CREW SYSTEMS - AcqNotes
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.NOT MEASUREMENTSENSITIVEJSSG-2010-730 October 1998SUPERSEDING(See 6.2)DEPARTMENT OF DEFENSEJOINT SERVICE SPECIFICATION GUIDECREW SYSTEMSCRASH PROTECTION HANDBOOKThis specification guide handbook is for guidance only.Do not cite this document as a requirement.AMSCDISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.15GP
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7FOREWORDJSSG RELEASE NOTEThe specification guides support the acquisition reform initiative, and ispredicated on a performance based business environment approach to productdevelopment. As such it is intended to be used in the preparation of performancespecifications. It is one of a set of specification guides. It is the initial release of thisguide. In this sense this document will continue to be improved as the developmentprogram is accomplished.1. This specification guide handbook is approved for use by all Departments and Agencies ofthe Department of Defense (DoD).2. This Joint Service Specification Guide (JSSG) handbook, in conjunction with its companionJSSGs handbooks, is intended for use by Government and Industry program teams asguidance in developing program unique specifications. This handbook is for guidance only.This handbook cannot be cited as a requirement. If it is, the contractor does not have tocomply. This document may not be placed on contract.3. The complete set of JSSGs, and their respective handbooks, establish a commonframework to be used by Government-Industry Program Teams in the Aviation Sector fordeveloping program unique requirements documents for Air Systems, Air Vehicles, andmajor Subsystems. Each JSSG contains a compilation of candidate references, genericallystated requirements, verification criteria, and associated rationale, guidance, and lessonslearned for program team consideration. The JSSGs identify typical requirements for avariety of aviation roles and missions. By design, the JSSG sample language for“requirements” and “verification criteria” are written as generic templates, with blanks thatneed to be completed in order to make the requirements meaningful. Program teams needto review the JSSG rationale, guidance, and lessons learned to: (1) determine whichrequirements are relevant to their application; and (2) fill in the blanks with appropriate,program-specific requirements.4. This document is Part 2 of two parts. Part 1 of the JSSG-2010 is a template for developingthe program unique performance specification. As a generic document, it containsrequirement statements for the full range of aviation sector applications. It must be tailoredto delete non-applicable requirements to form the program unique specification. In addition,where blanks exist, these blanks must be filled in for the program unique specification toform a complete and consistent set of requirements to meet program objectives. Part 2 ofthe JSSG-2010 is a handbook which provides the rationale, guidance, and lessons learnedrelative to each statement in Part 1. The section 4, verification requirements, must betailored to reflect an understanding of: (1) the design solution; (2) the identified programmilestones; (3) the associated