{"id":"F2006L01030","name":"AD/CONVAIR/21 - FAA Non-Repetitive ADs","slug":"ad-convair-21-faa-non-repetitive-ads","collection":"legislative_instrument","jurisdiction":"commonwealth","status":"in_force","isInForce":true,"actNumber":null,"makingDate":null,"administeringDepartment":null,"currentVersion":{"id":58309,"registerId":"commonwealth-F2006L01030-current","compilationNumber":null,"startDate":"2026-04-02","status":"InForce","reasons":null,"registeredAt":null},"sections":[{"sectionNumber":"Kelowna Flightcraft (General Dynamics/Co","sectionType":"division","heading":"Kelowna Flightcraft (General Dynamics/Convair) Series Aeroplanes","content":"### Kelowna Flightcraft (General Dynamics/Convair) Series Aeroplanes\n\n| AD/CONVAIR/21 | FAA Non-Repetitive ADs | 5/2006 |\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=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>General Dynamics (CONVAIR) Model 240, 340 and 440 series aeroplanes.</span></p></td></tr><tr><td rowspan=\"19\" style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Requirement:</span></p></td><td colspan=\"3\" style=\"width:414.55pt; border-bottom:0.75pt solid #000000; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p style=\"margin-left:21.3pt; margin-bottom:12pt; text-indent:-21.3pt\"><span>1.</span><span style=\"width:12.3pt; text-indent:0pt; display:inline-block\"> </span><span>Determine the applicability of the AD’s listed in Table 1 of this AD.</span></p><p style=\"margin-top:12pt; margin-left:21.25pt; text-indent:-21.25pt\"><span>2.</span><span style=\"width:12.25pt; text-indent:0pt; display:inline-block\"> </span><span>If it is determined that an applicable AD has not been accomplished, perform the actions required by the AD.</span></p><p class=\"Note\" style=\"text-align:center\"><span style=\"font-weight:bold; font-style:normal\">Table 1</span></p></td></tr><tr><td style=\"width:93.9pt; 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\">FAA AD Number</span></p></td><td style=\"width:102.7pt; 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\">Effective Date</span></p></td><td style=\"width:196.55pt; 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\">Title</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>56-20-04</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Fire Seals</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>56-24-01</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Cylinder</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>56-24-02</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Carburettors</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>56-27-01</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Elevator Servo Tab Rod</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>58-01-03</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Carburettor Setting</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>59-01-01</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Fire Detector System</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>59-04-02</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Pilot's Direct-Vision Window</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>60-14-01</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>Upon Receipt</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Main Landing Gear</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>63-06-03</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>20 March 1963</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Electrical Fault Detection Panel</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><span>70-10-03</span></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>12 May 1970</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Engine Breather Oil Fumes</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/407BAAA98D38ADBF862569B5006ECBCA?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">78-17-0</span><span style=\"color:#000000\">4</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>5 September 1978</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Emergency Window Release Handle</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/748EB10B9C6A7516862569B5006ED97F?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">78-22-04</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>1 November 1978</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Emergency Exit Window</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/D4170D79E9B85BF486256A2A00541970?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">90-13-13</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>30 July 1990</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Fuselage Frames</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/C9DAF8DFB65E762B86256A2A00543B83?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">91-12-05</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>25 July 1991</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Elevator Hinge Pins</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/B9B5B75441ABB44B86256A2A0054D5CD?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">93-04-03</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>19 April 1993</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Horizontal And Vertical Stabilizers</span></p></td></tr><tr style=\"height:36.85pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/4DBF48CC34AFE46C86256A2A00552391?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">96-03-04</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>28 February 1996</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Aircraft Flight Manual - Limitation, Icing Conditions</span></p></td></tr><tr style=\"height:22.7pt\"><td style=\"width:93.9pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"text-align:center\"><a href=\"http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/5F753C1A4D7781AF86256A2A0055B503?OpenDocument\" target=\"_blank\" style=\"text-decoration:none\"><span style=\"color:#000000\">98-08-17</span></a></p></td><td style=\"width:102.7pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:1.75pt; text-align:center\"><span>19 May 1998</span></p></td><td style=\"width:196.55pt; border:0.75pt solid #000000; padding-right:4.97pt; padding-left:4.97pt; vertical-align:top\"><p style=\"margin-left:8.8pt\"><span>Aircraft Flight Manual - Power Levers</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p class=\"Note\"><span></span></p></td><td colspan=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p class=\"Note\"><span>Note:</span><span> </span><span>Prior to 1963 FAA AD’s did not have effective dates.