- Effective
- November 28, 1970
- Models
- NA-265, NA-265-20, NA-265-30, NA-265-40, NA-265-60, NA-265-65, NA-265-70, NA-265-80
- Data sheet
- TCDSA2WE
- Registered aircraft
- 44 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-1113
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
70-24-03 NORTH AMERICAN ROCKWELL: Amdt. 39-1113. Applies to all NA-265 Series Airplanes.
Compliance required within the next 100 hours' time in service, or 120 days, whichever occurs earlier, after the effective date of this AD, unless already accomplished.
To prevent unwanted actuation of the Engine Emergency Fire Control "T" handle to the emergency position, modify the fire emergency engine control fire pull assembly by replacing the two E858-15 interlock actuator pins with E858-21 pins in accordance with the instructions contained in Los Angeles Division of North American Rockwell Corporation Sabreliner Field Service Bulletin Number 70-13, dated November 11, 1970, or later FAA approved revision, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region.
This amendment becomes effective on November 28, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 44
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 |
| 1968 | 1 |
| 1972 | 1 |
| 1973 | 3 |
| 1974 | 3 |
| 1975 | 1 |
| 1976 | 2 |
| 1978 | 1 |
| 1979 | 5 |
| 1980 | 9 |
| 1981 | 12 |
| 1994 | 1 |
3 with no year recorded