Airworthiness Directive · Amendment 39-19852 · Air conditioning
The Boeing Company Airplanes
This AD applies to all The Boeing Company airplanes specified in paragraphs (c)(1) and (2) of this AD, certificated in any category.
(1) Model 757-200, -200PF, -200CB, and -300 series airplanes.
(2) Model 767-200, -300, and -300F series airplanes.
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 757 airplanes and Model 767-200, -300, and - 300F series airplanes. This AD was prompted by reports of excessively high flight deck or cabin temperatures. This AD requires revising certificate limitations and operating procedures of the existing airplane flight manual (AFM), to provide the flightcrew with procedures for hot flight deck or cabin temperatures to follow under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products.
Within 60 days after the effective date of this AD, do the actions specified in paragraphs (g)(1) and (2) of this AD.
(1) Revise the “Certificate Limitations” chapter of the existing AFM to include the information specified in figure 1 to paragraph (g)(1), figure 2 to paragraph (g)(1), or figure 3 to paragraph (g)(1) of this AD, as applicable. This may be accomplished by inserting a copy of this AD into the existing AFM. When information identical to that in figure 1 to paragraph (g)(1), figure 2 to paragraph (g)(1), or figure 3 to paragraph (g)(1) of this AD has been included in the “Certificate Limitations” chapter of the general revisions of the existing AFM, the general revisions may be inserted into the existing AFM, and the copy of this AD may be removed from the existing AFM.
(2) Revise the “Operating Procedures” chapter of the existing AFM to include the information specified in figure 4 to paragraph (g)(2), figure 5 to paragraph (g)(2), figure 6 to paragraph (g)(2), or figure 7 to paragraph (g)(2) of this AD, as applicable. This may be accomplished by inserting a copy of this AD into the existing AFM. When information identical to that in figure 4 to paragraph (g)(2), figure 5 to paragraph (g)(2), figure 6 to paragraph (g)(2), or figure 7 to paragraph (g)(2) of this AD has been included in the “Operating Procedures” chapter of the general revisions of the existing AFM, the general revisions may be inserted into the existing AFM, and the copy of this AD may be removed from the existing AFM.
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
Aircraft