level of maturity which is expected to be achieved at thosemilestones; and (4) the specific approach to be used in the design and verification of therequired products and processes. It must be recognized that the rationale, guidance, andlessons learned are not only generic in nature, but also document what has been successfulin past programs and practices. This must not be interpreted to limit new practices,processes, methodologies, or tools.5. Beneficial comments (recommendations, additions, deletions) and any pertinent data whichmay be of use in improving this document should be addressed to: ASC/ENSID, Bldg. 560,2530 Loop Road West, Wright-Patterson AFB OH45433-7101, by using theStandardization Document Improvement Proposal (DD Form 1426) appearing at the end ofthis document or by letter.ii
Downloaded from http://www.everyspec.com on PAGESCOPE . 11.1 Scope. . 12.APPLICABLE DOCUMENTS. 12.1 General. . 12.2 Government documents. . 12.2.1 Specifications, standards, and handbooks. . 12.2.2 Other Government documents, drawings, and publications. 92.3 Non-Government publications. . 92.4 Order of precedence. .103.REQUIREMENTS .103.1 Aircrew Systems Engineering (see JSSG-2010-1). .103.2 Crew Systems Automation, Information, and Control/Display Management(see JSSG-2010-2).103.3 Cockpit/Crew Station/Cabin (see JSSG-2010-3). .103.4 Aircrew Alerting (see JSSG-2010-4).103.5 Aircraft Lighting (see JSSG-2010-5).103.6 Sustenance and Waste Management (S&WM) Systems Requirements(see JSSG-2010-6).103.7 Crash Survivability. .103.7.1 Aircraft crash protection evelope. .173.7.2 Occupant exposure limits to crash hazards. .263.7.3 System functional requirements. .453.7.3.1 Pre-crash warning. .463.7.3.2 Contact injury protection.473.7.3.2.1Preservation of occupied space. .563.7.3.2.2Seat structural integrity and occupant retention. .643.7.3.2.3Cargo and Ancillary Equipment Retention.933.7.3.3 Acceleration Injury Protection .983.7.3.3.1Impact Energy Management .1153.7.3.4 Post-Crash Injury Protection.1213.7.3.5 Emergency Egress System .1343.7.3.5.1Emergency Exits .1373.7.3.5.2Emergency Egress Routes .1393.7.3.5.3Localized Entrapment Prevention .1413.7.3.6 Crash Data Recording .1433.7.3.7 Aircraft Integration and System Interfaces.1454.VERIFICATIONS (SEE REQUIREMENTS).1475.DEFINITIONS .147iii
Downloaded from http://www.everyspec.com on PAGENOTES .1476.1 Intended use.1476.2 Supersession data.1476.3 Subject term (key word) listing.148TABLESTable I. Crash Impact Design Conditions, With Landing Gear Extended, For Military RotorcraftAnd Light Fixed-Wing Aircraft. .18thTable II. 95 Percentile Velocity Changes For Survivable Class A And B Mishaps. .19Table III. Human Tolerance Limits To Acceleration.32Table IV. Abbreviated Injury Scale (AIS) And Sample Injury Types For Two Body Regions.33Table V. Recommended Military Lumbar Tolerance Levels. .34Table VI. Recommended Military Injury Assessment Test Methods. .43Table VII. Occupant Restraint Harness Strength Requirements (See Mil-Std-1290). .69Table VIII. Seat Crash Load Factors. .74Table IX. Cockpit Seat Design And Static Test Requirements. .84Table X. Typical Aviator Weights .87Table XI. Troop And Gunner Weights .87Table XII. FAA Summary Seat Dynamic Performance Standards .90Table XIII. Operational Energy Absorbers.103Table XIV. V-22 Crashworthiness Trade Options.118Table XV. Rotorcraft Crashworthiness Comparison .120Table XVI. Crash Resistant Fuel System Materials Comparison .131Table XVII. Summary Of Design Velocities For Rotary And Light Fixed Wing Aircraft .133iv
