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LPV. Retrofit experience from a Part 21J DOA
EGNOS workshop
27 September 2016
About us
• World-wide multi-disciplinary company. Charter,
management, maintenance.
• EASA/FAA Part 145, Part 21J & G, Part M
• UK MAOS and DAOS certified
• Engine repair and overhaul (Lycoming & CMI), including
components and NDT
• Fixed wing & rotary maintenance and modification
• Authorised service facilities (Beechcraft, Cirrus, Twin
Commander)
• Avionics specialists- Garmin design partner
LPV. How to certify the aircraft
Requirement of our STC
To approve an existing Garmin GPS installation for LPV
Provide a simple upgrade path for non-WAAS aircraft
Minimize any additional rework of the aircraft
Gain exemptions from restrictive certification requirements
Cessna 172 with single
GNS430W and raw
CDI – no slaved HSI.
The STC solution.
Garmin GNS 430W/530W.
The first LPV capable GPS
unit for general aviation.
Over 130,000 made
between 1998 and 2012.
What aircraft are included in this EASA
LPV STC?
• All EASA-certified single-crew Part 23 aircraft (including single and
twin turboprops such as Pilatus PC12 and Beech 1900).
• In total 1150 specific aircraft types or variants!
Excluded aircraft
• Part 23 Light jets which can be operated as 2-crew
per the EASA type certificate.
• Any aircraft on the Part 23 EASA orphaned list.
What specific GPS units are approved?
• Garmin GNS unit of the following versions:
• GNS530W, GNS530AW, GNS530W-TAWS, GNS530AW-TAWS
• GNS430W, GNS430AW
• Only one GPS unit is required.
• Additionally:
The STC includes upgrading any of the non-WAAS units to the
equivalent WAAS version
Note: You can’t add additional capability such as TAWS under this
STC.
Other LPV equipment for general aviation
• Garmin G1000 (with GIA63W units).
TC/STC upgrades or system retrofit STC
such as KingAir series
• Garmin GTN750/650 – existing EASA
Part 23 AML STC plus individual STCs for
light jets and helicopters.
• Avidyne IFD540/440 – existing EASA Part
23 AML STC
LPV STC approval history
• Sponsored by UK NATS through Professional Air Training.
• First locally available airport was Alderney in Channel Islands
• Initial STC issued in Dec. 2011 for Beech single/twin piston types
• Second STC in parallel for Aurigny Airlines using the BN Trislander.
• Aurigny were the first European commercial operator approved to
perform LPV operations
• STC extended in 2015 to include most Part 23 aircraft under a
sponsorship agreement with GSA and with support from PPL-IR.
Airworthiness requirements
• AMC20-4A for BRNav (RNav 5)
• AMC20-28 for LPV
• AMC20-27A for APV Baro VNav (but using geometric altitude per
EASA CM-AS-002 iss 2)
• JAA TGL-10 for PRNav
• Under the FAA, the above come under AC20-138d and AC90-107.
Pre-requisite LPV requirements
• An E/TSO C146 WAAS GPS
• A standard deviation display within the primary field of view (EFIS or
mechanical indicator)
• Alternate means of Nav (VOR, DME etc) in the event of GPS failure
(required by all compliance standards)
• Alternative means of Comm (to meet AC23-1309-1E appendix 1 –
total loss of all Nav and comm is hazardous).
• ADF to be retained where an LPV uses an NDB for the missed
approach procedure.
Specific LPV aircraft certification
requirements
• Displayed Nav source and GPS status annunciation within the
primary field of view.
• Auto-slewed course pointer
• Distance display to the fictitious threshold within the primary field of
view (AMC20-27A and 20-28 requirement)
Achieved deviations for GA aircraft
• No auto-slewed
course pointer
• No additional
annunciators in most
aircraft.
• GPS distance can be
on the GPS unit in
the radio stack
An easily compliant cockpit
Piper PA28 with Garmin G600 EFIS and dual GNS-W.
Key achievements
This STC harmonises the aircraft requirements with Garmin’s
GNS-W FAA STC and also matches the requirements of the
similar GTN650/750 series EASA STC
It allows LPV certification without the need to install a dedicated
set of remote annunciators subject to panel layout provisions
No Auto-slewed course pointer
Distance display can be on the GPS unit in the radio rack
The EASA approval process
Initial application and pay the STC fees
Agree the certification plan – compliance with regulations and
negotiate agreed deviations
Agree the content of the aircraft model list. Only include aircraft
that have a current EASA TC.
Complete a trial installation and gain an EASA permit-to-test
Conduct a series of test flights (witnessed by a UK CAA test pilot)
Submit the full data pack including flight test and AFM
supplement to EASA for approval.
The test flights
Three approaches flown on
each end of the runway.
