P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval - BHT Door Opener Kit (4 Door) for BHT

P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval is a bht door opener kit (4 door) manufactured by Bell Helicopter Textron Inc for the BHT. 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
P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval
Manufacturer
Bell Helicopter Textron Inc
Aircraft Model
BHT
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 P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval

Aircraft Applicability for P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval

P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval (Bell Helicopter Textron Inc) is listed as applicable to the following BHT family variants. Confirm eligibility against the aircraft IPC / Type Certificate Data Sheet for the specific tail and configuration.

  • 206 L/L-l/L-3

About the P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval for BHT

The BHT Door Opener Kit (4 Door) (P/N P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval) is a structural components for the BHT, manufactured by Bell Helicopter Textron Inc. This component supports the airframe's structural integrity and load-bearing capability. Documented applicability spans 1 BHT configuration (206 L/L-l/L-3). It is typically procured during line maintenance, scheduled overhaul, or AOG recovery depending on service intervals and configuration.

Depending on supplier availability, P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval 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 P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval subject to the source and condition of the specific unit.

Frequently Asked Questions about P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval

What aircraft does P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval fit?
P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval is a structural components associated with the BHT, manufactured by Bell Helicopter Textron Inc. Documented applicability includes 206 L/L-l/L-3. Eligibility for a specific tail still depends on serial number and modification status — verify against the aircraft IPC and Type Certificate Data Sheet.
Can P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval be supplied new, overhauled, or serviceable?
Subject to global supplier availability, P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval can typically be sourced new, overhauled, serviceable, or as-removed for the BHT, each with the airworthiness documentation appropriate to that condition.
What traceability and certification ships with P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval?
P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval 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 Bell Helicopter Textron Inc P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval be quoted for an AOG?
RFQs for P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval on the BHT are typically answered within 12-24 hours. AOG requirements are prioritized and sourced through the global supplier network on an expedited basis.
Can P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval be exported internationally?
Yes. P/N 206-510-175 I/A/W DLR AA-86001, No Rev. dtd May 13, 1986 or later FAA Approval 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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