Stage 48 Oral Flashcards
What are 6 airborne Navigation Instruments we use?
- HSI
- RMI
- ADF
- VOR
- GPS
- CDI
How would you describe control/performance, and what are the 4 steps?
- Setting attitude and power to achieve a desired performance
1. Establish
2. Trim
3. Cross-check
4. Adjust
What are the 3 common errors that occur during instrument cross-check/scan?
- Fixation
- Omission
- Emphasis
What are the 3 segments of the GPS system?
- Space (Satellites)
- Control (Ground Station)
- User (Aircraft)
How many satellites are required for triangulation, and what information will that provide?
- Need a minimum of 3 satellites
- Will provide Lat/Long coordinate only (no altitude)
What is RAIM? How many satellites does is need to function?
- Receiver Autonomous Integrity Monitoring
- An internal check (not augmentation) for bad satellite signals that will kick them out/replace with good ones
1. 5 Satellites to DETECT a bad signal
2. 6 Satellites to KICK IT OUT
What is WAAS? What does it augment, and how? (Draw a Picture)
- Wide Area Augmentation System
- Corrects GPS positioning signal errors
1. WAAS Satellites send signals to surveyed positions on the ground with known, unchanging coordinates
2. Satellite signal indications are compared with the real ground station coordinates
3. Any identified errors are signaled to a Mother-Ground Station
4. Mother-Ground Station signals a Broad-casting satellite of the error
5. Broadcasting Satellite sends out the correction to the a/c
If we lose WAAS, how does that limit us?
- Information will not be as accurate
- En-Route CDI deflection will increase to 5nm either side
- Airport you’re going to must have another type of approach available
How many satellites must be visible in order to have WAAS?
6 Satellites
Describe some aspects of the ADF. What navigation system does it rely on? What limits/errors is it subject to?
- Automatic Direction Finder (airborne)
1. Relies on NDB ground stations (HH, H, MH) - Limited to NDB SSVs and errors
2. No indication if signal is lost, must listen to Morse Code ID constantly
3. Transmits on a lower frequency, subject to more interference
4. Loop antenna and a Sense antenna determine a/c’s Relative Bearing
What is a good rule of thumb for knowing when to start you turn to establish yourself on a DME arc?
- 1% of you GS
ex: 100 knots…start your turn when you are 1nm our from the arc - UND: 0.5nm away
What 3 components are associated with the Localizer system? What equipment makes them up?
- Guidance (Localizer Antenna and Glideslope)
- Range (Marker Beacons (OM, MM, IM) picked up by DME)
- Visual (Approach, touchdown and centerline lights)
What is the SSV of a Localizer? What frequencies does it radiate?
- 35 degrees for 10nm, 10 degrees fo 18nm
- Localizer Beam: 3-6 degrees (varies), 700ft wide at Threshold (Localizer antenna always placed to achieve this)
- Right “blue” = 150 Hertz, Left “yellow” = 90 Hertz, where they intersect = centerline
What information does the Localizer Antenna provide? Where is it located and why?
- Course deviation to the Left and Right of centerline
- Full scale deflection shows 2.5 degrees on either side
- Positioned at the end of the runway to provide 3-6 degrees (varies) path and be 700ft wide at Threshold
What are some common errors when using a Localizer?
- Reflection - objects below 5,000’ AGL disrupting signal
- False Course - Glideslope
- Needle deflection when passing over - HOLD YOUR HEADING!
What is the SSV of a Glideslope? What guidance/information does it provide?
- Service Volume is 10 NM
- Based off a normal 3° glide path so that it intersects the MM at 200 feet and the OM at 1400 feet
- Course Deviation Up and Down of centerline
- Full Scale deflection shows 0.7 degrees on either side
If the ADC fails, what instruments will we lose?
- ASI
- VSI
- Altimeter
If AHRS fails, what instruments will we lose?
- Attitude Indicator
2. Heading Indicator
AS SOON AS YOU LOSE 1+ INSTRUMENTS, WHAT DO YOU DO?
RUN THE CHECKLIST
THEN: NOTIFY ATC
1. What you’ve lost
2. Whether you can continue operating IFR off the standbys
3. Whether you are in need of assistance now or in the future
- ASK FOR VECTORS
What is Equivalent airspeed?
- Calibrated AS corrected for compression error
What information does an HSI provide? What is one main component of its operation?
- Gives heading, course selector, glide slope and TO/FR indication (combines heading indicator with CDI)
- Improves situational awareness - When slaved to a Magnetic Flux Gate, it automatically updates with a/c rotation (adjusts to magnetic currents)
What is the purpose of a flux gate/valve?
- Enables compass to readily accept lines of magnetic from the Earth’s field and still indicate correct magnetic heading
(peace sign)
What gyroscopic instruments operate on Rigidity?
- Attitude Indicator
2. Heading Indicator
What gyroscopic instruments operate on Precession?
- Turn Coordinator
2. Turn-Slip Indicator