{"id":"F2008L03404","name":"AD/BEECH 33/47 - Circuit Breaker Toggle Switches","slug":"ad-beech-33-47-circuit-breaker-toggle-switches","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":120404,"registerId":"commonwealth-F2008L03404-current","compilationNumber":null,"startDate":"2026-04-03","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Beechcraft 33 and 35-33 (Debonair/Bonanz","sectionType":"division","heading":"Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes","content":"### Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes\n\n| AD/BEECH 33/47 | Circuit Breaker Toggle Switches | 10/2008 |\n| -------------- | ------------------------------- | ------- |\n\n```html\n<table cellspacing=\"0\" cellpadding=\"0\" style=\"width:510.3pt; margin-top:0pt; margin-bottom:0pt; border-collapse:collapse\"><tbody><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Applicability:</span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Aeroplane models and serial numbers listed in Table 1 that have any circuit breaker toggle switch with a part number (P/N) 35-380132-1 through 35-380132-53 installed.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p style=\"text-align:center\"><span style=\"font-weight:bold\">Table 1</span></p></td></tr><tr style=\"height:13.05pt\"><td rowspan=\"2\" style=\"width:74.35pt; border-right:0.75pt solid #000000; padding-right:4.97pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td style=\"width:201.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span style=\"font-weight:bold\">Model</span></p></td><td style=\"width:201.95pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span style=\"font-weight:bold\">Serial</span><span style=\"font-weight:bold\"> </span><span style=\"font-weight:bold\">Number</span><span style=\"font-weight:bold\"> </span><span style=\"font-weight:bold\">Range</span></p></td></tr><tr style=\"height:13.05pt\"><td style=\"width:201.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:72pt; text-indent:-72pt\"><span style=\"width:72pt; text-indent:0pt; display:inline-block\"></span><span>F33 and G33</span><br><span>F33A</span><br><span>F33C</span></p></td><td style=\"width:201.95pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:36pt; text-indent:-36pt\"><span style=\"width:36pt; text-indent:0pt; display:inline-block\"></span><span>CD-1235 through CD-1304</span><br><span>CE-290 through CE-1791</span><br><span>CJ-26 through CJ-179</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Requirement:</span></p></td><td colspan=\"2\" style=\"width:414.55pt; border-top:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p style=\"margin-left:21.3pt; text-indent:-21.3pt\"><span>1.</span><span style=\"width:12.3pt; text-indent:0pt; display:inline-block\"> </span><span>Unless previously accomplished, replace all circuit breaker toggle switches P/N 35-380132-1 through 35-380132-53 with an improved circuit breaker toggle switch, P/N 35-380132-61 through 35-380132-113, as applicable, as specified in Raytheon Aircraft Company (RAC) Recommended Service Bulletin SB 24-3735, Issued: August 2005.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p style=\"margin-left:21.3pt; text-indent:-21.3pt\"><span>2.</span><span style=\"width:12.3pt; text-indent:0pt; display:inline-block\"> </span><span>Circuit breaker toggle switches P/N 35-380132-1 through 35-380132-53 may not be installed on any aeroplane as an initial fit or as a replacement spare.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Later revisions of the above SB, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2008-13-17, are considered acceptable for compliance with the equivalent Requirements of this Directive.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p class=\"Note\"><span>Note:</span><span> </span><span>FAA AD 2008-13-17 Amdt 39-15580 refers.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Compliance:</span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>For Requirement 1 - Within the next 24 months after the effective date of this Directive.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>For Requirement 2 - Before further flight after the circuit breaker toggle switch has been replaced in accordance with Requirement 1.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span></span></p></td><td colspan=\"2\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>This Airworthiness Directive becomes effective on 25 September 2008.</span></p></td></tr></tbody></table>\n```\n\n| Background: | The FAA has received reports of certain circuit breaker toggle switches used in various electrical systems throughout Beech F33, F33A, F33C, G33, V35B, A36, A36TC, B36TC, 95-B55, D55, E55, A56TC, 58, 58P, 58TC, G58 and 77 model aeroplanes overheating. Failure of the circuit breaker toggle switch could result in smoke in the cockpit and the inability to turn off the switch.                                                                     |\n| ----------- | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |\n|             | This Directive follows the intent of the FAA Directive, requiring the replacement of circuit breaker toggle switches with a P/N 35-380132-1 through 35-380132-53. However, it is revised to allow prior accomplishment, as the RAC service bulletin was issued in 2005 and may have already been accomplished. The Directive also extends compliance by 13 months until 25 September 2010, the final compliance time required by the FAA was 6 August 2009. |\n|             | A draft version of this Directive was posted for public comment on the Civil Aviation Safety Authority (CASA) internet site on 9 July 2008. As of the date that this Directive was made, no comments or objections have been received by CASA.                                                                                                                                                                                                              |\n\n![](image.001.png)\n\nJames Coyne  \nDelegate of the Civil Aviation Safety Authority\n\n8 August 2008","sortOrder":0},{"sectionNumber":"AD/BEECH 33/47","sectionType":"part","heading":"AD/BEECH 33/47","content":"## AD/BEECH 33/47","sortOrder":1},{"sectionNumber":"Circuit Breaker Toggle Switches","sectionType":"part","heading":"Circuit Breaker Toggle Switches","content":"## Circuit Breaker Toggle Switches","sortOrder":2},{"sectionNumber":"10/2008","sectionType":"part","heading":"10/2008","content":"## 10/2008","sortOrder":3}],"analysis":{"kimi_summary":{"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"This Airworthiness Directive maintains its original scope focused on circuit breaker replacement for specific Beechcraft models. The directive explicitly follows the intent of the corresponding FAA directive while incorporating minor adjustments (extended compliance timeframe and recognition of prior accomplishment) that remain within the original safety purpose."},"complexity_factors":["Single, clearly defined applicability table with specific model and serial number ranges","Two straightforward requirements with clear compliance deadlines","Cross-reference to US FAA Airworthiness Directive (AD 2008-13-17) and manufacturer service bulletin (RAC SB 24-3735)","Limited conditional logic — only two main requirements with simple timing conditions","No nested exceptions or complex defined terms; technical language limited to specific part numbers"],"plain_english_summary":"This AD mandates owners/operators of certain Beechcraft Debonair and Bonanza (F33/G33/F33A/F33C) aircraft to replace specified overheating circuit breaker toggle switches with improved versions within 24 months, and prohibits reinstalling the old parts. It affects aircraft listed in Table 1 only if they still have the old switches and applies to maintenance organisations.\n\nThe action prevents cockpit smoke and loss of ability to switch off affected electrical systems; prior replacements done per the manufacturer's 2005 service bulletin are accepted."},"flash_summary":{"complexity_score":4,"scope_assessment":{"changed":true,"description":"This Directive follows the FAA's intent but was revised to allow prior accomplishment of the Raytheon SB (SB 24-3735, Issued Aug 2005) and to extend the compliance window. The AD extends the FAA's final compliance time by 13 months (this Directive became effective 25 Sep 2008 and extends compliance to 25 Sep 2010, whereas the FAA's final compliance time was 6 Aug 2009) (Background; Compliance)."},"complexity_factors":["Applicability tied to specific models and serial-number ranges in Table 1 (tracking required to determine whether an aeroplane is in scope).","Replacement mandated by part-number ranges (old P/Ns 35-380132-1–53 replaced by new P/Ns 35-380132-61–113) — maintenance parts-control burden (Requirement 1).","Absolute prohibition on installing old P/Ns as initial fit or replacement spare increases spare-parts inventory and procurement constraints (Requirement 2).","Compliance deadline mechanics: 'Within the next 24 months after the effective date' for Requirement 1, and 'before further flight' for subsequent flights after replacement — scheduling and operational planning impact (Compliance section).","Normative reference to external material: Raytheon Aircraft Company Recommended Service Bulletin SB 24-3735 (Aug 2005) is the specified method of work, and later FAA‑approved AMOCs are acceptable — reliance on manufacturer/FAA documents adds cross-jurisdictional dependency.","Cross-reference to FAA AD 2008-13-17 and acceptance of later SB revisions as AMOC creates regulatory linkage that may require monitoring for amendments.","Record-keeping and proof of 'prior accomplishment' (allowed by this Directive) will be necessary to demonstrate compliance at audit or inspection (Background and Requirement text)."],"plain_english_summary":"This directive requires owners/operators of the listed Beechcraft F33/F33A/F33C/G33 aeroplanes (serials in Table 1) that have circuit breaker toggle switches P/N 35-380132-1 through -53 to replace them with improved switches P/N 35-380132-61 through -113 per Raytheon SB 24-3735. It also prohibits installing the older P/Ns as new or replacement spares. The measure targets overheating switches that can cause cockpit smoke and loss of switch control."},"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"}},"importantCases":[],"_links":{"self":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches","history":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches/history","analysis":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches/analysis","conflicts":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches/conflicts","importantCases":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches/important-cases","documents":"/api/acts/ad-beech-33-47-circuit-breaker-toggle-switches/documents"}}