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SERVICE LETTER

LET L-410 UVP-E20 · Service Bulletins

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Overview

This document is a service letter for the L-410 UVP-E20 aircraft, issued to address a specific maintenance check on the nose landing gear leg. It outlines the procedure for checking the sleeve on the landing gear to ensure proper functionality.

  • Service letter SL No. L-410/008 issued on Jun 24, 2021.
  • Applies to L-410 UVP-E, E9, and E20 models.
  • Focuses on checking the sleeve on the nose landing gear leg.
  • Turning of the sleeve may prevent landing gear retraction.
  • Check the sleeve position using a red line indicator.
  • Ensure the nut on the sleeve is tightened to 6 to 7 Nm.
  • Contact AI a.s. if the sleeve has been rotated.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at let.cz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Service Bulletins
Year
·
2021
File size
·
132 KB
Copy found at
·
let.cz
Language
·
en
About this document
What is the SERVICE LETTER?

The SERVICE LETTER is a service bulletins for the LET L-410 UVP-E20, dated 2021.

What year was the SERVICE LETTER published?

The SERVICE LETTER — the LET L-410 UVP-E20 service bulletins on file — is dated 2021.

How rare is it?
267LET L-410 UVP-E20 registered worldwide · 265 active

Common. More common than 87% of the aircraft models we track.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the LET L-410 UVP-E20.

In this document

Service Letter Details

This section includes the service letter number, aircraft type, model applicability, and date of issue.

Reason for Service Letter

The letter addresses the need to check the sleeve on the nose landing gear leg.

Description of the Issue

Details the potential issue of the sleeve turning and its impact on landing gear retraction.

Maintenance Procedure

Outlines the steps to check the sleeve position and nut tightening.

Contact Information

Instructs to contact AI a.s. if the sleeve has been rotated.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Full document text

FQ050103E SERVICE LETTER SL No. L-410/008 Aeroplane Type: L-410 Model(s): L 410 UVP-E, E9, E20 Date of Issue: Jun 24, 2021 Reason: Check of a sleeve on the nose landing gear leg. Description: Turning of the sleeve may disable the LG from retracting. 1. Check via the red line that the sleeve has not been rotated – see Fig. 1. 2. Check correct tightening of the nut on the sleeve (6 to 7 Nm). If the sleeve has been rotated, contact AI a.s. Fig. 1 The sleeve on the nose landing gear leg