{"id":"F2008L03274","name":"AD/F2000/32 - Fuselage - LH Stringer 13 at Frame 8","slug":"ad-f2000-32-fuselage-lh-stringer-13-at-frame-8","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":120013,"registerId":"commonwealth-F2008L03274-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Dassault Aviation Falcon 2000 Series Aer","sectionType":"division","heading":"Dassault Aviation Falcon 2000 Series Aeroplanes","content":"### Dassault Aviation Falcon 2000 Series Aeroplanes\n\n| AD/F2000/32 | Fuselage - LH Stringer 13 at Frame 8 | 10/2008 |\n| ----------- | ------------------------------------ | ------- |\n\n| Applicability: | Falcon 2000EX aircraft from serial number 102 to 124 inclusive.                                                                                                                        |\n| -------------- | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n| Requirement:   | Action in accordance with EASA AD 2008-0143Note: Dassault Aviation Service Bulletin F2000EX-178 refers.                                                                                |\n| Compliance:    | Required as indicated unless previously accomplished,Before accumulation of 3 750 Total Flight Cycles or within 74 months since the date of airplane delivery, whichever occurs first. |\n|                | This Airworthiness Directive becomes effective on 25 September 2008.                                                                                                                   |\n| Background:    | This Airworthiness Directive mandates an inspection and a conditional rework or replacement of the web of the LH stringer 13 between frames 7 and 8.                                   |\n\n![](image.001.png)  \nDavid Villiers  \nDelegate of the Civil Aviation Safety Authority\n\n11 August 2008","sortOrder":0},{"sectionNumber":"AD/F2000/32","sectionType":"part","heading":"AD/F2000/32","content":"## AD/F2000/32","sortOrder":1},{"sectionNumber":"Fuselage - LH Stringer 13 at Frame 8","sectionType":"part","heading":"Fuselage - LH Stringer 13 at Frame 8","content":"## Fuselage - LH Stringer 13 at Frame 8","sortOrder":2},{"sectionNumber":"10/2008","sectionType":"part","heading":"10/2008","content":"## 10/2008","sortOrder":3}],"analysis":{"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":3,"scope_assessment":{"changed":false,"description":"The AD applies only to Falcon 2000EX serial numbers 102–124 and mandates inspection and conditional rework or replacement of LH stringer 13 between frames 7 and 8, implementing EASA AD 2008‑0143 and referencing Dassault Service Bulletin F2000EX‑178. The text contains no indication that the instrument broadened or narrowed that scope relative to the EASA directive; no scope change is evident in the AD itself."},"complexity_factors":["Narrow applicability to specific serial numbers (Applicability).","Technical inspection and conditional repair/replacement of a structural component (Background).","Cross-reference to an external EASA AD and manufacturer service bulletin creates dependency on external documents (Requirement).","Dual compliance deadline expressed in flight cycles or months increases tracking burden (Compliance).","Potential operational disruption and direct costs to aircraft operators for inspection and corrective work (Compliance/Background).","Regulatory implementation and effective date set by CASA delegate requires timely administrative action (effective date and signature block)."],"plain_english_summary":"Requires operators of Dassault Falcon 2000EX aircraft (serials 102–124) to inspect the left‑hand fuselage stringer 13 between frames 7 and 8, and to rework or replace the web if defects are found, following EASA AD 2008‑0143 and Dassault Service Bulletin F2000EX‑178. Compliance is mandatory before 3,750 total flight cycles or within 74 months of delivery, whichever is earlier; the operator bears inspection, repair and downtime costs to address the structural risk identified by the regulator."},"kimi_summary":{"content_quality":"ok","complexity_score":2,"scope_assessment":{"changed":false,"description":"This is a standard, narrow airworthiness directive targeting a specific structural defect in a specific aircraft model range. It has not expanded beyond its original safety purpose."},"complexity_factors":["Very short document (under 300 words)","Only one defined applicability criterion (serial number range)","Single compliance trigger with simple 'whichever occurs first' logic","No nested exceptions or conditional sub-clauses","Cross-reference to only one external document (EASA AD 2008-0143)","Straightforward mechanical/technical requirement (inspect, then repair if needed)"],"plain_english_summary":"This CASA Airworthiness Directive mandates inspection of the left-hand stringer 13 near frame 8 on certain Dassault Falcon 2000EX jets (serials 102–124). Operators of these 23 aircraft must inspect and, if defects are found, repair or replace the part to address a potential structural weakness. Compliance is required before 3,750 flight cycles or within 74 months of delivery; effective 25 Sep 2008."}},"importantCases":[],"_links":{"self":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8","history":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8/history","analysis":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8/analysis","conflicts":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8/conflicts","importantCases":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8/important-cases","documents":"/api/acts/ad-f2000-32-fuselage-lh-stringer-13-at-frame-8/documents"}}