| AD Number | 85-14-07 | Status | Active |
| Effective Date | August 16, 1985 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-5094 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Sud Aviation |
| Model(s) | Caravelle SE 210 Model I Caravelle SE 210 Model III Caravelle SE 210 Model VIR |
85-14-07 AEROSPATIALE (formerly SUD): Amendment 39-5094. Applies to all Caravelle SE-210 Models I, III, and VIR airplanes, certificated in any category, which do not embody Modification 1753. Accomplish the following, unless previously accomplished:
A. Prior to the accumulation of 7000 landings or before the next 100 landings after the effective date of this AD, whichever occurs later, inspect the wing rib 44 web and angle doubler in accordance with SUD Service Bulletin 57-64 dated December 12, 1978.
B. Repeat the inspections of paragraph A., above, at intervals not to exceed:
1. rib 44 lower cap - 10,000 landings
2. webs and doublers - 3,000 landings.
C. Parts found cracked must be repaired prior to further flight.
D. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.
E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD.
This amendment becomes effective August 16, 1985.