113T2000-39 Shim, Tapered

The Boeing Company

Part # 113T2000-39

The tapered shim 113T2000-39 is vital for KC-46A stability and support, featuring two bolt holes for secure attachment. FAA certified, it meets high safety standards. Its tapered design allows precise adjustments for specific alignment, enhancing overall aircraft integrity and performance.
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Overview

The tapered shim 113T2000-39 is an essential component for the KC-46A aircraft, designed to provide stability and support during operation. This rectangular shim features two bolt holes, ensuring secure attachment. FAA certification confirms compliance with rigorous safety and performance standards. The tapered design allows for precise adjustments, making it suitable for applications that require specific alignment, contributing to the overall structural integrity and performance of the aircraft.

Features & Benefits

Features
  • FAA certified for compliance with safety standards.
  • Rectangular shape with two bolt holes for secure installation.
  • Tapered design for precise alignment and support.
Benefits
  • Enhances structural integrity of the KC-46A aircraft.
  • Facilitates accurate adjustments for optimal performance.
  • Ensures reliable operation in several conditions.

Technical Information

ATA Number

27

ATA Chapter

Flight Controls

ATA Group

Airframe Systems

ATA Section

TRAILING EDGE FLAP SYSTEM

NIIN

017146799

NSN

5365-01-714-6799

FSCG

5365

FSCG Category

Bushings, Rings, Shims, and Spacers

Lead Time (Days)

91

Certification Status

CERTIFIED

ATA Part Number

113T2000-39

CAGE Code

81205

Commercial Part

Yes

Harmonized Tariff Schedule Code

8807300030

Repairable

No

Specification Part Number

113T2000-39

Supplier Part Number

113T2000-39

Landing Gear Part

No

Leasable

No

Returnable

No

Aircraft Makes

Boeing

Aircraft Models

767-300
767-400ER
767-400
767-200
767-300EREM
767-300BCF
4 more

Shipping Details

ITAR Compliant

No

Part Explosive

No

ECCN

9A991.d

Dry Ice

No
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Commercial Spares
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