AD 77-08-07

Active

External Load Release

Key Information
77-08-07
Active
May 06, 1977
Not specified
Unknown
39-2880
Applicability
["Aircraft"]
["Rotorcraft"]
Airbus Helicopters Deutschland GmbH
BO-105A BO-105C
Regulatory Text

77-08-07 MESSERSCHMITT-BOLKOW-BLOHM (MBB): Amendment 39-2880. Applies to Model BO-105A and BO-105C helicopters, serial numbers S101 through S200, certificated in all categories, that incorporate external load hook assembly P/N 105-80322.
Compliance is required as indicated, unless already accomplished.
To prevent the possible inability to release an external load, accomplish the following:
(a) Within the next 5 hours time in service after the effective date of this AD, either -
(1) Install an operating limitation placard on the instrument panel in full view of the pilot, setting forth the following limitation "EXTERNAL LOAD OPERATIONS PROHIBITED"; or
(2) Replace wire bundle 22VB, P/N 105-98327, with new bundle, P/N 105- 98326, and change the wiring connection of the associated connector plug 5MDA in accordance with subparagraph 2B of MBB Service Bulletin No. 80-21, dated July 25, 1975, or equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, A.P.O. New York, N.Y. 09667.
(b) The operating limitation placard required by paragraph (a)(1) of this AD may be removed upon compliance with paragraph (a)(2) of this AD.
This amendment becomes effective May 6, 1977.

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References
This information is not available.
--- - Part 39
FAA Documents