– two manual and one auto-
pilot coupled.
Flight test data
Data recorded using a Shadin
Avionics portable GPS logger and
data imported into Google Earth for
map overlay.
The STC process – good and bad
• EASA Positives:
• Mutual recognition of TSOs between EASA and FAA.
• AML STCs - allowing multiple aircraft types within a single STC.
• Negatives:
• Lack of harmonised requirements between EASA and FAA. Need a
single GPS airworthiness AMC as per FAA AC20-138d
• Need to allow the DOA to work fully within the terms of it’s approval:
• Timescales – STCs can easily take over 6 months!
• Automatic repeat fees if a project rolls over 12 months!
Future STC plans
• Additional STCs on Part 23 2-crew light jets
• STCs for orphaned aircraft.
• Helicopter approvals.
• Part 25 regional turbo-props and business jets.
I’ve bought this STC. What next?
• The aircraft requires a conformity inspection and for some specific
testing to be carried out. This work must be certified by an approved
maintenance company or Part 66 B2 engineer.
• If the aircraft is compliant, then issue the logbook entry, install the
new AFM supplement and you’re approved.
• Part NCO has removed the need for any specific operational
approval for non-commercial operators in GA but there are future
PBN training requirements.
• AOC holders will need specific approvals in their operations manuals
and provide crew training.
How much does it cost?
• STC data package is €300 per aircraft.
Note: No additional changes can be incorporated into the data to suit a particular aircraft.
• The STC can be bought directly by owners or maintenance
companies.
• Must work with a Garmin dealer if WAAS upgrade required.
• Implementation cost is between the owner and their maintenance
provider who will be carrying out the aircraft conformity inspection.
Typically around 4 hours of labour for an aircraft that is physically
compliant.
• Garmin’s retail price for a GNS WAAS upgrade is US $3300 (plus
local taxes) and includes the new GA35 antenna.
Any questions?
Contact details
Questions on the STC and certification:
Harry Lees (Project Specialist)
Harry.lees@gamaaviation.com.
+44 (0) 7860 860744
To buy a copy of the STC:
Contact the Part 21J design office
doa@gamaaviation.com
+44 (0) 1276 857888
To have your aircraft upgraded by us:
Nigel Smith (Avionics Manager)
Nigel.smith@gamaaviation.com
+44 (0) 1276 859283
+44 (0) 7557 160806
Thank you for listening.

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LPV aircraft certification. EGNOS workshop

  • 1. LPV. Retrofit experience from a Part 21J DOA EGNOS workshop 27 September 2016
  • 2. About us • World-wide multi-disciplinary company. Charter, management, maintenance. • EASA/FAA Part 145, Part 21J & G, Part M • UK MAOS and DAOS certified • Engine repair and overhaul (Lycoming & CMI), including components and NDT • Fixed wing & rotary maintenance and modification • Authorised service facilities (Beechcraft, Cirrus, Twin Commander) • Avionics specialists- Garmin design partner
  • 3. LPV. How to certify the aircraft
  • 4. Requirement of our STC To approve an existing Garmin GPS installation for LPV Provide a simple upgrade path for non-WAAS aircraft Minimize any additional rework of the aircraft Gain exemptions from restrictive certification requirements Cessna 172 with single GNS430W and raw CDI – no slaved HSI.
  • 5. The STC solution. Garmin GNS 430W/530W. The first LPV capable GPS unit for general aviation. Over 130,000 made between 1998 and 2012.
  • 6. What aircraft are included in this EASA LPV STC? • All EASA-certified single-crew Part 23 aircraft (including single and twin turboprops such as Pilatus PC12 and Beech 1900). • In total 1150 specific aircraft types or variants!
  • 7. Excluded aircraft • Part 23 Light jets which can be operated as 2-crew per the EASA type certificate. • Any aircraft on the Part 23 EASA orphaned list.
  • 8. What specific GPS units are approved? • Garmin GNS unit of the following versions: • GNS530W, GNS530AW, GNS530W-TAWS, GNS530AW-TAWS • GNS430W, GNS430AW • Only one GPS unit is required. • Additionally: The STC includes upgrading any of the non-WAAS units to the equivalent WAAS version Note: You can’t add additional capability such as TAWS under this STC.
  • 9. Other LPV equipment for general aviation • Garmin G1000 (with GIA63W units). TC/STC upgrades or system retrofit STC such as KingAir series • Garmin GTN750/650 – existing EASA Part 23 AML STC plus individual STCs for light jets and helicopters. • Avidyne IFD540/440 – existing EASA Part 23 AML STC
  • 10. LPV STC approval history • Sponsored by UK NATS through Professional Air Training. • First locally available airport was Alderney in Channel Islands • Initial STC issued in Dec. 2011 for Beech single/twin piston types • Second STC in parallel for Aurigny Airlines using the BN Trislander. • Aurigny were the first European commercial operator approved to perform LPV operations • STC extended in 2015 to include most Part 23 aircraft under a sponsorship agreement with GSA and with support from PPL-IR.
