INFO Flashcards

1
Q

Most recent INFO

A

New lavatory oxy sys

  • bottle 3000 psi
  • expires 25 yrs after production
  • completed by Sept 2015
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2
Q

PWS

A

one pilot monitor WX the other TERR
if the WX radar is not on PWS scans for windshear 12 secs after thrust levers in TO range, so WX on will prevent the need for a high speed RTO.

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3
Q

ADS-B

A

transmits GPS position, speed, altitude, aircraft ID etc from FMS via the transponder

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4
Q

ADS-B OUT

A

uses transponder (limited range due to ground antenna) uses line of sight

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5
Q

ADS-C

A

uses VHF/SATCOM

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6
Q

ADS-B IN

A

displays information in cockpit, few airlines use this

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7
Q

ADS-B GPS and TX

A

if 1 GPS fails must select Tx on same side as functional GPS
ALT OFF - TX works and ADS-B transmits Extended Squitter.
Flt no. input transmitted on Extended Squitter

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8
Q

RNAV and RNP ops ANP

A

ANP - aircraft is 95% of the time within the RNP, when perf is not satisfied ‘UNABLE RNP’

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9
Q

XTK error

A

difference between LNAV and FMS position
does not consider ANP
deviation call at 1 * RNP track error
If XTK error > RNP no alert. UNABLE RNP only when ANP>RNP. Therefore, XTK error must be monitored by flt crew.

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10
Q

RNAV

A

onboard performance monitoring and alerting not required
decision of whether or not to continue is not dependent on display of UNABLE RNP and XTK error
verify/entering RNP value and XTK error monitoring required
conducted in radar coverage where controller monitors deviation from route

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11
Q

RNP

A

onboard performance monitoring and alerting required
decision of whether or not to continue is ependent on display of UNABLE RNP and XTK error
verify/entering RNP value and XTK error monitoring required
assumed outside radar coverage where pilots must monitor

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12
Q

RNP values

A

< FAF 1.0NM
>FAF 0.3NM
>MAP 1.0NM

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13
Q

RNAV 10 RNP 10

A

onbaord performance monitoring and alerting not required

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14
Q

RNAV (GNSS) app

A

FMS required to be updated by GPS but not onboard perf monitoring and alerting not reqd
GPS updating and RNP 0.3 reuired prior FAF by company (for convenience not having to monitor)
> initiating approach UNABLE RNP must discontinue app

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15
Q

RNP 4

A

no need to set RNP except for RNP 4 or RNP AR
don’t manually enter as it cannot then auto change
RNP airspace enter the RNP of 4, exiting RNP 4 DEL

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16
Q

DO NOT MONITOR XTK ERROR

A

during app monitor aircraft symbol versus magenta line, avoid head down checking of XTK error on PROG P2 (WTF??)

17
Q

XTK deviation call

A

XTK RNP * 1 or more ‘COURSE 0.3NM L/R’

GA unless visual reference established and can be maintained

18
Q

MISC

A

company mandates AP for RNP app
no RNP AR for B767 as OCT 2013
RNP chart specifies RNP 0.3 required in notes section
must use LNAV for RNP app therefore if XTK error increase cannot fix using HDG SEL.

19
Q

Circling

A

wings level by 300’ AFE

20
Q

Handy speed book

A

HIGH - Pressure Ht > 3000’, temp at SL > 44 deg

21
Q

why the ‘60kts’ call?

A

reduce REV THR to prevent FOD damage, for emergency ie RTO can use FULL REV until stopping and no 60kts call

22
Q

Why depressurise R HYD last?

A

as C + R share brake lines this prevents fluid transfer

23
Q

CTR L/R FUEL PUMP EICAS

A

TAXI - usable fuel in tank - recycle pumps
CLB - if C tank nearly empty - OFF
in CRZ with usable C tank fuel turn ON

24
Q

Range of CI

A
20
40
73
110
150
200
25
Q

CI 200

A

max due to fuel and max M0.83 for strong HW

26
Q

CI 20

A

lowest as CI 0 is MRC but for small fuel reduction is large increase in flt time

27
Q

Changing CI for TOD

A

< CI 73 by 10nm TOD for sys logic

>CI 73 by 50 nm

28
Q

Taxi time

A

80% of taxi time in same month for last year or most recent 3 months.

29
Q

STD callout definition

A

minimum required callouts relating to the items shown below and exclude those callouts which instruct specific operation or timing such as ‘gear up’ among many callouts made in normal operation

  • altitude, position or speed
  • significant deviation in flt path, speed or descent rate
  • information to aid in judgment for making landing or missed approach
  • flight and navigation instruments, autopilot system status
30
Q

STD callout objectives

A

1) to confirm information on altitude, position, speed and system status which does not require crew action
2) enhance crew coordination, common recognition, and fail safe function.

31
Q

What type of precip is TO prohibited for cold wx ops

A
SMALL HAIL GS
ICE PELLETS PL
HEAVY SNOW
HAIL GR
FZRA AND +FZRA
32
Q

Nitrogen generation sys

A

indicator left main wheel well
uses bleed air from L side pneumatic sys
starts after takeoff and continuously during flight

33
Q

NGS indicator

A

GREEN - fully operational
BLUE - degraded mode
AMBER - inoperative
NO LT - indicator failure

34
Q

Disengage AP by?

A

DA or 50’ < MDA

35
Q

Flt deck DECALS

A
UNDER STBY ALT 
 - 300 BCF AND PWS
LEFT SIDE OF R RDMI 
 - WINGLET VMO 340, HYD DRIVEN GEN INST, AND LAS EQUIPPED
BESIDE EACH INST SOURCE ADC
 - ALTN- R ADC or L ADC
36
Q

disengage AP by?

A

DA or 50’<MDA

37
Q

Vmo/Mmo recovery

A

not a big problem as spd still less than Vd which is certified dive speed
use AP as 0.3 deg/sec recovery where manually will likely overcontrol.
AP recovers at 0.15G/sec
use V/S and manually reduce thrust
DO NOT MANUALLY PITCH UP WITH AP ENGAGED IE USE OVER 27LBS OF FORCE
do not use SB rapidly
near Vmo/Mmo be aware of large wind changes/shears

38
Q

CI =

A

fuel cost

39
Q

AP and ADC SEP 2006

A

non- Pegasus FMC - ADC L FAIL use AP R with other than VNAV