Kalitta Air OKE (300 - 425) |126questions with verified answers

Kalitta Air 747-400 2021 OKE (300 - 425) |
126questions with verified answers
300. With a left bleed duct isolated due to a bleed leak, what systems are
affected? (AOM Vol II, Pg 2-36) Ans✓✓✓-• Left leading edge flap operates
electrically in secondary mode
• Demand pump 1 is selected OFF, to avoid the EICAS alert message HYD PRESS
DEMAND from being displayed during approach
• A maximum of one air conditioning pack on assures sufficient thrust is available
from the two engines which supply air to the unaffected duct sections


301. What conditions will cause a Zone System (SYS) Fault light? (AOM Vol II, Pg.2-
2) Ans✓✓✓-• Temperature zone duct overheat or zone temperature controller
fault has occurred
• Master trim air valve switch is closed
• Trim Air switch is off
• Master trim air valve closed and pack air continues to flow


302. Bleed air is available for NAI operation with the Engine Bleed Air switch OFF,
except when? (AOM Vol II, Pg. 2-35) Ans✓✓✓-• The PRV had failed closed, or
• The PRV has closed due to a bleed air overheat, or
• The start valve is not closed, or
• The HP bleed valve is failed open


303. Bleed air is available for reverse thrust operation with the Bleed Air switch
ON or OFF, except when? (AOM Vol II, Pg. 2-35) Ans✓✓✓-• The PRV has failed
closed, or
• The PRV has been closed due to a bleed air overheat, or

,• The start valve is not closed


304. If you received a PACK 2 Status message after pushback, what would you do?
(AOM Vol I, Pg. NP-7) Ans✓✓✓-• Before engine start investigate
• After engine start nothing


305. Do you have to do a cross-bleed start from the supplemental procedures for
a delayed engine start with the APU off? Why not? Ans✓✓✓-• No, cross-bleed
start in supplemental procedures is for starting first engine.


306. On the ground, what condition must be met to configure EQUIPMENT
COOLING for flight? (AOM Vol II, Pg. 2-29) Ans✓✓✓-• On the ground one engine
on each wing must be running to configure for flight


307. What does the EICAS message "EQUIPMENT COOLING" mean on the ground?
How can you reconfigure for light mode? (AOM Vol II, Pg. 2-30) Ans✓✓✓-•
Equipment cooling is not configured for flight (ground valve still open),
reconfigure, move selector to STBY (to close ground valve)


308. Reserved Ans✓✓✓-Reserved


309. The forward cargo compartment receives heat how? (AOM Vol II, Pg. 2-29)
Ans✓✓✓-• Air exhausted from the (E&E) compartment


310. If both isolation valves are closed, what do you lose? (AOM Vol II, Pg. 2-37)
Ans✓✓✓-• Cargo smoke detection
• Portable water pressurization

, • Lower lobe air conditioning
• Trim air


311. With a PRV valve deferred, are you restricted from flight into known icing
conditions? (MEL, Pg. 36-22) Ans✓✓✓-• Yes


312. Is known icing and forecast icing the same thing? Ans✓✓✓-• No


313. Reserved Ans✓✓✓-Reserved


314. With Engine Bleed Valve closed, NACELLE ANTI-ICE bleed air is supplied by
which bleed? (AOM Vol II, Pg. 3-6) Ans✓✓✓-• The IP (intermediate pressure)
Bleed.


315. When is the wing anti-ice system inhibited? (AOM Vol II, Pg. 3-2) Ans✓✓✓-•
On the ground
• With flaps extended


316. What is the procedure for descending into icing conditions near convective
weather? (AOM Vol I, Pg. SP-112) Ans✓✓✓-• Pack high flow
switch ............................................... On
• Nacelle Anti-ice switches ......................................... On
• (at or below 22,000 feet) Wing Anti-ice switch .... On


317. You are in the Commonwealth of Independent States, and you need to be
de-iced. They are using ARTIKA 200 fluid, are there any additional procedures?