Downloaded from http://www.everyspec.com on GEFIGURESFigure 1. Crash Resistant Features for Rotocraft - MIL-STD-1290.13Figure 2. Aircraft Coordinate and Attitude Directions. .20Figure 3. Impact Attitude Envelope for Rotary-Wing and Light Fixed Wing Aircraft.20Figure 4. Comparison of Survivable Impact Velocity Changes For Army, Navy, and CivilRotorcraft. .23Figure 5. Comparison of Vertical Velocity Change at Major Terrain Impact vs CumulativeFrequency of Occurrence for Survivable Mishaps. .24Figure 6. NATO Designated Directions of Accelerative Forces on Body. .29Figure 7. Duration and Magnitude of Headward Acceleration (EIBAND). .30Figure 8. Duration and Magnitude of Spineward Acceleration (EIBAND). .31Figure 9. Table of Injury Assessment Values for Hybrid III ATD And HIC Injury Risk Curve. .37Figure 10. IARV Curves for Axial Neck Tension and Compression Loading.38Figure 11. IARV Curves For Neck Shear Loading and Fracture of Patella, Femur, or Pelvis. .39Figure 12. Occupant Strike Envelope with Lap Belt Only Restraint. .50Figure 13. Occupant Strike Envelope with Shoulder Harness and Lap Belt. .51Figure 14. Inflatable Body And Head Restraint System (above) and Cockpit Airbag System(below).55Figure 15. MIL-S-58095 Five-Point Restraint Harness Configuration .67Figure 16. Comparison of Lap Belt Only Versus Lap Belt–Shoulder Restraint Protection. .70Figure 17. Troop Seat Restraint Configurations .71Figure 18. View of MA-6 Inertia Reel’s Ratchet/Pawl Assembly. .78Figure 19. View of MA-6 Inertia Reel’s Damaged Ratchet Teeth. .79Figure 20. Seat Forward Load-Deflection Requirements for All Types of Rotorcraft and LightFixed-Wing Aircraft .85v
Downloaded from http://www.everyspec.com on GEFigure 21. Dynamic Test Parameters for Military Rotary-Wing and Light Fixed-Wing Aircraft.86Figure 22. Floor and Bulkhead Misalignment Diagrams for Military Seats.89Figure 23. Forward Load-Displacement for Energy Absorbing Cargo Restraint. .97Figure 24. Cargo Lateral Load-Displacement Requirements.98Figure 25. Relative Frequency of Spinal Injuries vs. Change in Vertical Velocity .100Figure 26. Occupant Response (Ride-Down) Curve .107Figure 27. Typical Vertical Response Parameters of 50th Percentile Hybrid III ATD at 20 GPeak; 7.625 m/s Velocity Change .108Figure 28. Recommended Stress-Strain Corridors for Cushion Materials .111Figure 29. V-22 Crashworthiness Trade Study Approach.117Figure 30. Schematic of V-22 Energy Management System .119Figure 31. Comparison of Fuel System Injury Patterns .130Figure 32. Distribution of Flight Mishaps According to Helicopter Series.132Figure 33. Factors to be Included in a Time-Line Analysis for Underwater Emergency EgressFrom a Helicopter .135vi
