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PSA > FOM and Random stuff for Oral > Flashcards

FOM and Random stuff for Oral Flashcards

0
Q

Captain will conduct the takeoff when vis. is

A

1600 RVR or less

1/4 statute mile or less (if no RVR is reported for that runway).

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1
Q

On the approach what must we have to be considered stabilized
(1000’ COOT)

A
  • 1000’ descent rate by 1000’ AGL
  • Configured
  • On proper flight path
  • On speed
  • Trimmed
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2
Q

When vis is less than 3/4 mile or RVR is 4000 on a CAT 1 ILS the aircraft must have:

A

Dual or single flight director and a coupled autopilot

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3
Q

If a low time FO, the captain will make all Takeoff, Approach below 3000’ and all landings if any of the following conditions exist:
(AABCCRVW)

A
  • Anytime Captain deems necessary
  • Airports (special)
  • Braking action less than good.
  • Crosswind greater than 15kts.
  • Contaminated RWY
  • RVR 4000 or less
  • Visibility 3/4 miles or less
  • Windshear in the vicinity
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4
Q

Without TDZ light and or CL lights, including runways with installed but inoperative TDZ lights and or CL lights RVR cannot be blow

A

1800 RVR

If 10-9 says 600 RVR and you have CL lights and RWY edge light you can land. PSA lowest minima is 500 RVR

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5
Q

What are standard turbo jet landing mins

A

4000 RVR or 3/4 statute mile vis

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6
Q

What are standard turbo jet takeoff mins

A

5000 RVR or 1 statute mile vis.

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7
Q

What is fuel burn

A

Fuel to destination plus 1 approach at Destination

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8
Q

What is Takeoff fuel

A

Burn, Reserve, Hold and Alt if needed

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9
Q

Takeoff Alternate requirements

A

4600 lbs of fuel, one hour from departure airport at normal cruise speed in still air one engine inop. (300nm)

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10
Q

Flex Takeoff is prohibited when

ABCDEFG

A

Anti-skid inop
Bleeds-14th stage anti-ice is on
Contaminated RWY
De-iced
Engine is unable to produce max rated thrust
Field limitation
Gusts-windshear warning or forecast are present

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11
Q

Fuel required if Takeoff Alternate is required

A

4600lbs Per Flap AD.

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12
Q

Pitch trim is provided by

A

2 independent motors that actuate a jackscrew and moves the whole horizontal stabilizer

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13
Q

Flaps are powered by

A

2 PDU’s and a flex drive

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14
Q

If one PDU fails on the flaps what speed will they operate

A

Half speed

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16
Q

GND LIFT DUMPING switch in AUTO, arming of the system is achieved by:

A

Both engines greater than 79% N1
Thrust levers position to T/O power
Wheel speed greater than 45kts

16
Q

Spoilerons will deploy when:

A

Thrust levers at idle or less than 40% N1 AND, WOW
and 1 of the 2 conditions:
Wheel speed greater than 16kts
RA less than 5 feet

17
Q

Ground and flight spoilers deploy when:

A

Thrust levers at idle or less than 40% N1 AND any 2 of the 3 conditions:
L or R MLG WOW
Wheel speed greater than 16 kts
RA less than 5 feet AGL

18
Q

Anti-Skid is armed when

A

35kts wheel speed
WOW signal for 5 secs.
Less than 10kts wheel speed Anti-skid will disengage

19
Q

Tiller and rudder limits

A

Tiller-70 degrees

Rudders-5 degrees

20
Q

After landing when will CPAM change CPC’s

A

WOW and after 3 mins.

21
Q

Reserve fuel is based upon

A

No less than 45 minutes, long range cruise power setting at FL250.

22
Q

Each generator control unit (GCU) controls and monitors the related AC generator system and provides protection and voltage regulation for its
respective generator.

A

Over/ Undervoltage
Over/ Underfrequency
Generator or bus overcurrent

24
Q

What is powered by the AC ESS BUS

BATE

A 
Bleed detection controllers L/R
AOA probe heater Left
TCAS
ESS TRU 1
• This bus is normally fed from AC BUS 1.
25
Q

What does ALT/MSAP fuel include

A

Missed Approach at Destination and Fuel to Most Distant Alternate

26
Q

Areas Containing Dual Loops

A
  • engines
  • jet pipes
  • pylons
  • APU
27
Q

Single Loop

A
  • both main landing gear (MLG) wheel wells
28
Q

Areas of Detection and Protection

A
  • L/R engine
  • APU
  • Lav.
  • Cargo Bay
29
Q

Area of Detection only

A
  • Main Landing Gear bays
30
Q
  • Fire Push Switchlight is pressed:
A
  • both squibs are armed
  • both bottle armed push to discharge
    switchlights illuminate
  • fuel, bleed air, hydraulic SOV’s all close
  • generator is tripped offline
31
Q

CVR starts recording

A

as soon as
electrical power is applied to the
aircraft

32
Q

AUTO will cause pumps to operate under following conditions:

A
  • Respective bus is powered
  • Cross side Gen is operating
  • Flaps are out of zero
33
Q

EMER LTS ON, OFF and ARMED

A

ON- Lights are on
OFF- Prevents activation of the lights when power is lost or turned off
AUTO-EMER LTS activate if DC ESS power is lost or turned off

PSA (4 decks)

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