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 TEITEl•  , . ·  ll l." ,EII.T EI,.,.,IM. CRASHWORTHY TROOP/UTILITY SEAT MAXI MUM PROTECTI ON * HI GH PERFORMANCE EAS T/ WES T AAATS* SYSTEM • VARI ABLE LOAD ENERGY ATTENU ATI ON SYSTEM (VL EAS )- PATENTED**  AND EASI LY REPL ACEABLE • MAXIMUM OCCUPANT PROTECTION UP TO 30 G @ 42 FPS • ACCOMMODATES FULL OCCUPANT RANGE (5% FEMALE TO 95% MALE) MOUNTS ON BULKHEAD, FLOOR OR CEIL ING ST OWABLE - SEAT FOLDS UP WHEN NOT IN USE SEAT CAN BE INSTALLED IN FORWARD, AF T AND SIDE FACI NG CONFI GURAT IONS • RAPID INST ALLATI ON-REMOVAL TIME LESS THAN 10 SECONDS WEIGHT - 15.4 POUNDS WI TH CUSHION 14. 8 POUND S WIT HOUT CUSHION DESI GNED AND TESTED TO MEET UH-1Y REQUIREMENTS ST ATIC TESTED TO 20- 20-10 G TEST ED TO MI L-ST D 810 ENVI RONME NTAL REQUIREME NTS • VERTI CAL ST ROKI NG DI STANCE UP TO 13. 5 INC HES • ADJUSTABLE SEAT BACK  ACCOMMODATES OCCUPANT WI TH ALI CE PACK ·  ADAPTIVELY ATTENUATED AIRBORNE TROOP SEAT ··U.S.  PAT.  6,378,939 B1 EAST/WESTINDUSTRIES, INC. 80 THIRTEENTH AVENUE,  RONKONKOMA,  NY 1177 9-6800 TEL: 631 981-59 00 · F AX:  63 1 981-5990 EMAIL:  info@eastwestindustr ies.com WEB:  www.eastwestindustr ies.com

Crashworthy Troop Utility Seat

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Crashworthy Troop Utility Seat

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MAXIMUM PROTECTION * HIGH PERFORMANCE
• ACCOMMODATES FULL OCCUPANT
• MOUNTS ON BULKHEAD,
FLOOR OR CEILING
FORWARD, AFT AND SIDE
14.8 POUNDS WITHOUT CUSHION
UH-1Y REQUIREMENTS
• TESTED TO MIL-STD 810
··U.S.   PAT.  6,378,939 B1
TEL: 631 981-5900· FAX:   631 981-5990
EMAIL:   info@eastwestindustr ies.com
WEB:   www.eastwestindustr ies.com
Crashworthy Troop/Utility Seat System are:
• Energy Absorption System   - Variable Load Energy Attenuation
System (VLEAS) is Patented** and is a new state-of-the-art passive energy
absorption system designed by East/West.   This system is designed to absorb
and limit impact loads, thereby providing pelvic and spinal protection upon
vertical impact in an emergency crash situation.
• Easy Replacement of the VLEAS  - In the event the VLEAS has
been activated due to hard landings during normal flight maneuvers, it can be
easily replaced in minutes.
• Harness Restraint System   - The AAATS System is designed for a
three(3), four(4), or five(5) point occupant restraint system which is released by
means of a single centerpoint rotating release buckle. The five(5) point restraint
system includes a strap between the occupant's legs, which prevents submarining
under the lap belt.
The AAATS System is a versatile Troop/Utility Seat which can
be bulkhead, floor, or ceiling mounted for forward, aft and side
facing seat configurations. It is easily retrofitable in any rotary
wing aircraft (such as: H-1, UH-1Y, H-3, H-46, H-47, H-53,
H-60, and V-22). It has been designed for quick and easy
installation and removal by maintenance personnel for rapid
mission reconfiguration of aircraft.