Download - Galon Industry Seats
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Crashworthy Seating Systems
Design, Certification, Production
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IAI/GOLAN is a Division of Israel Aerospace Industries Ltd
IAI/Golan’s main product line is the Crashworthy Airborne Seats
since 1978
IAI/Golan’s seats comply with the standards specified in the FAR/EASA Parts 23,25,27,29 and the MIL-STD requirements
During the past few years IAI/GOLAN has successfully developed Mine Blast Resistant Seats (MBRS) for ground vehicles
About IAI/GOLAN
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Design and Production Cycle
Solid Model Design
XYZ Inspection Assembly
CNC Manufacturing
Certification
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IAI/GOLAN Q.A. is approved by authorities for:
- ISO9001 : 2000
- AS9100
- TSO FAA (APA)
Quality System Certified
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DECADES OF SUCCESSFUL SEATS PRODUCT LINE AND SATISFIED CUSTOMERS
2000-2009 1990-1999 1989-1990 SINCE 1978
GULFSTREAM G150
PILATUS PC12
BOEING V-22
IAI A/C
Westwind
Astra
EADS/SOCATA TBM 700/850
MD-HELICOPTERS
MD-EXPLORER
EMIVEST (SINO- SWERINGEN)
SJ30
Boeing 767 AWACS
HELICOPTERS (UNDER NDA)
AGUSTA WESTLAND AW101
NDA PROJECTS MINE BLAST
RESISTANT SEATS
Evolution
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IAI GOLAN
CRASHWORTHY SEATS
FIXED WING - CIVIL ( FAR PARTS 23/25 )
HELICOPTER - CIVIL (FAR PARTS 27/29)
HELICOPTER - MILITARY
MINE BLAST RESISTANT SEATS (MBRS)
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IAI GOLAN
CRASHWORTHY SEATS
PILOT SEATS ……………………………....... PASSENGER SEATS……………..………… MISSION CREW SEAT………………………
FIXED WING CIVIL (FAR PARTS 23/25)
Click on pictures for details
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IAI GOLAN
CRASHWORTHY SEATS
PILOT SEATS …….……….……………………
PASSENGER SEATS………………..……………
HELICOPTER - CIVIL (FAR PARTS 27/29)
Click on pictures for details
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IAI GOLAN
CRASHWORTHY SEATS
PILOT SEATS ……………………………....
TROOP SEATS ……………………………....
CREW / OPERATOR SEATS…………………
HELICOPTER - MILITARY
Click on pictures for details
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FIXED WING A/C COMFORTABLE PILOT SEAT
Built for long flights, contains various adjustable comfort
mechanisms
• Designed, tested and certified to TSO C127(a), FAR Part 25
• Accommodates range of 5% - 95% percentile pilots population
• “5 point” Restraint system complied with TSO C114
• Comfort cushions for long flights
• Successfully tested to RTCA/DO-160D - Environmental conditions
• Adjustable head rest
• Sheepskin cover optional
• Adjustments:
• Horizontal adjustments on a/c floor tracks
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• Vertical adjustments in a range of 6.5” in 0.5” increments
- Backrest recline up to 23°
• Adjustable lumbar support:
- Up/Down up to 3”
- Fwd/Aft up to 1.75”
• Cushioned armrests
- Adjustable +/- 15°
- Foldable and hidden (behind the backrest)
• Equipped with life vest and oxygen mask stowage
• Complies with flammability requirements as per FAR 25.853 Appendix F part II
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GULFSTREAM G-150 PILOT SEAT
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LUXURY PILOT SEAT FOR FIXED WING A/C
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• Designed, tested and certified to TSO C127(a),
FAR Part 23
• Comfort luxury cushions
• "4 Point" restraint system as per TSO C114
• Executive appearance
• Adjustments :
- Backrest recline up to 7°
- Vertical adjustment up to 84mm
- Horizontal adjustments on a/c floor tracks
• Foldable armrests and hidden behind the backrest.
