Oversight of FAA--reliability of "drilled" Turbine Fan Blades on CF-6 Engine Used to Power DC-10 and A-300B Aircraft: Hearings Before the Special Subcommittee on Investigations of the Committee on Interstate and Foreign Commerce, House of Representatives, Ninety-third Congress, Second Session ... July 2 and 10, 1974


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Página 175 - Interested persons are invited to participate in the making of the proposed rule by submitting such written data, views, or arguments as they may desire. Communications should identify the regulatory docket...
Página 23 - Do you solemnly swear or affirm that the testimony you are about to give this subcommittee is the truth, the whole truth, and nothing but the truth, so help you God ? Mr.
Página 176 - I have a map here [indicating], and if you will permit me to do so I would like to show it.
Página 9 - Do you solemnly swear (or affirm) that the testimony you are about to give in this case shall be the truth, the whole truth, and nothing but the truth, so help you God?
Página 175 - The proposals contained in this notice may be changed in the light of comments received. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons.
Página 73 - For turbopropeller powered airplanes, each turbine engine must be able to operate throughout its flight power range without adverse effect on engine operation or serious loss of power or thrust, under the icing conditions specified in Appendix C of Part 25 of this chapter.
Página 95 - Your predecessor said if he had to do it over again he would do the same thing over again.
Página 286 - In consideration of the foregoing and pursuant to the authority delegated to me by the Secretary (31 FR 13952) and (32 FR 1005), Sec.
Página 198 - Council finds that publication in accordance with normal rule making procedure is impracticable and that good cause exists for making this amendment effective in less than 30 days.
Página 77 - Service and test experience indicate that the drilled GE CF-6 engine fan blade is very sensitive to FOD. The resulting damage to the engine and aircraft is considered excessive and presents a serious threat to the safely of the aircraft.

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