IP Library › Granted Patent US 8,936,419
Granted Patent B1
US 8,936,419 · App. 13/967,830 · Granted Jan 20, 2015

Restraint system for restraining a unit load device in an aircraft

Inventor: Amirul Islam (Clayton, NC)
Assignee: AAR Corp.
B64D9/003
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,936,419
App. No.
13/967,830
Granted
Jan 20, 2015
Kind
B1
Abstract

A restraint system for releasably restraining a unit load device in an aircraft. The restraint system includes a guide rail adapted to be connected to the aircraft and one or more restraint mechanisms connected to the guide rail. Each restraint mechanism includes a pawl that is selectively pivotal between a locked position and an unlocked position. The guide rail is adapted to restrain movement of the unit load device in the transverse direction and the pawl of the restraint mechanism is adapted to restrain movement of the unit load device in the longitudinal and vertical directions when the pawl is in the locked position.

Claims (57)

1. A restraint mechanism for releasably restraining a unit load device in an aircraft, the restraint mechanism comprising:

a housing adapted to be connected to the aircraft;

a pawl pivotally coupled to said housing for pivotal movement about a pivot axis with respect to said housing between a locked position and an unlocked position, said pawl including a first foot pivotally coupled to said housing, and a head adapted to releasably restrain movement of the unit load device when said pawl is in said locked position;

a first cam assembly having a first end and a second end, said second end of said first cam assembly coupled to said pawl, said cam assembly including a first link and a second link, said first link pivotally coupled to said second link, said first link including said first end of said cam assembly and said second link including said second end of said cam assembly; and

an actuator shaft coupled to said housing for selective rotation about a rotational axis with respect to said housing, said actuator shaft being coupled to said first link of said first cam assembly such that said first link conjointly pivots with said actuator shaft about said rotational axis;

whereby rotational movement of said actuator shaft in a first rotational direction about said rotational axis pivots said pawl about said pivot axis toward said locked position of said pawl wherein said pawl is adapted to restrain movement of the unit load device, and wherein rotational movement of said actuator shaft in a second rotational direction about said rotational axis pivots said pawl about said pivot axis toward said unlocked position of said pawl wherein said pawl permits movement of the unit load device.

2. The restraint mechanism of claim 1 wherein said head of said pawl includes a top wall, a first side wall, and a second side wall spaced apart from said first side wall, said top wall, first side wall and said second side wall forming a cavity adapted to receive at least a portion of the unit load device when said pawl is in said locked position, said top wall adapted to restrain movement of the unit load device along a vertical axis of the aircraft, and said first side wall and said second side wall are adapted to restrain movement of the unit load device along a longitudinal axis of the aircraft.

3. The restraint mechanism of claim 1 wherein said first link of said first cam assembly includes a first end and a second end, said first end of said first link coupled to said actuator shaft for conjoint rotation with said actuator shaft about said rotational axis, said second link of said first cam assembly including a first end and a second end, said first end of said second link being pivotally coupled to said second end of said first link for pivotal movement about a first cam pivot axis, said second end of said second link being pivotally coupled to said pawl for pivotal movement about a second cam pivot axis.

4. The restraint mechanism of claim 3 wherein said second link includes a recess, said recess adapted to receive said actuator shaft such that said rotational axis of said actuator shaft is located between said first cam pivot axis and said second cam pivot axis when said pawl is in said locked position.

5. The restraint mechanism of claim 4 wherein said rotational axis of said actuator shaft, said first cam pivot axis of said first cam assembly and said second cam pivot axis of said first cam assembly are substantially coplanar with one another when said pawl is in the locked position.

6. The restraint mechanism of claim 3 wherein said first cam assembly includes a third link having a first end pivotally coupled to said second end of said first link for pivotal movement about said first cam pivot axis and a second end pivotally coupled to said pawl for pivotal movement about said second cam pivot axis, said first link being located between said second link and said third link.

7. The restraint mechanism of claim 1 including a connector member pivotally coupling said second end of said first cam assembly to said pawl.

