7-45880-3 - Boeing 777 Latch Control Assembly for Boeing 777

7-45880-3 is a boeing 777 latch control assembly manufactured by Triumph Controls Inc for the Boeing 777. This structural components part supports the airframe's structural integrity and load-bearing capability. Units are sourced through a vetted supplier network and released with the airworthiness documentation appropriate to their condition and source (FAA Form 8130-3 / EASA Form 1 where applicable).

Part Number
7-45880-3
Manufacturer
Triumph Controls Inc
Aircraft Model
Boeing 777
Category
Structural Components
Conditions Available
New / Overhauled / Serviceable / As-Removed — quoted per unit
Certification
FAA Form 8130-3 / EASA Form 1 available subject to source and condition
Price
Quoted per unit, condition, and trace documentation
Availability
Sourced on request — availability confirmed per RFQ, same-day response
Warranty
As per manufacturer
Request a Quote for 7-45880-3

Aircraft Applicability for 7-45880-3

7-45880-3 (Triumph Controls Inc) is listed as applicable to the following Boeing 777 family variants. Confirm eligibility against the aircraft IPC / Type Certificate Data Sheet for the specific tail and configuration.

  • Boeing 777-200LR
  • Boeing 777-300ER

About the 7-45880-3 for Boeing 777

The Boeing 777 Latch Control Assembly (P/N 7-45880-3) is a structural components for the Boeing 777, manufactured by Triumph Controls Inc. This component supports the airframe's structural integrity and load-bearing capability. Documented applicability spans 2 Boeing 777 configurations (Boeing 777-200LR, Boeing 777-300ER). It is typically procured during line maintenance, scheduled overhaul, or AOG recovery depending on service intervals and configuration.

Depending on supplier availability, 7-45880-3 may be sourced in the following conditions, each released with its corresponding airworthiness documentation:

  • New / Factory New
  • Overhauled (OH)
  • Serviceable (SV) / As-Removed

FAA-PMA certification and EASA Form 1 dual release may be available for 7-45880-3 subject to source and condition.

Frequently Asked Questions about 7-45880-3

What aircraft does 7-45880-3 fit?
7-45880-3 is a structural components associated with the Boeing 777, manufactured by Triumph Controls Inc. Documented applicability includes Boeing 777-200LR, Boeing 777-300ER. Eligibility for a specific tail still depends on serial number and modification status — verify against the aircraft IPC and Type Certificate Data Sheet.
Can 7-45880-3 be supplied new, overhauled, or serviceable?
Subject to global supplier availability, 7-45880-3 can typically be sourced new, overhauled, serviceable, or as-removed for the Boeing 777, each with the airworthiness documentation appropriate to that condition.
What traceability and certification ships with 7-45880-3?
7-45880-3 can be supplied with FAA-PMA where available; EASA Form 1 dual release and back-to-birth or teardown traceability may also be available depending on the source and condition of the specific unit.
How quickly can Triumph Controls Inc 7-45880-3 be quoted for an AOG?
RFQs for 7-45880-3 on the Boeing 777 are typically answered within 12-24 hours. AOG requirements are prioritized and sourced through the global supplier network on an expedited basis.
Can 7-45880-3 be exported internationally?
Yes. 7-45880-3 can be shipped worldwide subject to ITAR/EAR screening and destination-country import compliance; export and customs documentation is coordinated per shipment.

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