- Effective
- March 12, 1963
- Models
- Caravelle SE 210 Model III, Caravelle SE 210 Model VIR
- Data sheet
- TCDS7A6
- Product
- Aircraft · Large 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.
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The airworthiness directive
63-04-03 SUD AVIATION: Amdt. 534 Part 507 Federal Register February 9, 1963. Applies to All SE-210 Caravelle Mark III and VIR Aircraft Except Serial Numbers 117, 120, 125 and Subsequent.
Compliance required as indicated.
To prevent the flight control system push-pull rod from jamming adjacent components in the event of loss of a connecting bolt, and thereby preventing emergency control of the aircraft by means of trim controls, accomplish the following:
(a) For aircraft with 2,700 or more hours' time in service as of the effective date of this AD, compliance with (c) is required within the next 300 hours' time in service.
(b) For aircraft with less than 2,700 hours' time in service as of the effective date of this AD, compliance with (c) is required prior to 3,000 hours' time in service.
(c) Install push-pull rod guards at each aileron, elevator and rudder control rod in accordance with Sud Aviation Caravelle Service Bulletins Nos. 27-130, revised May 9, 1962, and 27-157 dated July 20, 1962, or an FAA approved equivalent.
This directive effective March 12, 1963.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.