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Flight Test Hazard Planning Near the Speed of Light

· NASA (NTRS) · 2007

Public domain · NASA (NTRS)Technical Reports

Overview

A viewgraph presentation describing flight test safety near the speed of light is shown. The topics include: 1) Concept; 2) Portal Content; 3) Activity to Date; 4) FTS Database Updatd FAA Program; 5) FAA Flight Test Risk Management; 6) CFR 14 Part 21.35 Current and proposed changes; 7) An Online…

Publisher
NASA (NTRS)
Document
Year
2007
Pages
46
Chapters
2

PART 21 CHANGES

PART 21 CHANGES

PART 21 CHANGES

FTS Database Update Federal Aviation Administration May. 2007

CFR 14 Part 21.35 Current

CFR 14 Part 21.35 Current

• Para (d) only requires parachutes and emergency • Para (d) only requires parachutes and emergency egress provisions for certification flight tests egress provisions for certification flight tests • Para (e) excludes gliders and manned free balloons • Para (e) excludes gliders and manned free balloons in pilot decision to discontinue flight test due to in pilot decision to discontinue flight test due to hazards hazards • These rules are severely outdated • These rules are severely outdated FTS Database Update Federal Aviation Administration May. 2007

CFR 14 Part 21.35 Proposed Changes

CFR 14 Part 21.35 Proposed Changes

• • Para (d) will require a Para (d) will require a Risk Assessment Risk Assessment (may (may include parachutes and/or emergency egress) include parachutes and/or emergency egress) • Broader in scope and in line with industry standard • Broader in scope and in line with industry standard • Para (e) will include gliders and manned free • Para (e) will include gliders and manned free balloons in pilot decision to discontinue flight test balloons in pilot decision to discontinue flight test due to hazards due to hazards • Unknown why these were excluded • Unknown why these were excluded • Immediately Adopted Rule (IAR) expected in 2007 • Immediately Adopted Rule (IAR) expected in 2007 FTS Database Update Federal Aviation Administration May. 2007

CONCEPT

Regulation Regulation Guidance Guidance Part 21.35 Part 21.35 4040.26A 4040.26A Tools Tools Database Database FTS Database Update Federal Aviation Administration May. 2007

Database

Database

• FAA needs a database to complete the process • FAA needs a database to complete the process • We joined forces with NASA ’ s lessons Learned • We joined forces with NASA ’ s lessons Learned Handbook process Handbook process • We established an MOU with NASA • We established an MOU with NASA • NASA contracted with NTPS for populating the data • NASA contracted with NTPS for populating the data • • We provided funding for initial data development for We provided funding for initial data development for civil certification CFR Parts 23, 25, 27, 29, 31 civil certification CFR Parts 23, 25, 27, 29, 31 • Part 25 THA ’ s “ complete ” • Part 23/27/29/31 under construction FTS Database Update Federal Aviation Administration May. 2007

An Online Resource for

Flight Test Safety Planning

Greg Lewis National Test Pilot School T e s t H a z a r d A n a l y s i s W o r k s h e e t T e s t T i t l e : H a z a r d S u b j e c t i v e P r o b a b i l i t y o f O c c u r r e n c e S t a l l C h a r a c t e r i s t i c s C a t e g o r y h i g h p r o b a b l e u n c e r t a i n r e m o t e i m p r o b a b l e c a t a s t r o p h i c A i r c r a f t / S y s t e m : c r i t i c a l N T P S D e m o S o r t i e m a r g i n a l n e g l i g i b l e

Hazard

H a z a r d : A i r c r a f t d e p a r t s c o n t r o l l e d f l i g h t a n d i m p a c t s g r o u n d .

C a u s e : L o s s o f c o n t r o l .

Cause

E f f e c t : L o s s o f a i r c r a f t a n d c r e w .

M i n i m i z i n g P r o c e d u r e s : 1 . M i n i m u m e n t r y a l t i t u d e - 2 0 0 0 f t . A G L ( B - 3 5 4 0 0 0 f t A G L , t u r p o p r o p / j e t 5 0 0 0 f t A G L )

Effect

2 . N o a g g r a v a t e d i n p u t s t a l l s . A l l s t a l l s a c c o m p l i s h e d “ b a l l - c e n t e r e d ” 3 . N o a s y m m e t r i c p o w e r s t a l l s i n m u l t i e n g i n e a i r c r a f t .

