{"id":"F2006B06928","name":"AD/SEATS/22 - Sicma Aero Seat Passenger Seats","slug":"ad-seats-22-sicma-aero-seat-passenger-seats","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":114812,"registerId":"commonwealth-F2006B06928-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"AIRWORTHINESS DIRECTIVE","sectionType":"part","heading":"AIRWORTHINESS DIRECTIVE","content":"# ![](image.001.png)  \nAIRWORTHINESS DIRECTIVE\n\nFor 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.\n\n![](image.001.png)\n\nSeats and Berths","sortOrder":0},{"sectionNumber":"AD/SEATS/22 Sicma Aero Seat Passenger Se","sectionType":"part","heading":"AD/SEATS/22 Sicma Aero Seat Passenger Seats 12/2002","content":"# AD/SEATS/22 Sicma Aero Seat Passenger Seats 12/2002\n\nDM\n\nApplicability: Sicma Aero Seat 9801 and 9802 Series passenger seats listed in Paragraph A of Sicma Aero Seat Service Bulletin (SB) 98-25-014 Issue 1 dated 1 October 2001.\n\nNote 1: These seats are known to be installed on, but not limited to, Airbus Industrie A330 and A340 series aeroplanes.\n\nRequirement: 1. Perform a visual inspection of electrical wires in the vicinity of the swivel part of the foldable central armrest of the affected seats on which Sicma Aero Seat SB 98-25-008 dated 4 February 2000, or SB 98-25-009 dated 22 February 2000, or SB 98-25-014 Issue 1 has not been embodied.\n\n    2. If any damaged electrical wire is found during the Requirement 1 inspection, either replace the wire or deactivate the seat ‘in flight entertainment’ (IFE) system.\n\n    3. Accomplish the following:\n\n    For seats without SB 98-25-009 embodied \\- Incorporate Part 1 of SB 98- 25-014 Issue 1.\n    For seats with SB 98-25-009 embodied \\- Incorporate Part 2 of SB 98-25- 014 Issue 1.\n\n    4. Record, on the seat modification record placard, the incorporation of SB 98-25- 14 Issue 1 by following the instructions at Paragraph C of “Accomplishment Instructions” of the SB.\n\nNote 2: DGAC AD 2002-505(AB) refers.\n\nCompliance: For Requirement 1 \\- Within seven days after the effective date of this Directive and thereafter at intervals of seven days.\n\nIncorporation of either SB 98-25-008, or SB 98-25-009, or SB 98-25-014 Issue 1 is terminating action for the repetitive inspections.\n\nFor Requirement 2 \\- Before further flight after the Requirement 1 inspection.","sortOrder":1}],"analysis":{"flash_summary":{"complexity_score":3,"scope_assessment":{"changed":false,"description":"Scope remains focused on the identified Sicma 9801/9802 seats and prescribes inspections, immediate corrective action (wire replacement or IFE deactivation), incorporation of specified SB parts as terminating action, and placard recording (Requirements 1–4; Compliance). It does not expand applicability beyond seats listed in the SB; compliance costs (inspections, repairs, or IFE deactivation) fall to operators and their maintenance organisations (Requirement 1–3; Compliance)."},"complexity_factors":["Targeted, narrow applicability limited to Sicma Aero Seat 9801/9802 listed in Paragraph A of SB 98-25-014 (Applicability).","Multiple referenced service bulletins with conditional actions (SB 98-25-008, SB 98-25-009, SB 98-25-014 Issue 1) requiring different parts to be incorporated depending on prior embodiment (Requirement 3).","Short, repetitive inspection interval until terminating action (visual inspections every 7 days) creating ongoing operational/maintenance burden (Compliance for Requirement 1).","Branching corrective options after inspection: replace damaged wire or deactivate IFE system before further flight (Requirement 2; Compliance for Requirement 2).","Recordkeeping obligation to update seat modification placard following manufacturer instructions (Requirement 4; Paragraph C of Accomplishment Instructions).","Cross-reference to a foreign airworthiness directive (DGAC AD 2002-505(AB)) adds an external regulatory linkage (Note 2).","Regulatory enforcement basis under CAR 1998 subregulation 39.1(1) establishes legal force (preamble)."],"plain_english_summary":"Mandates that operators of aircraft fitted with Sicma Aero Seat 9801/9802 passenger seats visually inspect electrical wiring near the swivel of the central foldable armrest every seven days until the required Sicma service bulletin is embodied; damaged wires must be replaced or the in‑flight entertainment (IFE) system deactivated before the next flight. Installing the appropriate parts of Sicma SB 98‑25‑014 is terminating action and must be recorded on the seat modification placard. Affects airlines, maintenance providers and seat owners."},"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"},"kimi_summary":{"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"This AD maintains its original narrow scope — addressing a specific wiring defect in specific seat models. The reference to multiple Service Bulletins reflects the evolution of the manufacturer's fix, not scope creep in the regulatory instrument itself."},"complexity_factors":["Multiple cross-referenced Service Bulletins (SB 98-25-008, SB 98-25-009, SB 98-25-014) that operators must consult to determine which modification path applies","Conditional logic based on prior modification status (whether SB 98-25-009 has been 'embodied' or not)","Dual compliance timelines (7-day repetitive inspections vs before-next-flight immediate action)","Specific technical terminology requiring aviation maintenance knowledge ('embodied', 'terminating action', 'modification record placard')","External reference to French aviation authority directive (DGAC AD 2002-505(AB)) for additional context"],"plain_english_summary":"This AD requires operators of Airbus A330/A340 aircraft fitted with Sicma Aero Seat 9801/9802 series to inspect wiring at foldable armrests every 7 days, immediately repair or disable any damaged wiring before flight, and install the manufacturer’s modification (Service Bulletin 98‑25‑014) as a permanent fix, with the repair recorded on a seat placard. It addresses wire chafing that could cause electrical faults or fire, so it’s urgent for safety."}},"importantCases":[],"_links":{"self":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats","history":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats/history","analysis":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats/analysis","conflicts":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats/conflicts","importantCases":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats/important-cases","documents":"/api/acts/ad-seats-22-sicma-aero-seat-passenger-seats/documents"}}