  • 11. Airworthiness requirements • AMC20-4A for BRNav (RNav 5) • AMC20-28 for LPV • AMC20-27A for APV Baro VNav (but using geometric altitude per EASA CM-AS-002 iss 2) • JAA TGL-10 for PRNav • Under the FAA, the above come under AC20-138d and AC90-107.
  • 12. Pre-requisite LPV requirements • An E/TSO C146 WAAS GPS • A standard deviation display within the primary field of view (EFIS or mechanical indicator) • Alternate means of Nav (VOR, DME etc) in the event of GPS failure (required by all compliance standards) • Alternative means of Comm (to meet AC23-1309-1E appendix 1 – total loss of all Nav and comm is hazardous). • ADF to be retained where an LPV uses an NDB for the missed approach procedure.
  • 13. Specific LPV aircraft certification requirements • Displayed Nav source and GPS status annunciation within the primary field of view. • Auto-slewed course pointer • Distance display to the fictitious threshold within the primary field of view (AMC20-27A and 20-28 requirement)
  • 14. Achieved deviations for GA aircraft • No auto-slewed course pointer • No additional annunciators in most aircraft. • GPS distance can be on the GPS unit in the radio stack
  • 15. An easily compliant cockpit Piper PA28 with Garmin G600 EFIS and dual GNS-W.
  • 16. Key achievements This STC harmonises the aircraft requirements with Garmin’s GNS-W FAA STC and also matches the requirements of the similar GTN650/750 series EASA STC It allows LPV certification without the need to install a dedicated set of remote annunciators subject to panel layout provisions No Auto-slewed course pointer Distance display can be on the GPS unit in the radio rack
  • 17. The EASA approval process Initial application and pay the STC fees Agree the certification plan – compliance with regulations and negotiate agreed deviations Agree the content of the aircraft model list. Only include aircraft that have a current EASA TC. Complete a trial installation and gain an EASA permit-to-test Conduct a series of test flights (witnessed by a UK CAA test pilot) Submit the full data pack including flight test and AFM supplement to EASA for approval.
  • 18. The test flights Three approaches flown on each end of the runway. – two manual and one auto- pilot coupled.
  • 19. Flight test data Data recorded using a Shadin Avionics portable GPS logger and data imported into Google Earth for map overlay.
  • 20.
  • 21. The STC process – good and bad • EASA Positives: • Mutual recognition of TSOs between EASA and FAA. • AML STCs - allowing multiple aircraft types within a single STC. • Negatives: • Lack of harmonised requirements between EASA and FAA. Need a single GPS airworthiness AMC as per FAA AC20-138d • Need to allow the DOA to work fully within the terms of it’s approval: • Timescales – STCs can easily take over 6 months! • Automatic repeat fees if a project rolls over 12 months!
  • 22. Future STC plans • Additional STCs on Part 23 2-crew light jets • STCs for orphaned aircraft. • Helicopter approvals. • Part 25 regional turbo-props and business jets.
  • 23. I’ve bought this STC. What next? • The aircraft requires a conformity inspection and for some specific testing to be carried out. This work must be certified by an approved maintenance company or Part 66 B2 engineer. • If the aircraft is compliant, then issue the logbook entry, install the new AFM supplement and you’re approved. • Part NCO has removed the need for any specific operational approval for non-commercial operators in GA but there are future PBN training requirements. • AOC holders will need specific approvals in their operations manuals and provide crew training.
  • 24. How much does it cost? • STC data package is €300 per aircraft. Note: No additional changes can be incorporated into the data to suit a particular aircraft. • The STC can be bought directly by owners or maintenance companies. • Must work with a Garmin dealer if WAAS upgrade required. • Implementation cost is between the owner and their maintenance provider who will be carrying out the aircraft conformity inspection. Typically around 4 hours of labour for an aircraft that is physically compliant. • Garmin’s retail price for a GNS WAAS upgrade is US $3300 (plus local taxes) and includes the new GA35 antenna.
  • 26. Contact details Questions on the STC and certification: Harry Lees (Project Specialist) Harry.lees@gamaaviation.com. +44 (0) 7860 860744 To buy a copy of the STC: Contact the Part 21J design office doa@gamaaviation.com +44 (0) 1276 857888 To have your aircraft upgraded by us: Nigel Smith (Avionics Manager) Nigel.smith@gamaaviation.com +44 (0) 1276 859283 +44 (0) 7557 160806
  • 27. Thank you for listening.