- Effective
- September 7, 1963
- Published
- September 7, 1963
- Models
- D.H. 104 Dove Series 1A, D.H. 104 Dove Series 2A, D.H. 104 Dove Series 5A, D.H. 104 Dove Series 5BA, D.H. 104 Dove Series 6A, D.H. 104 Dove Series 6BA and 4 more
- Data sheet
- TCDSA-807
- Registered aircraft
- 3 matched by model
- Product
- Aircraft · Small airplane
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.
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On this page
The airworthiness directive
63-19-01 de HAVILLAND: Amdt. 611, Part 507, Federal Register September 7, 1963. Applies to All Model DH 104 Dove Aircraft.
Compliance required as indicated.
As a result of cracks in the aileron, rudder, elevator and flap hinge links and hinge brackets, accomplish the following:
(a) Hinge links and brackets not incorporating Modifications 841, 842 or 843 shall be inspected for cracks at intervals not exceeding 600 hours' time in service, or each 12 months, whichever occurs first. Remove the point from the components before inspection, and reapply protective coating after inspection.
(b) Hinge links and brackets incorporating Modifications 841, 842 or 843 shall be inspected for cracks at intervals not exceeding 1,800 hours' time in service.
(c) Replace cracked parts before further flight.
(de Havilland Service Technical News Sheet CT (104) No. 123, Issue 5 dated March 19, 1962, covers this subject.)
This supersedes AD 56-15-05. This directiveeffective September 7, 1963.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 3
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.