8. The restraint mechanism of claim 1 including a connector member fixedly coupled to said pawl and pivotally coupled to said housing.

9. The restraint mechanism of claim 8 wherein said connector member comprises a pivot shaft extending into said first foot of said pawl, and including a fastener fixedly coupling said pivot shaft to said first foot of said pawl, said pivot shaft being pivotally coupled to said housing.

10. The restraint mechanism of claim 9 including a resilient biasing member coupled to said pivot shaft, said biasing member adapted to resiliently bias said pawl about said pivot axis.

11. The restraint mechanism of claim 1 wherein said housing includes a front wall, a rear wall and a first pawl chamber, said rear wall including a first pawl aperture in communication with said first pawl chamber, said pawl including a first leg coupling said first foot of said pawl to said head of said pawl, said first foot of said pawl located in said first pawl chamber and said first leg of said pawl extending outwardly from said first pawl chamber through said first pawl aperture in said rear wall of said housing.

12. The restraint mechanism of claim 11 wherein said housing includes a second pawl chamber and a third pawl chamber, said rear wall of said housing including a second pawl aperture in communication with said second pawl chamber and a third pawl aperture in communication with said third pawl chamber, said pawl including a second leg coupled to a second foot and a third leg coupled to a third foot, said second foot located within said second pawl chamber and pivotally coupled to said housing, said second leg extending outwardly from said second pawl chamber through said second pawl aperture, said third foot located in said third pawl chamber and pivotally coupled to said housing, said third leg extending outwardly from said third pawl chamber through said third pawl aperture, said second foot and said third foot of said pawl adapted to pivot about said pivot axis.

13. The restraint mechanism of claim 12 wherein said front wall of said housing includes a first pawl aperture in communication with said first pawl chamber, a second pawl aperture in communication with said second pawl chamber, and a third pawl aperture in communication with said third pawl chamber.

14. The restraint of claim 11 wherein said housing includes a first cam chamber located adjacent said first pawl chamber, said rear wall of said housing including a first cam aperture, said first end of said first cam assembly being located within said first cam chamber, said first cam assembly adapted to extend outwardly from said first cam chamber through said first cam aperture.

15. The restraint mechanism of claim 14 including a second cam assembly having a first end and a second end, said second end of said second cam assembly coupled to said pawl, said first end of said second cam assembly coupled to said actuator shaft, said housing including a second cam chamber, said rear wall of said housing including a second cam aperture, said first end of said second cam assembly being located within said second cam assembly chamber, said second cam assembly adapted to extend outwardly from said second cam chamber through said second cam aperture.

16. The restraint mechanism of claim 1 including an actuator coupled to said actuator shaft, said actuator adapted to selectively rotate said actuator shaft in said first rotational direction or said second rotational direction about said rotational axis.

17. The restraint mechanism of claim 1 including a first proximity sensor adapted to sense when said pawl is in said locked position, and a second proximity sensor adapted to sense when said pawl is in said unlocked position.

18. The restraint mechanism of claim 16 wherein the actuator includes a drive motor and a controller electrically coupled to the drive motor by a power-signal cable harness.

19. The restraint mechanism of claim 1 including a plate coupled to a wall of the housing for reinforcing and stiffening the housing.

20. A restraint assembly for releasably restraining a unit load device in an aircraft, the restraint assembly comprising:

a guide rail adapted to be connected to the aircraft, said guide rail including a wall having an aperture; and

a restraint mechanism including a housing connected to said guide rail,

a pawl pivotally coupled to said housing for pivotal movement about a pivot axis with respect to said housing between a locked position and an unlocked position, said pawl including an exterior surface, a first foot pivotally coupled to said housing, and a head adapted to releasably restrain movement of the unit load device when said pawl is in said locked position, said pawl being aligned with said aperture in said wall of said guide rail,

a first cam assembly having a first end and a second end, said second end of said first cam assembly coupled to said pawl, and

an actuator shaft coupled to said housing for selective rotation about a rotational axis with respect to said housing, said first end of said first cam assembly coupled to said actuator shaft;

whereby rotational movement of said actuator shaft in a first rotational direction about said rotational axis pivots said pawl about said pivot axis toward said locked position of said pawl wherein said pawl is adapted to restrain movement of the unit load device, and whereby rotational movement of said actuator shaft in a second rotational direction about said rotational axis pivots said pawl about said pivot axis toward said unlocked position of said pawl wherein said pawl extends outwardly from said housing and through said aperture in said wall of said guide rail such that said pawl is adapted to permit movement of the unit load device.

