- Effective
- March 4, 1976
- Models
- BO-209-150 FF, BO-209-150 FV, BO-209-150 RV, BO-209-160 FV, BO-209-160 RV
- Data sheet
- TCDSA27EU
- Product
- Aircraft · Small airplane
- Amendment
- 39-2526
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 21 KB | d18fa623…57391c2 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.