Commonwealth legislation

AD/CESSNA 210/73 - Upper Shoulder Harness Adjuster Spring

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires operators of specified Cessna 210 models (serial numbers listed in Cessna SB SEB86-8 Rev 1) to inspect the upper shoulder harness adjuster (part 443030-401) for a small retainer spring. If present, the spring must be cut off and the -401 identification stamped out before next flight; if absent, make a logbook entry. It also prohibits installing accessory kits unless they have been inspected and modified per the service bulletin. The stated aim is to prevent shoulder harness slippage.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/CESSNA 210/73 - Upper Shoulder Harness Adjuster Spring.

AD/CESSNA 210/73 - Upper Shoulder Harness Adjuster Spring

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

View image in the official source

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

View image in the official source

Cessna 210 Series Aeroplanes

AD/CESSNA 210/73 Upper Shoulder Harness Adjuster Spring

13/2004

Applicability: Models 210, 210-5, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K,

T210F, T210G, T210H, T210J, and T210K aircraft, with serial numbers listed in Cessna Single Engine Service Bulletin (SB) SEB86-8 Revision 1, dated 28 July 2003.

Requirement: 1. Inspect only the upper shoulder harness adjuster (part number 443030-401) for the presence of a retainer spring, in accordance with SB SEB86-8 Revision 1.

If a retainer spring is found during the above inspection of the upper shoulder harness adjuster (part number 443030-401), before further flight, remove the spring by cutting each side, and stamp out the -401 identification number; in accordance with SB SEB86-8 Revision 1.

If a retainer spring is not found during the above inspection of the upper shoulder harness adjuster (part number 443030-401), before further flight, make an entry in the aircraft log book showing compliance with this Directive.

2. Only incorporate Cessna Accessory Kits that have been identified, inspected, and modified in accordance with the Requirement document.

Note: FAA AD 2004-19-01 Amdt 39-13795 refers.

Compliance: 1. Within the next 25 hours time in service or at the next annual inspection after 23 December 2004, whichever occurs first.

2. As of the effective date of this Directive.

Note: Compliance with SB SEB86-8 original issue, dated 21 November 1986, constitutes terminating action for the requirements of this Directive, if shoulder harness adjuster part number 443030-401 was used.

This Airworthiness Directive becomes effective on 23 December 2004.

Cessna 210 Series Aeroplanes

AD/CESSNA 210/73 (continued)

Background: The manufacturer determined that some of the shoulder harness belt adjusters included in the affected shoulder harness accessory kits may have had a small wire spring inadvertently installed on the belt friction pin. The actions required by this Directive are intended to prevent slippage of the pilot/co-pilot shoulder harness, which could result in failure of the shoulder harness to maintain proper belt length adjustment and tension.

View image in the official source

David Villiers

Delegate of the Civil Aviation Safety Authority 12 November 2004

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 1 December 2004.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

AIRWORTHINESS DIRECTIVE

Cessna 210 Series Aeroplanes

AD/CESSNA 210/73 Upper Shoulder Harness Adjuster Spring

13/2004

Applicability: Models 210, 210-5, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K,

T210F, T210G, T210H, T210J, and T210K aircraft, with serial numbers listed in Cessna Single Engine Service Bulletin (SB) SEB86-8 Revision 1, dated 28 July 2003.

Requirement: 1. Inspect only the upper shoulder harness adjuster (part number 443030-401) for the presence of a retainer spring, in accordance with SB SEB86-8 Revision 1.

2. Only incorporate Cessna Accessory Kits that have been identified, inspected, and modified in accordance with the Requirement document.

Note: FAA AD 2004-19-01 Amdt 39-13795 refers.

Compliance: 1. Within the next 25 hours time in service or at the next annual inspection after 23 December 2004, whichever occurs first.