- Effective
- February 12, 1963
- Models
- 707-100 Long Body, 707-100B Long Body, 707-100B Short Body, 707-200, 707-300 Series, 707-300B Series and 4 more
- Registered aircraft
- 6 matched by model
- 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.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
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| FAA DRS HTML | 19 KB | e6f3b61c…c13d2f4 | FAA DRS (API key needed) |
On this page
The airworthiness directive
63-02-01 BOEING: Amdt. 527 Part 507 Federal Register January 11, 1963. Applies to All 707/720 Series Aircraft.
Compliance required within the next 500 hours' time in service, unless already accomplished.
The upper and lower fairings installed over the anticollision lights have been found to disturb the light distribution in certain peripheral areas. To prevent a reduction in the effective light intensity:
(a) Remove the anticollision light upper fairing, (P/N's 69-10789, 9-66041-3000) and the lower fairing, (P/N's 69-10789-1, 9-66041 or 9-66041-3000); and
(b) Plug the mounting holes for the fairing assembly fasteners with Boeing material specification 5-13 Type A aerodynamic smoother or equivalent.
(Boeing Service Bulletin No. 1651 covers the same subject.)
This directive effective February 12, 1963.
Affected TCDS · 3
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 6
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 1 |
|---|---|
| 1977 | 1 |
4 with no year recorded