IP Library › Granted Patent US 7,410,128
Granted Patent B2
US 7,410,128 · App. 10/515,092 · Granted Aug 12, 2008

Transport device in cargo spaces in aircrafts

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Quick Facts
Patent No.
US 7,410,128
App. No.
10/515,092
Granted
Aug 12, 2008
Kind
B2
Abstract

The present invention relates to a transport device in cargo spaces in aircrafts, the transport device including a frame structure which, using retaining devices, is provided at the fuselage in the cargo space. The frame structure includes at least one conveyor belt for transport and storage of goods in the cargo space. The retaining devices are provided to retain the frame structure at the fuselage such that it can move in the retaining devices when it is subjected to abnormally high loads.

Claims (120)

1. A transport system including a transport device in cargo spaces in aircrafts,

said transport device comprising a first frame structure which by means of retaining devices is provided at the fuselage in the cargo space,

wherein the first frame structure includes at least one conveyor belt for transport and storage of goods in the cargo space,

characterized in that the retaining devices are provided to retain the first frame structure at the fuselage such that the first frame structure can move in said retaining devices when the first frame structure is subjected to abnormally high loads in order to prevent damage on the aircraft body, and wherein each retaining device includes at least one elongated flexible means which is located between the first frame structure and the fuselage and which permits movement of the first frame structure relative thereto, characterized in that said at least one flexible means is provided in parallel or substantially in parallel with the transport direction of the conveyor belt.

2. The transport device system according to claim 1 , characterized in that the retaining devices permit distribution of forces affecting the first frame structure to a plurality of locations on the fuselage situated after each other along the longitudinal direction of the first frame structure.

3. The transport system according to claim 1 , characterized in that the retaining devices are provided to permit, if the first frame structure subjects any of said retaining devices to abnormally high loads, movement of the first frame structure in this or these retaining devices relative to other retaining devices such that said abnormally high loads can be taken up by several retaining devices.

4. The transport system according to claim 1 , characterized in that the retaining devices are provided to permit movement of the first frame structure relative to that or those retaining devices which is/are not capable of taking up abnormally high loads which are subjected thereto or applied thereon by the first frame structure.

5. The transport system according to claim 1 , characterized in that the retaining devices are provided to permit movement of the frame structure relative to that or those retaining devices which is/are not capable of taking up abnormally high loads which are applied thereon by the first frame structure when the conveyor belt is loaded with goods.

6. The transport system according to claim 5 ,

wherein the transport device has a front end portion through which goods are loaded onto and unloaded from a conveyor belt and a rear end portion opposed to the front end portion,

wherein the conveyor belt has a separating device separating said belt in a front part on which goods can be placed and a rear part closest to the rear end portion of the transport device,

wherein the separating device moves with the conveyor belt between the front and rear end portions of the transport device, and

wherein the conveyor belt can be set such that the separating device is situated in an intermediate position between the front and rear end portions of the transport device, characterized in

that the retaining devices are provided to permit movement of the first frame structure relative to that or those retaining devices which is/are not capable of taking up abnormally high loads applied thereon by the first frame structure when the conveyor belt is loaded with goods and when the separating device is set in an intermediate position between the front and rear end portions of the transport device.

7. The transport system according to claim 1 , characterized in that the retaining devices are provided to permit movement of the first frame structure in a plane that is parallel or substantially parallel with the transport and storing plane of the conveyor belt.

8. The transport system according to claim 1 , characterized in that the retaining devices are provided to permit movement of the first frame structure in parallel or substantially in parallel with the transport direction of the conveyor belt.

9. The transport system according to claim 1 , characterized in that if the first frame structure twists or tends to twist in any of the retaining devices, said devices are provided to permit transfer and braking of this twisting movement by other retaining devices.

10. The transport system according to claim 1 , characterized in that the retaining devices are provided at a plurality of locations after each other in a longitudinal direction of the first frame structure and on opposite sides of said first frame structure.

11. The transport system according to claim 10 , characterized in that the retaining devices are provided at three locations.

12. The transport system according to claim 1 , characterized in that if a retaining device is loaded by the first frame structure relative to the fuselage with abnormal high loads, the elongated flexible means can slide relative to said fuselage.

