Airworthiness Directive 80-20-03
one-timeAirworthiness Directives; new shielded wires between the engine firewall and the partial pressure bulkhead in accordance with Fokker Service Bulletin F27/61
Which aircraft AD 80-20-03 applies to
Install new shielded wires between the engine firewall and the partial pressure bulkhead per Fokker Service Bulletin F27/61-35 dated March 23, 1979, or an FAA-approved equivalent; applies to airplane serial numbers 10249 through 10518 except those with Fokker Service Bulletin F27/61-10(G7) already incorporated.
Whether AD 80-20-03 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.