IP Library › Granted Patent US 8,777,323
Granted Patent B2
US 8,777,323 · App. 13/187,265 · Granted Jul 15, 2014

Restraint harnesses and associated methods of use and manufacture

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Quick Facts
Patent No.
US 8,777,323
App. No.
13/187,265
Granted
Jul 15, 2014
Kind
B2
Abstract

Various embodiments of restraint harnesses for use in land, air, and sea vehicles are described herein. In one embodiment, for example, a restraint harness can include a first shoulder web, a second shoulder web, and a torso web. A first end portion of the torso web can include a buckle that is configured to engage a connector at a second, opposite end portion of the torso web. The restraint harness can further include first and second portions of a stiffening material attached to first and second portions of the first and second shoulder webs, respectively. The stiffening material can form the first and second shoulder webs into preformed openings with inverted U-like shapes.

Claims (72)

1. A restraint system, comprising:

a first shoulder web having a first end portion opposite a second end portion;

a second shoulder web having a first end portion opposite a second end portion;

a torso web coupled to the first and second end portions of the first and second shoulder webs, wherein a first end portion of the torso web is coupled to a buckle configured to engage a connector coupled to a second, opposite end portion of the torso web;

a first portion of a stiffening material attached to a first portion of the first shoulder web;

a second portion of the stiffening material attached to a second portion of the second shoulder web, wherein the stiffening material forms the first and second shoulder webs into preformed openings with inverted U-shapes;

a tail web coupled to the torso web, the tail web having an end fitting configured to releasably engage an engagement feature on a vehicle; and

a retainer clip having an engagement feature, wherein the engagement feature of the retainer clip includes an opening configured to receive the end fitting and at least two opposing protrusions extending into the opening, and wherein the engagement feature of the retainer clip is configured to releasably retain the end fitting between the at least two opposing protrusions.

2. The restraint system of claim 1 wherein the stiffening material comprises at least one of spring steel, foam, molded plastic, formed metal pieces, layers of webbing, and structural sewing.

3. The restraint system of claim 1 wherein the first and second shoulder webs each include an outer layer of webbing substantially enclosing the stiffening material.

4. The restraint system of claim 1 , wherein the encasement feature of the retainer clip is a first engagement feature, and wherein the end fitting is configured to releasably engage a second engagement feature on the vehicle proximate a turret gunner position.

5. The restraint system of claim 1 wherein the engagement feature further comprises a spring portion extending at least partially between the at least two opposing protrusions.

6. A restraint system, comprising:

a first shoulder web having a first end portion opposite a second end portion;

a second shoulder web having a first end portion opposite a second end portion;

a torso web coupled to the first and second end portions of the first and second shoulder webs, wherein a first end portion of the torso web is coupled to a buckle configured to engage a connector coupled to a second, opposite end portion of the torso web;

a first portion of a stiffening material attached to a first portion of the first shoulder web;

a second portion of the stiffening material attached to a second portion of the second shoulder web, wherein the stiffening material forms the first and second shoulder webs into preformed openings with inverted U-shapes;

a tail web coupled to the torso web, the tail web having an end fitting configured to releasably engage an engagement feature on a vehicle; and

a retainer clip attached to at least one of the first shoulder web, the second shoulder web, and the torso web, wherein the retainer clip includes a magnet configured to releasably retain the end fitting.

7. The restraint system of claim 6 wherein the first and second portions of the stiffening material are configured to facilitate insertion of a wearer's arms into the preformed openings.

8. The restraint system of claim 6 , further comprising:

a back web between the first and second shoulder webs, wherein the first and second shoulder webs and the back web form an opening; and

a back panel substantially covering the opening.

9. The restraint system of claim 6 , further comprising:

a first identifying feature on the first shoulder web and on a portion of the torso web proximate to the first shoulder web; and

a second identifying feature on the second shoulder web and on a portion of the torso web proximate to the second shoulder web, wherein the second identifying feature is different from the first identifying feature.

