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AD 78-20-04 ACTIVE

Slat Drive Arm And Drive Shaft
Key Information
AD Number 78-20-04 Status Active
Effective Date November 07, 1978 Issue Date Not specified
Docket Number Unknown Amendment 39-3308
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) DC-10-10 DC-10-10F DC-10-30 DC-10-30F (KC-10A, KDC-10) DC-10-40
Regulatory Text

78-20-04 MCDONNELL DOUGLAS: Amendment 39-3308. Applies to DC-10-10, -10F, -30, -30F and -40 airplanes certificated in all categories. \n\n\tCompliance is required as indicated unless already accomplished. \n\n\tTo prevent failure of an outboard slat drive arm or drum shaft, accomplish the following: \n\n\t(a)\tWithin the next 1500 hours' time in service after the effective date of this AD, unless the inspection and modifications specified in McDonnell Douglas DC-10 Service Bulletin 27-160, dated March 1, 1978, are already accomplished, inspect the outboard slat drive arms ultrasonically for cracks in accordance with McDonnell Douglas DC-10 Service Bulletin A27-160 Revision 2, dated March 22, 1978. \n\n\t(b)\tWithin the next 4,000 hours' time in service after the effective date of this AD, inspect by magnetic particle methods for cracks and modify or replace the outboard slat drive arms and drum shafts in accordance with McDonnell Douglas DC-10 Service Bulletin 27-160, dated March 1, 1978. \n\n\t\t(1)\tAs an alternate to applying sealant in accordance with Service Bulletin 27-160, it is permissible to install a lubrication fitting and fillet seal in accordance with McDonnell Douglas DC-10 Service Bulletin 27-161, dated March 3, 1978, and, thereafter, at intervals not to exceed 2500 hours' time in service apply MIL-G-81322 grease or equivalent to the ARH 7011-1 bolt assembly fitting. \n\n\tNOTE: Service Bulletin A27-160 Revision 2 dated March 22, 1978, Service Bulletin 27-160 dated March 1, 1978 and Service Bulletin 27-161 dated March 3, 1978 are the only versions of the service bulletins suitable for compliance with paragraphs (a) and (b) of this AD. \n\n\t(c)\tAny outboard slat drive arm or drum shaft found to be cracked must be replaced prior to further flight. \n\n\t(d)\tEquivalent inspections, modifications or parts may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\t(e)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for accomplishment of inspections required by this AD. \n\n\tThis amendment becomes effective November 7, 1978.