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  Ejection Seat Cushions
- Testing
- X-Ray: Sitting Position
- APECSŪ I: For ACES II Seat
- APECSŪ I: F-22
- APECSŪ I-A:
F-15, A-10, B-2
- APECSŪ I-B: F-16
- APECSŪ I-C: B-1
- APECSŪ I-D: F-117
- APECSŪ II:
Universal Propulsion
- APECSŪ III: FA-18
- APECSŪ III-C: CF-18
- APECSŪ III-N:
NACES FA-18
- APECSŪ IV: S-3 Viking
- APECSŪ V: OV-10
- APECSŪ VI: B-52, T-38
- APECSŪ VII: U-2, SR-71
- APECSŪ VIII: F-4
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We’ve designed 17 ejection seat Cushion systems and continue to add to the list.
 
 
The cushion systems have been tested at seven military and independent testing facilities, including Wright Patterson Air Force Base, where the APECSŪ I went through drop tower testing installed on the ACES II ejection seat (above).
 
The APECSŪ I kept spinal lumbar loads to less than 1500 lbs., up to 18.6Gs when tested during high-G terrain-following missions and crash testing.
 
The pelvic angle, lumbar spine radius and relative positions of vertebrae create an ideal sitting position.
 
All 27 pilots recommended the Oregon Aero seat cushion system as standard equipment.
 
"...this is the first time in my engineering experience I have seen an evaluation go this well." — Testing engineer for Oregon Aero APECSŪ I Cushion System for the ACES II ejection seat
 
Oregon Aero often has access to military equipment
 
Oregon Aero often has access to military equipment such as this Oregon Air National Guard simulator the company used when designing the APECSŪ I Ejection Seat Cushion System.
 
digital measuring arm
 
We use this portable, digital measuring arm to reverse engineer an ejection seat (in this case, an F-4). The 3-D image is used to make an exact plastic or metal seat model we work with to manufacture the seat cushion system.

 



Click here for ways to support helmet safety for our troops.

 

 


Oregon Aero proprietary designs, cutting equipment, molding techniques and other manufacturing methods make us the leader in using visco-elastic foam and other materials.
Oregon Aero®SM Seat Cushion Systems:
  Ejection Seats
 


Seventeen custom designs (and counting). Painless seating, no matter how long the flight. Improved impact protection. Unanimous praise from pilots. Dramatically reduced maintenance.

Oregon Aero’s Ejection Seat Cushion Systems solve a lot of problems and let pilots focus on the job at hand without the distraction of seat pain.

Everybody Wanted the Oregon Aero® Seat Cushions!

Evaluation of Oregon Aero's APECS® I Cushion System for ACES II ejection seat went unusually well - to the point that the evaluation engineer stated: " I can only add that this is the first time in my engineering experience that I have seen an evaluation go this well."

Testing performed in the F-15 and F-16. Twenty-seven different pilots flew with the cushion, all pilots recommended the Oregon Aero® APECS® I Cushion System be made standard equipment for the ACES II ejection seat.



<b>APECSŪ</b>I installed on the ACES II ejection seat.
APECSŪ I installed on the ACES II ejection seat. Five custom designs of the APECSŪ I accommodate variations among aircraft.

Testing
X-Ray: See Actual Sitting Position
APECSŪ I: For ACES II Seat
APECSŪ I: F-22 Raptor Stealth Fighter
APECSŪ I-A: B-2 Bomber
APECSŪ I-B: F-16 Falcon
APECSŪ I-C: B-1 Bomber
APECSŪ I-D: F-117 Stealth Fighter
APECSŪ I-E: A-10 Warthog
APECSŪ I-F: F-15 Eagle
APECSŪ II: For Universal Propulsion Ejection Seat
APECSŪ III: FA-18
APECSŪ III-C: CF-18
APECSŪ III-N: NACES FA-18
APECSŪ IV: S-3 Viking
APECSŪ V: OV-10 Bronco
APECSŪ VI: B-52 Bomber, T-38
APECSŪ VII: U-2, SR-71
APECSŪ VIII: F-4 Phantom

Coastal Aircraft Parts LLC is the exclusive worldwide distributor of Oregon Aero® Seat Cushion Systems for military fixed wing and rotor wing aircraft.

