Back to AD

AD 62-08-05 ACTIVE

Electrical System
Key Information
AD Number 62-08-05 Status Active
Effective Date Not specified Issue Date Not specified
Docket Number Unknown Amendment N/A
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 707-100 Long Body 707-100B Long Body 707-100B Short Body 707-200 707-300 Series 707-300B Series 707-300C Series 707-400 Series 720 Series 720B Series
Regulatory Text

62-08-05\tBOEING: Amdt. 422 Part 507 Federal Register April 17, 1962. Applies to All 707 and 720 Series Aircraft. \n\n\tAs a result of a recent incident involving loss of the electrical system and accumulation of dense smoke in the cockpit and cabin, the following is required: \n\n\t(a)\tUnless already accomplished in accordance with recommendations contained in the telegram dated March 23, 1962, issued by Boeing Aircraft Company, within the next 25 hours' time in service, inspect electrical components and wiring within the J6 electrical panel to determine that: \n\n\t\t(1)\tLugs and braided leads are tightly secured to the contractor studs; \n\n\t\t(2)\tBraid jumpers are adequately separated from adjacent jumpers to prevent contact; \n\n\t\t(3)\tThere is no evidence of overheating in wiring and braided leads; and \n\n\t\t(4)\tThere is no evidence of capacitor leaks, swelling or overheating. \n\n\t(b)\tIf any of the foregoing items require corrective action, repair in accordance with acceptable maintenance practices. \n\n\tThis directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated March 30, 1962.