• Adjustable headrest fwd/aft
Luxuriously comfortable flying
TBM850 PILOT SEAT
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COMMERCIAL FIXED WING A/C PILOT SEAT
A practical and proven life saving Pilot Seat design
• Designed, tested and certified as per FAR
Part 23
• “4 Point” Restraint system , with an Inertia
Reel ( equipped also with manual lock)
• Comfort cushions for long flights
• Adjustments :
- Vertical adjustment range : 5.7”
- Horizontal adjustment on a/c floor tracks
as desired
• Foldable, adjustable and hidden armrests
• Foldable seat pan
• Certification : FAR Parts 23.561, 23.562,
23.785
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PC-12 PILOT SEAT
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EXECUTIVE PASSENGER SEAT
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• Designed and certified to TSO C127(a),
FAR Part 23
• Floor/bulkhead installation
• Fwd facing configuration
• Comfort luxury cushions
• Executive appearance
• Adjustments :
- Double folding of backrest and entire
seat to allow access to baggage
compartment
- Backrest recline up to 20° and horizontal
adjustment (internally) of 150mm
simultaneously
- Foldable armrests
- Height Adjustable headrest
TBM850 REAR- PSSENGER SEAT Double Folding Seat allows easy passage to rear baggage compartment
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Luxury aft facing seat
HELICOPTER TROOP SEAT
FIXED WING A/C PASSENGER LUXURY SEAT
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TBM850
MID PASSENGER SEAT
• Designed and certified to TSO C127(a), FAR Part 23
• 3 point Restraint System with Inertia Reel
• Aft facing configuration
• Executive appearance
• Floor mounted
• Comfort luxury cushions.
• Adjustments :
- Backrest recline up to 20°
- Foldable armrests and hidden behind the backrest.
- Height Adjustable headrest
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Shaped to A/C contour - Proven ergonomic design
FIXED WING A/C PASSENGER LUXURY SEAT
• Designed, tested and certified to TSO C127(a), FAR
Part 23
• Aft facing configuration
• Floor mounted
• Comfort luxury cushions.
• Executive appearance
• Adjustments :
- Backrest recline up to 35°
- Horizontal adjustment on A/C floor tracks
- Foldable armrests and hidden behind the backrest.
- Fixed cushioned headrest
SJ30-2 AFT FACING SEAT
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FIXED WING A/C PASSENGER LUXURY SEAT
SJ30-2 REAR SEAT Classic forward facing comfortable seat design
• Designed and certified to TSO C127(a),
FAR Part 23
• Weight : 56 lb. (25.4 Kg.)
• Fwd facing configuration
• Floor mounted
• Comfort luxury cushions.
• Executive appearance
• Adjustments :
- Backrest recline up to 65°
- Horizontal adjustment on A/C floor tracks
- Foldable armrests
• Fixed cushioned headrest
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FIXED WING UTILITY PASSENGER SEAT
Comfortable, crash-proof Passenger Seat
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• Design tested and certified as per
FAR Part 23
• “3 Point” Restraint system with an
inertia reel
• Comfort cushions for long flights
• Floor mounted
• Adjustments :
- Backrest recline : 11°
- Foldable armrest
- Adjustable headrest – up/down
- Certification : FAR Parts 23.561,
23.562, 23.785
PC-12 PASSENGER SEAT
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• Qualified to FAR Part 25 requirements – Part 25.561
• Floor mounted
• “4 Point” Restraint system with an Inertia Reel
• Comfort cushions for long flights
A seating system for AWACS
HELICOPTER TROOP SEAT
FIXED WING A/C MISSION CREW SEAT
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COMFORTABLE LONG
FLIGHT MISSION CREW SEAT
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• Qualified to FAR Part 25 requirements – Part 25.561 • Floor mounted • “ 4 Point” Restraint system with an Inertia Reel • Comfort cushions for long flights • Tested to RTCA/DO-160D - Environmental conditions
• Adjustments :
- Horizontal adjustment on floor tracks
- Vertical adjustment in a range of ± 5”
- Backrest inclination 27°
- Foldable, adjustable and hidden armrests
- Adjustable lumbar support (Vacuum type)
- Adjustable headrest (fwd/aft)
- Equipped with life vest and smoke goggle compartments
FIXED WING A/C MISSION CREW SEAT
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HELICOPTER UTILITY PILOT SEAT
Easy adjustable DEP (Design Eye Point)
• Designed tested and certified as per FAR Part 29 for
100 Kg. pilot weight
• Equipped with an energy attenuator for 5% - 95%
percentile pilots population
• “ 4 Point” Restraint system
• Comfort cushions for long flights
• Successfully tested to MIL-STD 810 Environmental
requirements
• Adjustments :
- Horizontal adjustment 100mm and vertical adjustment
30mm simultaneously (on an inclined rail)
• Certification : FAR Parts 29.561, 29.562, 29.785 for pilot
weight of 100 Kg.