13. The transport system according to claim 1 , characterized in that said at least one elongated flexible means by means of tightening devices is connected to the first frame structure on opposite sides of anchoring means through which said at least one elongated flexible means is connected to the fuselage.

14. The transport system according to claim 1 , characterized in that parts of said at least one elongated flexible means are provided to be able to move in lateral directions relative to the transport direction of the conveyor belt if said at least one elongated flexible means is subjected to abnormally high loads in said lateral directions.

15. The transport system according to claim 1 , characterized in

that each retaining device includes at least one lower and one upper tightening element and at least one tightening device,

that the lower tightening element cooperates with the fuselage and said at least one elongated flexible means with the first frame structure,

that said at least one elongated flexible means grasps in between the lower and upper tightening elements, and

that the tightening device is provided to tighten the lower and upper tightening elements against said at least one elongated flexible means with such a force that if the first frame structure is loaded with abnormally high forces relative to the fuselage, said at least one elongated flexible means can slide relative to the lower and upper tightening elements by overcoming the tightening forces thereof.

16. The transport system according to claim 15 , characterized in

that the tightening device includes a tightening screw which cooperates with brackets on the fuselage by grasping into and protruding therefrom,

that the tightening screw protrudes between said lower tightening element which engage said brackets, and

that the tightening screw protrudes through a hole in the upper tightening element and has above said element a tightening nut allowing tightening of the upper tightening element in a direction towards the bracket.

17. The transport system according to claim 1 , characterized in that said at least one elongated flexible means is a wire.

18. The transport system according to claim 1 , characterized in that the first frame structure is insertable into the cargo space through a door opening in the aircraft through which goods can be brought into and out of said aircraft.

19. The transport system according to claim 18 , characterized in that the first frame structure along with a conveyor belt and transport device provided thereon is insertable into the cargo space through said door opening.

20. The transport system according to claim 18 , characterized in

that the conveyor belt is provided pre-stressed on the first frame structure before said first frame structure is inserted into the cargo space through the door opening, and

that the conveyor belt is finally stressed after the first frame structure has been inserted into the cargo space through the door opening.

21. The transport system according to claim 18 , characterized in

that the first frame structure is foldable to a least length,

that the first frame structure in folded condition is insertable through the door opening and into the cargo space, and

that the first frame structure can be unfolded to its full length after its insertion in folded condition into the cargo space and before it is attached to brackets.

22. The transport system according to claim 1 , characterized in

that a driving device for driving or operating the conveyor belt has at least two drive gears which are provided substantially in level with separating means of the first frame structure such that lower parts thereof are found substantially in a first level with the underside of said separating means of the first frame structure or somewhat below said level,

that on the first frame structure, adjacent to each drive gear, there is provided a roll which is located such that lower parts thereof are found substantially in a second level with the upper side of the separating means of the first frame structure,

that a lower part of the convey or belt extends at the first level from the lower parts of the drive gears and in under the separating means, and

that an upper part of the conveyor belt extends from the drive gears and in under the roll and after the lower parts thereof on the second level along the upper side of the separating means.

23. The transport system according to claim 22 , characterized in

that the drive gears have teeth,

that the conveyor belt has toothed transport belts which cooperate with the drive gears, and

that the conveyor belt further comprises a transport mat on which the transport belts are provided.

24. The transport system according to claim 22 , characterized in

that the driving device has the at least two drive gears with which transport belts forming part of the conveyor belt cooperate,

that the drive gears are proved right behind and on mounting means through which the driving device is provided on the first frame structure, and

that rolls are provided in front of the drive gears, an upper part of the transport belts running under said rolls from the drive gears of the driving device to a transport mat forming part of the conveyor belt at which said transport belts are provided, whereby said rolls are mounted on the mounting means.

25. The transport system according to claim 22 , characterized in that the driving device on one of at least three transport elements located beside each other comprises on the intermediate transport elements at least one driving motor, the drive or working power of which is transferred to drive gears on the intermediate transport element as well as on the other transport elements.