Oregon Aero selected Coastal Aircraft Parts for the company's experience with all types of military aircraft and in-depth knowledge of Oregon Aero products. You can rely on Coastal Aircraft Parts to assist with the proper selection and purchase of the seat cushions systems that you require.

For more information or to place an order, please contact Coastal Aircraft Parts directly.
Website: www.coastalaircraftparts.com
E-mail: sales@coastalaircraftparts.com
Tel. 954-260-6280
Fax: 954-337-2806


Price List/Ordering Price List/Ordering
 

    Oregon Aero APECSŪ Ejection Seat Cushion Systems have been tested at NASA’s Dryden Flight Test Center, Rosamond, CA; Wright-Patterson Air Force Base, Dayton, OH; Patuxent River Naval Air Station, Lexington Park, MD; Brooks Air Force Base, San Antonio, TX; McDonnell Douglas, St. Louis, MO; National Institute for Aviation Research, University of Wichita, Wichita, KS; and MGA Laboratories, Burlington, WI.

An Example of Oregon Aero’s Attention to Detail

    During testing of the APECSŪ I design in an F-15 cockpit procedures simulator, the jet fighter’s seat felt fine when the pilot was in street clothes. When pilots tested the same seat during a mission, however, they complained of pressure on the lower back. Oregon Aero discovered a strap of the pilot’s body harness was located directly over a pelvic support wedge, causing pressure. A simple change cured the problem.
    The APECSŪ I cushions kept spinal lumbar loads to less than 1500 pounds, up to 18.6G’s, when tested during high-G terrain-following missions and crash testing.


X-ray of Person Sitting In the Oregon Aero®
APECSŪ
I Ejection Seat Cushion System

X-ray     This x-ray should convince anybody who’s still a skeptic! It shows that what we illustrate with models and say with words IS TRUE. The position shown in this x-ray is ideal for painless sitting. This position also produces the greatest resistance by the spine to injury from a vertical acceleration in the straight-up "Z" axis of the spine.

Line A: Horizontal datum (point from which other data is measured).
Line B: Angle of the pelvis relative to the Line A. Angular difference from the horizontal datum (Line A) is +13°. Ideal position.
Arc XX : Radius of the lumbar spine, 24.5 cm. Ideal position.
Line C-1: Surface of the vertebra relative to Line D-1, the surface of the adjacent vertebra (i.e., angular measurement of the vertebrae relative to each other). Angular difference is 9°. Ideal position.
Line C-2: Surface of the vertebra relative to Line D-2, the surface of the adjacent vertebra (i.e. angular measurement of the vertebrae relative to each other). Angular difference is 7°. Ideal position.

See the Seat Cushion Introduction for more information.




APECSŪ
I Ejection Seat Cushion System

(Advanced Performance Escape Cushion System I)
For Boeing/McDonnell Douglas ACES II Ejection Seat*
Five custom designs of the
APECSŪ I accommodate variations among aircraft.

APECS I installed on the ACES II ejection seat. APECS I™ (Advanced Performance Escape Cushioning System I)
APECSŪ I Ejection Seat Cushion System installed on the ACES II ejection seat.
APECSŪ I
(Advanced Performance Escape Cushion System I)

APECS I seat back base unit can be stressed without failure APECS I flexible snap mounting on tabs can be used with any seat assembly model’s stud placement.
APECSŪ I seat back base unit can be stressed without failure. No more cut fabric or bent stiffeners, which cause repairs and replacement! Our cushion uses a flexible inner plastic stiffener, not aluminum.
APECSŪ I flexible snap mounting on tabs can be used with any seat assembly model’s stud placement. Leather anti-chafe plate keeps the visible screw heads from cutting into fabric — another maintenance saver!

* ACES II Ejection Seats currently manufactured by BFGoodrich.