</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=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Within 30 days after the effective date of this AD.</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=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>This Airworthiness Directive becomes effective on 11 May 2006.</span></p></td></tr><tr><td style=\"width:74.35pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>Background:</span></p></td><td colspan=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>The AD’s listed in Table 1 of this AD have been evaluated and found to require one-time inspections or modifications as at the effective date of this AD.</span><span> </span><span>In addition the compliance period for these AD’s has passed.</span><span> </span><span>With the introduction of the aeroplane onto the Australian register, the intention of this AD is to ensure compliance with the AD’s listed in Table 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=\"3\" style=\"width:414.55pt; padding-right:5.35pt; padding-left:5.35pt; vertical-align:top\"><p><span>CASA appreciates that not all AD’s listed in Table 1 of this AD may be applicable, due to the incorporation of STC’s or other modifications.</span></p></td></tr></tbody></table>\n```\n\n![](image.001.png)  \nJames Coyne  \nDelegate of the Civil Aviation Safety Authority\n\n31 March 2006","sortOrder":0},{"sectionNumber":"AD/CONVAIR/21","sectionType":"part","heading":"AD/CONVAIR/21","content":"## AD/CONVAIR/21","sortOrder":1},{"sectionNumber":"FAA Non-Repetitive ADs","sectionType":"part","heading":"FAA Non-Repetitive ADs","content":"## FAA Non-Repetitive ADs","sortOrder":2},{"sectionNumber":"5/2006","sectionType":"part","heading":"5/2006","content":"## 5/2006","sortOrder":3}],"analysis":{"flash_summary_failed":{"failed":true,"reason":"Unauthenticated. Configure AI_GATEWAY_API_KEY or use a provider module. Learn more: https://ai-sdk.dev/unauthenticated-ai-gateway","source":"analysis-cron"},"flash_summary":{"complexity_score":4,"scope_assessment":{"changed":false,"description":"The AD's scope matches its stated intent in the Background: ensure listed FAA non-repetitive ADs are complied with when the specified Convair models are entered on the Australian register. It requires determination of applicability and completion of outstanding one-time actions; it does not expand obligations beyond those listed FAA ADs or create ongoing repetitive mandates (Background; Requirement; Table 1)."},"complexity_factors":["Cross-referencing numerous FAA ADs across varied systems and vintages (see Table 1).","Determining applicability requires review of maintenance records, STCs and prior modifications (Requirement 1; Background).","One-time inspections/modifications cover diverse technical disciplines (fire seals, landing gear, structural frames, controls, etc.), increasing coordination and specialist requirements (Table 1).","Short compliance window: within 30 days of the AD effective date (Compliance).","Historical ambiguity for pre-1963 FAA ADs that lacked effective dates (Note).","Responsibility and cost borne by the operator/owner to arrange and perform any outstanding AD work (Requirement 2)."],"plain_english_summary":"This Airworthiness Directive requires operators of General Dynamics (Convair) Model 240/340/440 aeroplanes introduced to the Australian register to check the FAA ADs listed in Table 1 and, where a listed AD has not been accomplished, carry out the one‑time inspections or modifications those FAA ADs require. Compliance must be completed within 30 days of this AD becoming effective (11 May 2006).\n\nOperators/owners pay for and arrange the work. CASA requires this measure to ensure legacy FAA non‑repetitive ADs are met on Australian‑registered examples; applicability may be affected by STCs or other modifications."},"kimi_summary":{"content_quality":"ok","complexity_score":3,"scope_assessment":{"changed":false,"description":"The directive maintains its original narrow purpose: ensuring baseline airworthiness compliance for newly registered Convair aircraft by consolidating specific historical FAA ADs. The scope has not expanded beyond this targeted safety catch-up function."},"complexity_factors":["Simple two-step compliance structure: (1) determine applicability, (2) perform required actions","Single defined applicability class (Convair 240/340/440 series)","No nested conditional logic or exceptions within the main requirements","One explicit carve-out noted in background (STC modifications may render some ADs inapplicable)","Relies entirely on external references to 17 separate FAA ADs without reproducing their technical content","Straightforward 30-day compliance deadline with no phased or variable timelines","Minimal legislative cross-referencing — operates under standard CASA AD issuance powers"],"plain_english_summary":"Owners and operators of General Dynamics/Convair Model 240, 340 and 440 aircraft on the Australian register must, within 30 days of the 11 May 2006 effective date, verify whether 17 older US FAA safety directives have been complied with and carry out any missed corrective actions. The AD bundles those legacy fixes to bring imported/introduced aircraft up to baseline safety; some items may not apply where Supplemental Type Certificates alter the aircraft."}},"importantCases":[],"_links":{"self":"/api/acts/ad-convair-21-faa-non-repetitive-ads","history":"/api/acts/ad-convair-21-faa-non-repetitive-ads/history","analysis":"/api/acts/ad-convair-21-faa-non-repetitive-ads/analysis","conflicts":"/api/acts/ad-convair-21-faa-non-repetitive-ads/conflicts","importantCases":"/api/acts/ad-convair-21-faa-non-repetitive-ads/important-cases","documents":"/api/acts/ad-convair-21-faa-non-repetitive-ads/documents"}}