EMBRAER – Safety Review Board Three Flags Test Point Execution Scale Proposal for Flight Test Risk Assessments.

Slides:



Advertisements
Similar presentations
RVSM AIRWORTHINESS PRESENTED BY COSCAP-SA.
Advertisements

1 Documentation Legal Framework Air Navigation Orders Guidelines ATS Manual Airport Manual Safety Management Manual ICAO Annexes Licenses / Certificates.
1 Regulation. 2 Organisational separation 3 Functional Separation.
The Truth… About Stalls
Stabilized Constant Descent Angle NPA’s
International Coordinating Council of Aerospace Industries Associations Preventing Runway Excursions Technical solutions From the Design and Manufacturing.
Contact Maneuvers.
NCSA SAFETY SEMINAR, 2/11/06 STALL/SPINS: HUMAN FACTORS IN ACCIDENT PREVENTION Monique Weil.
Maj Cody Allee / Tom Hanrahan Embedded Terrain Awareness Warning System (eTAWS) Adventures in testing a CFIT protection system Got Protection?
Failure Mode and Effect Analysis
1 Golden Rules Known and Not Known Every fixed-wing pilot knows that it takes more power to go slower (safely) when flying “behind the power curve”, i.e.,
Multi-Engine Training And The PTS GHAFI John Sollinger/Larry Hendrickson October 28, 2000.
By Diego M. Alfonso. DISCLAIMER JUST IN CASE WE MAY HAVE A DIFFERENCE OF OPINION, ALL THE INFORMATION USED FOR THIS PRESENTATION HAS BEEN OBTAINED FROM.
P-2028 Minnesota Wing Aircrew Training: Tasks P-2028 Crew Resource Management.
Tailwinds Flying Club Fall Safety Session Know your airplane Piper Arrow III PA28R- 201T.
Chandelles.
Aero Engineering 315 Lesson 33 GR3 Review. General strategy  Prior to class Review reading for lessons 23 – 32 Work / review problems #26 – 42 Review.
EDGE™ MAV Control System - P09122 Final Project Review Erik Bellandi – Project Manager Ben Wager – Lead Engineer Garrett Argenna – Mechanical Engineering.
#4918. When an airplane is accelerated, some attitude indicators will precess and incorrectly indicate a A- climb. B- descent. C- right turn.
Tailwinds Flying Club Spring Safety Session Know your airplane Cherokee Six 300 (PA )
1 Model 162 SkyCatcher Update Julie Filucci Cessna Pilot Center Manager.
David Gill Team Leader Airworthiness. 2 Introduction to Performance and Flying Qualities Flight Testing Two Week Short Course May 8 – 19, 2006 Intended.
Utilizing your notes and past knowledge answer the following questions: 1) Define load factor. 2) Describe the two reasons for understanding load factors.
PERFORM MULTIAIRCRAFT OPERATIONS TASK 2010 CONDITIONS: In an H-60 helicopter. STANDARDS: Appropriate common standards plus the following additions/modifications:
Stabilized Constant Descent Angle NPA’s
Office of Research and Engineering Safety Study Report: Introduction of Glass Cockpit Avionics into Light Aircraft Qualitative Analysis Results Loren Groff.
AVAT11001: Course Outline Aircraft and Terminology
Slide 1Lesson 14: Fundamentals of the CAP Flying Safety Program Fundamentals of the CAP Flying Safety Program.
B757 Review Questions. AutoFlight At what RA does flare mode engage? 45 feet RA.
READY OR NOT THE FLIGHT REVIEW. FLIGHT REVIEW A FLIGHT REVIEW IS REQUIRED WITHIN THE PREVIOUS 24 CALENDAR MONTHS TO ACT AS PIC.
AvSport of Lock Haven What’s the Spin on Stalls? Presentation Copyright © 2015 Mastering the most dreaded maneuver in flight training Prof. H. Paul Shuch,
