FMS-HGS Flashcards

1
Q

Can the FMS be used if the database is out of date?

A

Yes

Current charts shall be used when comparing instrument flight procedures against an out-of-date navigation database.

Enroute and Terminal Operations (SIDs, STARs, and DPs)

FOM2.3.1

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2
Q

VNAV vertical path angles are limited to not more than:

A

VNAV

• VNAV vertical path angles greater than 6° in enroute and terminal mode and greater than 4° in approach mode are prohibited.

FSM 1.8.6

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3
Q

FMS temperature compensation procedures must be applied to approaches at what reported airfield temperature?

A

For temperatures of 0°C or less, pilots shall apply temperature compensation to published Instrument Approach Procedures to ensure adequate obstacle clearance.

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4
Q

What types of FMS approaches require two operational FMSs?

A

Two operational UNS-1Ew FMSs with functioning GPS sensors are required for any RNAV (RNP) approach or for any RNAV approach to LPV minimums.

FSM 7.6.19

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5
Q

Can an FMS-based approach be continued beyond the FAF with a POS annunciation on the PF FMS?

A

No, an FMS missed approach is required.

FSM 7.6.32

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6
Q

Does an FMS approach and the associated approach transition (if required) have to be retrieved from the FMS database?

A

A transition shall always be loaded with an approach. If a transition is not loaded, FMS may not fly approach properly.

FSM 7.6.9

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7
Q

Can you manually build a missed approach procedure in the FMS and fly it if IMC?

A

No, all missed approaches must be loaded from the database

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8
Q

Which type of FMS approach requires tuning of a ground based NAVAID?

A

Localizer Approaches
Localizer approaches may be flown using the FMS provided:
• The approach procedure is titled LOC or BC. Do not use the LOC-only minimums of an ILS.
• Both VHF nav receivers are tuned to the localizer frequency.

FSM 7.6.20

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9
Q

Can the final segment of an ILS approach be flown utilizing the FMS as primary navigation?

A

• Any portion of an ILS approach may be flown via the FMS except for the final segment. The final segment of an ILS shall be flown via ground-based ILS guidance. Normally the missed approach is flown via LNAV.

FSM 7.6.20

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10
Q

Is the autopilot required to be used during RNP less than .3 approaches?

A

RNAV (RNP) Approaches
• The UNS-1Ew FMS is approved for RNAV (RNP) approaches to an RNP level of:
- With flight director, 0.30 nm for approach,
- With Autopilot, 0.10 nm for approach, and
- Less than 1.0 nm for missed approach.

Bulletin 13-16FSM

Use of autopilot is required for approaches when using lines of minima less than RNP 0.30.

Bulletin 13-6 FSM

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11
Q

Is manually selecting the RNP value to .1 in the FMS prohibited?

A

Yes
Manual selection of RNP value in the FMS is prohibited.

Bulletin13-08 FSM

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12
Q

Under what conditions do you not have to go missed approach when the CDI
is full scale deflection on a RNP approach?

A

NOTE: Momentary full scale deflection of the CDI needle associated with a waypoint crossing that includes a course change or a reduction in RNP does not require an immediate missed approach provided the aircraft acquires the new course in an appropriate manner.

Bulletin 13-12

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13
Q

What is the maximum glideslope angle when using the HGS in AIII mode?

A

Is a takeoff abort required if the HGS fails when the RVR is less than 500?

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14
Q

When conducting an ILS approach in AIII mode, the gear and flaps must be in the landing configuration prior to what point?

A

HGS must be in the AIII mode, with gear and flaps in the landing configuration prior to passing the Final Approach Fix. QX FSM 1.8.2

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15
Q

What is the proper response to an APCH WARN annunciation when below 500 feet?

A

APCH WARN is annunciated in the combiner or on the HAP below 500′ above DH. FSM 7.7.3

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16
Q

During an AIII approach, what will the first officer verify is annunciated on the HAP prior to passing the FAF?

A

First Officer shall verify AIIIRO ARM is annunciated on the HAP prior to passing the final fix. FSM 7.7.2

17
Q

Is a takeoff abort required if the HGS fails when the RVR is less than 500?

A

HGS failure, “TO WARN,” or loss of HGS symbology during takeoff below 500 RVR when the runway centerline is not in sight. FSM 2.1.13

18
Q

What are the wind limitations for Cat III approaches?

A
  • Maximum crosswind component is 15 knots. -Maximum tailwind component is ten knots. -Maximum Headwind component is 25 knots. FSM 1.8.2