26. The transport system according to claim 22 , characterized in

that the first frame structure is elongated and includes two longitudinal frame profiles which at the back are connected to each other by means of a transverse rear frame profile and at the front by means of a transverse front frame profile,

that the driving device is provided on the transverse rear frame profile,

that at least one roll is provided on the transverse front frame profile, and

that the conveyor belt at the back cooperates with the driving device and at the front with the roll and transforms or changes from its upper part into its lower part at these locations.

27. The transport system according to claim 26 , characterized in

that the rear frame profile is provided in an elongated groove at the back in the separating means which is designed as at least one plate-like means,

that the front frame profile is provided in a groove at the front in the separating means, and

that the separating means is connected to the rear and front frame profiles while the walls of the grooves engage and are connected to the walls of the frame profiles.

28. The transport system according to claim 27 , characterized in that the rear and front frame profiles have a four side cross section and engage a lower and an upper layer of the separating means as well as inner parts of the separating means lying there between.

29. The transport system according to claim 26 , characterized in that at least one of the transverse rear and transverse front frame profile has a body of a metallic material and that said body is surrounded by a carbon fiber material which is wound around the body.

30. The transport system according to claim 29 , wherein the metallic material comprises aluminum.

31. The transport system according to claim 26 , characterized in

that each longitudinal frame profile has upper parts which extend in over longitudinal edge portions of an upper part of the convey belt,

that each longitudinal frame profile has lower parts which extend in under longitudinal edge portions of a lower part of the conveyor belt,

that each longitudinal frame profile has a groove which is engaged by the separating means, and

that the separating means and the longitudinal frame profiles are fixedly connected or attached to each other.

32. The transport system according to claim 31 , characterized in

that each longitudinal frame profile includes an outer rail having a substantially C-shaped cross section and defining the upper and lower parts of the frame profile,

that each longitudinal frame profile includes an inner rail which is fixedly connected or attached to the outer rail and which has a substantially U-shaped cross section such that it defines an inwardly directed groove, and

that the separating means engages said groove, whereby the separating means and the inner rail are fixedly connected to each other.

33. The transport system according to claim 22 , characterized in

that the system comprises a second frame structure and a third frame structure, each located beside each other and the first frame structure,

that the driving device on an intermediate frame structure includes at least one driving motor, at least one drive shaft protruding therefrom and at least two drive gears driven or operated by the driving motor and cooperating with driving belts forming part of the conveyor belt on said first frame structure, and

that the driving device on two outer frame structures has shafts which through universal or cardan devices can be connected to the drive shaft protruding from the driving motor and which each includes two drive gears which cooperate with transport belts forming part of the conveyor belt on said outer frame structures.

34. The transport system according to claim 33 , characterized in that at least one of first and second positioning and retaining means is provided for at least one of setting and retention of the frame structures in predetermined mutual positions relative to each other in their longitudinal directions and for setting and retention of the frame structures at predetermined mutual distances from each other.

35. The transport system according to claim 33 , characterized in

that at least one first cover means can be provided between two adjacent frame structures for covering longitudinal gaps therebetween, and

that each first cover means is attached to longitudinal frame profiles of two adjacent frame structures.

36. The transport system according to claim 35 , characterized in

that at least one second cover means is provided in front of each conveyor belt for covering said belt from the front, and

that at least one third cover means is provided in front of a gap between the conveyor belts for covering gaps between said two first conveyor belts.

37. The transport system according to claim 33 , characterized in

that a wall extending in traverse direction relative to the conveyor belts of the first frame structure, is common to the conveyor belts of all three frame structures,

that the transverse wall is connected to all three conveyor belts such that it is brought along therewith during their transport movement,

that at least one transverse support beam for supporting the transverse wall is connected to and extends from one outer conveyor belt to the other outer conveyor belt, and

that said support beam is located at a distance above the conveyor belt of the intermediate frame structure.

38. The transport system according to claim 1 , characterized in

that a separating means between an upper and a lower part of the conveyor belt is a plate-like means of sandwich type and comprises inner parts which are honeycomb shaped and which include aramid fibers or aluminum, and

that the plate-like means includes a lower layer of a carbon fiber material, which is provided on the inner parts of honeycomb type, and an upper layer of a carbon fiber material, which is also provided on the inner parts of honeycomb type.

