B-747 Oral Question Bank & Review AC Gen, Limitations, & Performance Flashcards

1
Q

What is the wingspan of the 400F / -8?

A

213 feet (64.9 meters)
224.5 feet (68.4 meters)

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2
Q

With body gear steering, what is the
minimum width of pavement for a 180 degree turn of the 400F / -8?

A

4 153 feet (46.6 meters)
8 172 feet (52.4 meters)

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3
Q

What happens when you rotate the Oxygen Mask Emergency/Test selector to emergency?

A

Supplies 100% oxygen under positive pressure at all cabin altitudes, and protects against smoke and harmful vapors
FCOM, VOL 2; 1.30.25 16

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4
Q

With the Emergency (EMER) Lights Switch ARMED, when do the emergency lights
illuminate?

A

If airplane electrical power (DC) fails or is turned off.

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5
Q

What is the electrical power source for the emergency lighting system, and for what duration?

A

Remote batteries for 15 minutes

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6
Q

Where is the portable ELT located on the -400 freighter?

A

Upper deck lavatory exterior wall

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7
Q

IMMEDIATE ACTION ITEMS
Give examples of Immediate Action Items on the Quick Reference Checklist.

A
  • CABIN ALTITUDE-Rapid Depressurization
  • ENG 1,2,3,4 AUTOSTART-Aborted Engine start
  • Engine Limit or Surge or Stall
  • IAS DISAGREE-Airspeed Unreliable
  • FIRE ENG 1,2,3,4-Engine Severe Damage or Separation
  • Multiple Engine Flameout or Stall
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8
Q

What is the maximum Takeoff and Landing Tailwind component for the -400/-8 and LCF?

A
  • 15 knots (LCF-10 KTS)
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9
Q

What is maximum headwind component for autoland

A
  • 25 knots
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10
Q

What are maximum and minimum glideslope angles for ILS autoland?

A

3.25 degrees (max); 2.5 degrees (min)

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11
Q

What VNAV limitation applies to level-off within 2,000 feet after changing the altimeter setting from QNE to QNH, or QNH to QNE?

A

Do not use VNAV for level-off if the QNH is less than 29.70in/1006 hPa.
FCOM, VOL 1; L.10.17

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12
Q

Without LAND 2 or LAND 3 annunciated, the autopilot
must not remain engaged below what RA altitude?

A
  • 100 feet RA
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13
Q

What is turbulent air penetration speed -400 and -8?

A
  • 290 to 310 KIAS/0.82 to 0.85 Mach,
    whichever is lower.
  • 310 KTS/0.83 Mach.
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14
Q

What is the minimum in-flight fuel temperature for the -8?

A
  • -48◦C
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15
Q

What is the maximum altitude for flap extension?

A
  • 20,000 feet
    FCOM, VOL 1; L.10.15
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16
Q

Are operations allowed when the reported braking action is NIL?

A
  • No
17
Q

Name some places you can you can find the maximum takeoff and landing weights for the aircraft
you are operating?

A
  • Page one of the OFP
  • FCOM Vol 1 Limitations
18
Q

What is the Difference in the Basic Operating Weight (BOW) on the Operational Flight Plan (OFP) and the Sable Loadsheet? Is there a difference between the Sable and OFP final calculated ZFW and TOGW?

A
  • BOW (OFP) – Basic Operating Weight ( includes weight of all cockpit and cabin crew)
  • BOW (Sable) – Basic Operating Weight ( Acft basic wt + 2 crew)
19
Q

What are pitch attitude and N1 for flaps up, level flight cruise, at 35,000 Feet, gross weight 300.0 kgs?

A

FCOM, QRH; PI.20.5
* Pitch: 2.5 degrees up
* N1: 91.3%

20
Q

What BTMS number on the GEAR synoptic display will cause an EICAS advisory message of BRAKE TEMP?

A
  • 5 or more
21
Q

What is VREF for flaps 30, 300.0 kgs gross weight?

A
  • 157 KIAS
22
Q

What is flap maneuvering speed for flaps 10 gross weight 300.0 kgs?

A
  • 177 KIAS
23
Q
A
  • 177 KIAS
24
Q

On the 400F, 400C and -8, the Final Upper Deck/Cockpit Procedure requires the FO to do what with the Smoke Barrier Door?

A

Ensure the door is closed and all three security locks are moved to the locked position.