PILOT SEAT
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UTILITY HELICOPTER PILOTSEAT
Durable & economical, lightweight and comfortable Pilot Seat
• Designed, tested and certified as per FAR Part 27
• Equipped with an energy absorbing system (EAS)
for 5% - 95% percentile pilots population
• “ 4 Point” Restraint system with an inertia reel,
per TSO C114
• Adjustable lumbar support height
• Comfort cushions for long flights
• Cushioned headrest
• Tested to MIL-STD 810 Environmental requirements
• Adjustments :
- Horizontal adjustment 2.8”and vertical adjustment
1.9”simultaneously (on an inclined rail) - to keep
the Design Eye Point in constant location
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MD-EXPLORER PILOT SEAT
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UTILITY HELICOPTER PASSENGER SEAT
Durable & economical lightweight design
• Design, tested and certified as per FAR Part 27
• Equipped with an energy absorbing system (EAS)
for 5% - 95% percentile pilots population
• Floor/Ceiling mounted, easy installation and removal
• “ 3 Point” Restraint system
• Cushioned headrest
• Foldable seat pan up
• Foldable backrest to allow easy access to baggage
compartment
• Tested to MIL-STD 810 Environmental requirements
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MD-EXPLORER PASSENGER SEAT
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Comfortable Proven in Service
HELICOPTER UTILITY PASSENGER SEAT
• Designed tested and certified as per FAR Part 29
• Floor mounted
• “4 Point” Restraint system with an inertia reel
• Comfort cushions for long flights
• Tested to MIL-STD 810 Environmental requirements
• Certification : FAR Parts 29.561, 29.562, 29.785
PASSENGER SEAT
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Pilot Seat reconfigurable in the field to Mission Crew Seat and/or
to Light Weight non-armored seat.
AW101 PILOT SEAT - Versatile, Comfortable with Ballistic Armor
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• Equipped with an energy absorbing system
(EAS) for 5% - 95% percentile pilots population
(for pilot weight up to 120 Kg)
• “ 5 Point” Restraint system with Inertia reel
(including manual lock)
• Comfort cushions for long flights
• Successfully tested to MIL-STD 810
Environmental requirements
• Adjustments :
- Horizontal and vertical adjustments : 127mm.
- Backrest inclination 6° with headrest
- Adjustable thigh support (30° up/down)
- Foldable, adjustable and hidden armrest
AW-101 PILOT SEAT
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• Up/down adjustable lumbar support
• Easy and quick re-configuration between
armor and non-armor configurations
• Qualification (pilot weight of 120 Kg.)
• Static load factors :
- 15g down
- 9g fwd/aft
- 6g lateral
- 6g up
• 15g resultant combined
• Dynamic emergency conditions load factors :
- 22g combined vertical
- 13g combined horizontal
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AW-101 PILOT SEAT
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TILT-ROTOR HELICOPTER MILITARY TROOP SEAT
Optimal design for Lightweight, Comfort and Safety.
Chosen by the U.S. Navy
V-22 TROOP SEAT
• Designed tested and qualified as per NAVAIR
requirements, tailored to the V-22 aircraft characteristics. • Equipped with an energy absorbing system (EAS) for 5% - 95% percentile fully equipped troops population • “3 Point” or “4 point” restraint system • Tested to MIL-STD 810 Environmental requirements • Easy installation and removal • Wall mounted • Fwd and side facing configurations • Foldable seat pan • Qualified for personal weight of 265 lb.- fully equipped • Static combined load factor : - 20 G FWD - 20G DOWN • Dynamic load factors : - 14 G Combined horizontal - 30G Combined vertical
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MILITARY HELICOPTER TROOP SEAT
Zippered backrest for Backpack
• Designed tested and qualified as per AWL
requirements, tailored to the EH101 helicopter
characteristics.
• Equipped with an energy absorbing system
(EAS) for 5% - 95% percentile fully equipped
troops population
• “4 point” restraint system
• Tested to MIL-STD 810 Environmental
requirements
• Easy installation and removal
AW-101 TROOP SEAT
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WALL-FLOOR
MOUNTED
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• Design tested and qualified as per AWL
requirements, tailored to the AW101
helicopter characteristics.
