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AIM 

cases this operation will be invisible to the pilot since the receiver will continue to operate with other available 

satellites after excluding the “bad” signal. This capability increases the reliability of navigation. 

4. 

Both lateral and vertical scaling for the LNAV/VNAV and LPV approach procedures are different than 

the linear scaling of basic GPS. When the complete published procedure is flown, 

±

1 NM linear scaling is 

provided until two (2) NM prior to the FAF, where the sensitivity increases to be similar to the angular scaling 

of an ILS. There are two differences in the WAAS scaling and ILS:  1) on long final approach segments, the initial 

scaling will be 

±

0.3 NM to achieve equivalent performance to GPS (and better than ILS, which is less sensitive 

far from the runway); 2) close to the runway threshold, the scaling changes to linear instead of continuing to 

become more sensitive. The width of the final approach course is tailored so that the total width is usually 700 

feet at the runway threshold. Since the origin point of the lateral splay for the angular portion of the final is not 

fixed due to antenna placement like localizer, the splay angle can remain fixed, making a consistent width of final 

for aircraft being vectored onto the final approach course on different length runways. When the complete 

published procedure is not flown, and instead the aircraft needs to capture the extended final approach course 

similar to ILS, the vector to final (VTF) mode is used. Under VTF, the scaling is linear at 

±1

 NM until the point 

where the ILS angular splay reaches a width of 

±

1 NM regardless of the distance from the FAWP. 

5. 

The WAAS scaling is also different than GPS TSO

C129() in the initial portion of the missed approach. 

Two differences occur here. First, the scaling abruptly changes from the approach scaling to the missed approach 

scaling, at approximately the departure end of the runway or when the pilot selects missed approach guidance 

rather than ramping as GPS does. Second, when the first leg of the missed approach is a Track to Fix (TF) leg 

aligned within 3 degrees of the inbound course, the receiver will change to 0.3 NM linear sensitivity until the 

turn initiation point for the first waypoint in the missed approach procedure, at which time it will abruptly change 

to terminal (

±

1 NM) sensitivity. This allows the elimination of close in obstacles in the early part of the missed 

approach that may otherwise cause the DA to be raised. 

6. 

There are two ways to select the final approach segment of an instrument approach. Most receivers use 

menus where the pilot selects the airport, the runway, the specific approach procedure and finally the IAF, there 

is also a channel number selection method. The pilot enters a unique 5

digit number provided on the approach 

chart, and the receiver recalls the matching final approach segment from the aircraft database. A list of 

information including the available IAFs is displayed and the pilot selects the appropriate IAF. The pilot should 

confirm that the correct final approach segment was loaded by cross checking the Approach ID, which is also 

provided on the approach chart. 

7. 

The Along

Track Distance (ATD) during the final approach segment of an LNAV procedure (with a 

minimum descent altitude) will be to the MAWP. On LNAV/VNAV and LPV approaches to a decision altitude, 

there is no missed approach waypoint so the along

track distance is displayed to a point normally located at the 

runway threshold. In most cases, the MAWP for the LNAV approach is located on the runway threshold at the 

centerline, so these distances will be the same. This distance will always vary slightly from any ILS DME that 

may be present, since the ILS DME is located further down the runway. Initiation of the missed approach on the 

LNAV/VNAV and LPV approaches is still based on reaching the decision altitude without any of the items listed 

in 14 CFR Section 91.175 being visible, and must not be delayed while waiting for the ATD to reach zero. The 

WAAS receiver, unlike a GPS receiver, will automatically sequence past the MAWP if the missed approach 

procedure has been designed for RNAV. The pilot may also select missed approach prior to the MAWP; however, 

navigation will continue to the MAWP prior to waypoint sequencing taking place. 

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19.  Ground Based Augmentation System (GBAS) Landing System (GLS) 

a. 

A GBAS ground installation at an airport can provide localized, differential augmentation to the Global 

Positioning System (GPS) signal

in

space enabling an aircraft’s GLS precision approach capability. Through 

the GBAS service and the aircraft’s GLS installation a pilot may complete an instrument approach offering 

three

dimensional angular, lateral, and vertical guidance for exact alignment and descent to a runway. The 

operational benefits of a GLS approach are similar to the benefits of an ILS or LPV approach operation. 

Navigation Aids 

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