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-71. SCOPE1.1 Scope.This handbook establishes guidance for the development requirements and verifications foroccupant crash protection and for crash protective aspects of seating, restraint, and crewstationand passenger/troop station design. This handbook is for guidance only. This handbookcannot be cited as a requirement. If it is, the contractor does not have to comply.2. APPLICABLE DOCUMENTS2.1 General.The documents listed below are not necessarily all of the documents referenced herein, but arethe ones that are needed in order to fully understand the information provided by this handbook.2.2 Government documents.2.2.1 Specifications, standards, and handbooks.The following specifications, standards, and handbooks form a part of this document to theextent specified herein. Unless otherwise specified, the issues of these documents are thoselisted in the latest issue of the Department of Defense Index of Specifications and Standards(DoDISS) and supplement thereto.NUMBERMIL-STD-1290ADS-36USAAVSCOM 89-22 ATHROUGH-22ETITLELIGHT FIXED AND ROTARYWING AIRCRAFT CRASHRESISTANCEROTARY WING AIRCRAFTCRASH RESISTANCEAIRCRAFT CRASH SURVIVALDESIGN GUIDE VOL. I: Design Criteriaand Checklists VOL. II: Aircraft DesignCrash Impact Conditions andHuman Tolerance VOL. III: Aircraft StructuralCrash Resistance VOL. IV: Aircraft Seats,Restraints, Litters, andCockpit/CabinDelethalization VOL. V: Aircraft PostcrashSurvival1TYPE(Canceled)AERONAUTICALDESIGN STANDARDTECHNICAL REPORT
Downloaded from http://www.everyspec.com on R PART 23FAR PART 25FAR PART 27FAR PART 29ADS-24REPORT NO. FAA-ED-18-6JUNE 1982ADS-11B-86-SE-03-H000GEORGIA INSTITUTE OFTECHNOLOGY CENTER OFEXCELLENCE FOR ROTARYWING AIRCRAFTTECHNOLOGY MEETING ONCRASHWORTHY DESIGNJ.D. CRONKHITE,PRESENTED AT AHSCRASHWORTHY DESIGN OFROTORCRAFT MEETING,ATLANTA, GEORGIA, APR1986DTIC AD-A212606MIL-STD-1530AR-56GENERAL SPECIFICATIONFOR DESIGN ANDCONSTRUCTION OFAIRCRAFT WEAPONSYSTEMSCRASH SURVIVABILITY OFAIRCRAFT PERSONNELAIRWORTHINESSSTANDARDS: NORMAL,UTILITY, ACROBATIC, ANDCOMMUTER CATEGORYAIRPLANESAIRWORTHINESSSTANDARDS: TRANSPORTCATEGORY AIRPLANESAIRWORTHINESSSTANDARDS: NORMALCATEGORY ROTORCRAFTAIRWORTHINESSSTANDARDS: TRANSPORTCATEGORY ROTORCRAFTCRASHWORTHY AIRWORTHINESSSURVIVABILITY PROGRAMROTARY WINGSURVIVABILITY ANDCRASHWORTHINESS DESIGNCRITERIALETTER OF ISSUANCEFEDERAL AVIATIONREGULATIONSFEDERAL AVIATIONREGULATIONSFEDERAL AVIATIONREGULATIONSFEDERAL AVIATIONREGULATIONSAERONAUTICALDESIGN STANDARDFAA TECHNICALCENTERENGINEERING ANDDEVELOPMENT PLANAERONAUTICALDESIGN STANDARDDESIGN OF AIRFRAMESTRUCTURES FOR CRASHIMPACTTHE DESIGN OF HELICOPTERCRASHWORTHINESSAIRCRAFT STRUCTURALINTEGRITY PROGRAM,AIRPLANE REQUIREMENTSSTRUCTURAL EQUIREMENTS
Downloaded from http://www.everyspec.com on 118FAAAC 21-22NBDL-89R003SAE PAPER 851847SAE J885ISBN Number:1-56091-499-8ISBN Number:1-56091-363-0MEMORANDUM REPORT AAC119-81-8 CIVIL AEROMEDICALINSTITUTE FAA, 1983PROCEEDINGS OF THEEIGHTEENTH STAPP CARCRASH CONFERENCE, SAE,pp 303-338AIRPLANE STRENGTH ANDRIGIDITY, GROUND LOADSFOR NAVY REQUIREDAIRPLANESAIRPLANE STRENGTH ANDRIGIDITY- MISCELLANEOUSLOADSAIRPLANE STRENGTH ANDRIGIDITY- GROUND TESTSOCCUPANT CRASHPROTECTION IN MILITARY INMILITARY AIR TRANSPORTSPECIAL STUDY-CABINSAFETY IN LARGETRANSPORT AIRCRAFTCRASH INJURY PROTECTIONIN SURVIVABLE AIRTRANSPORT ACCIDENTSCIVIL AIRCRAFT EXPERIENCE1970 T0 1978INJURY CRITERIA FORHUMAN EXPOSURE TOIMPACTGUIDELINES