- Effective
- August 18, 1975
- Models
- Phoebus A1, Phoebus B1
- Data sheet
- TCDSG16EU
- Registered aircraft
- 11 matched by model
- Product
- Aircraft · Glider
- Amendment
- 39-2318
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 | dab11318…b78355e | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-18-01 ENTWICKLUNGSGEMEINSCHAFT (MESSERSCHMITT-BOLKOW-BLOHM GmbH): Amendment 39-2318. Applies to Phoebus A1 and B1 gliders, serial numbers 702 thru 751, certificated in all categories.
Compliance is required as indicated.
To prevent loss of rudder control, accomplish the following:
(a) Within the next 10 hours' time in service after the effective date of this AD, unless already accomplished, and thereafter at intervals not to exceed 100 hours' time in service from the last inspection, inspect the rudder control cable lever as follows:
(1) Remove headrest, luggage container, and seat.
(2) Disconnect rudder control cables from cable lever.
(3) Remove rudder control rod and rudder control cable lever (P/N 15120-4236).
(4) Inspect rudder control cable lever weld for cracks using a magnifying glass with a magnification power of not less than five.
(5) If a crack is found comply with paragraph (b) of this AD.
(b) If a rudder control cable lever weld crack is found during an inspection required by paragraph (a), replace the rudder control cable lever P/N 15120-4236 with a serviceable part of the same part number or an FAA-approved equivalent.
(MBB Service Bulletin No. PHOEBUS 27-20/1, dated March 1975, pertains to this AD.)
This amendment becomes effective August 18, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 11
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1965 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 3 |
| 1968 | 1 |
| 1969 | 2 |
3 with no year recorded