The U.S. aircraft register, updated daily
FAA orders · airworthiness directive · current

76-24-06 R2: Oxygen System

FAA order 76-24-06 R2 is an airworthiness directive in force since November 14, 1983. The FAA's subject line: Oxygen System. System: emergency equipment.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus SAS
Models
BAC 1-11 200 Series, BAC 1-11 400 Series

Dates and paperwork

In force since
November 14, 1983
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,127 characters)
76-24-06 R2 BRITISH AIRCRAFT CORPORATION: Amendment 39-2779 as amended by Amendment 39-2800 is further amended by Amendment 39-4734. Applies to BAC 1-11 200 and 400 series airplanes, certificated in all categories. Compliance is required as indicated. To detect oxygen leaks, due to fractures in the flexible oxygen hoses of the emergency oxygen system, and prevent possible in-flight fires, accomplish the following: (a) Within the next 250 hours time in service after the effective date of this AD, unless already accomplished in the last 1500 hours time in service, conduct a leak test of the emergency oxygen system in accordance with paragraph 2.3 of the section entitled "Accomplishment Instructions" of British Aircraft Corporation Alert Service Bulletin 35-A-PM 5394, issue 3, dated June 29, 1979, or an FAA-approved equivalent. (b) If, during the leak test required by paragraph (a) of this AD, a leak is found, before further flight, locate the source of the leak and replace the defective part with a new part of the same part number or with a serviceable FAA-approved part and then retest the emergency oxygen system in accordance with paragraph (a) of this AD. (c) Inspect and rework the flexible hoses of the emergency oxygen system within the next 1000 hours time in service or six months after the effective date of this AD, whichever occurs sooner, unless already accomplished within the proceeding 1500 hours time in service, and thereafter at intervals not to exceed one year, in accordance with paragraph 2.4, Figure 1 through 3, and Table 1 of the service bulletin. (d) If, during an inspection required by paragraph (c) of this AD, the flexible oxygen hoses are found fractured or embrittled, before further flight, replace the affected parts with new parts of the same part number or with serviceable FAA-approved parts and then retest the oxygen system for leaks in accordance with paragraph (a) of this AD. Amendment 39-2779 became effective December 14, 1976. Amendment 39-2800 became effective January 6, 1977. This Amendment 39-4734 becomes effective November 14, 1983.

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/76-24-06 R2.json · aircraft systems.