21. The restraint assembly of claim 20 wherein said guide rail and said restraint mechanism are conjointly moveable between a deployed position and a stowed position with respect to a cargo floor of the aircraft, said exterior surface of said pawl being generally coplanar with an exterior surface of said wall of said guide rail when said pawl is in said locked position, such that said exterior surface of said pawl and said exterior surface of said wall of said guide rail are adapted to be generally coplanar with a surface of the cargo floor when said guide rail and said restraint mechanism are in said stowed position, said guide rail and said restraint mechanism adapted to selectively restrain a unit load device when said guide rail and said restraint mechanism are in said deployed position.

22. A restraint mechanism for releasably restraining a unit load device in an aircraft, the restraint mechanism comprising:

a housing adapted to be connected to the aircraft;

a pawl pivotally coupled to said housing for pivotal movement about a pivot axis with respect to said housing between a locked position and an unlocked position, said pawl including a first foot pivotally coupled to said housing, and a head adapted to releasably restrain movement of the unit load device when said pawl is in said locked position;

a first cam assembly having a first end and a second end, said second end of said first cam assembly coupled to said pawl; and

an actuator shaft coupled to said housing for selective rotation about a rotational axis with respect to said housing, said first end of said first cam assembly coupled to said actuator shaft;

whereby rotational movement of said actuator shaft in a first rotational direction about said rotational axis pivots said pawl about said pivot axis toward said locked position of said pawl wherein said pawl is adapted to restrain movement of the unit load device, and wherein rotational movement of said actuator shaft in a second rotational direction about said rotational axis pivots said pawl about said pivot axis toward said unlocked position of said pawl wherein said pawl permits movement of the unit load device;

wherein said head of said pawl includes a top wall, a first side wall, and a second side wall spaced apart from said first side wall, said top wall, first side wall and said second side wall forming a cavity adapted to receive at least a portion of the unit load device when said pawl is in said locked position, said top wall adapted to restrain movement of the unit load device along a vertical axis of the aircraft, and said first side wall and said second side wall are adapted to restrain movement of the unit load device along a longitudinal axis of the aircraft.

23. A restraint mechanism for releasably restraining a unit load device in an aircraft, the restraint mechanism comprising:

a housing adapted to be connected to the aircraft;

a pawl pivotally coupled to said housing for pivotal movement about a pivot axis with respect to said housing between a locked position and an unlocked position, said pawl including a first foot pivotally coupled to said housing, and a head adapted to releasably restrain movement of the unit load device when said pawl is in said locked position;

a first cam assembly having a first end and a second end, said second end of said first cam assembly coupled to said pawl; and

an actuator shaft coupled to said housing for selective rotation about a rotational axis with respect to said housing, said first end of said first cam assembly coupled to said actuator shaft;

whereby rotational movement of said actuator shaft in a first rotational direction about said rotational axis pivots said pawl about said pivot axis toward said locked position of said pawl wherein said pawl is adapted to restrain movement of the unit load device, and wherein rotational movement of said actuator shaft in a second rotational direction about said rotational axis pivots said pawl about said pivot axis toward said unlocked position of said pawl wherein said pawl permits movement of the unit load device;

wherein said housing includes a front wall, a rear wall and a first pawl chamber, said rear wall including a first pawl aperture in communication with said first pawl chamber, said pawl including a first leg coupling said first foot of said pawl to said head of said pawl, said first foot of said pawl located in said first pawl chamber and said first leg of said pawl extending outwardly from said first pawl chamber through said first pawl aperture in said rear wall of said housing.

