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RADIO NAV — CH.16

Area Navigation (RNAV)Radio Navigation — DGCA CPL practice questions

Question 1 of 14

The accuracy required of a precision area navigation system is:

A.0.25 NM
B.2 NM
C.1 NM
D.0.5 NM

All 14 questions — Area Navigation (RNAV)

Radio Navigation · DGCA CPL. The correct option is marked on each.

  1. Q1. The accuracy required of a precision area navigation system is:

    • A.0.25 NM
    • B.2 NM
    • C.1 NM✓
    • D.0.5 NM

    Why: P-RNAV requires position accuracy of 1 NM on 95% of occasions. B-RNAV requires 5 NM.

  2. Q2. A basic 2D RNAV system will determine tracking information from:

    • A.twin DME
    • B.VOR/DME✓
    • C.twin VOR
    • D.any of the above

    Why: A basic 2D RNAV system uses VOR/DME (rho/theta — range and bearing) to define position and compute track to waypoints.

  3. Q3. Aircraft on track WP1→WP2 (45 NM). Aircraft 20 NM from phantom station, phantom 270°/30 NM from VOR/DME. Aircraft 15 NM from VOR. Range read-out:

    • A.15 NM
    • B.20 NM✓
    • C.25 NM
    • D.30 NM

    Why: The DME display shows distance to the phantom station (waypoint) , not the real VOR/DME. The aircraft is 20 NM from the phantom station → 20 NM .

  4. Q4. The sequence of displays accessed on FMC initialization is:

    • A.POS INIT, IDENT, RTE
    • B.IDENT, RTE, POS INIT
    • C.IDENT, POS INIT, RTE✓
    • D.POS INIT, RTE, IDENT

    Why: Correct pre-flight sequence: IDENT → POS INIT → RTE . IDENT first to verify database, then position initialization, then route entry.

  5. Q5. The IRS position can be updated:

    • A.on the ground only✓
    • B.at designated positions en route and on the ground
    • C.on the ground and overhead VOR/DME
    • D.at selected waypoints and on the ground

    Why: The IRS position can only be initialized on the ground . In flight, the FMC uses Kalman filtering with external references (DME/DME, GPS) to correct IRS drift, but the IRS itself is not manually updated in flight.

  6. Q6. The position used by the FMC in the B737-400 is:

    • A.an average of the two IRS positions
    • B.an average of the two IRS positions smoothed by Kalman filtering
    • C.taken from the selected IRS, smoothed by Kalman filtering and updated to external reference✓
    • D.generated from external reference, updated by IRS as part of Kalman filtering

    Why: The FMC uses the position from the selected IRS , processed by Kalman filtering and updated by external references (DME/DME, VOR/DME, GPS).

  7. Q7. The FMC position will be at its most inaccurate:

    • A.on take-off
    • B.at TOC
    • C.at TOD✓
    • D.on final approach

    Why: IRS drift accumulates over time. The position is most inaccurate at Top of Descent (TOD) — the end of a long cruise, furthest from the last IRS alignment. FMC tries to correct with DME/GPS updates.

  8. Q8. Positions input to FMC using maximum 5 alphanumerics:

    • A.SIDs & STARs, reporting points and airways
    • B.Navigation facilities, reporting points and airways✓
    • C.SIDs & STARs and latitude/longitude
    • D.Latitude/longitude, reporting points and airways

    Why: Max 5 alphanumerics: navigation facilities (NAVAIDS), reporting points, and airways designators . SIDs/STARs use up to 7. Lat/long uses special format N5000.0E00527.0.

  9. Q9. The FMC navigation database can be accessed by pilots:

    • A.to update the database
    • B.to read information only✓
    • C.to change between 28-day updates
    • D.to change data for sector requirements

    Why: Pilots can read (interrogate) the database only . The database cannot be modified by pilots; it is updated by maintenance/data service providers every 28 days.

  10. Q10. Above 84° latitude, a twin FMS/triple IRS system goes to de-coupled operations because:

    • A.to prevent error messages as IRS longitudes show large differences✓
    • B.to ease pilot workload
    • C.to improve system accuracy
    • D.because magnetic variation changes rapidly

    Why: Above 84° latitude, the secant of latitude increases rapidly. Longitude calculations from the two IRS systems show increasingly different values → de-coupled mode prevents false gross error messages.

  11. Q11. Maximum range at which VOR bearing information is used by the B737-400 FMC:

    • A.160 NM
    • B.180 NM✓
    • C.200 NM
    • D.250 NM

    Why: The B737-400 FMC uses VOR bearing up to 180 NM from the station. Beyond this range, bearing accuracy is insufficient for Kalman filtering updates.

  12. Q12. Which of the following is NOT a waypoint definition format for the CDU:

    • A.5-letter alphanumeric
    • B.Lat/Long
    • C.range and bearing from NAVAID
    • D.bearing from two NAVAIDs✓

    Why: The bearing/bearing (BB) format (e.g. GOW167.0/TRN090.5) IS a valid waypoint format. The format NOT available is bearing from two NAVAIDs as a simple format — the CDU uses only the BB format with specific syntax.

  13. Q13. Correct format to input position 50°N 005°27'E to the CDU:

    • A.5000.0N00527.0E
    • B.N50E00527
    • C.N5000.0E00527.0✓
    • D.N5000E00527

    Why: CDU latitude/longitude format: N5000.0E00527.0 — hemisphere prefix, degrees and decimal minutes, with decimal point mandatory.

  14. Q14. The period of validity of the FMC navigation database is:

    • A.28 days✓
    • B.1 month
    • C.determined by national authority (28 to 91 days)
    • D.91 days

    Why: The FMC navigation database is valid for 28 days (one AIRAC cycle). It must be updated every 28 days to remain current.