FOR SAFEHUMAN EXPOSURE TOIMPACT ACCELERATIONHUMAN INJURY CRITERIARELATIVE TO CIVIL AIRCRAFTSEATS AND RESTRAINTSYSTEMSHUMAN TOLERANCE TOIMPACT CONDITIONS ASRELATED TO MOTORVEHICLE DESIGNHEAD AND NECK INJURYBIOMECHANICS OF IMPACTINJURY AND INJURYTOLERANCES OF THE HEADNECK COMPLEXLOADS MEASURED DURINGPASSENGER SEAT TESTSEFFECT OF HEAD AND BODYPOSITION AND MUSCULARTENSING AN RESPONSE TOIMPACT3SPECIAL STUDYREPORTADVISORY CIRCULARJUNE 20, 1985Update A New Orleans,LA:Naval BiodynamicsLaboratory, 1989PAPERSAE Information Report,July 19861994,SAE order number: P2761993,SAE order nunber: PT-43MEMORANDUMREPORTPAPER
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7PROCEEDINGS OF THEFIFTEENTH STAPP CARCRASH CONFERENCE, SAE,1971, pp 207-255DOT/FAA/CT-90/24ISBN 0-8139-0634-2THE UNIVERSITY PRESS OFVIRGINIAUSAARL REPORT NO. 93-15Vol. 60, pp 112-121, AviationSpace and EnvironmentalMedicine, February, 1989NADC 88106-60DYNAMIC 472MIL-STD-1800NACA TN 4158(FEB 1958)STRENGTH AND RESPONSEOF THE HUMAN NECKPAPERA LITERATURE SURVEY OFAIRBORNE VEHICLESIMPACTING WATER ANDSOIL: HEAD INJURYCRITERIA AND SEVERITYINDEX DEVELOPMENT OFCOMPUTER PROGRAMKRASHAIRCRAFTCRASHWORTHINESSFINAL REPORTBASIC PRINCIPLES OFHELICOPTERCRASHWORTHINESSKINEMATICS OF U.S. ARMYHELICOPTER CRASHES:1979-1980THE NAVAL AIRCRAFT CRASHENVIRONMENT: AIRCREWSURVIVABILITY ANDAIRCRAFT STRUCTURALRESPONSEA SURVEY OF NAVALAIRCRAFT CRASHENVIRONMENTS WITHEMPHASIS ON STRUCTURALRESPONSEAIRCREW STATIONGEOMETRY FOR MILITARYAIRCRAFTAIRCREW STATION ANDPASSENGERACCOMMODATIONSHUMAN ENGINEERINGDESIGN CRITERIA FORMILITARY SYSTEMS,EQUIPMENT AND FACILITIESHUMAN ENGINEERINGPERFORMANCE,REQUIREMENTS FORSYSTEMSACCELERATIONS EPORT
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7NACA TN 2991(1953)FAA-RD-77-188(FEB. 1977)TI-83402U.S. DEPARTMENT OFTRANSPORTATION, FEDERALAVIATION ADMINISTRATIONTECHNICAL CENTERMIL-STD-210QSTAG-360MIL-S-58095SAE TECHNICAL PAPER NO.850853SAE TECHNICAL PAPER 88ACCELERATIONS ANDPASSENGER HARNESSLOADS MEASURED IN FULLSCALE, LIGHT AIRPLANECRASHESFULL SCALE CRASH TESTEXPERIMENTALVERIFICATION METHOD OF AMETHOD ANALYSIS FORGENERAL AVIATIONCRASHWORTHINESSDEVELOPMENT OFROTORCRAFT CRASHSCENARIOSCLIMATIC INFORMATION TODETERMINE DESIGN ANDTEST REQUIREMENTS FORMILITARY SYSTEMS ANDEQUIPMENTCLIMATIC ENVIRONMENTALCONDITIONS AFFECTING THEDESIGN OF MILITARYMATERIELSEAT SYSTEM: CRASHRESISTANT, NON-EJECTION,AIRCREW, GENERALSPECIFICATION FORTHE DEVELOPMENT OFDYNAMIC PERFORMANCESTANDARDS FOR GENERALAVIATION AIRCRAFT SEATSDATA FOR THEDEVELOPMENT OF CRITERIAFOR GENERAL AVIATIONSEAT AND RESTRAINTSYSTEM PERFORMANCEREEL, SHOULDER HARNESS,INERTIA LOCKRESTRAINT SYSTEM,AIRCREWMAN’SSEATS, HELICOPTER CABIN,CRASHWORTHY, GENERALSPECIFICATION FORSEAT, PASSENGER, AFTFACING, ONTECHNICAL PAPERTECHNICAL PAPER
