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76-04-08: Engine Mount

FAA order 76-04-08 is an airworthiness directive in force since March 4, 1976. The FAA's subject line: Engine Mount. It names Messerschmitt-Bolkow-Blohm BO 209: about 5 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
DaimlerChrysler Aerospace AG
Models
BO-209-150 FF, BO-209-150 FV, BO-209-150 RV, BO-209-160 FV, BO-209-160 RV
On this site
Messerschmitt-Bolkow-Blohm BO 209 5 registered

Dates and paperwork

In force since
March 4, 1976
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,322 characters)
76-04-08 MESSERSCHMITT-BOLKOW-BLOHM: Amendment 39-2526. Applies to all Model BO 209 "Monsun" airplanes, certificated in all categories, except those having engine mount, P/N 209-61016-b, installed. Compliance is required as indicated, unless already accomplished. To prevent possible failure of the engine mount, accomplish the following: (a) Within the next 10 hours' time in service after the effective date of this AD and, thereafter, at intervals not to exceed 100 hours' time in service from the last inspection, until modified in accordance with paragraph (b) of this AD, visually inspect the connection point of all three bent tubes of the engine mount, P/N 209-61016, for cracks in accordance with Messerschmitt-Bolkow-Blohm Service Bulletin No. 209-15/71-20, dated July 1975, or an FAA-approved equivalent. (b) If a crack is found during an inspection required by paragraph (a) of this AD, before further flight, except that the airplane may be flown in accordance with FAR Section 21.197 and 21.199 to a base where the work can be performed, replace the engine mount with an engine mount of new design, P/N 209-61016-b, in accordance with Messerschmitt-Bolkow-Blohm Service Bulletin No. 209-15/71-20, dated July 1975, or an FAA-approved equivalent. This amendment becomes effective March 4, 1976.

Related safety bulletins advice on the same designs, not orders

2009-07-24CE-09-43 · Alternative Method of Compliance for AD 87-09-01
2003-03-14CE-03-31 ·

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/76-04-08.json · aircraft systems.