Discrete, trackable obligations extracted from proposed rules, final rules, and the Code of Federal Regulations.
Each requirement represents a specific legal duty, prohibition, or condition imposed on regulated parties, and is tracked over time as it is proposed, adopted, modified, codified, or corrected.
Under the general safety zone regulations in subpart C of this part, you may not enter the safety zone described in paragraph (a) of this section unle...
Where Transport Canada AD CF-2023-15 refers to hours air time, this AD requires replacing those words with flight hours.
As of the effective date of this AD, do not install a T/R blade that is identified in paragraph (c) of this AD on any helicopter.
If there is any chordwise crack as a result of any action required by paragraph (g)(1)(ii), (g)(2)(i), or (g)(3) of this AD, within 7 days after compl...
For each T/R blade marked with an “X,” within 25 hours time-in-service after accomplishing the actions required by paragraph (g)(1)(ii)(B) of this AD ...
Before the second flight after accomplishing the actions required by paragraph (g)(1)(ii)(B) of this AD, and thereafter before each subsequent flight,...
For each T/R blade marked with an “X,” accomplish the actions required by paragraph (g)(2)(i) and (ii) of this AD.
If there is no coating over the T/R blade abrasion strip, clean the abrasion strip by following the Accomplishment Instructions, part I, paragraph 3, ...
If there is any coating (such as a protective tape or protective coating) over the T/R blade abrasion strip, accomplish further actions in accordance ...
For each T/R blade identified in paragraph (c) of this AD, within three days or prior to the second flight after the effective date of this AD, whiche...
Where the service information referenced in EASA AD 2023-0090 specifies discarding parts, this AD requires removing those parts from service.
Where paragraph (1) of EASA AD 2023-0090 requires compliance within 165 flight hours, this AD requires accomplishing paragraph (1) of EASA AD 2023-009...
Within 200 hours TIS or 12 months, whichever occurs first after the initial inspection required by paragraph (i)(2) of this AD, and thereafter at inte...
Within 50 hours TIS or 50 days, whichever occurs first after the effective date of this AD, accomplish the initial inspection of the safety hook, safe...
Modification of an airplane by replacing each affected part as defined in paragraph (f)(1) of this AD with a new part as defined in paragraph (f)(2) o...
At the next engine shop visit after the effective date of this AD, replace the thermal management system (TMS) clevis mount with redesigned TMS clevis...
Within 30 days after the effective date of this AD or upon installation of an affected engine, whichever occurs later, remove one loop cushion clamp, ...
For airplanes with flexible hydraulic hoses part number (P/N) AS117-04-0205 or P/N 98E0520FAMA000W (landing gear (LG) up and LG down lines); or flexib...
Instead of contacting Honda if proper aileron balance cannot be attained using adjustable balance weights, this AD requires attaining proper aileron b...
Instead of discarding parts, you must remove those parts from service.