Downloaded from http://www.everyspec.com on 52SAE AEROSPACE STANDARD8049ADVISORY CIRCULAR NO.23.562-1ADVISORY CIRCULAR 4SAE AEROSPACE 3469MIL-B-8242MIL-B-5428MIL-H-5364MIL-W-4088SEAT SYSTEM; AIRCREW,GENERAL SPECIFICATIONFORSEAT, AIRCREW,ADJUSTABLE SWIVEL, TYPEE-1PERFORMANCE STANDARDFOR SEATS IN CIVILROTORCRAFT ANDTRANSPORT AIRPLANESDYNAMIC TESTING OF PART23 AIRPLANESEAT/RESTRAINT SYSTEMSAND OCCUPANTPROTECTIONDYNAMIC EVALUATION OFSEAT RESTRAINT SYSTEMSAND OCCUPANTPROTECTION ONTRANSPORT AIRPLANESSEAT, AIRCRAFTSEAT, AIRCRAFT, WALLSTYLESEAT, TROOP, VARIABLESEATING WIDTHTORSO RESTRAINT SYSTEMTORSO RESTRAINT SYSTEMSEAT PASSENGER, CABINFOLDINGBELT, AIRCRAFT SAFETY,LAP, TROOP, MC-1ABELTS, AIRCRAFT SAFETY,LAP, TROOP, TYPES MD-1AND MD-2ADJUSTER, LAPBELT, 13/4WEBBINGBELT, SAFETY, LAP, TROOP,TYPE C-3ABELT, SAFETY, SHOULDER,HARNESS, TROOP, TYPE, D-2HARNESS, SHOULDERSAFETY, GENERALSPECIFICATION FORWEBBING, TEXTILE, WOVENNYLON6SAE AEROSPACESTANDARDADVISORY CIRCULAR(JUNE 22, 1989)ADVISORY CIRCULAR(MARCH 6, 1990)FAA TECHNICALSTANDARD ORDERSAR AEROSPACESTANDARD
Downloaded from http://www.everyspec.com on -27422SER-13298; SIKORSKY,31 AUGUST 1977USAAVLABS TR-71-8(AD723988)AD-A217 575 (DTIC)JOURNAL OF AHS, 1979DOT/FAA/CT-84/3(FEB 1984)NACA-TR-1347(1958)SAFE SYMPOSIUMPROCEEDINGS 1995, pp142151WEBBING, TEXTILE,POLYESTER, LOWELONGATIONADAPTERS, QUICKDISCONNECT, PASSENGERSEAT TO FLOORFITTINGS AND CARGORINGS, TIE-DOWN AIRCRAFTFLOORSLINGING AND TIEDOWNPROVISIONS FOR LIFTINGAND TYING DOWN MILITARYEQUIPMENTFIRE AND EXPLOSIONHAZARD PROTECTIONSYSTEMS, AIRCRAFT,GENERAL SPECIFICATIONFORFIRE PROTECTION DESIGNHANDBOOK FOR U.S. NAVYAIRCRAFT POWERED BYTURBINE ENGINESTANK, FUEL, CRASHRESISTANT, AIRCRAFTCRASHWORTHY FUELSYSTEM DESIGN CRITERIACRASHWORTHY FUELSYSTEM DESIGN CRITERIAAND ANALYSISAIRCRAFT FIRE SAFETYDESIGN AND TESTING OFFLOAT LANDING GEARSYSTEMS FOR HELICOPTERSSTUDY OF TRANSPORTAIRPLANE UNPLANNEDWATER CONTACTDITCHING INVESTIGATIONSOF DYNAMIC MODELS ANDEFFECTS OF DESIGNPARAMETERS ON DITCHINGCHARACTERISTICSDEVELOPMENT OF APASSENGER AIRCRAFTAIRBAG SYSTEM7ref from REPORT ONANALYSIS OF H-53FUEL SYSTEMCRASHWORTHINESSTECHNICAL REPORTAGARD CONFERENCEPROCEEDINGS No. 467PAPERTECHNICAL REPORTPAPER
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7SAFE SYMPOSIUMPROCEEDINGS 1994,pp 66-73SAFE SYMPOSIUMPROCEEDINGS 1994, pp 157163SAFE SYMPOSIUMPROCEEDINGS 1993,pp 356-365SAFE SYMPOSIUMPROCEEDINGS 1993,pp 288-297SAFE SYMPOSIUMPROCEEDINGS 1992,pp 246-253SAFE SYMPOSIUMPROCEEDINGS 1991,pp 63-80SAFE SYMPOSIUMPROCEEDINGS 1990,pp 196-202SAFE SYMPOSIUMPROCEEDINGS 1990,pp 84-89SAFE SYMPOSIUMPROCEEDINGS 1987,pp 190-195SAFE SYMPOSIUMPROCEEDINGS 1986,pp 264-269SAFE SYMPOSIUMPROCEEDINGS 1986,pp 147-152SAFE SYMPOSIUMPROCEEDINGS 1986,pp 80-87SAFE SYMPOSIUMPROCEEDINGS 1985,pp 76-80SAFE SYMPOSIUMPROCEEDINGS 1985,pp 137-140ADVANCED TECHNOLOGYFOR ROTARY-WINGAIRCRAFTCRASHWORTHINESSMODEL OF ANDERGONOMICALLY DESIGNEDHELICOPTER SEATHELICOPTER TROOP SEATS:THE PRESENT AND THEFUTURERECENT HELICOPTERINFLATABLE RESTRAINTDEVELOPMENTSNAVAL AIRCRAFT CRASHSIMULATION USINGPROGRAM KRASHSTRUCTURAL TESTING OFCOMMERCIAL ROTORCRAFTSEATS: AN OVERVIEWSTANDARDIZATION OFNATOPS EMERGENCYEGRESS PROCEDURESINERTIA REELS FORAIRCREW RESTRAINTSYSTEMSENERGY ABSORBINGSYSTEM DESIGN ANDEVALUATION USING ADISCRETE ELEMENT MODELOF THE SPINEDELETHALIZED CYCLICCONTROL STICKPAPERH-46 HELICOPTEREMERGENCY FLOTATIONSYSTEM (HEFS)KOCH EMERGENCY EGRESSLIGHTING SYSTEMS FORADVERSE OPTICALCONDITIONS FOR MILITARYAND COMMERCIAL AIRCRAFTAND OTHER APPLICATIONSRETROFIT ENERGYABSORBING CREWSEAT FORSH-3 (S-61 SERIES SEA KINGHELICOPTERADVANCEMENTS IN INERTIAREELS FOR FIXED RPAPERPAPERPAPERPAPERPAPERPAPER
