FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 34 > Section 10 - Applicability
section 34.7 |
section 34.11

(a) The provisions of this subpart are applicable to all new aircraft gas turbine engines of classes T3, T8, TSS, and TF equal to or greater than 36 kilonewtons (8090 pounds) rated output, manufactured on or after January 1, 1974, and to all in-use aircraft gas turbine engines of classes T3, T8, TSS, and TF equal to or greater than 36 kilonewtons (8090 pounds) rated output manufactured after February 1, 1974.
(b) The provisions of this subpart are also applicable to all new aircraft gas turbine engines of class TF less than 36 kilonewtons (8090 pounds) rated output and class TP manufactured on or after January 1, 1975, and to all in-use aircraft gas turbine engines of class TF less than 36 kilonewtons (8090 pounds) rated output and class TP manufactured after January 1, 1975.
  
Current page: FARs > Part 34 > Section 10 - Applicability
section 34.7 |
section 34.11

page stats: viewed 787 unique times - last change 25-Jan-2005
» DOWNLOADING (PARTS OF) THIS WEBSITE AUTOMATICALLY IS NOT ALLOWED! «
THIS IS NO OFFICIAL SOURCE --
[DISCLAIMER]
[FAA WEBSITE]
See also:
AIM | ATC | FSS | NOTAMS | PCG | |