10. A restraint system, comprising:

a first shoulder web having a first end portion opposite a second end portion;

a second shoulder web having a first end portion opposite a second end portion;

a torso web coupled to the first and second end portions of the first and second shoulder webs, wherein a first end portion of the torso web is coupled to a buckle configured to engage a connector coupled to a second, opposite end portion of the torso web;

a first portion of a stiffening material attached to a first portion of the first shoulder web;

a second portion of the stiffening material attached to a second portion of the second shoulder web, wherein the stiffening material forms the first and second shoulder webs into preformed openings with inverted U-shapes;

a tail web extending from the torso web, wherein the tail web includes an end fitting configured to releasably engage an engagement feature on a vehicle;

a back web between the first and second shoulder webs, wherein the first and second shoulder webs and the back web form an opening;

a back panel substantially covering the opening, wherein the back panel comprises a mesh material;

a retainer clip having an engagement feature and an attachment feature, wherein the engagement feature of the retainer clip is configured to releasably retain the end fitting, and wherein the attachment feature is configured to mount the retainer clip on at least one of the first shoulder web, the second shoulder web, and the torso web;

a first identifying feature on the first shoulder web and on a portion of the torso web proximate to the first shoulder web;

a second identifying feature on the second shoulder web and on a portion of the torso web proximate to the second shoulder web, wherein the first identifying feature is different from the second identifying feature; and

wherein the stiffening material comprises spring steel.

11. A restraint system, comprising:

a first shoulder web configured to receive a right shoulder of a wearer, wherein a portion of the first shoulder web includes a first portion of a stiffening material, and wherein the stiffening material is configured to preform the first shoulder web into a shape substantially corresponding to a shape the first shoulder web takes when in use;

a second shoulder web configured to receive a left shoulder of the wearer, wherein a portion of the second shoulder web comprises a second portion of the stiffening material, wherein the stiffening material is configured to preform the second shoulder web into a shape substantially corresponding to a shape the second shoulder web takes when in use; a torso web coupled to distal end portions of the first and second shoulder webs, wherein the torso web is configured to releasably engage around a portion of the wearer's torso;

a tail web coupled to the torso web, the tail web having an end fitting configured to releasably engage a portion of a vehicle; and

a retainer clip having an engagement feature, wherein the engagement feature includes an opening configured to receive the end fitting and at least two opposing protrusions extending into the opening, and wherein the engagement feature of the retainer clip is configured to releasably retain the end fitting between the opposing protrusions.

12. The restraint system of claim 11 wherein the stiffening material comprises at least one of spring steel, foam, molded plastic, formed metal pieces, additional layers of webbing, and structural sewing.

13. The restraint system of claim 11 wherein the end fitting of the tail web is configured to releasably engage a feature proximate a turret gunner position of the vehicle.

14. The restraint system of claim 11 wherein the retainer clip has an attachment feature configured to mount the retainer clip to an easily accessibly portion of the restraint system.

15. The restraint system of claim 11 , further comprising:

a back web; and

a back panel positioned between the back web and the first and second shoulder webs.

16. The restraint system of claim 11 , further comprising identifying features on the first and second shoulder webs, wherein the identifying features are configured to distinguish the first shoulder web from the second shoulder web.

17. A method of making a restraint harness, comprising:

attaching a first portion of a stiffening material to a first portion of a first shoulder web, wherein the stiffening material shapes the first portion of the first shoulder web into an inverted U-shape to define a first preformed opening;

attaching a second portion of the stiffening material to a second portion of a second shoulder web, wherein the stiffening material shapes the second portion of the second shoulder web into an inverted U-shape to define a second preformed opening; and

attaching the first and second shoulder webs to a torso web, the torso web having a buckle at a first distal end portion and a connector at a second distal end portion, wherein the buckle is configured to engage the connector,

wherein the step of attaching the first and second portions of the stiffening material to the respective first and second portions of the respective first and second shoulder webs further comprises integrating a spring steel through the first and second portions of the first and second shoulder webs.

18. The method of claim 17 wherein:

the step of attaching the first portion of the stiffening material to the first portion of the first shoulder web comprises enclosing the stiffening material with a first outer layer of webbing; and

the step of attaching the second portion of the stiffening material to the second portion of the second shoulder web comprises enclosing the stiffening material with a second outer layer of webbing.