APECSŪ I Ejection Seat Cushion System:
F-22 Raptor Stealth Fighter

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
#3032012
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
#30320
Full Bottom Assembly w/fabric #37320
Full Bottom Assembly
w/fabric & wool
#37324
Bottom Core
w/muslin cover
#37321
Full Back Assembly
(Lumbar, Back)
w/fabric
#35320
Back Only (fabric) #36320
Lumbar Only (fabric) #38320
F-22


APECSŪ I-A Ejection Seat System:
B-2 Bomber

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
#3034012
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
#30340
Full Bottom Assembly w/fabric #3734012
Full Bottom Assembly
w/fabric & wool
#3734014
Bottom Core
w/muslin cover
#373401
Full Back Assembly
(Lumbar, Back)
#3534012
Back Only (fabric) #35340
Lumbar Only (fabric) #38340
B-2

Oregon Air National Guard F-15 hangar. Oregon Air National Guard F-15 hangar. Oregon Aero worked closely with the unit as the company developed the APECSŪ I Ejection Seat Cushion System.


APECSŪ I-B Ejection Seat Cushion System:
F-16 Falcon

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
(USAF Safe-to-Fly Approved)
#3035012
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
(USAF Safe-to-Fly Approved)
#30350
Full Bottom Assembly w/fabric #3735012
Full Bottom Assembly
w/fabric & wool
#3735014
Bottom Core
w/muslin cover
#373501
Full Back Assembly
(Lumbar, Back)
w/fabric
#3535012
Back Only (fabric) #35350
Lumbar Only (fabric) #38350



Full Seat Assembly
w/fabric & wool



Courtesy DoD



APECSŪ I-C Ejection Seat Cushion System:
B-1 Bomber


B-1

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
#3036012
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
#30360
Full Bottom Assembly
w/fabric
#3736012
Full Bottom Assembly
w/fabric & wool
#3736014
Bottom Core
w/muslin cover
#373601
Full Back Assembly
(Lumbar, Back) w/fabric
#3536012
Back Only (fabric) #35360
Lumbar Only (fabric) #38360


APECSŪ I-D Ejection Seat Cushion System:
F-117 Stealth Fighter

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
#3037012
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
#30370
Full Bottom Assembly w/fabric #3737012
Full Bottom Assembly
w/fabric & wool
#3737014
Bottom Core
w/muslin cover
#373701
Full Back Assembly
(Lumbar, Back) w/fabric
#3537012
Back Only (fabric) #35370
Lumbar Only (fabric) #38370


F-117


APECSŪ I-E Ejection Seat Cushion System:
A-10 Warthog

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
(USAF Safe-to-Fly Approved)
#30A100
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
(USAF Safe-to-Fly Approved)
#34A100
Full Bottom Assembly w/fabric #37A10012
Full Bottom Assembly
w/fabric & wool
#37A10014
Bottom Core
w/muslin cover
#37A1001
Full Back Assembly
(Lumbar, Back) w/fabric
#35A10012
Back Only (fabric) #35A100
Lumbar Only (fabric) #38A100



Full Seat Assembly
w/fabric & wool


A-10 Warthog



APECSŪ I-F Ejection Seat Cushion System:
F-15 Eagle

Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric
(USAF Safe-to-Fly Approved)
#30F150
Full Seat Assembly
(Lumbar, Bottom, Back)
w/fabric & wool
(USAF Safe-to-Fly Approved)
#34F150
Full Bottom Assembly w/fabric #37F15012
Full Bottom Assembly
w/fabric & wool
#37F15014
Bottom Core
w/muslin cover
#37F1501
Full Back Assembly
(Lumbar, Back) w/fabric
#35F15012
Back Only (fabric) #35F150
Lumbar Only (fabric) #38F150
F-15 Eagle


Full Seat Assembly
w/fabric & wool

Price List/Ordering Price List/Ordering

Testing
X-Ray: See Actual Sitting Position
APECSŪ I: For ACES II Seat
APECSŪ I: F-22 Raptor Stealth Fighter
APECSŪ I-A: B-2 Bomber
APECSŪ I-B: F-16 Falcon
APECSŪ I-C: B-1 Bomber
APECSŪ I-D: F-117 Stealth Fighter
APECSŪ I-E: A-10 Warthog
APECSŪ I-F: F-15 Eagle
APECSŪ II: For Universal Propulsion Ejection Seat
APECSŪ III: FA-18
APECSŪ III-C: CF-18
APECSŪ III-N: NACES FA-18
APECSŪ IV: S-3 Viking
APECSŪ V: OV-10 Bronco
APECSŪ VI: B-52 Bomber, T-38
APECSŪ VII: U-2, SR-71
APECSŪ VIII: F-4 Phantom

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Price List/Ordering

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