Header Information
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Amendment 39-325; AD 66-30-01 R1

Airworthiness Directives; BEECH Model JRB-6, D18C, D18S, E18S, E18S-9700 Airplanes


Preamble Information
AGENCY: Federal Aviation Administration, DOT


DATES: Effective March 1, 1967.






Regulatory Information

66-30-01 BEECH: Amdt. 39-325 Part 39 Federal Register December 21, 1966. Applies to Model JRB-6, D18C, D18S, E18S, E18S-9700 with Serial Numbers prior to BA445, C-45G, TC-45G, C-45H, and TC-45J (SNB-5) Airplanes That Have Been Modified in Accordance with Volpar, Inc., Supplemental Type Certificate No. SA4-1531 or SA111WE.

Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent moisture from collecting in the static line of the subject airplanes, accomplish the following:

Install a drain in the static line in accordance with Volpar, Inc., Drawing No. 857, titled "Drain Installation - Static Pressure Line" dated 9-22-66 (Volpar, Inc., Service Bulletin No. 10, page 2) or an equivalent approved by the Chief, Aircraft Engineering Division, FAA Western Region.

Upon request of the operator, an FAA maintenance inspector, subject to prior approval of the Regional Director, FAA Western Region, may adjust the compliance time if the request contains substantiating data to justify the adjustment for that operator.

This directive effective December 21, 1966.

This amendment effective March 1, 1967.

Revised March 1, 1967.



Footer Information



Federal Register Information
[Federal Register: December 21, 1966]







Comments