24. The restraint mechanism of claim 23 wherein said housing includes a second pawl chamber and a third pawl chamber, said rear wall of said housing including a second pawl aperture in communication with said second pawl chamber and a third pawl aperture in communication with said third pawl chamber, said pawl including a second leg coupled to a second foot and a third leg coupled to a third foot, said second foot located within said second pawl chamber and pivotally coupled to said housing, said second leg extending outwardly from said second pawl chamber through said second pawl aperture, said third foot located in said third pawl chamber and pivotally coupled to said housing, said third leg extending outwardly from said third pawl chamber through said third pawl aperture, said second foot and said third foot of said pawl adapted to pivot about said pivot axis.

25. The restraint mechanism of claim 24 wherein said front wall of said housing includes a first pawl aperture in communication with said first pawl chamber, a second pawl aperture in communication with said second pawl chamber, and a third pawl aperture in communication with said third pawl chamber.

26. The restraint of claim 23 wherein said housing includes a first cam chamber located adjacent said first pawl chamber, said rear wall of said housing including a first cam aperture, said first end of said first cam assembly being located within said first cam chamber, said first cam assembly adapted to extend outwardly from said first cam chamber through said first cam aperture.

27. The restraint mechanism of claim 26 including a second cam assembly having a first end and a second end, said second end of said second cam assembly coupled to said pawl, said first end of said second cam assembly coupled to said actuator shaft, said housing including a second cam chamber, said rear wall of said housing including a second cam aperture, said first end of said second cam assembly being located within said second cam assembly chamber, said second cam assembly adapted to extend outwardly from said second cam chamber through said second cam aperture.

28. A restraint mechanism for releasably restraining a unit load device in an aircraft, the restraint mechanism comprising:

a housing adapted to be connected to the aircraft;

a pawl pivotally coupled to said housing for pivotal movement about a pivot axis with respect to said housing between a locked position and an unlocked position, said pawl including a first foot pivotally coupled to said housing, and a head adapted to releasably restrain movement of the unit load device when said pawl is in said locked position;

a first proximity sensor adapted to sense when said pawl is in said locked position, and a second proximity sensor adapted to sense when said pawl is in said unlocked position;

a first cam assembly having a first end and a second end, said second end of said first cam assembly coupled to said pawl; and

an actuator shaft coupled to said housing for selective rotation about a rotational axis with respect to said housing, said first end of said first cam assembly coupled to said actuator shaft;

whereby rotational movement of said actuator shaft in a first rotational direction about said rotational axis pivots said pawl about said pivot axis toward said locked position of said pawl wherein said pawl is adapted to restrain movement of the unit load device, and wherein rotational movement of said actuator shaft in a second rotational direction about said rotational axis pivots said pawl about said pivot axis toward said unlocked position of said pawl wherein said pawl permits movement of the unit load device.