4 . B u i l d u p a p p r o a c h : i . f o r w a r d c g b e f o r e a f t i i . p o w e r o f f b e f o r e p o w e r o n i i i . w i n g s l e v e l b e f o r e t u r n i n g Minimizing i v . 1 k t / s e c b e f o r e a c c e l e r a t e d v . t e r m i n a t e b u i l d u p i f F A R b a n k a n g l e l i m i t s a r e e x c e e d e d Procedures 5 . D o n o t a d d p o w e r d u r i n g r e c o v e r y u n t i l a b o v e 1 . 2 V s 6 . D e p a r t u r e / s p i n r e c o v e r y d i s c u s s e d i n p r e f l i g h t b r i e f i n g .

E m e r g e n c y P r o c e d u r e s : 1 . I f a i r c r a f t d e p a r t s c o n t r o l l e d f l i g h t , i m m e d i a t e l y r e t a r d p o w e r t o i d l e a n d c e n t r a l i z e c o n t r o l s .

EP ’ s

2 . I f a i r c r a f t e n t e r s s p i n , a c c o m p l i s h s p i n r e c o v e r y p r o c e d u r e .

Residual

R i s k L e v e l ( a f t e r m i n i m i z i n g p r o c e d u r e s t a k e n i n t o a c c o u n t ) : H i g h M e d i u m L o w X .

NTPS

Risk

Data Gathering

• NTPS THA ’ s – Demonstration of classic Flight Test Techniques – Conservative limits • Added inputs from the FAA – Aircraft Certification Offices in New York and Atlanta • Next collected data from manufacturer ’ s – Boeing Long Beach, Gulfstream, Lockheed, Bombardier, Cessna, Raytheon, Boeing Seattle, Schweizer, Tiger, Boeing Rotary Systems, New Piper and Sikorsky – data still coming in • All existing safety planning info, freely shared

NTPS

NTPS Role

• After gathering data – We put the data into a common format – Not asking industry to change their process • just share what they have

Hazard

Cause

Test

Mitigation

Details

NTPS

NTPS Role (cont ’ d)

• Too many ways of saying nearly the same thing • “ Mature ” the data – To make the database useful to a user, there must be some integration of inputs – Mitigations consolidated by • Hazard (e.g. Loss of Control) and by • Maneuver (e.g. Stalls) – Mine the data to: • Extract the unique safety suggestions in each area • Remove duplication • Make the database easier to use

NTPS

Part 25 Stall Hazards

Example Maturation

Part 25 Stall Hazards

Many Varied Inputs

• Six different organizations submitted inputs for stalls • Total of 66 different THA ’ s – Many redundant / nearly the same “ There is a risk of stall/departure • Used 19 different Hazard Titles from controlled flight when • Used 14 different Maneuver Names increasing angle-of-attack at low • A plethora of verbose Hazards identified airspeeds. ” • Hundreds of mitigations – Again many were redundant

NTPS

Matured Stall Hazards

• In the end, six stall hazards were identified 1. Loss of control 2. Loss of operating engine(s ) 3. Stall/spin chute fails to deploy 4. Stall/spin chute fails to jettison when commanded 5. Recovery chute uncommanded deployment 6. Departing runway surface (During ground test of stall spin chute)

NTPS

Loss of Control Mitigations

• “ Loss of Control ” mitigations matured into just twelve • The matured mitigations include: 1. Do stall testing in a buildup approach : a. from least risk to highest risk i. forward cg, mid cg, aft cg ii. Power off before power on iii. Wings level before turning iv. 1 kt /sec before 3 kt /sec b. terminate buildup if FAR limits on bank angle are exceeded at any point of the buildup

NTPS

Mitigations (continued)

2. Establish minimum altitudes for: a. entry, b. recovery initiation, c. recovery chute deployment and d. manual bailout.

3. Perform pre-flight checks of stall warning and stick pusher, as applicable.

4. Anti-spin chute must be installed, functional and armed. Perform pre-flight and pre-maneuver checks of chute as applicable.

5. Minimum crew onboard.

6. Emergency Egress system must be installed and armed. Perform pre-flight and pre-maneuver checks of egress system as applicable.

