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Flight Validation Process of RNP APCH Procedures: Thailand Case Study

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Presentation on theme: "Flight Validation Process of RNP APCH Procedures: Thailand Case Study"— Presentation transcript:

1 Flight Validation Process of RNP APCH Procedures: Thailand Case Study
ICAO Asia-Pacific GNSS Seminar Bangkok, Thailand 26 March 2012 1

2 Presentation Outline Background
Objectives of Flight Validation for RNP APCH Requirements Step-by-step process Pre-flight In-flight Post-flight Reporting

3 Background RNP APCH = RNAV (GNSS) Using GNSS for approach operation
For aircraft with RNP 0.3 capability Utilize Aircraft-Based Augmentation System (ABAS) May include Baro-VNAV

4 Phuket PBN Implementation
4

5 Procedures for Phuket 09 Yellow – Current VOR Track Green - PBN Track
5 5

6 Objectives of Flight Validation
Proposes of Flight Validation of RNP APCH Correctness of Procedure Correctness of Chart Correctness of Navigation Database Reliability of Navigation System Signal interference Important GNSS parameters will be automatically recorded Conformity with ground based Navaids (VOR, DME) as necessary Environmental Conditions Obstacle Clearance  thus FLC needs to be conducted during day-time Flyability

7 Requirements Standards Qualification Equipment
ICAO Doc 9906 Vol 5 and 6 (Flight Validation) ICAO Doc 8071 (as necessary) Qualification Pilots and FIS technicians trained on RNAV flight validation and GNSS (ICAO Doc 9906 Vol 6) Equipment Flight Management System (FMS) Baro-VNAV capability for Baro-VNAV procedures Flight Inspection System (FIS) Navigation Database

8 Requirements: Flight Management System
FMS – HS-CNS equipped with Pro Line 21 avionics Certified GPS Receiver – TSO 129a is continuously checking the integrity of the GPS position solution through RAIM Fault Detection Capability

9 Requirements: Flight Inspection System
Automatic Flight Inspection System (AFIS) Fully automated Record archives both as print-out and electronic database

10 Pre-Flight Activities Initial Validation ATC coordination
Weather forecast GNSS service prediction Number of GPS satellite Dilution of Precision (DOPs) RAIM Outage Satellite image of expected flight path (recommended) Assessment of GNSS interference as needed

11 Pre-flight: Initial Validation
Simulation of Procedure Using FMS simulator and FIS software to validate the design Reduce risks of error If no error detected, upload to aircraft FMS and FIS

12 Pre-flight: GNSS Service Prediction

13 Pre-flight: Satellite Image
Yellow – Current VOR Track Green - PBN Track 13 13

14 In-Flight For each RNAV(GNSS) Approach Fly all segments and holdings
At least one FLC for each LNAV and LNAV/VNAV profiles At least one FLC for entire missed approach profile Preferably fly using auto-pilot Fly final approach segment as designed and at 100 ft below the designed altitude Identify controlling obstacles Check obstacle clearance Assess fly-ability and workloads Record GNSS data for all legs flown

15 In-Flight: GNSS Interference
As necessary Under scope of flight inspection, not flight validation Look at impact on service interruption RAIM Alert Loss of GNSS Service Interference may not result in full loss of GNSS services

16 In-Flight: GNSS Interference
Importance Parameters Number of Satellites Signal to Noise Ration Dilution of Precision

17 Post-Flight Activities Data Analysis and Interference Assessment
Flight Validation Report

18 Post-flight: Automated Data Recording

19 Post-flight: GNSS Interference Assessment
Record and analysis of satellite availability, signal-to-noise ratio, and Dilution of Precision (DOPs).

20 Post-flight: Flight Validation Report

21 Summary To ensure safety of flight operation, proper flight validation needs to be conducted using: Proper equipments Qualified personal Proven process

22 Thank you for your attention.


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