Assignments (14)
SECURITY INTEREST Recorded Aug 26, 2025
From: TRANSDIGM INC.; 17111 WATERVIEW PKWY LLC; 4455 GENESEE PROPERTIES, LLC; 4455 GENESEE STREET, 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.; ASHFORD PROPERTIES, LLC; 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.; CALSPAN, LLC; CALSPAN AIR FACILITIES, LLC; CALSPAN AIR SERVICES, LLC; CALSPAN ASE PORTUGAL, INC.; CALSPAN HOLDINGS, LLC; CALSPAN JETS LLC; CALSPAN TECHNOLOGY ACQUISITION LLC; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; CHELTON AVIONICS HOLDINGS, INC.; CHELTON AVIONICS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; CPI EDB INTERMEDIATE HOLDINGS, INC.; CPI ELECTON DEVICE BUSINESS, INC.; CTHC 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; FPT INDUSTRIES LLC; GENESEE HOLDINGS, LLC; GENESEE HOLDINGS II, LLC; GENESSE HOLDINGS III, LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ICEMAN HOLDCO, INC.; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KING NUTRONICS, 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; MEDTHERM LABS, LLC; MICROWAVE POWER PRODUCTS, INC.; 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; RAPTOR LABS HOLDCO, LLC; RAPTOR LABS INTERMEDIATE, LLC; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SENSOR CONCEPTS, LLC; SERVOTRONICS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SPACE ELECTRONICS LLC; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTIAR FLUID CONTROLS, INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TESTVONICS, INC.; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; BRIDPORT ERIE AVIATION, INC.; TRANSDIGM GROUP INCORPORATED; TRANSDIGM UK HOLDINGS LIMITED
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 072473/0485 →
SECURITY INTEREST Recorded Sep 20, 2024
From: TRANSDIGM GROUP INCORPORATED; TRANSDIGM INC.; TRANSDIGM UK HOLDINGS LIMITED; 17111 WATERVIEW PKWY LLC; 4455 GENESEE STREET, LLC; 4455 GENESEE PROPERTIES, LLC; 703 CITY CENTER BOULEVARD, 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.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; AMSAFE GLOBAL HOLDINGS, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; ASHFORD PROPERTIES, LLC; 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; BRIDPORT ERIE AVIATION, INC.; BRUCE AEROSPACE, INC.; CALSPAN AERO SYSTEMS ENGINEERING LLC; CALSPAN AIR FACILITIES, LLC; CALSPAN AIR SERVICES, LLC; CALSPAN ASE PORTUGAL, INC.; CALSPAN HOLDINGS, LLC; CALSPAN, LLC; CALSPAN JETS LLC; CALSPAN SYSTEMS LLC; CALSPAN TECHNOLOGY ACQUISITION LLC; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; CHELTON AVIONICS, INC.; CHELTON AVIONICS HOLDINGS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; CPI INTERMEDIATE HOLDINGS, INC.; CPI INTERNATIONAL, INC.; CPI SUBSIDIARY HOLDINGS LLC; CTHC 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; FPT INDUSTRIES LLC; GENESEE HOLDINGS, LLC; GENESEE HOLDINGS II, LLC; GENESEE HOLDINGS III, LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ICEMAN HOLDCO, INC.; ICEMAN INTERMEDIATE MIDCO, LLC; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KIRKHILL INC.; KING NUTRONICS, LLC; 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; MEDTHERM LABS, LLC; MICROWAVE POWER PRODUCTS, INC.; 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.; POWER DEVICE CORPORATION; PNEUDRAULICS, INC.; RAPTOR LABS HOLDCO, LLC; RAPTOR LABS INTERMEDIATE, LLC; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SENSOR CONCEPTS, LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SPACE ELECTRONICS LLC; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTAIR FLUID CONTROLS INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TESTVONICS, INC.; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 068951/0001 →
RELEASE OF PATENT SECURITY AGREEMENT RECORDED MAY 1, 2023 AT REEL/FRAME 063500/0312 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: KORRY ELECTRONICS CO.; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC CO.; SOURIAU USA, INC.; 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; 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 067640/0618 →
SECURITY INTEREST Recorded Mar 1, 2024
