4E7870-25 - Boeing 787 Heated Composite Floor Panel Assy, Door 4 Lh for Boeing 787

4E7870-25 is a boeing 787 heated composite floor panel assy, door 4 lh manufactured by UTC Aerospace Systems, Goodrich Sensors & Integrated Systems for the Boeing 787. 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
4E7870-25
Manufacturer
UTC Aerospace Systems, Goodrich Sensors & Integrated Systems
Aircraft Model
Boeing 787
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 4E7870-25

Aircraft Applicability for 4E7870-25

4E7870-25 (UTC Aerospace Systems, Goodrich Sensors & Integrated Systems) is listed as applicable to the following Boeing 787 family variants. Confirm eligibility against the aircraft IPC / Type Certificate Data Sheet for the specific tail and configuration.

  • Boeing 787-8

About the 4E7870-25 for Boeing 787

The Boeing 787 Heated Composite Floor Panel Assy, Door 4 Lh (P/N 4E7870-25) is a structural components for the Boeing 787, manufactured by UTC Aerospace Systems, Goodrich Sensors & Integrated Systems. This component supports the airframe's structural integrity and load-bearing capability. Documented applicability spans 1 Boeing 787 configuration (Boeing 787-8). It is typically procured during line maintenance, scheduled overhaul, or AOG recovery depending on service intervals and configuration.

Depending on supplier availability, 4E7870-25 may be sourced in the following conditions, each released with its corresponding airworthiness documentation:

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

FAA Form 8130-3 or EASA Form 1 dual release may be available for 4E7870-25 subject to the source and condition of the specific unit.

Frequently Asked Questions about 4E7870-25

What aircraft does 4E7870-25 fit?
4E7870-25 is a structural components associated with the Boeing 787, manufactured by UTC Aerospace Systems, Goodrich Sensors & Integrated Systems. Documented applicability includes Boeing 787-8. Eligibility for a specific tail still depends on serial number and modification status — verify against the aircraft IPC and Type Certificate Data Sheet.
Can 4E7870-25 be supplied new, overhauled, or serviceable?
Subject to global supplier availability, 4E7870-25 can typically be sourced new, overhauled, serviceable, or as-removed for the Boeing 787, each with the airworthiness documentation appropriate to that condition.
What traceability and certification ships with 4E7870-25?
4E7870-25 is supplied with the airworthiness documentation appropriate to its condition and source (FAA Form 8130-3 or 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 UTC Aerospace Systems, Goodrich Sensors & Integrated Systems 4E7870-25 be quoted for an AOG?
RFQs for 4E7870-25 on the Boeing 787 are typically answered within 12-24 hours. AOG requirements are prioritized and sourced through the global supplier network on an expedited basis.
Can 4E7870-25 be exported internationally?
Yes. 4E7870-25 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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