19. A method of making a restraint harness, comprising:

attaching a first portion of a stiffening material to a first portion of a first shoulder web, wherein the stiffening material shapes the first portion of the first shoulder web into an inverted U-shape to define a first preformed opening;

attaching a second portion of the stiffening material to a second portion of a second shoulder web, wherein the stiffening material shapes the second portion of the second shoulder web into an inverted U-shape to define a second preformed opening;

attaching the first and second shoulder webs to a torso web, the torso web having a buckle at a first distal end portion and a connector at a second distal end portion, wherein the buckle is configured to engage the connector;

attaching a tail web to at least one of the torso web, the first shoulder web, and the second shoulder web, the tail web having an end fitting configured to engage an engagement feature of a vehicle; and

attaching a retainer clip to at least one of the first shoulder web, the second shoulder web, and the torso web, wherein the retainer clip includes an engagement feature configured to releasably retain the end fitting.

20. The method of claim 19 , further comprising:

attaching a back web between the first and second shoulder webs, wherein the first and second shoulder webs and the back web form an opening; and

positioning a back panel at least substantially over the opening.

21. The method of claim 19 , further comprising:

attaching a first identifying feature to the first shoulder web and on a first portion of the torso web proximate to the first shoulder web; and

attaching a second identifying feature on the second shoulder web and on a second portion of the torso web proximate to the second shoulder web, wherein the first identifying feature is different from the second identifying feature.