SPUD TC (OCT 07) REVISION ACADEMICS. SPUD TASK 1114 PERFORM A ROLLING TAKEOFF.
Structural Design Considerations and Airspeeds
Air Operations Branch Director Course Safety Issues Part 1 U.S. AIR FORCE AUXILIARY U.S. AIR FORCE AUXILIARY.
1 World Dispatch Summit Toronto, Canada May 2002 ETOPS Presentation Ralph Webster Transport CanadaTransports Canada Safety & SecuritySécurité et sûreté.
Functional Check Flight Symposium Andre Tousignant C.I.M. Director Air Safety Investigation Office (ASIO) Bombardier Aerospace Vancouver Feb 8, 2011.
Office of Aviation Safety US Airways Flight 1549 Ditching on the Hudson River January 15, 2009 Katherine Wilson, Ph.D. Human Performance Capt. David Helson.
Audit Sampling: An Overview and Application to Tests of Controls
SMS Planning.  Safety management addresses all of the operational activities of the entire organization.  The four (4) components of an SMS are: 1)
Office of Aviation Safety Airspeed Selection and Stall Training Procedures Operations presentation.
Presented to: By: Dennis H. Whitley Date: March 1, 2011 Federal Aviation Administration SOUTHERN REGION FAASTeam/Area 1 Approach and Landing Accidents.
Slow Flight Chris Evans.
Presented to: By: Date: Federal Aviation Administration Noise 101: Federal Noise Laws and Regulations Town of Payson M.L. Chittick, Scottsdale FSDO January.
Single Pilot Resource Management (SRM) And The CFI
Threat and Error Management. What is TEM?  “Defensive flying”
Maintaining and Sustaining System Integrity Configuration Management for Transportation Management Systems Configuration management (CM) describes a series.
READY OR NOT THE FLIGHT REVIEW.
Ensuring the Safety of Future Developments
Lecture 6: CRUISE PERFORMANCE
VNY FSDO FAASTeam Representative
Ex. 6 - Straight-and-Level Flight Ex. 6 – Straight-and-Level Flight.
SEVESO II transposition and implementation: Possible approaches and lessons learned from member states and new member states SEVESO II transposition and.
The New Face of Assessment in the Common Core Wake County Public Schools Common Core Summer Institute August 6, 2013.
Utilizing your notes and past knowledge answer the following questions: 1) The intensity or strength of the vortices is directly proportional to the ________.
Glass cockpit safety initial transition training recurrent training ongoing proficiency program.
Flight Test Introduction 2016 Introduction to Flight Test Engineering Dan Hrehov Flight Test Engineer.
Settling with Power (vortex ring state)
Mission Aircrew Course Search Planning and Coverage
Soaring Safety Foundation
Engine Control Systems
Air Carrier Continuing Analysis and Surveillance System (CASS)
Chapter 13 Overall Audit Plan and Audit Program
Case Study Title CRM CASE STUDY.
Warm-Up – 9/14 – 10 minutes Utilizing your notes and past knowledge answer the following questions: What are the most dangerous phases of flight for.
NBAA Single Pilot Working Group
Mastering the most dreaded maneuver in flight training
NBAA Single Pilot Working Group
Chapter 13 Overall Audit Plan and Audit Program
Case Study Title CRM CASE STUDY.
MISCELLANEOUS PERF. The performance data for takeoff and landing an aircraft can be obtained from the aircraft's flight manual or pilot's operating handbook.
Presentation transcript:

EMBRAER – Safety Review Board Three Flags Test Point Execution Scale Proposal for Flight Test Risk Assessments

EMBRAER – Safety Review Board Objective Propose an alternative method to evaluate Flight Test Point Execution during Risk Assessments

EMBRAER – Safety Review Board Risk Assessment Present Day Concept Cooper Harper Application to Test Point Execution Three Flags Application to Test Point Execution Agenda

EMBRAER – Safety Review Board Test Point Execution System Failure Flight Envelope Greater of All Three Final Risk Classification OBS: Each one of them are analyzed separately and considered mutually exclusive. Risk Assessment Present Day Concept

EMBRAER – Safety Review Board Final Risk Classification Risk Assessment Present Day Concept Minimizing Risk Procedures Mitigation Procedures -simulation -training -systems improvements -analysis…etc -helicopter standing by -ambulance -firefighters -helmets parachutes -Tailchute…etc

EMBRAER – Safety Review Board Methodology came from past experience and was based on the FAA and ANAC (Brazilian Certification Authority) approved Risk Assessment Methodology Nowadays, at Embraer, the CH is used to evaluate TPE Risk along with Three Flags Scale Focused on TPE point of view only Risk Assessment Present Day Concept

EMBRAER – Safety Review Board Risk Assessment Present Day Concept Cooper Harper Application to Test Point Execution Three Flags Application to Test Point Execution Agenda

EMBRAER – Safety Review Board Cooper Harper Application to Test Point Execution Risk According to the Methodology:

EMBRAER – Safety Review Board Cooper Harper Application to Test Point Execution Risk Few more points to take into account Cooper-Harper scale is intended to evaluate the Flying Qualities of an aircraft for a specific MISSION. Cooper-Harper scale is supposed to be applied to a defined TASK. This task should define what is DESIRABLE and ADEQUATE flying performance. The CH rate is obtained AFTER the maneuver is done by the test pilot. A high Cooper Harper grade DO NOT necessarily mean a HIGH Risk maneuver.

EMBRAER – Safety Review Board Risk Assessment Present Day Concept Cooper Harper Application to Test Point Execution Three Flags Application to Test Point Execution Agenda

EMBRAER – Safety Review Board “Three Flags” Application to Test Point Execution 1.Alternative way to go 2.Participation of several test pilots and FTEs 3.Focus on what a test pilot should consider 4.DETECT if certain risks are present 5.Designed ONLY for test point execution risk evaluation

EMBRAER – Safety Review Board THREE FLAGS Test Point Execution SCALE I – Detect training or gradual approach necessities Training Try-outs Gradual Approach Can the lack or necessity of these affect Safety ? Is Needed ? And III – Detect Recovering or Discontinuing possibilities Recovering Discontinuing When The maneuver, is there a probable chance to get into unsafe situation ? II – Detect Errors Tolerances Test Tolerances Positioning Tolerances Do Affect safety if exceeded or disregarded ? And Can be Considered to be tight ?

EMBRAER – Safety Review Board QUESTION 1 RATIONALE -Indication of increased execution risk -Focus ONLY on the safety point of view (NO performance aspects) QUESTION 2 RATIONALE -How close to the aircraft limits X margins for errors -Area Restriction QUESTION 3 RATIONALE - “Difficult to handle” - Robustness and easiness of the recovering - Experience on the type of aircraft and lessons learned HELPS !! “Three Flags” Application to Test Point Execution

EMBRAER – Safety Review Board “Three Flags” TPE was successfully applied during the Embraer Phenom 100 development phase for the following Flight Test Campaigns: 1.Automatic Flight Control System 2.Controllability and Maneuverability 3.Stability 4.Autopilot Servo Sizing 5.Takeoff Transition 6.Minimum Control Speeds 7.Fuel Heat Management 8.Steering Test Without Shimmy Damper 9.In-Flight Thrust Determination 10.Engine In-Flight Start 11.Engine Inlet Distortion 12.ANAC Familiarization Flight “Three Flags” Application to Test Point Execution

EMBRAER – Safety Review Board Example: Test Point – Maximum Dive Speed Demonstrated in Flight ( Vdf ) Determination Aircraft: Choose an aircraft you are currently flying. Configuration: UP/0 Initial Altitude: ±1000 ft Trim Speed: Vmo Minimum Recovery Altitude: ft 1. TRIM aircraft at Vmo/Mmo during 10 seconds; 2. ESTABLISH a pitch attitude 7.5° (pushover maneuver Nz=0.5g) below the trimmed attitude and maintain during 20 seconds. Do not reduce thrust; 3. PERFORM a pull up maneuver with load factor 1.5g. After start pull up, THRUST REDUCTION may be used, if required. “Three Flags” Application to Test Point Execution

EMBRAER – Safety Review Board MANEUVER QUESTIONS FLAGSTPE 123 Vdf/Mdf Determination 2MEDIUM Example: Vdf is the maximum speed demonstrated in dive flight.

EMBRAER – Safety Review Board Embraer Phenom 100 Aircraft

EMBRAER – Safety Review Board CONCLUSIONS “Three Flags” Test Point Execution Scale R.A. Easier and Straight to the Point Focused on what WILL be done (future) Simple to use Consistent grades attribution

EMBRAER – Safety Review Board “Flying is an unnatural act so be ready. Prepare yourself till you think you were born that way.”

EMBRAER – Safety Review Board Three Flags Test Point Execution Scale Proposal for Flight Test Risk Assessments Maximilian Kleinübing, B.S.,Flight Test Engineer