{"id":"F2007L04082","name":"AD/PREMIER/1 - State of Design Airworthiness Directives","slug":"ad-premier-1-state-of-design-airworthiness-directives","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":160905,"registerId":"commonwealth-F2007L04082-current","compilationNumber":null,"startDate":"2026-04-04","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Hawker Beechcraft (Raytheon) 390 Series ","sectionType":"division","heading":"Hawker Beechcraft (Raytheon) 390 Series Aeroplanes","content":"### Hawker Beechcraft (Raytheon) 390 Series Aeroplanes\n\n| AD/PREMIER/1 | State of Design Airworthiness Directives | 12/2007 DM |\n| ------------ | ---------------------------------------- | ---------- |\n\n```html\n

Applicability:

Model 390 Premier 1 aeroplanes, as identified in the individual Airworthiness Directive (AD) listed in Table 1.

Note 1: The United States Federal Aviation Administration (FAA) Type Certificate for these aeroplanes was previously held by the Raytheon Aircraft Company.

Requirement:

1. Determine the applicability of the ADs issued by the FAA, listed in Table 1.

2. If it is determined that an FAA AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD.

Table 1

FAA AD

Effective Date

Title

2002-19-04

4 October 2002

Inboard Fuel Probe Mounting Brackets

2003-09-10

13 May 2003

Aft Power Distribution Box

2004-15-01

23 August 2004

Hydraulic System Assemblies

2004-25-15

18 January 2005

Main Landing Gear Squat Switch Wiring

2005-18-22

14 November 2005

Left-hand and Right-hand Engine Assembly Cable

2005-19-07

31 October 2005

Rudder Pedal Arm Assemblies

2005-25-07

23 January 2006

Air Conditioning Motor Module

2006-18-16

13 October 2006

Wing Spigot Bearing Retainer Kit

Note 2: FAA ADs may be accessed via the internet at the following URL:

http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/MainFrame?OpenFrameSet

\n```\n\n| Compliance: | For Requirements 1 and 2 - Within 30 days after the effective date of this Directive or prior to the issue of a Certificate of Airworthiness, whichever occurs first. |\n| ----------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n| | This Airworthiness Directive becomes effective on 17 October 2007. |\n| Background: | The FAA ADs listed in Table 1 of this Directive require either one time actions for which the compliance date and/or period has passed or multiple inspection/actions until a terminating action has been applied and the compliance date and/or period for the terminating action has passed. CASA has determined that these ADs may be applicable to recently registered or imported Australian aircraft. This Directive is issued to ensure all State of Design ADs are complied with. |\n| | CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, not all the ADs listed in Table 1 will be applicable to all Model 390 aeroplanes. |\n\n![](image.001.png) \nDavid Punshon \nDelegate of the Civil Aviation Safety Authority\n\n10 October 2007","sortOrder":0},{"sectionNumber":"AD/PREMIER/1","sectionType":"part","heading":"AD/PREMIER/1","content":"## AD/PREMIER/1","sortOrder":1},{"sectionNumber":"State of Design Airworthiness Directives","sectionType":"part","heading":"State of Design Airworthiness Directives","content":"## State of Design Airworthiness Directives","sortOrder":2},{"sectionNumber":"12/2007 DM","sectionType":"part","heading":"12/2007 DM","content":"## 12/2007 DM","sortOrder":3}],"analysis":{"kimi_summary":{"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"This is a standard State of Design Airworthiness Directive, which is a well-established category of CASA instrument. Its purpose is to adopt foreign (FAA) safety requirements for Australian-registered aircraft, which is exactly what it does. There is no scope creep beyond the original intent of ensuring compliance with foreign design authority directives."},"complexity_factors":["Short, single-purpose directive with only 2 substantive requirements","No defined terms section - relies on external FAA AD references","Simple conditional logic (if applicable and not done, then do it)","Single table with 7 external references to foreign legislation","No nested exceptions or complex cross-referencing within the instrument itself","Straightforward compliance deadline structure"],"plain_english_summary":"This is an Australian aviation safety rule that applies to specific business jets called Hawker Beechcraft (Raytheon) 390 Premier 1 aeroplanes. It requires Australian aircraft owners and operators to check whether certain safety fixes issued by the American aviation authority (the FAA) apply to their aircraft, and if so, to carry out those fixes. The rule covers seven specific safety issues including fuel probe brackets, power distribution boxes, hydraulic systems, landing gear wiring, engine cables, rudder pedals, and air conditioning motors. Owners must comply within 30 days of the rule taking effect or before getting an airworthiness certificate, whichever comes first. This ensures Australian-registered planes meet the same safety standards as those in the United States."},"flash_summary_failed":{"failed":true,"reason":"A positive credit balance is required for all requests, including BYOK, so fallback providers remain available. Add credits at https://vercel.com/d?to=%2F%5Bteam%5D%2F%7E%2Fai%3Fmodal%3Dtop-up to continue.","source":"analysis-cron"},"flash_summary":{"complexity_score":5,"scope_assessment":{"changed":false,"description":"The Directive maintains the original scope of requiring Model 390 Premier 1 aeroplane operators to determine applicability of specified State of Design (FAA) ADs and to perform those AD actions if applicable (see Requirement 1–2; Table 1). It is targeted at recently registered or imported Australian aircraft (Background) and sets the compliance timing (30 days or before Certificate of Airworthiness). The instrument does not widen obligations beyond determining applicability and enforcing the listed ADs."},"complexity_factors":["Cross-reference to multiple external FAA ADs listed in Table 1 (each with its own effective date and technical requirements).","Different AD types in Table 1: one‑time actions, recurring inspections/actions, and terminating actions (varying compliance logic).","Requirement to determine applicability for each individual aircraft based on manufacture date, configuration and modification status (administrative and technical assessment).","Short compliance window: within 30 days or before issue of a Certificate of Airworthiness (time pressure on operators/maintainers).","Dependence on access to and interpretation of FAA AD texts (URL provided) to identify required actions.","Potential costs and operational disruption for owners/operators who must perform inspections/repairs and maintain compliance records."],"plain_english_summary":"Requires owners/operators of Model 390 Premier 1 aeroplanes to check whether specific FAA airworthiness directives (listed in Table 1) apply and, if they do and have not been done before, to carry out the required inspections or fixes. Applies mainly to recently registered or imported Australian aircraft; compliance must occur within 30 days of this Directive or before issuing a Certificate of Airworthiness. CASA states the purpose is to ensure State of Design ADs are complied with for these aircraft."}},"importantCases":[],"_links":{"self":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives","history":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives/history","analysis":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives/analysis","conflicts":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives/conflicts","importantCases":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives/important-cases","documents":"/api/acts/ad-premier-1-state-of-design-airworthiness-directives/documents"}}