39. The transport system according to claim 1 , characterized in that the convey belt comprises a transport mat having a net structure with fiber threads running substantially in and transverse to the transport direction of the transport mat, said fiber threads being at least one of provided and designed such that the transport mat is considerably more rigid in transverse than in longitudinal direction relative to its transport direction.

40. The transport system according to claim 39 , characterized in that the transverse fiber threads of the transport mat comprise carbon and glass fibers in a carbon and glass fiber layer and the longitudinal fiber threads comprise aramid fibers and form part of an upper carbon and glass fiber layer, which above the longitudinal fiber threads of aramid fibers comprises fiber threads of aramid fibers running crosswise relative to each other and at about 45° relative to said transport direction.

41. The transport system according to claim 1 , characterized in that front parts of three transport devices located beside each other in a first group are provided or substantially provided on a first line extending straight or directly into the cargo space from a first side edge of a door opening through which goods can be loaded into and unloaded from the cargo space.

42. The transport system according to claim 41 , characterized in

that the first group and a second group comprising three transport devices which are located beside each other, are provided in the cargo space,

that front parts of the transport devices of the first group are provided or substantially provided on the first line extending straight into the cargo space from a first side edge of a door opening through which goods can be loaded into and unloaded from the cargo space, and

that front parts of the three transport devices of the second group may be provided or substantially provided on a second line extending straight into the cargo space from a second side edge of the door opening, such that between the transport devices of the first group and the second group, there is a free space within the door opening.

43. A transport system in cargo spaces in aircrafts,

said transport device comprising a first frame structure which by means of retaining devices is provided at the fuselage in the cargo space,

wherein the first frame structure includes at least one conveyor belt for transport and storage of goods in the cargo space,

characterized in that the retaining devices are provided to retain the first frame structure at the fuselage such that the first frame structure can move in said retaining devices when the first frame structure is subjected to abnormally high loads in order to prevent damage on the aircraft body, and wherein each retaining device includes at least one elongated flexible means which is located between the first frame structure and the fuselage and which permits movement of the first frame structure relative thereto, wherein the transport system further comprises:

a second frame structure is located beside the first frame structure, wherein each said retaining device comprises two of said at least one elongated flexible means,

that each elongated flexible means is connected to a frame structure,

that each elongated flexible means are provided in parallel or substantially in parallel with each other,

that one lower tightening element is provided for each elongated flexible means, and

that an upper tightening element is provided for both elongated flexible means.

44. A transport device in cargo spaces in aircrafts,

said transport device comprising a first frame structure which by means of retaining devices is provided at the fuselage in the cargo space,

wherein the first frame structure includes at least one conveyor belt for transport and storage of goods in the cargo space,

characterized in that the retaining devices are provided to retain the first frame structure at the fuselage such that the first frame structure can move in said retaining devices when the first frame structure is subjected to abnormally high loads in order to prevent damage on the aircraft body, and wherein each retaining device includes at least one elongated flexible means which is located between the first frame structure and the fuselage and which permits movement of the first frame structure relative thereto, wherein,

said at least one elongated flexible means is connected to the first frame structure by a lower tightening element provided on the first frame structure, an upper tightening element and a tightening screw, and

that the lower and upper tightening elements can be tightened together around said at least one elongated flexible means.

45. The transport system according to claim 44 , characterized in

that the first frame structure and at least one second frame structure are located beside each other, and

that each elongate flexible means is mounted on the respective frame structure by means of a first lower and upper tightening element and a tightening screw cooperating with an associated elongated flexible means which cooperates with an associated frame structure.

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 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 →
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
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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
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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
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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
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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.
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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
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SECURITY INTEREST Recorded Feb 27, 2023
From: TRANSDIGM, INC.; TRANSDIGM GROUP INCORPORATED; TRANSDIGM UK HOLDINGS PLC; 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.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ 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 ERIE AVIATION; 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.
To: GOLDMAN SACHS BANK USA, AS ADMINISTRATIVE AGENT AND COLLATERAL AGENT
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CHANGE OF NAME Recorded May 23, 2022
From: TELAIR INTERNATIONAL AB
To: TURNTIME TECHNOLOGIES AB
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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
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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.,
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ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 19, 2004
From: NORDSTROM, CLAES
To: TELAIR INTERNATIONAL AB
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