AD 74-17-01

Active

Regulator

Key Information
74-17-01
Active
September 16, 1974
Not specified
Unknown
39-1913
Applicability
["Appliance"]
Not specified
The Boeing Company Lockheed Martin Corporation Sargent Industries, Pico Division
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 727-100 Series 727-100C Series 727-200 Series 727 Series 727C Series 737-100 Series 737-200 Series 737-200C Series DC-10-10 DC-10-10F DC-10-15 DC-10-30 DC-10-30F (KC-10A, KDC-10) DC-10-40 DC-10-40F DC-6 DC-6A DC-6B DC-7 DC-7B DC-7C DC-8-11 DC-8-12 DC-8-21 DC-8-31 DC-8-32 DC-8-33 DC-8-41 DC-8-42 DC-8-43 DC-8-51 DC-8-52 DC-8-53 DC-8-55 DC-8-61 DC-8-61F DC-8-62 DC-8-62F DC-8-63 DC-8-63F DC-8-71 DC-8-71F DC-8-72 DC-8-72F DC-8-73 DC-8-73F DC-8F-54 DC-8F-55 DC-9-11 DC-9-12 DC-9-13 DC-9-14 DC-9-15 DC-9-15F DC-9-21 DC-9-31 DC-9-32 DC-9-32 (VC-9C) DC-9-32F DC-9-32F (C-9A) DC-9-32F (C-9B) DC-9-33F DC-9-34 DC-9-34F DC-9-41 DC-9-51 DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87) 188A 188C Inflatable Slide Regulator
Regulatory Text

74-17-01 SARGENT INDUSTRIES, PICO DIVISION: Amendment 39-1913. Applies to Sargent Industries, Pico Division Regulator P/N 30001 incorporated in passenger evacuation slides and slide/rafts on aircraft certificated in all categories. \n\n\tNote: This regulator is installed in, but not limited to, Pico, Air Cruiser and International Inflatable slides on B-707, B-727, B-737, DC-6, DC-7, DC-8, DC-9, DC-10, and L-188 aircraft. \n\n\tCompliance required within two years after the effective date of this AD, unless already accomplished. \n\n\tTo prevent delayed actuation of regulator P/N 30001, modify the Sargent Industries, Pico Division regulator, P/N 30001, in accordance with Sargent Industries, Pico Division Service Bulletin 25-51, dated March 14, 1974, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\tThis amendment becomes effective September 16, 1974.

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References
This information is not available.
--- - Part 39
FAA Documents