ETOPS & Navigation Systems Flashcards

1
Q

ETOPS

A

Extended Range Operations with Two-Engine Airplanes / Twin Engine Operations:
Routes that contain point(s) farther than 60 mins flying time from an adequate airport, whilst flying one-engine-out-cruise-still-air-ISA.

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2
Q

ETOPS Area of Ops defined by

A

diversion distances to suitable airports. It’s using the ISA-still-air-etc… and does not need to be recalculated every flight. Therefore, due to weather, actual diversion time might exceed the 2- or 3-hour diversion!

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3
Q

Equal Time Points (ETP)

A

the points at which diversion times between acceptable airports is Equal. Can be several along the way. Denoted as ETP1, ETP2, etc…

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4
Q

Period of Validity

A

Earliest possible time for the ALT. Time of Departure + T1 + t1

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5
Q

All Diversion airports must meet ARFFs

A

> or = ICAO cat 4.

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6
Q

Diversion fuel req’d for ETOPS

A

At every ETP, must have enough fuel for:

  • all-engine decompression
  • one-engine-out decomp.
  • one-engine out decomp. + drift-down.
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7
Q

ETOPS fuel =

A

Trip Fuel + Critical fuel (catastrophe at critical point, descend to 10,000 or MORA, cruise to diversion airport, hold there at 1500’ for 15 mins, instrument approach). + add 5% fuel for mileage deterioration, 5% for wind during cruise portion, icing penalties are 10% for time in icing forecast, or 100% of time forecast to be using ANTI-ice, and APU fuel.

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8
Q

Determining alternates before t/o:

A

1 nav / 2 nav. rule. 400 & 1, or 200 & 1/2. High mins cap. mins are not applicable in pre-departure trip planning.

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9
Q

Before entering ETOPS segments, pilots must

A

check wx for alternates. if not satisfactory, then re-route or get new alternate.

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10
Q

What requires re-route or diversions during ETOPS flight?

A
  • wx at ETOPS alternate unacceptable
  • req’d ETOPS equipment failure
  • diversion airport becomes otherwise unfit.
  • excessive fuel consumption affecting available reserve.
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11
Q

2-way Comm’s priority for required ETOPS position reports between 5-25mins prior to entry.

A
  1. ACARS. (CAL053, ETOPS entry AT 1935Z, FL 350, FR 25.2)
  2. SATCOM or HF voice (same)
  3. ATC Relay
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12
Q

ADIRU

A

2 indep. systems of Air Data & IRS

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13
Q

STBY instruments for Nav Systems include

A

Mag Compass, Indpt. Stby Att., RMI

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14
Q

VOR & APP mode in EFIS control Panel (ECP) are displayed as “Heading Up” while Map mode is displayed as ____

A

Track up.

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15
Q

Big Letters replacing tuned VOR freq’s represent

A

Decoded & ID’d VOR/DME info

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16
Q

little letters in a tuned freq?

A

DME only. ID mismatch.

17
Q

STBY RMI powered by?

A

STBY AC bus

18
Q

Red HDG Flag on RMI?

A

when ADIRU signal is unavailable

19
Q

If using STBY instruments for Nav, don’t forget to consult the ___?

A

Deviation card

20
Q

ANT position of ADF?

A

Bearing position unavailable, but audio is optimized

21
Q

ADIRU is made of?

A

2 independent IRS: 3 gyros, 3 accelerometers. 2 independent Air Data units.

22
Q

Heading and Att. are primarily sourced from?

A

IRS. Back up w/ stby inst.

23
Q

Outputs of ADIRU?

A

Attitude, Heading, Present Position, Acceleration, Vertical Speed, Ground Speed, ground track. And, therefore, derives wind info.

24
Q

IRS Calculation = True North + ____?

A

Database Variation based on known location.

25
Q

Left IRS is powered by____, and the right?

A

Left by AC Standby Bus, right side by AC Transfer 2.

26
Q

Both lights say “ON DC” in amber on IRS Display Unit…

A

They’re being powered by the Switched Hot Battery Bus, and expect the right to shut down in 5 mins. If on ground, horn will sound to shout the battery draining condition.

27
Q

ALIGN on MSU

A

For alignment only; make sure no a/c movement; enter most accurate position in POS INIT page: (N/S)DD,MM.m(E/W)DDDMM.m

28
Q

Flashing ALIGN on IRDU?

A

LEAVE IN nav MODE!!!!
Poss 1: Entered & Stored position differ. (so enter correct one twice)
Poss 2: in spite of correct entry, make a 3rd correct entry because perhaps the ADIRUs disagree.
Poss 3: Format
Poss 4: A/c moving.

29
Q

How long to align?

A

5-17 mins, but not more than 10 between N60 and S60. LEAVE IN NAV mode.

30
Q

ATT mode on IRS Display Unit?

A

can enter manual heading with key pad. after done once, it is automatically calculated. If you did this in flight because of a FAULT light,
a) for L side IRS, pitch A and Roll B are failed.
b) WXR stab failed both sides
c) L: Intertial Attitude, VS, and Nav: are failed.
Use the Both on R function of IRS cont.panel.
Auto-throttle automatically made the jump to the right side. AFTER initial entry of hdg, get att and hdg restored.

31
Q

How to test IRS and what to expect?

A

Use function of IRSDU during alignment only

32
Q

HDG/STS mode?

A

5, 4, 3, 2, 1, HDG.

33
Q

NAV detent to Align detent on IRS?

A

zeroes the GS error.

34
Q

OFF to Align detent on IRS?

A

Initializes alignment process

35
Q

When would you use ALIGN instead of just going to NAV?

A

Fast Re-alignment, after entering LAST POS in POS INIT. But the inaccuracies mount more quickly.

36
Q

MASTER caution “IRS” on panel?

A

FAULT, DC FAIL, ON DC