Assignments (11)
RELEASE OF PATENT SECURITY AGREEMENT RECORDED FEBRUARY 19, 2019 AT REEL/FRAME 048365/0499 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROSONIC LLC; MOUNTAINTOP TECHNOLOGIES, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; SHIELD RESTRAINT SYSTEMS, INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS, INC.; AEROSONIC CORPORATION; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE INC.; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; PURE TECHNOLOGIES LTD.; HARCO LABORATORIES, INC.; HARCO LLC; HARCO TECHNOLOGIES CORPORATION; CORRPRO COMPANIES, INC.; HARCO CORPORATION; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL GMBH; TELAIR INTERNATIONAL AB; NORDISK AVIATION PRODUCTS AS; TURNTIME TECHNOLOGIES AB; AEROCONTROLEX GROUP, INC.; TRANSICOIL INC.; SOUTHCO, INC.; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS COMPANY; JOSLYN SUNBANK COMPANY LLC; LEACH INTERNATIONAL CORPORATION; SOURIAU USA, INC.; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; ROLLS-ROYCE PLC; MEMTRON TECHNOLOGIES CO.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.; AERO-INSTRUMENTS CO., LLC; AIRBORNE SYSTEMS NA, INC.; HARCOSEMCO LLC; HARCO, LLC (N/K/A HARCOSEMCO LLC); PEXCO AEROSPACE, INC.; TELAIR US LLC; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; ADAMS RITE AEROSPACE, INC.; ACME AEROSPACE, INC.; SCHNELLER, INC.; CEF INDUSTRIES, INC.
Reel/Frame 067640/0147 →
CORRECTIVE ASSIGNMENT TO CORRECT THE NATURE OF CONVEYANCE PREVIOUSLY RECORDED AT REEL: 064961 FRAME: 0671. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT OF PATENT AND TRADEMARK SECURITY INTEREST. Recorded Oct 5, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 065132/0644 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 20, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 064961/0671 →
RELEASE OF SECURITY INTEREST Recorded Apr 19, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TA AEROSPACE CO.; TRANSDIGM, INC.; TRANSDIGM GROUP INCORPORATED; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECH TYEE, INC.; BEAM'S INDUSTRIES; BREEZE EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INC.; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; LEACH INTERNATIONAL CORPORATION; NMC GROUP INC.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.
Reel/Frame 063363/0753 →
SECURITY INTEREST Recorded Feb 27, 2023
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; 17111 WATERVIEW PKWY LLC; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE ACQUISITION, INC.; AIRBORNE GLOBAL, INC.; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NA INC.; AIRBORNE SYSTEMS NORTH AMERICA INC.; AIRBORNE SYSTEMS NORTH AMERICA OF CA INC.; AMSAFE GLOBAL HOLDINGS, INC.; AMSAFE, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; AUXITROL WESTON USA, INC.; AVIATION TECHNOLOGIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BETA TRANSFORMER TECHNOLOGY LLC; BREEZE-EASTERN LLC; BRIDPORT HOLDINGS, INC.; BRIDPORT-AIR CARRIER, INC.; BRUCE AEROSPACE INC.; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CENTURY HELICOPTERS, INC.; CHAMPION AEROSPACE LLC; CHELTON AVIONICS HOLDINGS, INC.; CHELTON AVIONICS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; DART AEROSPACE USA, INC.; DART BUYER, INC.; DART HELICOPTER SERVICES, INC.; DART INTERMEDIATE, INC.; DART TOPCO, INC.; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; ESTERLINE EUROPE COMPANY LLC; ESTERLINE INTERNATIONAL COMPANY; ESTERLINE TECHNOLOGIES CORPORATION; ESTERLINE TECHNOLOGIES SGIP LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KIRKHILL INC.; KORRY ELECTRONICS CO.; LEACH HOLDING CORPORATION; LEACH INTERNATIONAL CORPORATION; LEACH MEXICO HOLDING LLC; LEACH TECHNOLOGY GROUP, INC.; MARATHONNORCO AEROSPACE, INC.; MASON ELECTRIC CO.; MCKECHNIE AEROSPACE DE, INC.; MCKECHNIE AEROSPACE HOLDINGS, INC.; MCKECHNIE AEROSPACE US LLC; NAT SEATTLE INC.; NMC GROUP, INC.; NORDISK AVIATION PRODUCTS LLC; NORTH HILLS SIGNAL PROCESSING CORP.; NORTH HILLS SIGNAL PROCESSING OVERSEAS LLC; NORWICH AERO PRODUCTS, INC.; OFFSHORE HELICOPTER SUPPORT SERVICES, INC.; PALOMAR PRODUCTS, INC.; PARAVION TECHNOLOGY, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; POWER DEVICE CORPORATION; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTAIR FLUID CONTROLS, INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; BRIDPORT ERIE AVIATION, INC.; TRANSDIGM UK HOLDINGS PLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063012/0788 →
PATENT SECURITY AGREEMENT Recorded Apr 9, 2020
From: AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION/LLC; AIRBORNE HOLDINGS, INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BEAM’S INDUSTRIES; BREEZE-EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INCORPORATED; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSDIGM, INC.; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; ARMTEC DEFENSE PRODUCTS CO.; LEACH INTERNATIONAL CORPORATION; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC COMPANY; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 052352/0704 →
SECURITY INTEREST Recorded Feb 19, 2019
From: TRANSDIGM, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC (F/K/A AEROSONIC CORPORATION); AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS OF NORTH AMERICA OF NJ INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BREEZE-EASTERN LLC (F/K/A BREEZE-EASTERN CORPORATION); BRUCE AEROSPACE, INC.; CEF INDUSTRIES, LLC (F/K/A CEF INDUSTRIES, INC.); CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC (F/K/A WESTERN SKY, INDUSTRIES, LLC); HARCOSEMCO LLC (F/K/A HARCO LABORATORIES, INCORPORATED) (F/K/A HARCO LLC); HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC. (F/K/A AMSAFE COMMERCIAL PRODUCTS INC.) (F/K/A BEAM'S INDUSTRIES, INC.); TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ACME AEROSPACE, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.,
Reel/Frame 048365/0499 →
SECURITY AGREEMENT Recorded Mar 9, 2012
From: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS, INC.; AMSAFE AVIATION, INC.
To: CREDIT SUISSE AG
Reel/Frame 027830/0183 →
TERMINATION AND SECURITY RELEASE Recorded Mar 8, 2012
From: ARES CAPITAL CORPORATION
To: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS, INC.; AMSAFE AVIATION, INC.
Reel/Frame 027830/0048 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 12, 2011
From: MERRILL, DAVID T.; WALTON, MICHAEL J.; ESTRADA, ZULMA Y.
To: AMSAFE, INC.
Reel/Frame 026890/0425 →
SECURITY AGREEMENT Recorded Jul 22, 2011
From: AMSAFE, INC.; AMSAFE COMMERCIAL PRODUCTS. INC.; AMSAFE AVIATION, INC.
To: ARES CAPITAL CORPORATION, AS ADMINISTRATIVE AGENT
Reel/Frame 026637/0591 →