwind: 15 knots |
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Engine vibration display |
Shall not be blanked during takeoff |
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Minimum inflight fuel tank temperature |
3 degrees C (5 degrees F) above the freezing point |
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Maximum fuel temperature |
49 degrees C |
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The center fuel tank may contain up to? |
22,050 pounds of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed maximum zero fuel weight, and center of gravity limits are observed |
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Reverse thrust limitations |
Ground use only |
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Maximum altitude for flap extension |
20,000 feet |
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Flight control limitations |
Avoid rapid, and large alternating control inputs with large changes in pitch, roll, or yaw. They may result in structural failure even below Va |
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EFB Airport map display |
Do not use as a primary navigation reference |
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EFB portable keyboard and cable |
Must be stowed during takeoff and landing |
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RNAV Departures |
Are not authorized from airports not stored in the FMC database |
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GPWS Look Ahead Alerting |
Do not use terrain display for navigation
Use of look ahead terrain alerting and display functions is prohibited within 15 NM of Takeoff, Approach, or Landing at an airport not contained in the GPWS database |
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In severe turbulence___ |
Continuous ignition must be on |
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With engine anti-ice on, what is provided? |
Continuous ignition |
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767 starter duty cycle |
Up to 5 minutes ON followed by ONE-HALF-MINUTE cooling for each minute on
Two 5 minute cycles, followed by a 10 minute cooling period |
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Do the Aborted Engine Start checklist for? |
EGT does not increase by 25 seconds after fuel control switch moved to run
EGT quickly nears or exceeds START LIMIT
ENGINE OIL PRESSURE is not normal by the time engine is stabilized at idle |
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Ignition on for? |
Takeoff Landing Icing Severe Turbulence |
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Engine Start Pressure |
30 PSI |
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Engine warm-up/cool down recommendations |
Run engines for at least 3 minutes at a thrust setting normally used for taxi operations |
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Engine warm-up requirement |
Engine oil temp must be above the bottom of the temperature scale |
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When engine anti-ice is required and the OAT is 3 degrees C or below? |
Do an engine run up, the following procedure:
Run up to a minimum of 60% N1 for approximately 30 seconds at intervals no greater than 30 minutes |
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Do not use speed brakes when? |
In flight below 800 feet AGL With Flaps in the Landing Position |
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When do icing conditions exist? |
10 degrees C with visible moisture in any form visibility 1 mile or less
Also includes standing water or slush on ramps |
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APU Starter duty cycle |
3 consecutive starts within a 60 minute period |
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APU bleed air is available up to? |
17,000 feet |
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APU electric is available? |
Throughout operating envelope |
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Cabin Altitude Light comes on? |
10,000 ft cabin altitude |
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Cabin Altitude Light extinguishes? |
8,500 ft cabin altitude |
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Outflow valve closes automatically by the aneroid switch at? |
11,000 ft cabin altitude |
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Passenger Oxygen masks automatically deploy at? |
14,000 ft cabin altitude |
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What fuel is prohibited in the center tank during ferry operations, and all tanks during passenger operations? |
JP-4 and Jet B |
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When does the fuel configuration light come on? |
1200 lbs in the center tank without pumps on Less than 2200 lbs in each wing Imbalance greater than 1500-2500 lbs |
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What is the jettison rate for the 767 |
1300 lbs per minute 2600 lbs per minute for N342AX |
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Min oil quantity for dispatch |
17 quarts |
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Min O2 pressure for non-ETOPS flight |
1250 PSI |
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Min O2 pressure for ETOPS flight |
1500 PSI |
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For engine start:
Position fuel control switch to RUN at? |
20% N2 or Max motoring (15% minimum) whichever is reached first |
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With autothrottles disengaged, use an approach speed wind correction of? |
HALF the STEADY STATE headwind plus all GUSTS not to exceed 20 KNOTS |
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What is significant about using stab trim settings less than 3 units? |
Must be set using ALT/MAN TRIM
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