Commonwealth legislation

AD/IAI-A/5 - Windshield Wiper Arm

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD/IAI-A/5 requires operators of IAI Model 1125 (serials 004–029 except 020) to inspect windshield wipers following Israel Aircraft Industries Alert Service Bulletin 1125-30A-222. Deadlines differ by total flight hours as of 30 Aug 2000 (see Requirement; Compliance).

Aircraft operators pay for and carry out the inspections; the CASA delegate issued the directive; the inspections aim to detect rivet failure and prevent possible in‑flight separation of the wiper arm tip assembly (Background).

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/IAI-A/5 - Windshield Wiper Arm.

AIRWORTHINESS DIRECTIVE

View image in the official source

View image in the official source
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 CAR 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.

AD/IAI-A/5 Windshield Wiper Arm 10/2000

AD/IAI-A/5 Windshield Wiper Arm 10/2000 DM

Applicability: Model 1125, serial numbers 004 through 029, except serial number 020.

Requirement: Inspect the windshield wipers in accordance with Israel Aircraft Industries Alert Service Bulletin 1125-30A-222.

Note: Israel CAA AD 30-00-07-10 refers.

Compliance: Within 10 flight hours after 30 August 2000 for aircraft with more than 4,000 total flight hours on 30 August 2000.

Before 30 November 2000 for aircraft with less than 4,000 total flight hours on 30 August 2000.

This Airworthiness Directive becomes effective on 30 August 2000.

Background: A report was received of rivet failure on a windshield wiper arm. This Directive requires inspections to prevent possible in-flight separation of the wiper arm tip assembly.

Signature of Steve Swift

Steve Swift

Delegate of the Civil Aviation Safety Authority 24 August 2000

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 30 August 2000.

Source text

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

AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE

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 CAR 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.

AD/IAI-A/5 Windshield Wiper Arm 10/2000 AD/IAI-A/5 Windshield Wiper Arm 10/2000 DM

AD/IAI-A/5 Windshield Wiper Arm 10/2000 DM

Applicability: Model 1125, serial numbers 004 through 029, except serial number 020.

Requirement: Inspect the windshield wipers in accordance with Israel Aircraft Industries Alert Service Bulletin 1125-30A-222.

Note: Israel CAA AD 30-00-07-10 refers.

Compliance: Within 10 flight hours after 30 August 2000 for aircraft with more than 4,000 total flight hours on 30 August 2000.

Before 30 November 2000 for aircraft with less than 4,000 total flight hours on 30 August 2000.

This Airworthiness Directive becomes effective on 30 August 2000.

Background: A report was received of rivet failure on a windshield wiper arm. This Directive requires inspections to prevent possible in-flight separation of the wiper arm tip assembly.

Steve Swift

Delegate of the Civil Aviation Safety Authority 24 August 2000

The above AD is notified in the Commonwealth of Australia Gazette on 30 August 2000.