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Page 1: 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


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