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SERVICE BULLETIN - Vashon Aircraft

Vashon Aircraft Ranger R7 · Service Bulletins

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Overview

This service bulletin addresses the issue of fatigue cracks found on the nose gear leg weld of the Vashon Aircraft Ranger R7. It outlines the necessary inspection procedures and compliance requirements to ensure safety.

  • Subject: Nose Gear Leg Weld Cracks
  • Effective for all Ranger R7 aircraft with serial numbers 10131-10171
  • Cracks may lead to failure of the nose landing leg if not addressed
  • Immediate inspection required, followed by 25-hour interval checks
  • Paint chipping may indicate metal fatigue cracks
  • Contact Vashon Aircraft Support for corrective action if cracks are found
  • No labor required for the inspection
  • Minimum certification level for inspection is Owner/Pilot

Document

Source

Originally published by vashonaircraft.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Service Bulletins
Year
·
2023
File size
·
240 KB
Publisher
·
vashonaircraft.com
Language
·
en
About this document
What is the SERVICE BULLETIN - Vashon Aircraft?

The SERVICE BULLETIN - Vashon Aircraft is a service bulletins for the Vashon Aircraft Ranger R7, dated 2023.

Where does the SERVICE BULLETIN - Vashon Aircraft come from?

This copy of the SERVICE BULLETIN - Vashon Aircraft was originally published by vashonaircraft.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the SERVICE BULLETIN - Vashon Aircraft published?

The SERVICE BULLETIN - Vashon Aircraft — the Vashon Aircraft Ranger R7 service bulletins on file — is dated 2023.

Documentation completeness
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In this document

Reason

Fatigue cracks have been identified on the welded connection of the nose gear landing leg due to insufficient weld penetration.

Required Action

Inspect the nose gear weld seam immediately and at specified intervals.

Time of Compliance

Inspect immediately, then every 25 hours until the 100-hour inspection.

Method of Compliance

Inspect the landing leg as shown in provided figures; look for signs of cracks.

Labor Required

None at this time.

Contact Information

For support, contact Vashon Aircraft at support@vashonaircraft.com or call (425) 527-9944.

Safety notes

  • Fatigue cracks can lead to failure of the nose landing leg.
  • Inspect immediately to prevent potential failure.
  • Chipping of paint is a strong indication of a crack.

Full document text

Light Sport Aircraft SERVICE BULLETIN VASHON AIRCRAFT 14929 141st PL NE Woodinville, WA 98072 425.527.9944 SB-06-13-23-1 REV A SUPPORT@VASHONAIRCRAFT.COM Page 1 of 3 SB-06-13-23-1 Rev A DATE RELEASED 06-13-23 DATE EFFECTIVE 06-13-23 SUBJECT Nose Gear Leg Weld Cracks EFFECTIVITY MODEL- Ranger R7 SERIAL NO: ALL AIRCRAFT IN THE RANGE OF: 10131-10171 REASON Fatigue cracks have been identified on the welded connection of the nose gear landing leg. This is due to insufficient weld penetration between the steel tubes. If the crack is left to propagate this could lead to a failure of the nose landing leg. REQUIRED ACTION Inspect the nose gear weld seam. TYPE OF MAINTENANCE Low. MINIMUM LEVEL OF CERTIFICATION Owner / Pilot. TIME OF COMPLIANCE Inspect immediately. After that, inspect in 25hr intervals until 100hr inspection. After this, the inspection interval can default to each annual inspection. METHOD OF COMPLIANCE Inspect the landing leg as shown in Figure 1. An example of what a crack could look like is shown in Figure 2. “Chipping” of the paint is a strong indication of a metal fatigue crack. If any cracks are present, contact Vashon Aircraft Support for corrective action: support@vashonaircraft.com (425) 527-9944 LABOR REQUIRED: None at this time. Light Sport Aircraft SERVICE BULLETIN VASHON AIRCRAFT 14929 141st PL NE Woodinville, WA 98072 425.527.9944 SB-06-13-23-1 REV A SUPPORT@VASHONAIRCRAFT.COM Page 2 of 3 Figure 1 Light Sport Aircraft SERVICE BULLETIN VASHON AIRCRAFT 14929 141st PL NE Woodinville, WA 98072 425.527.9944 SB-06-13-23-1 REV A SUPPORT@VASHONAIRCRAFT.COM Page 3 of 3 Figure 2