DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Amendment 39-1572; AD 72-25-06
Airworthiness Directives; BEECH Models C-45G, TC-45G, C-45H, TC-45H, TC-45J
(SNB-5), RC-45J (SNB-5P) D18C, D18S, E18S,
E18S-9700, G18S, H18, JRB- 6, 3N, 3NM and 3TM
72-25-06 BEECH: Amdt. 39-1572. Applies to Beech Models C-45G, TC-45G,
C-45H, TC-45H, TC-45J (SNB-5), RC-45J (SNB-5P) D18C, D18S,
E18S, E18S-9700, G18S, H18, JRB-
6, 3N, 3NM and 3TM Aircraft certificated in all categories with STC SA4-1531,
STC SA111WE, STC SA1832WE or any other STC modification incorporating the
provisions of the Volpar TriGear Installation.
Compliance required as indicated.
To prevent possible failure of the nose landing gear to extend from the
retracted position on those aircraft with Volpar TriGear installed, accomplish
For airplanes incorporating Volpar Tricycle Landing Gear, within the next 100
hours' time in service after the effective date of this AD unless already
accomplished, modify the Volpar nose walking beam assembly, P/N 261, in
accordance with Volpar Service Bulletin No. 21, as revised 7 August 1972, or
later FAA-approved revision, or an equivalent modification approved by the
Chief, Aircraft Engineering Division, FAA Western Region.
NOTE: For bulletins, parts or service information contact:
16300 Stagg Street
Van Nuys, California 91406
NOTE: Pilots are cautioned to conduct a through pre-flight inspection in this
area. A decal should be located on the nose gear shock strut housing listing the
recommended strut inflation pressure.
This amendment becomes effective December 9, 1972.