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7SAFE SYMPOSIUMPROCEEDINGS 1983,pp 66-74SAFE SYMPOSIUMPROCEEDINGS 1980,pp 196-201SAFE SYMPOSIUMPROCEEDINGS 1980,pp 202-208SAFE SYMPOSIUMPROCEEDINGS 1980,pp 209-215SAFE SYMPOSIUMPROCEEDINGS 1980,pp 216-220SAFE SYMPOSIUMPROCEEDINGS 1980,pp 106-109SAFE SYMPOSIUMPROCEEDINGS 1980,pp 16-24SAFE SYMPOSIUMPROCEEDINGS 1976,pp 132-136SAFE SYMPOSIUMPROCEEDINGS 1971,pp 114-123HELICOPTER CRASHSURVIVABILITY ANDEMERGENCY ESCAPETEST AND EVALUATION OFIMPROVED AIRCREWRESTRAINT SYSTEMSDESIGN OF ACRASHWORTHY CREW SEATFOR BOEING VERTOLCHINOOK HELICOPTERCRASHWORTHY MILITARYPASSENGER SEATDEVELOPMENTHASEP SURVIVAL FROMCRASHED NAVYHELICOPTERSA NEW SAFETY HARNESSFOR MOBILE AIRCREWPAPEREMERGENCY IN-FLIGHTOPENING FOR GENERALAVIATION AIRCRAFTUSAF EXPERIENCE INAIRCRAFT ACCIDENTSURVIVABILITYMETHOD FOR IMPROVINGHELICOPTER CREW ANDPASSENGER PER(Unless otherwise indicated, copies of the above specifications, standards, and handbooksare available from the Standardization Document Order Desk, 700 Robbins Ave., Bldg 4D,Philadelphia PA 19111-5094.)2.2.2 Other Government documents, drawings, and publications.The following other Government documents, drawings, and publications form a part of thisdocument to the extent specified herein.SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)SAE 942482 Racing Car Restraint System Frontal crash Performance TestingSAE 962522 Investigation of Indy Car Crashes Using Impact Recorders(Application for copies should be addressed to the Society of Automotiver Engineers, Inc,400 Commonwealth Dr., Warrendale PA 15096-0001.)2.3 Non-Government publications.The following document(s) form a part of this document to the extent specified herein. Unlessotherwise specified, the issue of the documents which are DoD adopted are those listed in theissue of the DoDISS, and supplement thereto.9
Downloaded from http://www.everyspec.com on 2011-11-30T16:55:08.JSSG-2010-7Computation of the Effective Intensity of Flashing Lights, C. Douglas, Illuminating Engineer, Vol52, No.12, Dec 19572.4 Order of precedence.In the event of a conflict between the text of this document and the references cited herein, thetext of this document takes precedence. Nothing in this document, however, supersedesapplicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS3.1 Aircrew Systems Engineering (see JSSG-2010-1).3.2 Crew Systems Automation, Information, and Control/Display Management (seeJSSG-2010-2).3.3 Cockpit/Crew Station/Cabin (see JSSG-2010-3).3.4 Aircrew Alerting (see JSSG-2010-4).3.5 Aircraft Lighting (see JSSG-2010-5).3.6 Sustenance and Waste Management (S&WM) Systems Requirements (see JSSG2010-6).3.7 Crash Survivability.The crash protection system shall provide means for protecting aircraft occupants (i.e. pilots,aircrew, troops, and passengers) from severe and fatal injuries caused by acceleration andcontact forces, fire, toxic gases, submersion, and other hazards associated with crashsurvivable aircraft crashed. The system shall also provide occupants both the time and themeans to egress rapidly and safely, once the aircraft has come to rest. In addition, survival andrescue equipment on-board the aircraft shall be protected from crash damage so thatoccupants can readily access the equipment after a crash to support post-crash survival,enemy evasion, and rescue. The system may consist of both autonomous elements integratedinto the aircraft solely for the purpose of providing crash protection, as well as aircraft structuraland subsystem elements modified to enhance occupant crash protection. The system shall beintegrated into the aircraft to achieve efficient overall protection for aircraft occupants, whilel