NTPS

Mitigations (continued)

7. Crew to wear helmets and parachutes .

8. Surface winds must be less than xx kts (parachute dependent).

9. No aggravated input stalls . All stalls will be ball centered.

10. No asymmetric power stalls.

11. If departing controlled flight retard throttles to idle and centralize controls .

12. Do not add power during recovery until airspeed is increasing above 1.2 Vs.

NTPS

Information Aviation Links Look for “ Test Hazard Database ”

NTPS

FAA Access

NTPS

FAA Access

NTPS

FAA Access

NTPS

http:// pbma.nasa.gov/ftsdb/home.aspx

NTPS

http:// pbma.nasa.gov/ftsdb /

NTPS

NTPS

NTPS

NTPS

NTPS

NTPS

NTPS

NTPS

Test

Details

Hazards

Causes

Mitigations

NTPS

NTPS

In Conclusion

• The matured THA database IS a wide array of test safety ideas and suggestions – But it is NOT an FAA-mandated solution – It is NOT a government-approved solution – And it is NOT an auto-safety planning device • The matured hazards, causes and mitigations are necessarily generic • Your test will have unique problems and will require unique solutions • The THA database can be an excellent starting point

NTPS

In Conclusion

• Military/Research Lead Date/Ti Test Database Status me Area – Data under development rd Kurt 3 Fixed Wing at monthly Webex/ telecon Blankenshi Wednesday Icing meetings p (Glen at 0900 Research PST Center) st Kim Hanks 1 Rotary (Army Test Thursday Wing Icing & Training at 0900 Center) PST th Brian 4 Propulsion Markowich Thursday (NAVAIR at 0900 Pax River) PST • Contact Joe Orwat FTS Database Update Federal Aviation (x3866) or Bart Administration May. 2007 Henwood (x5746) At NASA Dryden (661)

In Conclusion

In Conclusion

ν Military/Research Database Status ν Military/Research Database Status ν ν Data under development at monthly Webex/ telecon Data under development at monthly Webex/ telecon meetings meetings Lead Date/Tim Test Lead Date/Tim Test e Area e Area rd rd Kurt Blankenship (Glen 3 Wednesday Fixed Wing Kurt Blankenship (Glen 3 Wednesday Fixed Wing Research Center) Research Center) at 0900 PST at 0900 PST Icing Icing st st Kim Hanks (Army Test & 1 Thursday at Rotary Kim Hanks (Army Test & 1 Thursday at Rotary Training Center) 0900 PST Wing Icing Training Center) 0900 PST Wing Icing th th Brian Markowich (NAVAIR Pax 4 Thursday at Propulsion Brian Markowich (NAVAIR Pax 4 Thursday at Propulsion River) 0900 PST River) 0900 PST

Next Year ’ s activity

Next Year ’ s activity

ν ν Initiate DDC for research/military flight test Initiate DDC for research/military flight test ν ν High AoA High AoA ν Continue portal development activity ν Continue portal development activity ν Input/Data Submission Module ν Input/Data Submission Module ν ν Create reference information Create reference information ν ν Airworthiness and flight safety review process Airworthiness and flight safety review process ν ν Hazard management process Hazard management process

Come Join Us!

Come Join Us!

Lead Manager: Barton Henwood

Lead Manager: Barton Henwood

Aviation Safety Manager Aviation Safety Manager NASA Dryden Flight Research Center NASA Dryden Flight Research Center barton.e.henwood@nasa.gov barton.e.henwood@nasa.gov (661) 276-5746 (661) 276-5746

Deputy Manager: Joe Orwat

Deputy Manager: Joe Orwat

Lead System Safety Engineer Lead System Safety Engineer AS&M (NASA Contractor) AS&M (NASA Contractor) joe.orwat@nasa.gov joe.orwat@nasa.gov (661) 276-5746 (661) 276-5746

Come Join Us!

Come Join Us!

FAA Lead: Rod Huete

FAA Lead: Rod Huete

Flight Test Pilot Flight Test Pilot New York Aircraft Certification Office New York Aircraft Certification Office r odrigo.j.huete@faa.gov r odrigo.j.huete@faa.gov (516) 228-7318 (516) 228-7318

FAA Deputy: John Hed

FAA Deputy: John Hed

Flight Test Engineer Flight Test Engineer Seattle Aircraft Certification Office Seattle Aircraft Certification Office j ohn.hed@faa.gov j ohn.hed@faa.gov (425) 917-6518 (425) 917-6518

Flight Test Safety

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Source & rights

Source: ntrs.nasa.gov. Public-domain U.S. Government work (17 USC §105) — freely reproducible.

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Document details

Doc number
Publisher
NASA (NTRS)
Year
2007
Pages
46
File size
3.0 MB
Chapters
2