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; TRANSDIGM UK HOLDINGS LIMITED; 17111 WATERVIEW PKWY LLC; 4455 GENESEE STREET, LLC; 4455 GENESEE PROPERTIES, LLC; 703 CITY CENTER BOULEVARD, 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.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; AMSAFE GLOBAL HOLDINGS, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; ASHFORD PROPERTIES, LLC; 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; BRIDPORT ERIE AVIATION, INC.; BRUCE AEROSPACE, INC.; CALSPAN AERO SYSTEMS ENGINEERING LLC; CALSPAN AIR FACILITIES, LLC,; CALSPAN AIR SERVICES, LLC; CALSPAN ASE PORTUGAL, INC.; CALSPAN HOLDINGS, LLC; CALSPAN, LLC; CALSPAN SYSTEMS LLC; CALSPAN TECHNOLOGY ACQUISITION LLC; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; CHELTON AVIONICS, INC.; CHELTON AVIONICS HOLDINGS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; CTHC 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; GENESEE HOLDINGS, LLC; GENESEE HOLDINGS II, LLC; GENESEE HOLDINGS III, 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.; POWER DEVICE CORPORATION; PNEUDRAULICS, INC.; 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.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 066763/0138 →
SECURITY INTEREST Recorded Mar 1, 2024
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; TRANSDIGM UK HOLDINGS LIMITED; 17111 WATERVIEW PKWY LLC; 4455 GENESEE STREET, LLC; 4455 GENESEE PROPERTIES, LLC; 703 CITY CENTER BOULEVARD, 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.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; AMSAFE GLOBAL HOLDINGS, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; ASHFORD PROPERTIES, LLC; 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; BRIDPORT ERIE AVIATION, INC.; BRUCE AEROSPACE, INC.; CALSPAN AERO SYSTEMS ENGINEERING LLC; CALSPAN AIR FACILITIES, LLC; CALSPAN AIR SERVICES, LLC; CALSPAN ASE PORTUGAL, INC.; CALSPAN HOLDINGS, LLC; CALSPAN, LLC; CALSPAN SYSTEMS LLC; CALSPAN TECHNOLOGY ACQUISITION LLC; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; CHELTON AVIONICS, INC.; CHELTON AVIONICS HOLDINGS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; CTHC 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; GENESEE HOLDINGS, LLC; GENESEE HOLDINGS II, LLC; GENESEE HOLDINGS III, 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.; POWER DEVICE CORPORATION; PNEUDRAULICS, INC.; 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.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 066713/0308 →
SECURITY INTEREST Recorded Nov 29, 2023
From: TRANSDIGM INC.; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; APICAL INDUSTRIES, INC.; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE, INC.; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; HARCO LABORATORIES, INCORPORATED (N/K/A HARCOSEMCO LLC); HARCO, LLC (N/K/A HARCOSEMCO LLC); HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PALOMAR PRODUCTS, INC.; PEXCO AEROSPACE, INC.; SCHNELLER LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; TACTAIR FLUID CONTROLS, INC.; TELAIR INTERNATIONAL LLC (N/K/A NORDISK AVIATION PRODUCTS LLC); TELAIR US LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC DEFENSE PRODUCTS CO.; NMC GROUP, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; KORRY ELECTRONICS CO.; MASON ELECTRIC CO.; AIRBORNE SYSTEMS NA INC.; HARCOSEMCO LLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 065724/0903 →
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 →
SECURITY INTEREST Recorded Aug 22, 2023
From: TRANSDIGM INC.; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PALOMAR PRODUCTS, INC.; PEXCO AEROSPACE, INC.; SCHNELLER LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; TACTAIR FLUID CONTROLS, INC.; TELAIR INTERNATIONAL LLC (N/K/A NORDISK AVIATION PRODUCTS LLC); TELAIR US LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC DEFENSE PRODUCTS CO.; NMC GROUP, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; KORRY ELECTRONICS CO.; MASON ELECTRIC, CO.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 064661/0654 →
SECURITY INTEREST Recorded May 1, 2023
From: ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE SYSTEMS NA, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE, INC.; ARMTEC DEFENSE PRODUCTS CO.; AVTECHTYEE, INC.; BREEZE-EASTERN CORPORATION; CEF INDUSTRIES, INC.; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; HARCO, LLC (N/K/A HARCOSEMCO LLC); HARCOSEMCO LLC; HARTWELL CORPORATION; LEACH INTERNATIONAL CORPORATION; MARATHONNORCO AEROSPACE, INC.; MASON ELECTRIC CO.; PALOMAR PRODUCTS, INC.; PEXCO AEROSPACE, INC.; SCHNELLER LLC; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; TACTAIR FLUID CONTROLS INC.; TELAIR US LLC; WHIPPANY ACTUATION SYSTEMS, LLC; TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063500/0312 →
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 →
SECURITY AGREEMENT Recorded Apr 9, 2015
From: TELAIR US LLC
To: CREDIT SUISSE AG, AS AGENT
Reel/Frame 035401/0695 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2015
From: AAR CORP
To: TELAIR US LLC
Reel/Frame 035273/0787 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 10, 2013
From: ISLAM, AMIRUL
To: AAR CORP.
Reel/Frame 031379/0160 →