ADS-36 ROTARY WING AIRCRAFT CRASH RESISTANCE AERONAUTICAL DESIGN STANDARD USAAVSCOM 89-22 A THROUGH-22E AIRCRAFT CRASH SURVIVAL DESIGN GUIDE VOL. I: Design Criteria and Checklists VOL. II: Aircraft Design Crash Impact Conditions and Human Tolerance VOL. III: Aircraft Structural Crash Resistance VOL. IV: Aircraft Seats,
cabin crew 48 17. Cabin crew mandatory travel documents 48 18. Cabin crew (FDTL)-flight time, flight duty time, rest period limitation,duty roster & record 48-50 19. Cabin crew currency of Competency Card including First aid,CRM,Av Sec and DGR 50-51 20. Cabin crew currency of Health Card 51-52 21. Cabin crew pre-flight briefing 52-54 22.
The Air Crew Scheduler is an interactive computer software system for air crew scheduling. The system is used by planners to develop and modify crew pairings for flight crews and cabin crews. Currently the Air Crew Scheduler facilitates the pro-duction of legal crew schedules. The Preston Group wishes to enhance the product by
Sep 21, 2020 · CXC was BM2 Shaw, CXB/ Crew/ Navigator/ BTM BM3 Szep, BO/Engineer/ Crew MK1 Backman, Crew/ Engineer MK3 Shubin, Crew/ BTM/ Engineer, MK3 Beniot. CG EX 14. Initial Report Cont. The Crew launched fro
Service fire suppression crew was the "40-man" crew established in 1939 on an experimental basis (2). The 40-Man crew was located on the Siskiyou National Forest in southwestern Oregon. The crew was very effective in fire suppression in the Region 6 National Forests. The Oregon "Red Hats," co-sponsored by the School of Forestry at Oregon
Crew Resource Management 4 Afternoon: Modules 4Afternoon: Modules 4- -66 Endorsement "Crew Resource "Crew Resource management is a fantastic Introduction Crew Resource Management 5 program. It fits with our safety mission. I wholemission. I whole--heartedly believe in and endorse this program." Overall Course Objectives
Virgin Australia Cabin Crew Agreement 2021 6 PREFACE This Agreement was developed by Virgin Australia, its Cabin Crew Members and the Unions. It was a collaborative effort intended to provide terms and conditions for Cabin Crew which aims to deliver long term careers and enable Cabin Crew Member satisfaction, while supporting the
Crew Resource Management Dr. Brandon Stark, Director UC Center of Excellence on UAS Safety. Crew Resource Management Crew Communication Drone Crews . Type of flight: e.g., training, maintenance, normal. Note appropriate restrictions UAS Status -condition, recent maintenance, other items of note Crew -roles & responsibilities
Flight Crew Gulfstream GV / GV-SP (G500/G550) / GIV-X (G450/G350) 21 May 2015 . Operational Suitability Data - Flight Crew G-V . Crew Resource Management CS-FCD .Certification Specifications for Operational Suitability Data (OSD) Flight Crew Data CS-FCD, Initial issue, 31 January 2014 .