• Weight : 24.4 lb.(11.05 Kg.)
• Equipped with an energy absorbing
system (EAS) for 5% - 95% percentile
fully equipped troops population
• “4 point” restraint system
AW-101 TROOP SEAT
FLOOR
MOUNTED
Military, Floor Mounted, Side Facing
HELICOPTER TROOP SEAT
HELICOPTER TROOP SEAT
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• Design tested and qualified as per AWL requirements, tailored to the AW101 helicopter characteristics. • Weight : 24.4 lb.(11.05 Kg.) • Equipped with an energy absorbing system (EAS) for 5% - 95% percentile fully equipped troops population • “4 point” restraint system • Successfully tested to MIL-STD 810 Environmental
requirements
• Easy installation and removal
• Floor mounted
• Side facing configurations
• Foldable seat pan and seat back
• Qualification (trooper weight of 265 lb.- fully equipped) :
• Static load factors : 15g down, 9g fwd/aft, 6g lateral, 7.5g aft
• Dynamic load factors :
- 13g combined horizontal
- 22g combined vertical
AW-101 TROOP SEAT FLOOR MOUNTED
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Configuration in the field from Pilot Seat to Operator Seat
FAST AND EASY RECONFIGURATION IN THE FIELD FROM ARMORED TO NON-ARMORED SEAT
AW-101 MISSION CREW SEAT
• Equipped with an energy absorbing system
(EAS) for 5% - 95% percentile pilots population
(for pilot weight up to 120 Kg)
• “ 5 Point” Restraint system with Inertia reel
(including manual lock)
• Comfort cushions for long flights
• Tested to MIL-STD 810 Environmental
requirements
• Reconfiguration in the field from Pilot to Mission
Crew Seat
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OPERATOR BALLISTIC ARMORED SEAT FOR A MILITARY HELICOPTER
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• Equipped with an energy absorbing system (EAS) for 5% - 95% percentile
pilots population (for pilot weight up to 120 Kg)
• “ 5 Point” Restraint system with Inertia reel (including manual lock)
• Comfort cushions for long flights
• Successfully tested to MIL-STD 810 Environmental requirements
• Adjustments :
- Horizontal internally in the seat : 127mm.
- On a/c floor tracks : as desired
- Vertical – 127 mm.
- Backrest inclination 6°
- Adjustable thigh support (30° up/down)
- Foldable, adjustable and hidden armrests
Up/down adjustable lumbar support
Swivel : 360°
• Easily and quick re-configuration between armor and non-armor configurations
• Qualification (operator weight of 120 Kg.):
• Static load factors :
- 15g down, 9g fwd/aft, 6g lateral, 7.5g aft
- 15g resultant combined
• Dynamic emergency conditions load factors :
• 13g combined horizontal
• 22g combined vertical
AW-101 MISSION CREW SEAT
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MINE BLAST RESISTANT SEAT (MBRS)
Land vehicle application based on three decades of experience in Aviation Crashworthy Seats
• Seat orientation : Fwd facing or side facing
• Accommodated to fully equipped trooper - Up to 95% percentile.
• Equipped with comfort cushions for long rides and poor road conditions
• Protects seated occupants from mine blasts resulted in high acceleration above 100g’s in time frame of 8 msec.
• Energy absorption system (EAS) based on plastic deformation principle, for wide range of population
( from 5 % percentile female to 95% percentile male)
• Service life - 15 years
• Fire retardant materials
• Energy Absorbing System (EAS) technology tested by Weapons Material Division of the American Army Research Lab (ARL).
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• Easy re-configuration between fwd and side facing by rotating seat & seat pan
• Minimum parts – high reliability
• Special cushions provide comfortable seating for poor road conditions.
• The seat materials are of fire retardant characteristics – tested to the requirements of the aviation standards : FAA – FAR Part 25.853
• Estimated weight : 25 Kg.
• The prototype seat is scalable for different vehicles; may need to use a different adaptor for variations in vehicle design.
• The energy absorbing mechanism (EAM) is designed to be activated by the vertical load applied by the occupant on the seat pan as a result of mine blast.
• The seat is designed to sustain lateral loads resulted by side blast..
MINE BLAST RESISTANT SEAT